Response Spectrum

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1 1 First version: September 2003 (Last modified 2010) Ahmed Elgamal & Mike Fraser Single-Degree-of-Freedom (SDOF) and Response Spectrum Ahmed Elgamal 2 Ahmed Elgamal & Mike Fraser Dynamics of a Simple Structure The Single-Degree-Of-Freedom (SDOF) Equation References Dynamics of Structures, Anil K. Chopra, Prentice Hall, New Jersey, ISBN 0-13-855214-2 (Chapter 3). Elements of Earthquake Engineering And Structural Dynamics, André Filiatrault, Polytechnic International Press, Montréal, Canada, ISBN 2-553-00629-4 (Section 4.2.3). First version: September 2003 (Last modified 2010)

Transcript of Response Spectrum

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Single-Degree-of-Freedom (SDOF)

and Response Spectrum

Ahmed Elgamal

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Ahmed Elgamal & Mike Fraser

Dynamics of a Simple Structure

The Single-Degree-Of-Freedom (SDOF) Equation

References

Dynamics of Structures, Anil K. Chopra, Prentice Hall, New Jersey, ISBN 0-13-855214-2

(Chapter 3).

Elements of Earthquake Engineering And Structural Dynamics, André Filiatrault,

Polytechnic International Press, Montréal, Canada, ISBN 2-553-00629-4 (Section 4.2.3).

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Equation of motion (external force)

k

1

u

fs fD

c

1

ů

fs = k u fD = c ů

fS

fI

p(t)

fD

fI

fS

p(t)

fD

FBD

p(t)

u(t)

m

c

k

Mass-spring damper system

fI + fD + fs = p(t)

where fI,fD, and fs are forces due to

Inertia, Damping and Stiffness respectively:

)t(pkuucum

Free-Body Diagram (FBD)

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ug(t)

Earthquake Ground Motion (ug)

fI + fD + fs = 0

fI = m tu = m( gu +u )

0kuuc)uu(m g

gumkuucum

You may note that:

Earthquake

Excitation

Fixed base

(t)

External

force=

ug(t)

u = relative displacement (displacement of the structure relative to the ground)

ut = total displacement

fI = m x (total or absolute acceleration)

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Undamped natural frequency

Property of structure when allowed to vibrate freely without external excitation

m

kw Undamped natural circular frequency of vibration (radians/second)

p

w

2f natural cyclic frequency of vibration (cycles/second or 1/second or Hz)

f

1T natural period of vibration (second)

T is the time required for one cycle of free vibration

If damping is present, replace w by wD

where 2

D 1 xww natural frequency*, and

wx

m2

cfraction of critical damping coefficient (damping ratio, zeta)

cc

c (dimensionless measure of damping)

km2

c

km2m2ccw

T

* Note: In earthquake engineering, wD = w approximately, since z is usually below 0.2 (or 20%)

cc = critical damping

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in terms of x

gumkuucum

guum

ku

m

cu

g

2 uuu2u wxw

In general x < 0.2, i.e., wD w , fD f, T = TD

cc least damping that prevents oscillation

x may be in the range of 0.02 – 0.2 or 2% - 20%

5% is sometimes a typical value.

u

t

cc or larger

x 1

e.g., damper on a swinging door

in terms of x

gumkuucum

guum

ku

m

cu

g

2 uuu2u wxw

In general x < 0.2, i.e., wD w , fD f, T = TD

cc least damping that prevents oscillation

x may be in the range of 0.02 – 0.2 or 2% - 20%

5% is sometimes a typical value.

u

t

cc or larger

x 1

e.g., damper on a swinging door

cc is the least level of damping that prevents oscillation

in terms of x

gumkuucum

guum

ku

m

cu

g

2 uuu2u wxw

In general x < 0.2, i.e., wD w , fD f, T = TD

cc least damping that prevents oscillation

x may be in the range of 0.02 – 0.2 or 2% - 20%

5% is sometimes a typical value.

u

t

cc or larger

x 1

e.g., damper on a swinging door

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Note: After the phase of forced vibration (due to external force or base excitation, or initial

conditions), the structure continues to vibrate in a “free vibration” mode till it stops due to

damping. The ratio between amplitude in two successive cycles is

px

2

1i

i eu

u

where we define the logarithmic decrement as

px

1i

i

u

uln2 if you measure a free vibration response you can find x.

Note: for peaks j cycles apart

px

j2ju

uln

ji

i

ui ui+1

Free vibration

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Critical viscous damping

The free vibration equation may be written as 0kxxcxm

and the general solution is

tm

k

m2

c

m2

c

2

tm

k

m2

c

m2

c

1

22

eCeCx

if m

k

m2

c2

, the radical part of the exponent will vanish. This will produce aperiodic

response (non-oscillatory). In this case

m

k

)m2(

c

2

2

or cckm2c

since m

kw , cc is also equal to 2mw (note that ww m2mm2km2 2

)

and also w

wk2

)/k(k2km2c 2c

Why is km2m2ccw

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Deformation Response Spectrum

For a given EQ excitation calculate |umax|

from SDOF response with a certain x

and within a range of natural periods or

frequencies.

|umax| for each frequency will be found

from the computed u(t) history at this frequency.

A plot of |umax| vs. natural period is constructed

representing the deformation (or displacement)

response spectrum (Sd).

