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Page 1: DISTANT PLAIN EVENTS 6 AND 1A PROJECT 3.02A, … · technical report n.70-14 distant plain events 6 and 1a project 3.02a, earth motion and stress measurements by d. w. murrdl stptombtr

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TECHNICAL REPORT N.70-14

DISTANT PLAIN EVENTS 6 AND 1A PROJECT 3.02A, EARTH MOTION AND

STRESS MEASUREMENTS by

D. W. Murrdl

Stptombtr 1970

Spomorad by Dtftns« Atomic Support Agency

Conducted by U. S. Army Engineer Watorwayt Experiment Station, Vickfburg, Mittittippi

4iiMr-Miic viemaun«, MI**.

Thi» docuimnt has bMn tpprawd for public rtioiM and sal«; Its distribution is unlimited

i

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THE CONTENTS OF THIS REPORT ARE NOT TO

BE USED FOR ADVERTISING, PUBLICATION,

OR PROMOTIONAL PURPOSES. CITATION OF

TRADE NAMES DOES NOT CONSTITUTE All

OFFICIAL ENDORSEMENT OR APPROVAL OF

THE USE OF SUCH COMMERCIAL PRODUCTS.

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ABSTRACT

The objectives of this study were to measure and analyze the

earth motions produced by Events 6 and 1A of Operation Distant Pldin.

Event 6 was 100 tons of TNT stacked in a sphere, tangent to the

ground surface. Event 1A was 20 tons of TNT also stacked in a sphere,

but detonated on a tower at a height of burst of 29.5 feet.

Acceleration, particle velocity, and soil stress gages were

installed for both events in order to measure the ground motion. For

Event 6, these gages were placed in the region of 2,000- to 10-psi

overpressure (U9 to 680 feet from ground zero) and at depths of 1.5

to 30 feet. For Event 1A, gages were placed between the expected

10,000- and 500-psi overpressure levels (directly beneath the tower

to 80 feet away) and at depths of 1.5 to 10 feet. Time histories ob-

tained by this instrumentation are included in Appendixes A (Event 6)

and B (Event 1A).

For Event 6, ground shock arrival times indicated development

of outrunning ground motion at about the 30-psi level. Shock propa-

gation velocities were calculated to be 1,100 ft/sec for the soil

layer above the water table and 5,500 ft/sec below it.

Vertical particle accelerations for both events were correlated

with overpressure. The ratio of acceleration to overpressure for the

1.5-foot depth was about 0.U g/psi at the 1,000-psi level, and

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increased to 1.0 at the 20-psi level. At depths of 5 and 10 feet,

accelerations averaged 20 and 7.5 percent of the shallow data,

respectively.

Vertical particle velocities at the 1.5-foot depth were also

correlated on the basis of overpressure; the ratio of velocity to

overpressure varied from 0.03 ft/sec/psi at 1,000 psi to 0.08

ft/sec/psi at 10 psA. Velocities attenuated less sharply with depth

than did accelerations. Velocities at the 5-foot depth were about

^0 percent of those at 1.5 feet, while those from the 10-foot depth

were about 30 percent of those at 1.5 feet.

Horizontal velocities were dominated by the cratering-induced

motion. These motions attenuated as the -2.7 power of distance.

Vertical stresses attenuated more rapidly than did the veloci-

ties, with stresses at the 5-foot depth averaging 25 percent of those

at the 1.5-foot depth. Horizontal stresses measured below the water

table behaved similar to free-water measurements, attenuating as the

-1.15 power of distance, versus -1.13 power for water. Calculations

of shear stress were made for three locations on each shot. Peak

values ranged from ^0 to 70 psi.

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PREFACE

This report describes an experiment conducted by the U. S. Army

Engineer Waterways Experiment Station (WES) as a part of Operation

Distant Plain, Events 6 and 1A. This study was sponsored by the De-

fense Atomic Support Agency (DASA).

The work was conducted by personnel of the Nuclear Weapons Ef-

fects Division under the direction of Mr. G. L. Arbuthnot, Jr., Di-

vision Chief, Mr. L. F. Ingram, Chief, Physical Sciences Branch, and

Mr. J. D. Day, Chief, Blast and Shock Section. Project personnel

were Messrs. D. W. Murrell, Project Officer and author of this report,

M. A. Vispi, Field Operations Officer, and C. M. Wright, all of the

Blast and Shock Section, and Messrs. L. T. Watson, J. L. Pickens, and

C. E. Tompkins of the WES Instrumentation Branch.

The author acknowledges the able assistance of the WES drill

crew in drilling instrument holes and placing gages. The drill crew

operated under the direction of Mr. A. L. Mathews, Chief, Exploration

Section, Soils Division, and the immediate field supervision of

Mr. J. L. Gatz.

COL John R. Oswalt, Jr., CE, COL Levi A. Brown, CE, and

COL Ernest D. Peixotto, CE, were Directors of WES during this exper-

iment and the preparation of this report. Messrs. J. B. Tiffany and

F. R. Brown were Technical Directors.

► -■■:• • •. - .-i .4,..', J

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CONTENTS

ABSTRACT k

PREFACE - - 6

CONVERSION FACTORS, BRITISH TO METRIC UNITS OF MEASUREMENT ID

CHAPTEP. 1 INTRODUCTION 11

1.1 Objectives 11 1.2 Background H 1.3 Ground Motion and Stress Predictions 13

CHAPTER 2 PROCEDURE 18

2.1 Description of Teat Site 18 2.2 Instrumentation Layout 19 2.3 Instrumentation 20

2.3.1 Gages and Calibration - 20 2.3.2 Gage Canisters and Placement 21 2.3.3 Recording System- 22

CHAPTER 3 RESULTS AND DISCUSSION 32

3.1 Data Recovery — - 32 3.2 Arrival Times, Event 6 3^ 3.3 Vertical Particle Acceleration — 3^

3.3.1 Event 6 3h 3.3.2 Event 1A 35 3.3.3 Discussion and Correlation 36

3.^ Horizontal Acceleration 38 3.5 Vertical Particle Velocity 38

3.5.1 Event 6 ., 38 3.5.2 Event 1A 39 3.5.3 Discussion and Correlation kO

3.6 Horizontal Particle Velocities hi 3.7 Displacement k3 3.8 Soil Stress Measurements kh

3.8.1 Event 6 kk 3.8.2 Event 1A - U5 3.8.3 Three-Component Stress, Events 6 and 1A ^+5

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CHAPTER k CONCLUSIONS 8l

APPENDIX A EVENT 6 TIME HISTORIES 05

APPENDIX B EVENT 1A TIME HISTORIES 119

REFERENCES - 137

TABLES

1.1 Estimated Peak Motions and Stresses, Event 6— —- 16 1.2 Estimated Motion:, and Stresses, Event 1A 17 2.1 Particle Motion Instrumentation, Event 6 2h 2.2 Earth Stress Instrumentation, Event 6-- 25 2.3 Particle Motion Instrumentation, Event 1A— 26 2.U Earth Stress Instrumentation, Event iA—•——--- 27 3.1 Motion Data Summary, Event G—— -——— ^8 3.2 Stress Data Summary, Event 6——-—-—---— U9 3.3 Motion Data Summary, Event IA- —-— 50 3.^ Stress Data Summary, Event IA — 51 3.5 Peak Transient Displacements, Event 6- 52 3.6 Peak Transient Displacements, Event IA 53

FIGURES

2.1 Instrumentation layout, Event 6 — 28 2.2 Instrumentation layout, Event IA 29 2.3 Motion gage canister 30 2,k Interior of instrument ounker 31 3.1 Shock front profile. Event 6 5^ 3.2 Peak vertical downward acceleration versus horizontal

distance. Event 6-- 55 3.3 Peak vertical downward acceleration versus horizontal

distance. Event IA 56 3-4 Time histories of vertical acceleration, 53-foot

horizontal distance. Event IA 57 3.5 Correlation of vertical accelerations, 1.5-foot depth—— 58 3.6 Vertical acceleration attenuation with depth 59 3.7 Peak outward horizontal acceleration versus distance.

Event 6 60 3.8 Peak outward horizontal acceleration versus distance,

Event IA 6l 3.9 Pexk vertical downward particle velocity versus

distance, Event 6 62

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3.10 Peak vertical downward particle velocity versus distance, Event 1A 63

3.11 Velocity/overpressuie ratio versus overpressure, 1.5-foot depth ■ - 64

3.12 Vertical particle veio;." attenuaticn with depth 65 3.13 Time histories of selected horizontal velocities,

Event 6- — 66 3.1^ Peak outward airblast-induced particle velocities

versus distance, Event 6 6? 3.15 Peak outward airblast-induced particle velocities

versus distance. Event 1A 68 3.16 Peak outward cratering-induced particle velocity versus

distance, Event 6 69 3.17 Peak upward transient displacement versus distance.

Event 6 70 3.18 Peak outward transient displacement versus distance.

Event 6 71 3.19 Peak vertical stress versus horizontal distance.

Event 6 72 3.20 Peak horizontal stress versus horizontal distance,

30-foot depth, Event 6 - 73 3.21 Stress-time histories, ground zero, Event 1A 7U 3.22 Shear and principal stress data, Location 6105!+, Event 6- 75 3.23 Shear and principal stress data. Location 61062, Event 6- 76 3.2^ Shear and principal stress data. Location 61035, Event 6- 77 3.25 Shear and principal stress data. Location lloi+2.

Event 1A 78 3.26 Shear and principal stress data. Location II0U3,

Event 1A 79 3.27 Shear and principal stress data. Location 11062,

Event 1A 80

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CONYERSION FACTORS, BRITISH TO METRIC UNITS OF MEASUREMENT

British units of measurement used in this report can be converted to metric units as follows.

Multiply- By To Obtain

inches

feet

tons (2,000 pounds)

pounds per square inch

pounds per cubic foot

feot per second

2.5U centimeters

0.30U8 meters

907.185 kilograms

0.070307 kilograms per square centimeter

I6.OI85 kilograms per cubic meter

30.U8 centimeters per second

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CHAPTER 1

INTRODUCTION

1.1 OBJECTIVES

The objectives of Project 3.02a of the Distant Plain Series were

to measure earth motions and stresses on Events 6 and 1A and to ana-

lyze and correlate the results with those obtained on other pertinent

detonations such as Snow Ball, Flat Top II and III, and Distant Plain

2A and 3« Cratering-lnduced ground motions were of special interest

on Event 6, a 100-ton spherical TM detonation with the charge

placed tangent to the ground surface. Event 1A, a 20-ton spherical

TNT detonation with a height of burst of 29.5 feet, provided an op-

portunity to study airblast-induced ground motions at predicted over-

pressure levels up to 10,000 psi without significant crater-induced

motions.

