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PROJECT : PAGE :
CLIENT : DESIGN BY : JOB NO. : DATE : REVIEW BY :
WF Simply Supported Beam Design with Torsional Loading Based on AISC 14th (AISC 360-10)
INPUT DATA & DESIGN SUMMARY
BEAM SECTION = > W10X54 = > A dGRAVITY DISTRIBUTED LOAD w = 1.15 kips / ft 15.8 10.1 4.38 2.55 303 60
LATERAL POINT LOAD AT MID F = 5 kips lTORSION AT MID SPAN T = 5.1 ft-kips 103 20.6 0.01744 0.37 10.00 0.62
AXIAL LOAD P = 96 kips
BEAM LENGTH 15 ft
BEAM YIELD STRESS 50 ksi
VERTICAL BENDING UNBRACED LENGTH 15 ft
AXIAL VERTICAL UNBRACED LENGTH 15 ft
AXIAL HORIZONTAL UNBRACED LENGTH 7.5 ft
ANALYSIS
DETERMINE GOVERNING MOMENTS AT MIDDLE OF SPAN
32.3 ft-kips
18.8 ft-kips
22.7 ft-kips THE BEAM DESIGN IS ADEQUATE.
13.3 ft-kips
0.584 ,(Philip page 101)
CHECK TORSIONAL CAPACITY (AISC 360-10 H3.3 & Philip page 100)
0.73 < 1.00 [Satisfactory]
Where 21.93 ksi
29.94 ksi
CHECK COMBINED COMPRESSION AND BENDING CAPACITY (AISC 360-10, H1)
1.08 < 4/3 [Satisfactory]
Where 96 kips
109.7 ft-kips, (Sim. from Philip page 100)
18.8 ft-kips
721 / 1.67 = 431.971 kips, (AISC 360-10 Chapter E)
> [Satisfactory]
252.623 / 1.67 = 151.271 ft-kips, (AISC 360-10 Chapter F)
> [Satisfactory]
130.417 / 1.67 = 78.0938 ft-kips, (AISC 360-10 Chapter F)
> [Satisfactory]
DETERMINE DEFLECTIONS
0.22127
Where 11200 ksi 29000 ksi
J = 1.82
rx ry Ix Sx
Iy Sy tw bf tf
L =
Fy =
Lb =
Lx =
Ly =
Mx = w L2/ 8 =
My = F L / 4 =
M0 = T L / (4d) =
MT = bM0 =
fbx / Fnx =
fbx = Mx / Sx + 2MT / Sy =
Fnx = Fy / WT = Fy / 1.67 =
Pr =
Mrx = (Mx / Sx + 2MT / Sy) Sx =
Mry =
Pc = Pn / Wc =
3/4 Pr
Mcx = Mn / Wb =
Mrx
Mcy = Mn / Wb =
3/4 Mry
o , max twist angle at middle (Philip page 100)
G = Es =
in4
24 sinh
2sinh
L
L L
l
bl l
2sinh
2 sinh2 22 sinh
LT LL
GJ L
lll l l
8, 0.2
9
, 0.22
ryr rx r
c cx cy c
ryr rx r
c cx cy c
MP M PforP M M P
MP M PforP M M P
(cont'd)
0.15 in = L / 1207 , vertical deflection at middle
Where 303
0.20 in = L / 885 , horizontal deflection at middle
Where 103
Technical References: 1. AISC: "Steel Construction Manual 14th Edition", American Institute of Steel Construction, 2010. 2. Philip H. Lin: "Simplified Design for Torsional Loading of Rolled Steel Members", Engineering Journal, AISC, 1977.
I3 = Ix sin2(90-) + Iy cos2(90-) = in4 , (AISC 14th Page 17-42)
I4 = Ix cos2(90-) + Iy sin2(90-) = in4 , (AISC 14th Page 17-42)
4
3
5
384
wLvert E I
3
448
F Lhoriz E I
ROJECT : PAGE :
CLIENT : DESIGN BY :
JOB NO. : DATE : REVIEW BY :
Plate Girder Design Based on AISC Manual 13th Edition (AISC 360-05)
INPUT DATA & DESIGN SUMMARY
STEEL YIELD STRESS 50 ksi
SIMPLY SUPPORTED SPAN 15 ft
SUPERIMPOSED UNIFORM DEAD LOAD kips / ft
UNIFORM LIVE LOAD kips / ft
POINT DEAD LOAD kips
POINT LIVE LOAD kips
DISTANCE POINT LOAD TO END ft
TOP FLANGE WIDTH 10.00 in
TOP FLANGE THICKNESS 0.62 in
BOTTOM FLANGE WIDTH 10 in
BOTTOM FLANGE THICKNESS 0.615 in
WEB THICKNESS 0.37 inBEAM DEPTH 10.1 in Err:502
UNBRACED LENGTH 15 ft FLANGE TO WEB WELDING USE 1/4 in - 24 in @ 2293 in o.c.