From this figure, one can directly read the

maximum relative displacement of any structure

of natural period T (and a particular value of x

as damping)

From: Chopra, Dynamics of Structures, A Primer

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Example

Units for natural frequency calculation (SI units)

Weight = 9.81 kN = 9810 N = 9810 kg (m /s2)

Gravity (g) = 9.81m/s2

Mass (m) = W/g = 9180/9.81 = 1000 kg

Stiffness (k) = 81 kN/m = 81000 N/m = 81000 kg (m/s2)/m = kg /s2

w = SQRT (k/m) = SQRT (81000/1000) = 9 radians/sec

f = w / (2 p) = 1.43 Hz (units of 1/s or cycles/sec)

Units for natural frequency calculation (English units)

Weight (W) = 193.2 Tons = 193.2 (2000) = 386,400 lbs = 386.4 kips

g = 386.4 in/sec/sec (or in/s2)

Mass (m) = W/g = 1.0 kips s2 /in

Stiffness (k) = 144 kips/in

w =SQRT (k/m) = 12 radians/sec

f = w / (2 p) = 1.91 Hz (units of 1/s or cycles/sec)

Note: The weight of an object is the force of gravity on the object and may be defined as the

mass times the acceleration of gravity, w = mg. Weight is what is measured by a scale (e.g.,

weight of a person). Since the weight is a force, its SI unit is Newton.

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2

V

2

d

22

d

2

2

2

d

2

maxmax mS2

1Sm

2

1S

k

2

1kS

2

1ku

2

1E ωω

ω

Concept of Equivalent lateral force fs

If fs is applied as a static force, it would cause the deformation u.

Thus at any instant of time:

fs = ku(t) , or in terms of the mass fs(t) = mw2u(t) m

kw

The maximum force will be

maxmax2

max,s kuumf w da kSmS

da Sm

kS

d2

a SS w

Sd = deformation or displacement response spectrum

d2

a SS w = pseudo-acceleration response spectrum

The maximum strain energy Emax stored in the structure during shaking is:

= pseudo-velocity response spectrumdv SS wwhere

From: Chopra,

Dynamics of Structures, A Primer

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Note that Sd, Sv and Sa are inter-related by

vd2

a SSS ww

Sa, Sv are directly related to Sd

by w2 and w respectively or by (2pf)

2 and 2pf;

or

2

T

2

pand

p

T

2as shown in Figure.

Due to this direct relation, a 4-way plot

is usually used to display Sa, Sv and Sd

on a single graph as shown in Figure.

In this figure, the logarithm of

period T, Sa, Sv and Sd is used.

From: Chopra, Dynamics of Structures, A Primer

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From: Chopra, Dynamics of Structures

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From: Chopra, Dynamics of Structures, A Primer

Example (El-Centro motion):

Find maximum displacement

and base shear of tower

with f = 2 Hz, x = 2%

and k = 1.5 MN/m

Period T = 1/f = 0.5 second

Sd = 2.5 inches = 0.0635 m

Forcemax = kumax

= 1.5 MN/m x 0.0635m = 95.25 kN

In order to cover the damping

range of interest,

it is common to perform

the same calculations for

x =0.0, 0.02, 0.05, 0.10,

and 0.20 (see Figure)

Typical Notation:

Sv PSV V

Sa PSA A

Sd SD D

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(5% Damping)

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From: Chopra, Dynamics of Structures

Inspection of this figure shows

that the maximum response

at short period

(high frequency stiff structure)

is controlled by the ground

acceleration, low frequency

(long period) by ground

displacement, and intermediate

period by ground velocity.

Get copy of El-Centro

(May 18, 1940)

earthquake record

S00E (N-S component)

ftp nisee.ce.berkeley.edu

(128.32.43.154)

login: anonymous

password: your_indent

cd pub/a.k.chopra

get el_centro.data

quit

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Note that response spectrum

for relative velocity

may be obtained from

the SDOF response history,

and similarly for üt =(ü+üg).

These spectra are known

as relative velocity

and total acceleration

response spectra,

and are different from the

pseudo velocity

and pseudo acceleration

spectra S v and S a

(which are directly

related to S d).

e.g. for x = 0%

m(ü+üg) + k u = 0

or (ü+üg) + w2u = 0

From: Chopra, Dynamics of Structures

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Elastic Design Spectrum

Use recorded ground motions (available)

Use ground motions recorded at similar sites:

Magnitude of earthquake

Distance of site form earthquake fault

Fault mechanism

Local Soil Conditions

Geology/travel path of seismic waves

From: Chopra, Dynamics of Structures

Motions recorded at the same location.

For design, we need an envelope. One way

is to take the average (mean) of these values

(use statistics to define curves for mean

and standard deviation, see next page)

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From: Chopra, Dynamics of Structures

Mean response spectrum is smooth relative to any of the original contributing spectra

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The periods and values in Table 6.9.1

were selected to give a good match

to a statistical curve such as Figure 6.9.2

based on an ensemble

of 50 earthquakes on competent soils.

From: Chopra, Dynamics of Structures

As an alternative Empirical

approach, the periods shown on the

this Figure and the values in the

Table can be used to construct a

Median elastic design spectrum (or

a Median + one Sigma), where

Sigma is the Standard Deviation.

For any geographic location,

these spectra are built based on

an estimate of peak ground

acceleration, velocity, and

displacement as this location.

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(Design Spectrum may include more than one Earthquake fault scenario)

http://dap3.dot.ca.gov/shake_stable/

About Caltrans ARS Online

This web-based tool calculates both deterministic and probabilistic acceleration response spectra for any

location in California based on criteria provided in Appendix B of Caltrans Seismic Design Criteria