1.2 BACKGROUND

Events 6 and 1A of Operation Distant Plain, conducted at the De-

fence Research Establishment, Suffield (DRES), Alberta, Canada, dur-

ing July and August 1967» were the culmination of the Distant Plain

Series begun in July 1966.

A table of factors for converting British units of measurement to

metric units is presented on page 10.

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Event 6, a 100-ton TNT detonation, used a tangent-sphere charge

configuration to simulate as closely as possible the crater and air-

blast characteristics of a nuclear weapon surface burst. Briefly,

this design was expected to produce a smaller, shallower crater than

would a hemispherical (e.g. Snow Ball) or half-buried spherical (e.g.

Flat Top and Distant Plain 3 and 5) charge. An excellent opportunity

thus existed to obtain measurements of airblast-induced ground mo-

tions and stresses at air overpressure levels significantly higher

than those associated with previous measurements. At the same time,

this test allowed assessment of crater-induced motions which, within

a few crater radii of the charge, can equal or exceed the airblast-

induced motions. In regard to evaluating the response of buried

strategic structures, these motions are very significant.

The Watching Hill Blast Range, with a water table and attendant

seismic discontinuity at a depth of about 23 feet, presented a two-

layered system for this experiment. The outrunning ground motion

could then be easily documented and should correlate closely with

data from Snow Ball, detonated at the same site.

Event 1A, a 20-ton TNT tower shot with the center of the spheri-

cal charge placed at a height of 29.5 feet, was designed to obtain

experimental data on airblast and airblast-induced ground motions in

the 300- to 10,000-psi overpressure region. Measurements of

airblast-induced ground motions at these overpressures were needed

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to extend the accumulation of ground motion data into this unexplored

area.

1.3 GROUND MOTION AM) STRESS PREDICTIONS

Estimates of ground motions and stresses for selecting proper

gage ranges and making recording system gain settings for Event 6

were drawn from empirical data and empirically modified one-

dimensional elastic equations. Predictions of soil stress were based

on relative attenuations with depth observed on Operation Upshot-

Knothole (Reference l). Attenuation of vertical earth stress as a

function of depth, at least to a depth of 10 feet, was determined to

be

/ d \-0-37

'"ik) (1)

which describes the vertical stress P at a depth d in terms of

stress P.. at a depth d, (Reference 1). For the Distant Plain

events. P.. and d.. were arbitrarily fixed to be the surface over-

pressure and 0.5 foot, respectively, thus allowing calculation of ex-

pected pressures at any desired depth.

Peak vertical particle velocities were calculated from the one-

dimensional elastic equation relating stress and particle velocity

P = DCpu (2)

13

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where P is the stress, p is the in situ density, C is the wave

propagation velocity of the stress level of interest, and u is the

particle velocity. Stresses used to calculate particle velocity were

derived from Equation 1 above for the overpressure levels and depths

of Interest.

Estimates of peak vertical accelerations were made using peak

velocities calculated from Equation 2 and estimated rise times for

the velocity pulse. Assuming a parabolic velocity input, the peak

acceleration becomes

A = fi (3) r

where T is the velocity rise time. Rise times for Equation 3 were

computed as recommended by Reference 2

T = 0.001 + |- - §- CO P s

where Z is the depth below surface, C is the wave propagation ve-

locity of the peak stress, and C is the seismic velocity, or pr p- 5

agation velocity of very lew stresses. Equation k then accounts for

the observed increase of rise time with depth since C > C , which, s p '

in turn, produces a more rapid attenuation with depth of acceleration

than of velocity. This, too, is an empirically documented phenomenon.

Horizontal (radial) measurements of airblast-induced velocity

and acceleration were estimated to be 20 and 6? percent of the

Ik

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predicted vertical measurements in the superseismic and outrunning

regions, respectively. These empirical factors were determined from

measurements made on Operation Snow Ball (Reference 3) and Distant

Plain Events 1 through 5 (Reference k), all conducted at DRES. Hor-

izontal stress and stress measured on an axis inclined ^5 degrees to

the horizontal were both predicted to be 6? percent of the vertical

stress at all locations except below the water table,, where all three

parameters were assumed to be equal due to the saturated nature of the

material.

Table 1.1 lists estimated peak values expected for all param-

eters to be measured for Event 6. These values were, in most cases,

set up to be the upper bound of recording capability since prediction

information contained in Reference 5» made available Just before the

shot, indicated lesser motions, particularly at higher pressures.

Briefly, Reference 5 suggests that motion-to-overprcssure ratios,

predicted to be constant for a particular depth by Equations 1 and 2,

actually decrease at higher pressures due to the more rapid rate of

dccpy (öP/öt) of high pressures.

Estimated ground motions for Event 1A were calculated using the

methods of Reference 5. Recording ranges were then selected to be as

close as possible to the estimate. Soil stresses were calculated as

for Event 6, i.e. using Equation 1. Predicted motions and stresses

for Event 1A are listed in Table 1.2.

15

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CHAPTER 2

PROCEDUEE

2.1 DESCRIPTION OF TEST SITE

Distant Plain Events 6 and 1A were detonated on the Watching

Hill Blast Range of DRES. Over the area instrumented for this proj-

ect, the ground surface was essentially flat with an elevation of ap-

proximately 2}l6k feet above mean sea level. Geologically, the test

site lies in the southern end of the Ross Depression, which has appar-

ently once been covered by a large lake. The soils to a depth of 200

feet are lacustrine deposits consisting of fairly uniform beds of

clays and silts with occasional sand lenses (Reference 6).

Detailed accounts of the soil survey and testing are given in

References 7 and 8. Briefly, Project 3.10, Soil Sampling and Test-

ing (References 7 and 8), reported the upper 5^5 feet of soil to be

a tan, sandy, silty clay. From this point to a depth of about 30

feet, the soil was sandy silt. Below this depth to about 75 feet

was a gray plastic clay. The upper 30 feet of soil (both layers) was

about hO percent air by volume, resulting in a high compressibility.

For example, a dynamic uniaxial strain test on a sample taken from

the upper 5 feet produced a 23 percent vertical strain at U,000 psi.

Upon unloading, the material recovered only about 2 percent of this

strain (Reference 8).

18

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2.2 INSTRUMENTATION LAYOUT

A total of llh earth motion and stress gages were installed for

Event 6 to obtain measurements of particle velocity (38 channels),

acceleration (30 channels), and earth stress (U6 channels), ninety

gages, including all the stress gages, were installed in the pre-

dicted 300- to 2,0C0-psi overpressure range to assess strong earth

motions and stresses in the superseismic region, or region of first

arrival of the airblast-induced shock. Eleven locations were instru-

mented for ground motion in this region, at depths of 1.5 and 5 feet.

A single canister containing horizontal (radial) and vertical accel-

erometers and horizontal and vertical velocity gages was installed at

each location. A total of 23 locations were instrumented for earth

stress at depths of 1.5 to 30 feet. At each of eleven of these loca-

tions, three stress gages were installed, oriented so as to determine

vertical stress (PV), horizontal stress (PK), and stress at an angle

of U5 degrees with the horizontal (PS). By using the three gages

oriented as described, it was possible to calculate the principal

stresses, their directions, and the s'iear stress component. The

total gage array for Event 6 is listed in Tables 2.1 and 2.2, and is

depicted graphically in Figure 2.1,

For Event 1A, 51 gages were installed including 18 particle ve-

locity gages, 18 acceleroraeters, and 15 soil stress gages. For this

event, where assessment of airblast-induced motion was the objective,

19

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all c3^63 "were installed in the relatively high overpressure region

of ^00 psi to an estimated 10,000 psi directly beneath the shot tower.

The gage array for Event 1A is given in Tables 2.3 and 2.h, and in

Figure 2.2.

2.3 INSTRUMENTATION

2.3.1 Gages and Calibration. All particle motion gages used on

tnis project were commercially available units which have proved re-

liable in numerous field or laboratory soil motion experiments. The

particle velocity gages were the Sparton Southwest, Inc., Model 601.

This gage was developed under a Defense Atomic Support Agency contract

by Stanford Research Institute and modified by Sandia Corporation.

The Model 601 is a variable reluctance gage of the highly overdamped

accelerometer design.

Two different types of accelerometers were used. Pace Model Al8

variable reluctance gages were installed at expected acceleration

levels of less than 200 g's, while Endevco Model 226l semiconductor

strain gage accelerometers were used at higher levels.

The soil stress gages were constructed by the Waterways Experi-

ment Station (VTES) using our own design. Basically, the gage is a

dual diaphragm gage with two arms of a full semiconductor strain gage

bridge bonded to each diaphragm. Reference 9 gives a detailed ac-

count of the development and testing of this gage.

20

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All velocity gages were calibrated by using the free fall of the

pendulum method. The variable reluctance accelerometers were stati-

cally calibrated on a rotary accelerator (spin table), while the

strain gage moiels were dynamically calibrated with a dynamic shock

calibrator of the dropping ball type. The soil stress gages were

calibrated statically in a small pressure chamber.

The calibrations for all gages were reproduced just prior to

shot time by shunting a resistor across one arm of the bridge cir-

cuit, producing a circuit imbalance of a known velocity equivalence.

2.3.2 Gage Canisters and Placement. All motion gages installed

at a particular location were mounted in a single aluminum canister

along with associated calibration and line-matching electronics.

Figure 2.3 shows a typical canister with mounted gages. All canis-

ters were potted witn paraffin in order to (l) resist water leakage,

and (2) damp high frequency vibrations. The final density of the as-

sembled canister was 100 pcf, which provided a good match with the

in situ soil. The stress gages were cast in soil-cement plugs con-

sisting of native soil, about 3 percent portland cement, and about

10 percent water to enable compaction. For Event 1A, the motion gage

canisters were recovered after Event 6 and reinstalled intact. The

soil stress gages, however, were removed from their plugs, checked

out, and recast before installation for Event 1A.

21

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In all cases the instrument holes were backfilled with the same

soil-cement mixture used for the stress gage plugs. This mixture,

though perhaps slightly stiffer than the in situ soil, provided a

p;ood density match and is considered to be a significant improvement

over dry sand or cement grout for matching alluvial soils.

Instrument cables were protected downhole by heavy-duty rein-

forced rubber hose, and in the main cable trench were fed into 3-inch-

diameter plastic pipe. This method proved satisfactory since the few

cables which broke broke well after significant motion peaks had

occurred.

2.3«3 Recording System. Signal conditioning and recording

equipment, was housed in a wooden bunker located about 2 ,700 feet

southwest of Event 6 ground zero (GZ).

