Shear Wall Design.xls
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Transcript of Shear Wall Design.xls
PROJECT : PAGE : CLIENT : DESIGN BY :
JOB NO. : DATE : REVIEW BY :
Shear Wall Design
INPUT DATALATERAL FORCE ON DIAPHRAGM: 350 plf,for wind
350 plf,for seismic
GRAVITY LOADS ON THE ROOF: 262 plf,for dead load
0 plf,for live load
DIMENSIONS: 8 ft , h = 16 ft
L = 7 0 ft
PANEL GRADE ( 0 or 1) = 1 <= Sheathing and Single-Floor
MINIMUM NOMINAL PANEL THICKNESS = 15/32 in
COMMON NAIL SIZE ( 0=6d, 1=8d, 2=10d ) 1 8d
SPECIFIC GRAVITY OF FRAMING MEMBERS 0.5
EDGE STUD SECTION 2 pcs, b = 2 in , h = 6 in
DESIGN SUMMARYBLOCKED 15/32 SHEATHING WITH 8d COMMON NAILS
@ 4 in O.C. BOUNDARY & ALL EDGES / 12 in O.C. FIELD,
5/8 in DIA. x 10 in LONG ANCHOR BOLTS @ 34 in O.C.
HOLD-DOWN FORCES: 4.02 k , 3.87 k (USE PHD5-SDS3 SIMPSON HOLD-DOWN)
DRAG STRUT FORCES: -0.35 k
EDGE STUD: 2 - 2'' x 6'' DOUGLAS FIR-LARCH No. 1, CONTINUOUS FULL HEIGHT.
SHEAR WALL DEFLECTION: 0.97 in
ANALYSISTHE MAX SHEAR WALL DIMENSION RATIO L / B = 2.0 < 2 [Satisfactory]
THE UNIT SHEAR FORCE 306 plf, ( 1 Side Diaphragm Required, the Max. Nail Spacing = 4 in )
THE SHEAR CAPACITIES PER UBCTable 23-II-I-1 :
Panel Grade
Min. Min. Blocked Nail Spacing
Common Penetratio Thickness Boundary & All Edges
Nail (in) (in) 6 4 3 2
Sheathing and Single-Floor 8d 1 1/2 15/32 260 380 490 640
Note: The indicated shear numbers have reduced by specific gravity factor per note 1 of the table.
THE DRAG STRUT FORCE: -0.35 k 1 ) (Sec. 1633.2.6)
THE MAX SPACING OF 5/8" DIA ANCHOR BOLT (Tab.11E, NDS 2001, Page 85) S = 34 in
THE HOLD-DOWN FORCES:
Wall Seismic Overturning Resisting Safty Net Uplift Holddown
(plf) at mid-story (lbs) Moments (ft-lbs) Moments (ft-lbs) Factors (lbs) SIMPSON
SEISMIC 350 205 40838Left 10515 0.9 3922
Right 12349 0.9 3716
WIND 350 39200Left 10515 2/3 4024
Right 12349 2/3 3871
THE MAXIMUM SHEAR WALL DEFLECTION: ( Section 4.3, ASD MANUAL SUUP, Page SW-17)
= 0.971 in
Where: 306 plf 8 ft E = 1.7E+06 psi
A = 16.50 h = 16 ft G = 9.0E+04 psi
t = 0.298 in 0.037 in 0.15 in
CHECK EDGE STUD CAPACITY
1500 psi 1.6 0.14 A = 16.5
E = 1700 ksi 1.10 365 psi > 201 psi
[Satisfactory]
Techincal References:
1. "National Design Specification, NDS", 2001 Edition, AF&AP, AWC, 2001.