THE GIRDER DESIGN IS ADEQUATE.
ANALYSIS
CHECK LIMITING WIDTH-THICKNESS RATIOS FOR WEB (AISC 365-05 Table B4.1)
23.97 < 137.27
< 90.55
Compact Web
where E = 29000 ksi
137.27
87.03
90.55
8.87 in 9.46 in
277.5 ft-kips 250.0 ft-kips
CHECK LIMITING WIDTH-THICKNESS RATIOS FOR FLANGES (AISC 365-05 Table B4.1)
8.13 < 25.09
< 9.15
Compact Flanges
where 25.09
9.15
0.76
60 60
35 ksi, (AISC 360-05 Table note B4.1 & Eq F4-6)
DETERMINE CRITERIA FOR ALLOWABLE FLEXURAL STRENGTH (AISC 365-05 Table F1.1)
Required Conditions
Chapter F Sections
F2 F3 F4 F5
Double Symmetric x xCompact Web x x
xNoncompact Web
Slender Web 151.3 ft-kipsCompact Flanges x ( from following analysis)
Noncompact FlangesSlender Flanges
Applicable Section ok
9.02 ft
33.66 ft
where 2.55 in 60
Fy =
S =
DL =
LL =
PDL =
PLL =
c =
bf,top =
tf,top =
bf,bot =
tf,bot =
tw = d =
Lb =
hc / tw = lr =
lp =
lr = 5.7 (E / Fy)0.5 =
lp = (hc / hp) (E / Fy)0.5 / (0.54 Mp / My -0.09)2 = ,for Af,top ≠ Af,bot
lp = 3.76 (E / Fy)0.5 = ,for Af,top = Af,bot
hc = hp =
Mp = My =
0.5 bf,top / tf,top = lr =
lp =
lr = 1.0 (kc E / FL)0.5 =
lp = 0.38 (E / Fy)0.5 =
kc = Min [0.76 , Max (0.35 , 4 / (h / tw)0.5 )] =
Sxt = in3 Sxc = in3
FL =
Mallowable = Mn / Wb =
DETERMINE ALLOWABLE FLEXURAL STRENGTH , Mn / Wb , BASED ON AISC 365-05 Chapter F2
ry = Sx = in3
1.76p yy
EL r
F
2
0
0.7 01.95 1 1 6.760.7 0.7
r ts tsy x y
FE Jc Ey S hxL r rE JcS h FF
9.49 in 103h0 = Iy = in4
(cont'd)
2316.6 , (AISC 365-05 F2.2)
31.8102
(Use J = 1.82
2.85 in
1.0 1.0 , (AISC Manual 13th Table 3-1, page 3-10)
101.524 ksi
252.6 ft-kips
151.3 ft-kips where 1.67 , (AISC 365-05 F1)
<== Not Applicable.
284.1 ft-kips
where 8.13
9.15 25.09
151.3 ft-kips
<== Not Applicable.
6.33 ft
33.85 ft
where 0.53
2.87 in
277.5 ft-kips
250 ft-kips 250 ft-kips
23.97
87.03 137.27
1.11
102.385 0.50 > 0.23, AISC 360-05 F4-5 )
245.2238 ft-kips
Cw = Iy h02 / 4 =
J = [tw d (tw2 + d2)] / 12 = in4, (not applicable if taken web only, EIT Manual page 26)
in4 )
rts =[( Iy Cw)0.5/ Sx)]0.5 =
c = Cb =
Mallowable, F2 =Mn / Wb = Wb =
DETERMINE ALLOWABLE FLEXURAL STRENGTH , Mn / Wb , BASED ON AISC 365-05 Chapter F3
l = bf / (2 tf) =
lpf = lp = lrf = lr =
Mallowable, F3 =Min(Mn,F2 , Mn,F3) / Wb =
DETERMINE ALLOWABLE FLEXURAL STRENGTH , Mn / Wb , BASED ON AISC 365-05 Chapter F4
aw =hc tw/ (bfc tfc) =
Mp = Min [Zx Fy , 1.6Sxc Fy ] =
Myc = Sxc Fy = Myt = Sxt Fy =
l = hc / tw =
lpw = lp = lrw = lr =
ksi, (for Iyc / Iy =
22
20
1 0.078b bcr
tsxb
ts
E JcC LF
rS hL
r
, 2
,
0.7 , ,
, ,
p b p
b pp p y p p b rb xn F
r p
cr p r bx
forM L L
L LMin forC SM M F M L L LM
L L
Min forSF M L L
, 3
2
0.7 ,
0.9,
pfp p y x
rf pfn F
c x
for Noncompact FlangesSM M F
MEk S for Slender Flanges
l ll l
l
1.1p ty
EL r
F
2
0
01.95 1 1 6.76 Lr t
L xc
E J S hF xcL rE JS hF
, 4.2
,
, ,
, ,
pc yc b p
b ppc yc pc yc L pc yc p b rb xcn F
r p
cr pc yc r bxc
forR M L L
L LMin forC SR M R M F R M L L LM
L L
Min forSF R M L L
20
0
112
6
fct
w
br
h ha
d dh
, /
1 , , /
pc w pw
yc
pcp p pw p
c w pwyc yc ycrw pw
Mfor h t
MR
M M MMin for h t
M M M
l
l ll
l l
22
20
1 0.078b bcr
txcb
t
E JC LF
rS hLr
(cont'd)
277.5 ft-kips
1.11
146.8 ft-kips
<== Not Applicable.