The basic signal conditioning equipment for all variable reluc-

tance gages was the CEC 113-B (System D), a 3-kHz carrier-demodulator

amplifier. Outputs from this system were recorded on CEC 5-119 oscil-

lographs. The strain-gage transducer outputs were fed into an opera-

tional amplifier system desi£"3d and constructed by WES, and were re-

corded on CEC VR-3300 FM magnetic tape recorders.

Calibration and recorder start signals were produced by a cam-

type timing device which itself was triggered by the -30-second sig-

nal from DRES Control. The -2-second signal from Control was used as

a safety valve, and was programmed to jump all recorders to operating

22

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speed. The zero time pulse from Control was recorded directly on all

oscillographs, and was superimposed on the 1-kHz timing channel on

magnetic tape. Figure 2.h shows the interior of the Project 3-02a

instrument bunker.

23

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TABLE 2.1 PARTICLE MOTION INSTRUMENTATION, EVENT 6

Station Range Predicted Airblast Overpressure

Gag in

;esa at Depths, Feet, of

1.5 5 10

feet psi

6101 h9 2,000 a >m X

6102 60 1,500 X X

6103 80 1,000 X X

6lOU 98 750 X X

6105 ihO hOO X X

6IO6 162 300 X X

6107 325 50 Y Y

6IO8 koo 30 Y Y

6109 U80 20 Y Y

6110 680 10 Y Y

X = vertical acceleration, vertical velocity, horizontal ac- celeration, horizontal velocity; Y = vertical acceleration, vertical velocity, horizontal velocity.

2h

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TABLE 2.2 EARTH STRESS INSTRUMENTATION, EVENT 6

Station Range Predicted Airblast Overpressure

Gagesa at in Feet,

Depths, of

1.5 5 17 30

feet psi

6101 ^9 2,000 — V V Y

6102 60 1,500 V X X Y

6103 80 1,000 V X X X

610U 98 750 V X X Y

6105 li+0 hOO V X X X

6106 162 300 V X z Y

V = vertical stress; X = vertical stress, horizontal stress, U5-degree (shear) stress; Y = horizontal stress; Z = vertical stress, horizontal stress.

25

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TABLE 2.3 PARTICLE MOTION INSTRUMENTATION, EVENT 1A

Station Range Predicted Airblast Overpressure

Gagesa

in Feet at Depths, ;, of

1.5 5 10

feet psi

1101 0 10,000 -- Y Y

1103 35 3,000 X X

HOU 53 1,500 X X X

1106 80 500 X X X

X = vertical acceleration, vertical velocity, horizontal ac- celeration, horizontal velocity; Y = vertical acceleration, vertical velocity.

26

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TABLE 2.U EARTH STRESS INSTRUMENTATION, EVENT 1A

Station Range Predicted Airblast Overpressure

Gages8, at Depths, in Feet, of

1.5 5 10

feet psi

1101 0 10,000 Y Y Y

1101+ 53 1,500 — X X

1106 80 500 — X X

Y = vertical stress; X = 3-component stress (horizontal stress, vertical stress, U5-ciegree (shear) stress 1.

27

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>- I-

s 10

— o o 8 > < s ^1

o CO

. o o ii « » Z K M

> s til

< ' < . a + X4

8 - o o z

UI 0 UI J

z

> I U K K 0 U K 0 111 ^ s D 3 • • < M Z 0 i i i m

10 I > < Q. IS N m o o < 3 M • •

> > ? < < Q.

h ^ K aom o z

111 + X

u- S - a a < • u ^ ^ s < t « + X M O — * _ a a X X o - J

t ^ V

z 0 + X

a s - a a X •

1 > V

+ ><

s - a a X X

> ^ + X

s - D D X •

> K

+ 01

1

a

i 1

+

1

1 'ft itt o o o o

1 " w d rj s

OJ

I

X33J 'HJ.d3a

28

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h a X a

x a

t- u u IL

III'

< h M 5 j < z 0 N

8 X

!h a x a

x a

I

I It K ♦ r

SI h o n U 3 J >

I <

M Id Id B O HI

. O

ui 3

*" u ' I a. M

< J < U

> 3

K III J Ü 111 H U C U ill < > • i

< >

> <

o a o z

SO^ + o

+ o

§ •H

'S

•P w C H

CVJ

CM

id

o

133d 'HXdSQ

29

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?•/ •ii-fpl t

NOT REPRODUCIBLE

30

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HOT *o.

C/8

0) X c 3

r O

-P c V

-p w c

•H

o fs o

•H fn <U

+3 C

CJ <D U

•H Ct-

31

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CHAPTER 3

RESULTS AND DISCUSSION

3.1 DATA RECOVERY

The calibration and recording sequence initiating signal at -30

seconds was received and all equipment operated as programmed for

both Events 6 and 1A. A good zero time pulse was recorded for both

events.

Of the 11^ gages installed for Event 6, 110 yielded good quality-

data. Two gages were inoperable at shot time, and two additional

r;ages produced extremely noisy outputs and yielded no usable data.

A summary of peak measured motions, first integrals of accelerations,

and shock arrival times is presented in Table 3«1. Peak stress data

are summarized in Table 3.2.

Fifty-one gages were installed for Event 1A, and all were oper-

able at shot time and indicated shock arrival times. However, the

four motion gages located beneath the tower yielded no useful peaks

due to strong signals which overdrove the galvanometers and saturated

the magnetic tape systems. The remaining U7 gages all produced good

quality data. Table 3.3 presents peak measured and computed (inte-

grals) motions obtained on Event 1A, and Table 3.^- lists the corre-

sponding stress data.

Appendix A contains time histories of all motion and stress

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records obtained for Event 6. Appendix B is a similar presentation

of Event 1A data.

3.2 ARRIVAL TIMES, EVENT 6

Shock arrival times were established for all 110 successfully

recorded gages on Event 6. For the most part, good agreement was

noted for arrival times registered by the several gages located at

a single point. In the case of motion gages, the vertically oriented

accelerometer generally had the most rapid frequency response and in-

dicated the earliest shock arrival, as would be expected. The latest

arrivals were most often recorded by the horizontal velocity gages

partially because of the slower response of velocity gages and, addi-

tionally, because of the relatively low initial motion. (This point

will be discussed in more detail later.)

Shock propagation velocities were calculated from the measured

arrival times and were found to average approximately 1,100 ft/sec

for the near-surface layer and approximately 5,?00 ft/sec for the

saturated lower layer. Both of these values are in close agreement

with results obtained on Operation Snow Ball (Reference 3) and by

seismic surveys.

Figure 3.1 is a shock front profile for Event 6 constructed from

airblast arrival time data (Reference 10), ground shock arrival times

measured on this project, and the calculated propagation velocities.

33

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Development of outrunning refracted energy can easily be seen on this

plot. Directly induced energy, refracted along the higher velocity

layer, is continuously fed back into the overburden as an upward-

moving shock front. Figure 3.1 indicates that this upward-moving

wave began to outrun the airb last-induced wave at the surface at a

distance of about ^00 feet, or at a pressure level of about 30 psi.

The 30-psi level is very nearly the same point of outrunning noted

for Snow Ball, detonated at the same site but of five times the yield

of Event 6,

3.3 VERTICAL FARTICLE ACCELERATION

3.3»! Event 6. Peak vertical particle accelerations for Event

6 are plotted versus horizontal range in Figure 3.2. Data from all

three depths instrumented, i.e., 1.5» 5> and 10 feet, are shown, and

attenuation of motion with both increasing depth and distance is ap-

parent. In the superseismic region, at distances of less than ^00

feet, however, there is some data scatter, and attenuation patterns

are less pronounced. One point in particular (at a distance of 98

feet from GZ and a depth of 1.5 feet) appears high.

At both the 1.5- and 5-foot depths, a trend is noticeable toward

a flattening of the curve at shorter ground ranges (or conversely,

i.e. at larger distances, the curve steepens). This is what Refer-

ence 5 predicted would happen at high overpressures and lends support

3h

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to the proposed decrease of motio.i-to-overpressure ratios with in-

creasing overpressure.

Data presented in Flgui* 3.2 from locations in the outrunning

region are airblast-induced downward peaks in order to maintain con-

sistency for correlation purposes. In this region, the airblast-

induced motion arrived later than refracted energy but clearly domi-

nated that from the outrunning wave at the 1.5-foct depth, being an

order of magnitude or so higher. At the lO-foot depth, however, the

upward pulse from the refracted wave and the airblast-induced motions

were roughly equal in magnitude.

3.3»2 Event 1A. Figure 3«3 is a plot of peak downward acceler-

ation versus horizontal distance for Event 1A. A rapid attenuation

of acceleration is apparent with both depth and distance. A quite

rapid attenuation with depth, somewhat more rapid than noted on Event

6, can be seen between the 1.5- and 5-foot depths, although insuffi-

cient data points are available to establish a firm trend.

Figure 3.U shows time histories of the three vertical accelera-

tions at l.'i-, 5-> and 10-foot depths at a distance of 53 feet. The

sharp downward spike, characteristic of airblast-induced motion, is

seen at all three depths and is followed by an upward rebound. This

rebound was consistently about ho to 50 percent of the downward peak

magnitude, and was very nearly the same as for Event 6, indicating a

lack of effect of shot geometry or yield on this phenomenon. The

35

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airblast-induced pulses demonstrate clearly the pulse widening and

lengthening rise times at increasing depths which is generally asso-

ciated with the passage of a sharp disturbance through dissipative

materials. The rebound pulse is also noted to increase in width with

increasing depth.

3.3»3 Discussion and Correlation. In general, vertical parti-

cle accelerations appeared to be somewhat higher at equivalent over-

pressures for Event 1A than for Event 6. Figure 3.5 is a plot of the

ratio of acceleration to overpressure (g's/psi) versus overpressure

for the 1.5-foot depth. Included in this plot for comparison pur-

poses are data from Distant Plain Event 3 (Reference k) and Flat Top

Events II and III (data at a nominal 1-foot depth, Reference 11).

These three events were geometrically identical, i.e. 20-ton half-

buried spheres of TNT. Distant Plain Event 3 was detonated at DRES,

Drowning Ford Site, and the Flat Top shots were fired at the Nevada

Test Site (NTS). From Figure 3«5> it is obvious that a good correla-

tion exists among these several detonations to the extent that charge

weight (a factor of five between Distant Plain Event 6 and the

others) and location (ORES versus NTS) have no apparent effect. As

mentioned above, the data from Event 1A were somewhat higher at

equivalent overpressures than for Event 6, and fall clearly above the

body of the points in this figure. This may be explained by the fact

that rather disturbed airblast waveforms were noted for Event 1A,

36

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including secondary shocks and a somewhat flattened waveform as op-

posed to classical peaks (Reference 12).