2. Alan Williams: "Structuiral Engineering Reference Manual", Professional Publications, Inc, 2001.
vdia, WIND =
vdia, SEISMIC =
wDL =
wLL =
Lw =
ft , hp =
TL = TR =
F =
D =
vb =
F = (L-Lw) MAX( vdia, WIND, W0vdia, SEISMIC ) = ( W0 =
vdia
TL =
TR =
TL =
TR =
vb = Lw =
in2
en = da =
Fc = CD = CP = in2
CF = Fc' = fc =
PHD
5-SDS3
380.75b b a
Bending Shear Nail slip Chord splice slip nw w
h hv h v dheEA GtL L
D D D D D
PROJECT : PAGE : CLIENT : DESIGN BY :
JOB NO. : DATE : REVIEW BY :
Wood Column Design
INPUT DATA DESIGN SUMMARYMEMBER TYPE: 3 1 POST
2 STUD USE: 2 - 2'' x 6'' DOUGLAS FIR-LARCH No. 13 KING STUD
GEOMETRY DATA:HEIGHT h = 16 ft 201 psi < 365 psi okUNBRACED LENGTH Le x-x (H) = 16.0 ft
Le y-y (B) = 0 ftLOAD DATA: 0 psi < 2080 psi ok
DEAD LOAD 3324 lbsLIVE LOAD 0 lbsTOTAL 3,324 lbs 3. CHECK INTERACTION :LATERAL LOAD x-x 0 plf
M= 0 ft-lbsLOAD DURATION 5 WIND/EARTHQUAKE LOAD 0.305 < 1 ok
DESIGN CRITERIA:SECTION 2 pcs, B = 2 in
H = 6 in 6419SPECIES DOUGLAS FIR-LARCH 6648
GRADE No. 1 3 6214
LUMBER GRADING TYPE 1 VISUALLY GRADED 6444
SHAPE TYPE 1 SAWN LUMBER
WET / DRY USE ? 1 DRY
ANALYSISCOLUMN BASIC DESIGN STRESSES:
COMPRESSIVE STRESS 1500 psiMODULUS OF ELASTICITY E = 1700 ksi
BENDING STRESS (X-Axis) 1000 psi
BENDING STRESS (Y-Axis) 1000 psi
COLUMN PROPERTIES:COLUMN SECTION X-Dir dx = 5.50 in
Y-Dir dy = 1.50 in
AREA A = 16.5
SECTION MODULI Abt. xx Sx = 15.13
Abt. yy Sy = 4.13LENGTH-DEPTH RATIO Le x-x / dx = 34.9
Le y-y / dy = 0.0
ADJUSTMENT FACTORS:
DURATION FACTOR 1.60 1.60 1.60
MOISTURE FACTOR 1.00 1.00 1.00 0.90 COLUMN PARAMETER c = 0.80
TEMPERATURE FACTO 1.00 1.00 1.00 1.00 EULER BUCKLING COEFFICIENT
INCISING FACTOR 1.00 1.00 1.00 1.00 0.300
SIZE FACTOR 1.30 1.30 1.10 1.00 CRITICAL EULER BUCKLING VALUES
FLAT USE FACTOR 1.15 377 psi
COLUMN STABILITY 0.138 2640 psi
REPETITIVE MEMBER 1.00 1.00
BEAM STABILITY 1.00 1.00
ADJUSTED PROPERTIES:MODULUS OF ELASTICITY E' = 1530 ksi
BENDING STRESS (X-Axis) 2080 psi
BENDING STRESS (Y-Axis) 2392 psi
AXIAL STRESS 365 psi
ACTUAL STRESSES:
AXIAL 201.5 psi
BENDING STRESSES 0.0 psi
1. CHECK VERTICAL LOADS : fc < Fc' ?
2. CHECK BENDING LOADS : fb < Fb' ?
Fc =
Fbx =
Fby =
in2
in3
in3
Fbx' Fby' Fc' E'
CD
CM
Ct
Ci KcE =
CF
Cfu FcE =
CP Fc* =
Cr
CL
Fbx' =
Fby' =
Fc' =
fc =
fbx =
2
' '
11 ?
1bxc
c cEx bxc
ff
fF F F