The trend toward lesser motion/overpressure ratios at higher

pressures predicted by Reference 5 is evident in Figure 3*5• A

straight line fit to the data points indicates a decay of this ratio

from about 1 g/psi at 20 psi to about 0.U g/psi at 1,000 psi. There

is admittedly a lot of scatter in the data, but none of the detona-

tions, except Event 1A, produced data uniformly high or low with

respect to the average, and a +30 percent variation would include

most of the data points.

Figure 3«6 is a plot of accelerations normalized to the 1.5-foot

depth versus depth. This plot shows the relative attenuation with

depth below the 1.5-foot depth for Distant Plain Events 6, 1A, and

3. There is somewhat more data scatter at the 5-foot depth than at

the 10-foot depth, contrary to what might be expected. Again, dif-

ference in yield was not a significant contribution. From this plot,

accelerations at 10-foot depths are seen to drop off to about 0.075

+ 20 percent of those measured at 1.5-foot depths, while those at the

5-foot depths ran about 0.20 + 50 percent of the shallower data. For

Operation Snow Ball, no instrumentation was installed at the 1.5-foot

depth. However, accelerations measured at a depth of 15 feet aver-

aged 26 percent of those at 5 feet. An extrapolation of Figure 3.6

data to the 15-foot depth would indicate that 26 percent is a

37

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reasonable figure for attenuation from 5 to 15 feet. Thus a quite

rapid attenuation of acceleration in the DRES alluvium (above the

water table) is seen to exist. This can be attributed to the very-

high compressibility and hysteretic behavior of the upper layer of

soil, which, as stated previously, was about ho percent air by

volume.

3.^ HORIZONTAL ACCELERATION

Peak outward horizontal (radial) accelerations are plotted ver-

sus distance for Events 6 and 1A in Figures 3«7 and 3.8, respectively.

A rapid attenuation with both increasing distance and depth is ap-

parent for data from both events, although the Event 6 data (Figure

3.7) show some scatter and the attenuation patterns are less well

defined.

The peak horizontal accelerations (AH) for both events were con-

siderably less than corresponding vertical accelerations (AV) at all

pressure levels and depths instrumented. The ratio of AH to AV

ranged from 0.1 to 0.3, indicating the predominantly downward direc-

tion of the airblast-induced ground shock, at least at these rela-

tively high pressure levels (>300 psi),

3.5 VERTICAL PARTICLE VELOCITY

3.5.1 Event 6. Figure 3.9 presents peak vertical particle ve-

locities from Event 6 versus horizontal distance for all three depths

38

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instrumented. As with the accelerations, rapid attenuation with both

distance and depth is noted, with the flattening effect at closer

distances again apparent. The curve decay between the superseismic

region and the outrunning region is quite steep, in fact, is steeper

than the acceleration decay. This would seem to point out that

airblast-induced particle velocities are affected to some extent by

the phenomenon of outrunning itself. That the effect, whatever its

cause, is real is evidenced by the fact that the groups of data

points are consistent in themselves.

An interesting aspect of this plot is the seemingly large motion

measured at the 98-foot distance and 1.5-foot depth, exactly what was

noted in Figure 3«2, the acceleration-distance plot. This reinforces

the credibility of the data. At the same time, however, the measure-

ment at a depth of 5 feet was the least of all the superseismic meas-

urements at that depth. This would suggest a local anomaly at the

1.5-foot depth and 98-foot distance, possibly arising from inconsist-

ent or particularly soft backfill in the upper 1.5 feet.

3.5»2 Event 1A. Figure 3.10 shows peak vertical velocities

versus distance measured on Event 1A. A quite consistent pattern

can be seen, vith the flattening effect again prominent at both I.5-

and 10-foot depths.

The peak velocities are somewhat higher than were the

39

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measurements at similar pressure levels on Event 6. This, too, is

consistent with the acceleration data.

3.5.3 Discussion and Correlation. On past events, vertical

particle velocity data have been more easily correlatable, and con-

sequently more accurately predicted, than acceleration data. For the

same five experiments discussed in Section 3»3.3 (Distant Plain 6, 1A,

and 3, Flat Top II and III), however, this does not appear to be the

case.

Figure 3«H is a correlation based on the particle velocity to

overpressure ratio. More scatter is shown here than was noted for

the acceleration data, with Distant Plain Fvent 6 data points con-

tributing heavily to this. It was stated in Section 3«5.1, however,

that there was a very rapid decay of particle velocity in the out-

running region, and this shows up strikingly in the four Event 6 data

points in the lower right-hand corner of Figure 3.11. Neglecting

these four points, a more consistent relationship stands out, with

the majority of the points falling within +^0 percent of an average

curve. As expected, the ratio increases with decreasing overpressure,

from about 0.03 ft/sec/psi at 1,600 psi to 0.08 ft/sec/psi at 10 psi,

roughly the same rate of increase as the acceleration data. This, in

turn, would imply a constant relation between acceleration and veloc-

ity over the region discussed, i.e. 10 psi to about 1,600 psi, which

can be expressed as follows: a(in g's) - 13u (in ft/sec).

i+0

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The scatter in velocity data is again encountered when an at-

tempt is made to correlate depth attenuation, as in Figure 3.12.

Here only a very general attenuation with depth is noted, with con-

siderable overlapping of the data from various depths. Nevertheless,

useful information can be gained from this plot if the lack of pre-

cision is kept in mind when attaching significance to the decay char-

acteristics. At a depth of 5 feet, the velocities appear to be

roughly 0.^ + 50 percent of those at 1.5-foot depths, and at 10-foot

depths are about 0.3 + 50 percent of those at 1.5-foot depths. The

Flat Top III data are, with one exception, quite consistent in aver-

aging a ratio of O.lU for the 17-foot depth instrumented on that shot,

These rates of attenuation are all less than noted for accelerations,

which can be attributed to the dependence of peak acceleration not

only on the peak velocity, but also on the velocity rise time, which

increases with distance traveled by the shock wave.

3.6 HORIZONTAL PARTICLE VELOCITIES

Horizontal (radial) velocity, probably more than any other pa-

rameter, shows distinctly the arrival of two separate disturbances

for the crater-producing detonations: the airblast-induced and

direct- or cratering-induced motions. Figure 3.13 shows a selection

of horizontal velocity gage records from the 5-foot depth and at dis-

tances of i4-9> 60, and iho feet for Event 6. The initial arrival of

1+1

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the airblast-induced motion is clearly seen on each of these time

histories. It is followed by a crater-induced pulse of both greater

magnitude and significantly longer duration. The time period be-

tween arrivals steadily increases with distance, since in this re-

gion (>300 psi) the airblast wave is traveling several times as fast

as the directly transmitted energy.

Airblast-induced horizontal velocities have generally been dif-

ficult to correlate since well-defined attenuation patterns often do

not exist due to data scatter. Figures 3-Ik and 3.15 plot airblast-

induced horizontal velocity versus distance for Events 6 and 1A,

respectively, and in both cases this axiom holds true. Both events

exhibit broad patterns of attenuation with depth and distance. How-

ever, the fivefold scatter of the data would make any straight line

fit extremely tenuous at best.

Figure 3.16 is a plot of cratering-induced horizontal velocity

versus distance for Event 6. Regular decay is noted to exist, in

contrast to the airblast-induced motion, and there is relatively

small data scatter. The rate of attenuation with distance is as the

-2.7 power of distance, a reasonable number for energy transmission

through alluvial soil. Motions at 1.5- and 5-foot depths are not

significantly different, pointing out the primarily outward direction

of motion of this pulse.

U2

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3.7 DISPLACEMENT

Tables 3.5 and 3.6 list peak transient displacements calculated

from particle velocity measurements for Events 6 and 1A, respectively.

For Event 6, both peak upward and downward vertical displacements are

listed, while for Event 1A, where no cratering-induced motion existed,

only downward vertical displacements are listed.

From Table 3.^ it can be seen that the upward (cratering-

induced) displacements greatly exceed the downward (airblast-induced)

displacements at the smaller distances. This is caused by the very

much longer duration of the cratering-induced velocity. Cratering-

induced velocity attenuates more rapidly, however, such that its ad-

vantage in duration is diminished, and at the greater distances the

upward and downward displacements become roughly equal.

Figures 3.17 and 3.18 are plots of upward and outward cratering-

induced displacements, respectively. Rapid attenuation of displace-

ment is evident in both cases, with the vertical component decreasing

as the -3.7 power of distance and the horizontal as the -2.h power.

The airblast-induced displacements for Event 1A (Table 3.6)

show the sharp decrease with depth dictated by a highly compressible

medium. With the exception of the horizontal displacement at Loca-

tion llOl+l, which appears unreasonably low, both components of dis-

placement at the 1.5-foot depth were three to six times greater than

corresponding displacements at the 10-foot depth.

^3

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A comparison of vertical downward displacements at locations of

similar overpressure s:.ows that displacements for the two events were

at least similar. For example, displacements at Locations 61061 and

61062, Event 6, where the overpressure was 280 psi, were 0.31 and

0.10 foot, respectively; at Locations 11061 and 11062, Event 1A,

where the overpressure was 310 psi, displacements were 0.20 and

0.11 foot.

3.8 SOIL STRESS MEASUREMENTS

3.8.1 Event 6. Figure 3-19 is a plot of peak vertical stress

versus distance for Event 6. The data points plotted for the 1.5-

foot depths are consistent in themselves in defining a rather slow

rate of attenuation with distance. Inasmuch as all these points

are in the superse:smic region, the attenuation rate would seem to be

consistent with the flattening noticed for particle velocities (Fig-

ure 3-9' and accelerations (Figure 3.2) in the same region.

Vertical stresses measured at the 5- and 17-foot depths exhibit

a great deal more scatter than do stresses at the shal.ower loca-

tions. In particular, the data from both depths at the lUO-foot dis-

tance are significantly higher than the body of data and contribute

heavily to an anomalous decay pattern. Neglecting these two points

as being atypical, depth attenuations were calculated for comparison

with particle velocity data. Peak stresses at the 5-foot depth aver-

aged 0.25 + 50 percent of those at 1.5-foot depths, which is a more

kk

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rapid decay with depth than the O.U + 50 percent noted for velocities.

Figure 3.20 is a plot of peak horizontal stresses measured at the

30-foot depth. Figure 3.1 indicates the primary disturbance at this

depth to be a horizontally moving direct-induced wave. Since the

soil medium below a depth of about 22 feet is a saturated material of

low compressibility and low shear strength (approximately 10 psi,

Reference 8), the rate of stress attenuation could be expected to

approximate that in free water, i.e., attenuation as the -1.13 power

of distance. This is in fact the case in Figure 3.20, since the five

points measured over a horizontal distance of ky to 162 feet define

an attenuation as the -1.15 power of distance with only a small

amount of scatter present.

3.8.2 Event 1A. Soil stress measurements for Event 1A (Table

3.^) were limited to thr^e locations under the shot tower and four

additional locations; for this reason no graphic display of attenua-

tion with depth or distance would be pertinent. The only measurement

of stress at the 1.5-foot depth was beneath the shot tower, and the

peak was ^,960 psi. Peaks of 951 and 276 psi were measured at the

5- and 10-foot depths, respectively (Figure 3.21). The ratio of

stress at 5-foot depth to that at 1.5-foot depth was 0.19, which is

in reasonable agreement with ratios calculated for Event 6 data.

3.8.3 Three-Component Stress, Events 6 and 1A. Three compo-

nents of stress were successfully measured at eight of the eleven

^5

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ionations wliere arrays were installed for Event 6, and at all four

locations for LVent 1A. Not all of these measurements proved useful

for the calculation of shear stress, however, primarily due to ten-

nlle stress indications on the horizontally oriented gage. Calcula-

tions of s.'iear stress and principal stresses were accomplished for

tiirce arrays on each event, however; Figures 3.22 through 3.27 are

time histories of the calculated shear and principal stresses for

these locations.

The first two plots for Event 6 (Figures 3.22 and 3.23) are from

the 1'iO-foot range and 17-foot depth and the 162-foot range and 5-

foot depth, respectively. Data from both of these points show a

single major pulse of shear stress on the order of 60 psi. In both

cases the peak major principal stress is higher than the measured

vertical strecs (2h and 60 percent higher, respectively) and the mi-

nor principal stress is very low, often negative. The third plot for

Event 6 (Figure 3.2U) is from a point below the water table, 80-foot

range and 30-foot depth. The shear stress from this location rises

sharply to a peak of -Uo psi, then after several rather sharp oscil-

lations, oscillates with a longer period about a -25-psi mean. The

major and minor principal stresses are noted to have a very similar

waveform, and a nearly constant difference (a. - aO of 50 psi. This

implies a Mohr envelope with a j^ of 0 , which is consistent with

U6

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soils test data (Reference 8) from samples from below the water

table.

Figures 3.25, 3.26, and 3.27 present shear and principal stress

calculations for three locations from Event 1A. The first two plots

(Figures 3»25 and 3.26) are for the 5- and 10-foot depths at a dis-

tance of 53 feet from GZ. The major principal stress is somewhat

lower at the 10-foot depth than at the 5-foot depth, as expected, and

in both cases the major principal stress is within 20 percent of the

measured vertical stress. The peak shear stresses for the 5 and 10-

foot depths were hO and 50 psi, respectively, which is reasonably

close to that determined for the two points for Event 6 (approxi-

mately 60 psi).

Figure 3«27 presents the data from the 80-foot range and 5-foot

depth for Evem -'■.. The major principal stress calculation again

showed very close agreement with the measured vertical stress (350

psi calculated versus 317 psi measured). The peak shear stress was

100 psi, making both shear and major principal stresses considerably

higher than was found at the same depth but closer to GZ (Figure

3.25). The waveform at the closer stations (53-foot range), however,

is somewhat disturbed, and resembles more closely that measured below

the water table on Event 6 (Figure 3.2h), A local anomaly, perhaps

arising from a disturbed airblast wave, is thus suggested at the 53-

foot range.

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Page 50: DISTANT PLAIN EVENTS 6 AND 1A PROJECT 3.02A, … · technical report n.70-14 distant plain events 6 and 1a project 3.02a, earth motion and stress measurements by d. w. murrdl stptombtr

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TAhLK i.i M'TI n DATA HUMMAflY, KVEOT 1A

Luoation Ottge ilorizontal Depth Time of Acceleration Velocity Type Range Arrival and

... a rlontation

feet feet msec g's ft/sec

.1012 AV 0 5

11013 AV 0 10 UV

11031 AV 33 1.5 irv Al! im

11033 AV 35 10 uv AH UH

UO'il AV 53 1.5 UV AH UH

1101.2 AV 53 5 UV AH UH

U0U3 AV 53 10

All UH

11061 AV 80 1.5 UV AH UH

11062 AV 80 5 UV AH Uli

11063 AV 80 10 uv AH UH

6.2 No peak recorded 6,6 No peak recorded

12.8 No peak recorded 11.0 No peak recorded

5.3 731 38 .1 6.8 — 1+3 .1+ 5.9 10U 8.37 7.5 — 1+ .2

13.1 58.5 11 .25 13.5 mm 6 .52 12.6 13.9 2, .56 10.0 — 1 ■ 96

8.0 682 38. .0 8.8 -- 36. .1 8.0 103 l+. .3 8.6 -- 2. .6

11.7 61+.5 10, .5 12.9 — 11, .1 13.8 21.5 1, .1+7 Xh.Z — 1, .85

13.0 hk.2 9. ,1+ 15.1 — 6, .27 17.0 11.5 1, ,1+0 15.2 — 1, • 96

12.7 293 19. ,8 13.6 mm 11+, 3 11.0 60.2 2, ,0 13.U ~ 1, .73

15.7 1+6.1 7. ,1+ 17.6 .- 6. ,1+1 16.5 h.h 1. ,60 17.0 -m 0.7»+

21.5 2I+.7 1+. ,88 22.U mm 3. ,66 21.1 3.21+ O.63 22.8 — 0. 58

a A = acceleration, U - velocity, V = vertical, H = horizontal.

50

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TABLE 3.'+ STRESS DATA SUMMABY, FVKIIT 1A

Location Gage Horizontal Depti; Time of Peak Typ e Range 1 Arrival Stress and Orientation

feet feet msec psi

11011 PV 0 1.5 h .h U,96o

11012 PV 0 5 7 ,h 951

11013 PV 0 10 11 .8 276

1101+2 PV 53 5 11 ,2 161+ PH — — 10 .6 79.^ PS — — 9 .1 121

110U3 PV 53 10 13 .h 108 PH — — Ih .9 77 PS — — 15 .0 116

11062 PV 80 5 13 .8 317 PH mm — 13 .8 55.3 PS _M — 13 8 107

11063 PV 80 10 16 6 1+6 PH mm — 17 1 12.5 PS — — 16 0 75

P = stress, V = vertical, H = horizontal, S = shear (1+5 degrees).

51

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TABLE 3.5 PEAK TRANSIENT DISPLACEMENTS, EVENT 6

Location Range Depth Peak Displacement

Downward Upward Outwar

f e e t f e e t f ee t f e e t f e e t

61012 k9 5.0 0.17 5 . 1 6 .5

• 1021 60 1.5 0 .3 5.2 3 .2

u 1022 60 5.0 — — 6 .0

61031 80 1.5 0.17 1.56 1.52

'1032 80 5 .0 0.08 1.80 1.70

6l0Ul 98 1.5 0.32 0.18 l.hO

•101+2 98 5.0 0.08 0.65 0.80

61051 1U0 1.5 0 .31 — 0.68

61052 1U0 5 .0 0.15 0.17 0.82

' 1061 162 1.5 0 .31 — O.36

61062 162 5.0 0.10 __ 0.38

52

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TABLE 3.C PEAK TRAITS lEI.T DISPLACEKEIITS. EVEIIT 1A

Location Ran.^e Depth Peak Displacement

Downward 'utwarJ

feet feet feet Teet

11031 35 1.5 0.56 0.19

11033 35 10 0.13 O.O85

11041 53 1.5 0.50 0.040

110i+2 53 5 0.20 0.15

110^3 53 10 0.13 0.15

11061 80 1.5 0.20 0.27

11062 80 5 0.11 0.09

11063 80 10 0.06 0.0)45

53

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■P c 0)

■ H

g ft

■p c o ft

SH

A:

o .c

i33J 'Hid30

sU

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1000

soo

too

so z o p < y j u o u <

10

b ' ' ' 1 II 1 1 1 1 1

i i

i r

£

0 0

0 0

—^

1

6

i 4 I

^

A

0 0

—^

U- 0 J

1 LEGEND

0 1.5-FOOT DEPTH A 5.0-FOOT DEPTH D 10.0-FOOT DEPTH

1 III I.I 11

0

D D

1 1 1

III

D —

10 SO 100

HORIZONTAL DISTANCE, FEET

500 1000

Figure 3«2 Peak vertical downward acceleration versus horizontal distance, Event 6.

r)5

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z o h < tr iij _i UJ

u u <

1000

- T ■■" ' T ■■ T T 1 1 1

-^

- 0

0 -^

500 " |

- -J

-

0

LEGEND

1.5-FT DEPTH

0 —1

A

D

5-FT DEPTH

10-FT DEPTH

100

&

J

- D —j

50

Q A

5n 1 1 1 1 1

a

i i i

10 50 100

HORIZONTAL DISTANCE, FT

200

:'l"Mrc 3•3 Peak vortical 1 ovmvarci acceleration versus horizontal distance, FVent 1A.

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500n

h 53-1-fiV

-500-

-I.OOO-1

50n

z o h < IT Hi J u u u <

^-^

-50-

-100-»

53-5-flV

25

-25

-50.

A I X^-"'"-— n>*

"I

53-10-flV

i 1 1 1 i 1 1— 0.00 0.05 0.10 0.15 0.20 0.25 0.30

TIME FROM DETONATION, SECONDS

—I 1 0.35 0.40

Figure 3«^ Time histories of vertical acceleration, '3-foot horizontal distance, Event 1A.

S7

MMaaUMUnasa _>_aaaaaaa_Maai>aiaa_^^MBaBaaaaaaBa^MaBaB^Haaaa ■HMMMBi

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10.0

s.o

u c

c U 1.0 o -v z o p K 0.S u J Ul u u <

0.5 2,000

_ TTT-T- —r— n r 111 i 1—i—i—i :

: UKflKW : - 0 DISTANT PLAIN 6 -

• DISTANT PLAIN IA ' A DISTANT PLAIN 1

-

0 PLAT TOP II ■ PLAT TOP III

■ 0 0

_ ■ ^^ I _ 0 L *—-"^ •"^^ - \ o a t00g00. —^^ ■ - *~ a A

§ ^^0^ ■ 0 L ^0000» -— 1 i -

• 0 0 -

1 1 1 1 1 • " 1 1 1 1 i i i

1.000 500 100

OVERPRESSURE, PSI

SO 10

Figure 3.5 Correlation of vertical accelerations, 1.5-foot depth.

58

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0.05

0.02

DEPTH,FEET

Figure 3.6 Vertical acceleration attenuation with depth.

59

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100

80

z o P < K Id J U u

1 I—1—1-1 1 ' ' 1

0 | LEGEND

i 0 1.8-FOOT DEPTH 0 A 8.0-FOOT DEPTH

1 "1

i 1 i

A

0 J

o -

u A i i

A

1

1

1 1 1 1 1 III 20 SO too

HORIZONTAL DISTANCE, FEET

500

Figure 3.7 Peak outward horizontal acceleration versus distance, Event 6.

60

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200

too

so

z o p < III J 111 Ü

10

T 1 1 l i i |

LEQENP

0 1.8-FOOT DEPTH A 5.0-FOOT DEPTH 0 10.0-FOOT DEPTH

0 O

_ -■

- 0 -

- -

-

A

-

D

a

- -

- -

- -

- -

A

1 1 1 1 1 1 1 10 SO 100

HORIZONTAL DISTANCE, FEET

200

Figure 3.8 Peak outward horizontal acceleration versus distance, Event 1A.

61

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100

so

10

IL

ü 0 J u >

0.5

0.1

III II II I 1 1 1 I li

t

<

0 0 0

0 —

_

A A

«_

— —

, 0

0

LMENp

0 1.5-FOOT DEPTH

A S.O-FOOT DEPTH -" Q 10.0-FOOT DEPTH

1 1 1 II II

0 0

1 1 1

o —

a 1 1 II

10 SO 100

HORIZONTAL DISTANCE. FEET

500 1000

Figure 3.9 Peak vertical downward particle velocity versus distance, Event 6.

62

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too

u «

t > »-

J u > 111 J o h

< 0.

80

10

—1 1 1— 1 1 1 1

_

0

LEGEND

0

0

A

— 0 1.5-FT DEPTH A 5-FT DEPTH D 10-FT DEPTH

Q D A

.1.. 1 1 ,

D

-i 1 V \ 10 50

HORIZONTAL DISTANCE, FT

100 200

Figure 3-10 Peak vertical downward particle velocity versus distance, Event 1A.

63

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1.0

_ 0.5

ü M »- b.

|J E

U

>- h

-I U > UJ J o h

<

o.i

o.os

0.01

_ MM —1 1 1 i i 1 1 |—i 1 1 _ - LEfiEUD -

- 0 DISTANT PLAIN 6 • DISTANT PLAIN 1A - A DISTANT PLAIN 9

FLAT TOP II a

-

■ FLAT TOP III

-

a - _

- ■ 0

• n ^- -IP,».—•<

a

-

- 1

ö >-—VT ^ a

c

~ • ( .0 ■

i i i i

a

i i i ii i i

0

0

l i i

-

2,000 1,000 500 100

OVERPRESSURE, PSI

50 10

Figure 3«11 Velocity/overpressure ratio versus overpressure, 1.5-foot depth.

61+

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1.0

t o.s u 5 h 8

o.i

\ i 1 r RCFERCNCE POINT

\. \ \ \

-i—i—r

N.

N:

_i I I L

LEGEND

O DISTANT PLAIN 6 • DISTANT PLAIN 1A A DISTANT PLAIN 3 ■ FLAT TOP III

N \ \

■ \

i i i S 10

DEPTH, FEET

SO

Figure 3«12 Vertical particle velocity attenuation with depth.

65

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20-1

10 V—r

61012 •♦9-5-UH

-10

o w

i- u. >■"

h

8 J UJ >

10-.

6-

61022 60 5 UH

-sJ

61052 140 5 UM

-i ->

i— 0.00

-I— 0.06

—T- 0.10

I 0.20

—I— 0.25

—I 0.40 0.15 0.20 0.25 0.30

TIME FROM DETONATION, SECONDS

0.35

Figure 3.13 Time histories of selected horizontal velocities, Event 6,

66

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5,0

1.0

o.s

0,1

1 1 —1— 1—r-r- 1 r T ■—i—i—r-T i

kfiSEüC

0 1.5-FOOT DEPTH A 5.0-FOOT DEPTH

-

1 1 0 0 10.0 FOOT DEPTH

0

6 (

0

- 0 -

- & -

A

* 0 a

0

0

D

1 ' 1 i L_l_

0

1 —1— .

0

0

I 1 L_l 20 100

HORIZONTAL DISTANCE, FEET

500 1.000

Figure 3,lh Peak outward airblast-induced particle velocities versus distance, Event 6.

67

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10.0

s.o

10

J III >

1.0

0.B

-I 1 1 1 1 1 T-l- ~ LEGEND - -

- 0 A

1.5-FOOT DEPTH 5.0-FOOT DEPTH

' 0 10.0- FOOT DEPTH -

- 0

-

0

Q 8 o •

- -

- A - -

- a - ' ' i i i i

10 50

HORIZONTAL DISTANCE, FEET

100

Figure 3.1r Peak outward airblast-induced particle velocities versus distance, Event 1A.

68

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100

so

u

(- Ü.

>■" I- 0 3 8 u >

0.5

III II II 1 11-

: \

^

2.7

>

\

LEGEND

0 1.5-FOOT DEPTH A 5.0-FOOT DEPTH

\

1 1 1

III MM

II

1 1

10 80 100

HORIZONTAL DISTANCE, FEET

500

Figure 3.16 Peak outward cratering-induced particle velocity versus distance, Event 6.

69

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10.0

5.0

(- tu 111 U.

h" Z u i u u < J a V)

5

1.0

0.5

0.1 10

-L

1—I—I—I—I

LEGEND

O 1.5-FOOT DEPTH

A 5.0-FOOT DEPTH

3.7

J I I—L

SO 100

HORIZONTAL DISTANCE, FEET

200

Figure 3.17 Peak upward transient displacement versus distance, Event 6.

70

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10.0

5.0

I- u u U.

h Z ttl ! u u < J

Si i.o Q

0.2

1

1

1

1

—1—1—I—I—

V

i i 1

LEGEND

0 1.5-FOOT DEPTH

A 5.0-FOOT DEPTH

-

\ I

>

o\

i <

2.4

1 1 _ 1 1 1 1

i \ A

\ 0

i \ L .. .1 .... 20 50 100

HORIZONTAL DISTANCE, FEET

500

Figure 3.18 Peak outward transient displacement versus distance. Event 6.

71

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500

vi 100 lü E M

SO

20

—1

1 1

DO

O- c , r „._.1 r _„„

o 0 UEfiBiB

0 1.5-FOOT DEPTH

A A 5.0-FOOT DEPTH

G 17.0-FOOT DEPTH "

0

r T

i

i

>

i

a

i

I 1 I I

i

i .. I J 50 100

HORIZONTAL DISTANCE, FEET

500

Figure 3.19 Peak vertical stress versus horizontal distance, Event 6.

72

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1,000

500

id 8 Hi c h m

100

SO

T ■■ T— - 1 1 1 1

-

: \

-

0

\.

- 1.15 N.

-

-

1

I I i i -

20 50 100

HORIZONTAL DISTANCE, FEET

200

Figure 3«20 Peak horizontal stress versus horizontal distance, 30-foot depth, Event 6.

73

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1.000

500 - GZ-l-PS

-500 •-

t.OOO r-

500 -

x t-

bi

GZ-5-PS

-500 L-

300 i-

200 -

100 - GZ-IO-PS

0.00 0.10 0.20 0.30 0.40

TIME FROM DETONATION, SECONDS 0,50

Figure 3.21 Stress-time histories, ground zero, Event 1A.

7^

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m in Ui c (- w

< u I m

STATION - 61054 RANGE - 140 FEET DEPTH 17 FEET

100

200 i-

</) ill K (-

100 -

-100

MAJOR PRINCIPAL STRESS

20 40 60 80

TIME FROM DETONATION, MSEC

100

Figure 3.22 Shear and principal stress data, Location 6IO5U. Event 6.

75

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60

U a. i- ui IT -t UJ I 20 -

STATION -61062

RANGE - 162 FEET

DEPTH -5 FEET

20 40 60 BO 100

100 r-

50 -

HI

h

-50

MAJOR PRINCIPAL STRESS

V_/

MINOR PRINCIPAL STRESS y

± -L 20 40 60

TIME FROM DETONATION, MSEC

80 100

"igure 3.23 Shear and principal stress data, Location 61062, Event 6.

76

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20

(0 D: < Uj -20 in

-40

-50

STATION -61035 RANGE -80 FEET DEPTH -30 FEET

20 40 60 80 100

200

s

a v)

-200

MAJOR PRINCIPAL STRESS

MINOR PRINCIPA J"' L STRESS^

J_ l

20 40 60

TIME FROM DETONATION, MSEC

80 100

Figure 3«2^ Shear and principal stress data, Location 61035, Event 6.

77

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60 i-

if 40 in in ui IT I- VI a < Ui i in

20

20

STATION - 11042 RANGE -53 FEET DEPTH -5 FEET

40 60 60 too

200 r

100 -

Ui Hi K h

-too

7^

MINOR PRINICPAL STRESS

J_ X 20 40 60

TIME FROM DETONATION, MSEC

80 too

Figure 3.2? Shear and principal stress data, Location 1101+2, Event 1A.

78

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jj) 20 -

VI in U IT h «n IT < U z in

STATION -11043 RANGE-53 FEET DEPTH - 10 FEET

100

100 i-

-50 20 40 60 80

TIME FROM DETONATION, MSEC

100

Figure 3.26 Shear and principal stress data, Location II0U3, Event 1A.

79

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100 I-

STATION -11062 RANGE -80 FEET DEPTH-5 FEET

K

V)

K < UI I

too

400 r-

200 -

in UI at

MAJO« PRINCIPAL STRESS

-200 40 60

TIME FROM DETONATION, MSEC

100

^irure 3.27 Shear and principal stress data, Location 11062, Event 1A.

80

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CHAPTER U

CONCLUSIONS

Overall instrument performance for Distant Plain events 6 and

1A was excellent. O/er 95 percent of the gages installed for the two

events yielded good quality data of uniformly high signal-to-noise

ratio.

Arrival times were obtained for all successfully recorded niages,

and were used to calculate propagation velocities of both above- and

below-water-table soil layers. These velocities were 1,100 and 55500

ft/sec, respectively, and were both essentially the same as those de-

termined on Operation Snow Ball and by seismic surveys. Arrival

times also provided the first indication of outrunning ground motion,

and were used to construct a shock front profile for Event 6 (Figure

3.1). From this profile it was determined that the outrunning ground

motion, which had been refracted along the water table, arrived at

the ground surface prior to the airblast at a distance of hOO feet

from GZ, or at tiie 30-psi level. This was nearly the same pressure

level as was found for Snow Ball and indicates that yield plays a

minor part in the pressure level associated with outrunning, at least

for the Watching Hill test site.

Peak vertical accelerations attenuated sharply with both in-

creasing range and depth. The ratio of acceleration to overpressure

81

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for the l»r)-foot depth was found to increase from about O.k g/psi

at 1,000 psi to about 1 g/psi at 20 psi for Event 6 data, and corre-

late! very well witli data from the Distant Plain Event 3 and Flat

Top Events II and III. Event LA data were consistently above the

norm for this correlation, but were within the data scatter. Dis-

turbed airblast waveforms probably account for the deviation.

Peak vertical accelerations at the 5-foot depth were attenuated

to 20 percent of those at the 1.5-foot depth, and those at the 10-

foot depth averaged 7.5 percent of the shallower data. These figures

were in good agreement with Distant Plain Event 3 data.

The two correlation curves (Figures 3.5 and 3.6) would thus

provide predictions of acceleration with relatively high confidence,

at least for the range of yields encountered (20 to 100 tons).

Peak vertical particle velocities also attenuated sharply with

both increasing distance and depth, although the effect was less pro-

nounced than for accelerations.

Ratios of vertical particle velocity to overpressure for the

1.5-foot depth also increased with decreasing overpressure, and

varied from about 0.03 ft/sec/psi at 1,600 psi to about 0.08

ft/sec/psi at 10 psi.

Peak vertical velocities at the 5-foot depth were found to

average ho percent of those at the 1.5-foot depth, while velocities

at a depth of 10 feet averaged 30 percent of the 1.5-foot data.

82

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Horizontal particle velocities for Event 6 were dominated by the

cratering-induced pulse which attenuated in a regular manner as the

-2.7 power of distances. These velocities varied from 17.3 ft/sec at

Location 61012 to 1.35 ft/sec at Location l6o6l. In contrast, par-

ticle velocities induced by passage of the airblast were 2.9 ft/sec

and 0.30 ft/sec for the same two locations.

Displacements calculated for Event 6 were also dominated by the

cratering-induced pulse. This disturbance caused upward and outward

particle motion of considerable magnitude. The upward and outward

components of displacement at Location 16012, for example, were 5.1

and 6.5 feet, respectively. The vertical component decreased as

the -3.7 power of horizontal distance, while the horizontal displace-

ment attenuated as the -2.k power.

Displacements for Event 1A were airblast-induced only and were

consequently directed lownward and outward. The vertical displace-

ments were found to agree reasonably well with those calculated at

similar pressure levels for Event 6.

Soil stresses measured on Event 6 at locations above the water

table showed more scatter than did motion measurements, and attenuated

with depth more rapidly. Measurements from below the water table, at

a depth of 30 feet, attenuated as the -1.15 power of distance, a rate

which approximates that of free water.

Calculations of principal stresses and shear stresses were

83

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successfully made for three locations on each event. Peak major

principal stresses were found to run somewhat higher than the meas-

ured vertical stresses, emphasizing the obliquity of the airblast-

induced shock front. With one exception, Location 11062, all calcu-

lations of shear stress gave peak values of between kO and 70 psi.

Since these represent measurements for a variety of overpressures,

this region of shear stress would appear to be an upper bound for the

material.

81+

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APPENDIX A

EVENT 6 TIME HISTORIES

85

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o-J^U-

8J

61012 M9 5 flV

61021 60 1 flV

-fc—f*.

;j^— 61022 60 5 flV

mi mtm I<IIIIIIIIIIIIIIIIIIIII

gJ i 1 1 1 r ? 1 1 1 1 1 1 1 1 r 1 1 r 1 ! 1

-000 004 0. 10 0. 19 0.» 0.» 0 10 0.19 0.40 0-49 0-50 0.5S O.tO 0.H O.TO CIS 0.10 0.H 0.M 0-t9 I.0C

TIME FROM 0ET - SEC

86

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61031 80 1 RV

t '"

61032 80 5 nv

M-.

I 8 a. trt

r 61041 98 1 nv

61042 98 5 flV

I—"—T 1 r 1 1 ? 1 r 1 1 r~—r~—T 1— "i— —T 1 "i 1 1 •0.00 0-0» 0.10 0.19 0.20 0.29 O.)0 0 35 0.40 0.45 0.50 0--^ U 60 0.G5 Ü'l) 0 7; n 00 0 e-> 090 095 I . 00

TIME FROM DET - 5EC

87

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g

r 61061 162 IflV

r 61051 mo i fiv

t M"

■8 13 r

Z o

61052 140-5-flV

r 61062 162-5-flV

a 8.

i—i—i—i—i—i—i i i—i—i—i—i—i—i—i—i—i—i—i—i -.00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .65 .90 .95 1.00

TIME FROM GET - SEC

88

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a

61071 325-1-nV

o

a- 8.

t-

61073 325-10-flV

CD

£

TlTtf»

61081 400-lflV

n

WU- 61083 400-10-flV

i 1—i—i 1—i 1—i 1 1—i—i—i 1 1—"—i 1 1—i—i 1 .00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .65 .90 .95 1.00

TIME FROM DET - SEC

89

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61091 480-1-PV

19

flpu/U-

61093 480-10-flV

g

p^- 61101 680-1-flV

|W^ /■>

61103 680-10-flV

T r -i 1 1 .00.05 .10 .15 .20 .25 .30 .35 .HO .45 .50 *S5 .60 .65 .70 .75 .89 .85 of» .95 1.00

TIME FROM DET - SEC

90

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61012 49-5-UV so JU.T tan

BS

ÜJ

o

61021 60-1-UV

BS

§1

a o

i JULY ia

10

28

I I 1 1 1 1 1 1 1 1 1 1 1 1 ! 1 1 1 1 1 1 .00.05 .10 .15 .20 .25 .30 .55 .40 .H5 .50 .55 .60 .65 .70 .75 .80 .BS .90 .95 1.00

TIME FROM OET - SEC

91

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61031 80-1-UV » JULT INI

J 61032 80-5-UV

BS 50

BS 34

r .^

61041 9B-1-UV

S JULT II

BS 46

61042 98-5-UV 30 JULT 1968

BS 12

i 1 i—i—i—i—i—i—i—i—i—i—i—i—i—i—i—i 1—i—i .00.05 .10 .15 .20 .25 .30 .35 .MO .45 .50 .55 .60 .65 .70 .75 .80 .SS .90 .95 1.00

TIME FROM OET - 8EC

92

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61051 140-1-UV

61052 140-5-UV

UJ

>- *—•

61061 162-1-UV

61062 162-5-UV

J±^f

i—i—i 1—i 1 1 1 1 1—i—i 1 1 1 1 1 1—i—i 1 .00.05 .10 .15 .20 .25 .30 .35 .40 .15 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM DET - SEC

93

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61071 325-1-UV

—^r*-—"* J^_

61073 325-10-UV

"-^s-

8 ^ Ui > v/^^"

61081 400-1-UV

^w 61083 HOO-10-UV

i 1 1 1 1 1 1 1 1 1 1 1 1 1 1 r 1 1 1 1 1 -.00.05 .10 .15 .20 .25 .30 .35 .40 .M5 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM OET - SEC

9h

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61091 480-1-UV

o in.

61093 H80-10-UV

61101 680-1-UV

61103 680-lü-UV

.00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .7u .75 .80 .85 .90 .95 1.0(1

TIME FROM DET - SEC

95

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?■ 61022 60 5 RH

in

5 7

61021 60 1 RH

-«?•— 1^

61012 49 5 RH

-^

i—i—i—i 1—i—i—i—i—i—i— -0.00 0.01 0.10 O.IS O.M 0.« O.SO o.n 0.40 0.41 0.»

—r- O.M

—I 1 1 1 1 1 1 ! O.M O.M 0.10 0.11 0.00 O.M O.M O.M 1.00

TIME FROM DET - SEC

96

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-I[f—^v^

61031 80 1 fiH

t-f"

^ 2

4" 'y^—' ^^A^J*-

61032 80-5-nH

a UJ

U s 61041 98 1 HH

61042 98-5-flH

.^^•>..

i 1 i—1 1 1 1 1—i 1 1 1 1 1 1 1 1 1 1 1 1 -.00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM DET - SEC

97

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61051 140-1-nH

§1

V

en

61052 140-5-flH

a

§

V

61061 162-l-flH

S

8'

Y~ 162-5-RH

i 1 1 1 1—i—i—i—i 1 1 1 1—i—i—i 1 1 1 1 1 .00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .60 .65 .90 .95 1.00

TIME FROM OET - SEC

98

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61012 49-5-UH

BS 2M

u

? 8

61021 60-1-UH

5 JULY 196«

BS 45

Ö 2

61022 60-5-UH

BS 38

i 1 1 1 1 1 1 1 1 1 1 1 1 r——i 1 1 1 1 1 1 -.00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM OET - SEC

99

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61031 BS 80-1-UH 1 RUE 196«

53

61032 80-5-UH

BS 20

o

61041 98-1-UH 30 JULY 1968

BS 06

i 1 1 1 1 r- -.00.05 ,10 .15 .20 .25

610H2 98-5-UH

BS 40

-i 1—i 1—i—i—i—i 1 1 1 i—i i—i ,30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .85 .90 ,95 1.00

TIME FROM DET ■ SEC

100

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610b. 140-: UH

Ml

61052 140-5-UH

BS 36

o

61061 162-1-UH 5 JULT 1968

BS 30

162-5-UH BS 42

( 1 1 1 1 1 1 1 1 1 1—i 1 1 1 1 1 1 1 1 1 -.00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM OET - SEC

101

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^—\ "S^^V^"

61071 325-1-UH

^

61073 325-10-UH

o

jj\^.

61081 400-1-UH

61083 400-10-UH

i 1 1 1 1 1 1 1 1 1 1 1 r——i——i 1 1 1 1 1 \ .00.05 .10 .15 .20 .25 .30 .35 .40 .45 .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM DET ■ SEC

102

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61091 480-1-UH

61093 480-10-UH

61101 680-1-UH

o

61103 680-10-UH

i 1 1 1 1 1 1 1—i 1 1 1 1 1 1 1 1 1 1 1 1 -.00.05 .10 .15 .20 .25 .30 .35 .HO .MS .50 .55 .60 .65 .70 .75 .80 .85 .90 .95 1.00

TIME FROM DET - SEC

103

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610?] 6Q 1 PV

.|r_

i

61031 60 t PV

(*^^** *—^

■ MMMS

610HI 98 I PV

/V

6I0S1 moi-pv

61061

t 7" il« rm KT . xc

10k

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61014 49-17-PV

o a rr

o o i

o

03 I

61064 162 17 PV

!8

61064 162 17 PH

.» .• i.o TIME FWi DET - SEC

i.( i.«

105

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61015 49-30-PH

61025 60-30-PH

610HS 9e-30-PH

61065 162 30 PH

TT • .♦ i.b TIME rm KT - SEC

106

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61022 60 5 PV

61022 60 5 PH

61022 60 5 PS

—r- i.o

—r- i.t

—r —i

TIME FRH OET - SEC

107

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ah

i]

Cm 1 t-

\

61024 60 17 PV

61024 60 17 PH

61024 60 17 PS

0.0 0.2 0.4 0.6 0.8 LO 1.2 1.4 1.5 TIME FRON DET - 5ECS

1(38

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61032 80-5-PV

61032 80-5-PH

61032 80-5-PS

8.

-r- i.o

—r- i.f

—r* .2 .6 .6

TIME FRM OET - SEC 1.6

109

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61034 80 17 PH

61034 80 17 PS

•0.0 Q.2 0.4 0.6 0.8 1.0 1.2 1.4 TIME FROM DET - SEC5

1.6

110

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61035 80 30 PV

61035 80 30 PH

61035 80 30 PS

rr 1.2 1.1 .« .1 TIME FRM DET - SEC

1.6

111

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sn

if-

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TIME FRM DET - SEC

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T- T .6 .6

TIME FRM DET

—r i.o

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ii

61052 140 5 PV

t M***-

i-

I

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TIME FRM DET - SEC i.t l.H

—I 1.6

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61054 140 17 PV

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£

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8-

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8.

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—I 1 r .1 .6 .8 1.0 \.t

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117-118

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r

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APPENDIX B

EVENT LA TIME HISTORIES

119 Preceding page blank

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a, a.

r 1 1033 35 10 RV

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TIME FROM DET SEC

120

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r cc

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121

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►r

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1 1063 80-10-flV

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122

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11031 35 1-UV

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1 1041 53 1-UV

11042 S3 5-UV

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1 106 8G 1

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TIME FROM DET - SEC

~r 1 r 1 r 1 1 , 70 .7S .80 .85 .90 .95 1.00

125

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11 n 31 35 i m

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TIME FROM DET - SEC

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TIME FROM DET - SEC

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TIME FROM DET ■ 5EC

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REFERENCES

1. W. R. Perret and V.L. Gentry; "Operation Upshot-Knothole,

Project l,k, Free-field Measurements of Earth Stress, Strain, and

Ground Motion"; WT-716, February 1955» Atomic Energy Commission,

Oak Ridge, Tenn.; Unclassified.

2. N.M. Ilewmark and J. D. Haltiwanger; "Air Force Design

Manual; Principles and Practices for Design of Hardened Structures";

Technical Documentary Report No. AFSWC-TDR-62-138, December 1962', Air

Force Special Weapons Center, Kirtland Air Force Base, Nev Mexico;

Prepared by University of Illinois, Urbana, 111.; Tinclassified.

3. D. W. Murrell; "Operation Snowball, Project 3.6"-r.arbh

Motion Measurements"; Technical Report No. 1-759? March I9o7; U. S,

Army Engineer Waterways Experiment Station, CE, Vicksburg, Miss.;

Unclassified.

k. J. K. Ingram; "Project Officer's Final Report, Operation

Distant Plain, Events 1, 2A, 3, k, and 5j Project 3.02a, Earth Motion

and Stress Measurements"; (in preparation); U. S. Army Engineer

Waterways Experiment Station, CE, Vicksburg, Miss.; Unclassified.

5. P.M. Sauer; "Dista.it Plain, Events 6 and 1A, Report of

Special Assistant to Test Director"; October 1967; Stanford Research

137

Page 139: DISTANT PLAIN EVENTS 6 AND 1A PROJECT 3.02A, … · technical report n.70-14 distant plain events 6 and 1a project 3.02a, earth motion and stress measurements by d. w. murrdl stptombtr

Institute, Menlo Park, Calif.; Unclassified.

6. A. J. Hendron, Jr.; "Correlation of Operation Snowball

Ground Motions with Dynamic Properties of Test Site Soils";

Miscellaneous Paper No. 1-7U5, October I965; U. S. Army Engineer

Waterways Experiment Station, CE, Vicksburg, Miss.; Unclassified.

7. J. L. Gatz; "Soil Survey and Support Activities, Operation

Distant Plain Event 6"; Miscellaneous Paper No. 3-990, April 1968;

U. S. Army Engineer Waterways Experiment Station, CE, Vicksburg,

Miss.; Unclassified.

8. J. G. Jackson, Jr., and J. S. Windham; "Preliminary Report,

Operation Distant Plain, Event 6, Soil Property Investigation for

Project 3.10, Soil Sampling and Testing"; December 196?; Defense

Atomic Support Agency, Washington, D. C; Prepared by U. S. Army Engi-

neer Waterways Experiment Station, CE, Vicksburg, Miss.; Unclassified.

9. J. K. Ingram; "Development of a Free-Field Soil Stress Gage

for Static and Dynamic Measurements"; Technical Report No. l-BlU,

February 1968; U. S. Army Engineer Waterways Experiment Station, CE,

Vicksburg, Miss.; Unclassified.

10. R. E. Reisler; "Events 5, 6A, and 6, Project 1.01, Air Blast

Measurements"; Operation Distant Plain Symposium II, M. J. Dudash,

138

Page 140: DISTANT PLAIN EVENTS 6 AND 1A PROJECT 3.02A, … · technical report n.70-14 distant plain events 6 and 1a project 3.02a, earth motion and stress measurements by d. w. murrdl stptombtr

editor, DASA 220?, DASIAC SR-83, May I968, Pages 70-106; DASA Informa-

tion and Analysis Center, General Electric, TEMPO, Santa Barbara,

Calif.; For Offical Use Only.

11. F. M. Sauer and C. T. Vincent; "Ferris Wheel Series, Flat

Top Event; Project Officers Report—Project 1.2/1.3a, Earth Motion

and Pressure Histories (U)"; POP 3002 (WT-3002) April 1967; Defense

Atomic Support Agency, Washington, D. C; Unclassified.

12. E. E. Reisler; "Air Blast Measurements, Operation Distant

Plain, Event 1A"; Operation Distant Plain Symposium II, M. J. Dudash,

editor, DASA 2207, DASIAC SR-83, May 1968, Pages UU-69; DASA Informa-

tion and Analysis Center, General Electric, TEMPO, Santa Barbara,

Calif.; For Official Use Only.

139

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DISTRIBUTION LIST FOR TR N-70-14

No. of Addreu Copiet

Department of Defwiie

Director, Defenie Atomic Support Agency, Washington, D. C. 20S01 ATTN: Technical Library (APTL) 2

STSP 1 OAOP 1 OPQR 1

Commander, Field Command, Defense Atomic Support Agency, Sandia Base, Albuquerque, N. Mex. 87115 1

ATTN: Technical Library 1 FCTG-5 1 FCDV1

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ATTN: Document Control

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Unclassified »tcuiitY CtoMtflcittM

DKUMINT CONTROL DATA -R&D

. OKKINATIN« ACTIVITV aa.ncFonT iieumTv CLAMIPICATION

U. S. Army Engineer Waterways Experiment Station Vlcksburg, Mississippi

Unclassified M. anou*

t. MI^OHT TITLI

DISTANT PLAIN EVENTS 6 AND U, PROJECT 3.02a, EARTH MOTION AND STRESS MEASUREMENTS

KTrp»»i I iMlMln 4tf)

Final report

Donald W. Murrell

mPOdT OATK

September 1970 Sept TTOS C CTSTUtt

»«. TOTAk NO. OF r*«Cf

1U5 12

k. »KOJICT HO.

M. ONICINATOn*« «(»OKT NUMMRIW

Technical Report N-TO-lU

•M *•( aar k* —»I0tt4

It. «(TMSUTION ITATIMBNT

This docvunent has been approved for public release and sale; Its distribution : .■ unlimited.

K. (UPPLIMCNTAKV NOTC* 11. IFONMniN« MILITAMV «GTIVITV

■ Defense Atomic Support Agency Washington, D. C.

nnzrp - ^The objectives of this study were to measure and analyze earth motions produced by

Events 6 and 1A of Operation Distant Plain. Event 6 was a 100-ton TNT surface-tangent sphere, and Event 1A a 20-ton TNT sphere detonated at a height of burst of 29.5 feet. Acceleration, particle velocity, and soil stress gages were Installed for both events to measure ground motion. Time histories obtained by this Instrumentation are in- cluded in Appendixes A and B. For Event 6, ground shock arrival times indicated development of outrunning ground motion at about the 30-psi level. Shock propa- gation velocities were calculated to be 1,100 ft/sec above the water table and 5,500 ft/sec below it. The ratio of acceleration to overpressure for the 1.5-foot depth for both events was about O.U g/psi at the 1,000-psl level, and Increased to 1.0 g/psi at the 20-psi level. At depths of 5 and 10 feet, accelerations averaged 2,0 and 7.5 percent of the shallow data, respectively. At the 1.5-foot depth the ratio of velocity to overpressure varied from 0.03 ft/sec/psi at 1,600 psi to 0.08 ft/sec/psi at 10 psi. Velocities attenuated less sharply with depth than did ac- celerations. Velocities at the 5-foot depth were about 1*0 percent of those at 1.5 feet, while those from the 10-foot depth were about 30 percent of those at 1.5 feet. • Horizontal velocities were dominated by the cratering-Induced motion. These motions attenuated as the -2.7 power of distance. Vertical stresses attenuated more rapidly than did the velocities, with stresses at the 5-foot depth averaging 25 percent of those at the 1.5-foot depth. Horizontal stresses measured below the water table behaved similar to free-water measurements, attenuating as the -1.15 power of dis- tance, versus -1.13 power for water. Calculations of shear stress were made for three locations on^each^hot^ Peak values ranged from kO to 70 psi.

DD 3EJ37S 2»ä« Ärsriiv '•" - 11+7

Unclassified ■•curtljr Clatuncattea

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Unclassified

KKV KIOnDt nek* WT

Distant Plain (Operation)

Earth movements

Explosion effects

Ground motion

Stress gages (soils)

1U8 Unclassified