21.62 ft
41.4981 ksi
50 ksi
1
124.2 ft-kips
9 24 , 3.74
14.7 ft
5.00 1.000
112.11 kips
67.1317 kips 1.67 , (AISC 365-05 G1)
TOTAL SUPERIMPOSED GRAVITY LOAD
w = DL + LL = 0.000 kips / ft , 0.00 kips
CHECK EACH SECTION CAPACITIES
Section Left 0.00 S 0.00 S 0.00 S 0.00 S 0.00 S Point 0.17 S 0.33 S 0.50 S 0.67 S 0.83 S RightDistance 0 0.00 0.00 0.00 0.00 0.00 0.00 2.50 5.00 7.50 10.00 12.50 15.00
10 10 10 10 10 10 10 10 10 10 10 10 105 5 5 5 5 5 5 5 5 5 5 5 5
299 299 299 299 299 299 299 299 299 299 299 299 29953.0 53.0 53.0 53.0 53.0 53.0 53.0 53.0 53.0 53.0 53.0 53.0 53.00.40 0.40 0.40 0.40 0.40 0.40 0.00 -0.27 -0.13 0.00 0.13 0.27 0.40
0 0 0 0 0 0 0 1 1 1 1 1 0
Mallowable, F4 = Min( Mn,F4.2 , Mn,F4.3, RptMyt) / Wb =
DETERMINE ALLOWABLE FLEXURAL STRENGTH , Mn / Wb , BASED ON AISC 365-05 Chapter F5
Mallowable, F5 = Min( RpgFySxc , RpgFcr,F5.2Sxc , RpgFcr,F5.3Sxc , FySxt) / Wb =
DETERMINE ALLOWABLE SHEAR STRENGTH , Vn / Wv , BASED ON AISC 365-05 Chapter G2
h = d - tf,top - tf,bot = in , h / tw = Aw = in2 ,a =
Vn = 0.6 FyAwCv =
Vallowable = Vn / Wv = Wv =
P = PDL + PLL =
d (in)y (in)
I (in4)Wt (plf)V (kips)M (ft-k)
25
5 , / 3/
5 , / 3v
for a ha h
for a h
k
2
1.0 , / 1.10
1.10, 1.10 / 1.37
/
1.51, 1.37 /
/
vw
y
v v vwv
y y yw
v vw
y yw
Ekfor h tF
E E Ek k kfor h th t F F F
E Ek kfor h tF Fh t
C
0.7r t
y
EL r
F
, 5.2
2
2
,
0.3 , ,
, ,
y b p
b py y y p b rb
r p
cr F
by r b
forF L L
L LMin forC F F F L L L
L L
F
ECMin forF L LLbrt
, 5.3
2
,
0.3 ,
0.9,
2
y
pfy y
rf pfcr F
c
f
f
for Compact FlangesF
for Noncompact FlangesF F
FEk for Slender Flanges
b
t
l ll l
, 10
1 5.7 , 1.01200 300 , 10
w cpg
yw w
Min Ea hMinRMin a t F
, 5.3
2
,
,
0.9,
pc yc
pfpc yc pc yc L xc
n F rf pf
c xc
for Compact FlangesR M
for Noncompact FlangesSR M R M FM
Ek S for Slender Flanges
l ll l
l
, /
1 , , /
pc w pw
yt
ptp p pw p
c w pwyt yt ytrw pw
Mfor h t
MR
M M MMin for h t
M M M
l
l ll
l l
(cont'd)
1.491237 ft-kips @ 7.50 ft, from heel.
< 151.271 ft-kips[Satisfactory]
0.40 kips @ 15.00 ft, from heel.
< 67.1317 kips [Satisfactory]
DETERMINE DEFLECTION AT MID SPAN
0.01 in ( L / 25804 ) (for camber, self Wt included.)
where E = 29000 ksi w = 0.053 kips / ft
I = 299 P = 0 kipsb = 0.3 ft L = 15.0 ft
0.00 #DIV/0!
where P = 0 kips w = 0.000 kips / ft
DETERMINE FLANGE TO WEB WELDING (AISC 360-05 J2.4 )
1/4 in
3/16
4/162.0
0.40 kips
29
0.04 kips / in
A = 24 in 2293 in. o.c.
USE 1/4 in - 24 in @ 2293 in o.c.
DESIGN STIFFENERS
2. CHECK LOCAL WEB YIELDING FOR THE CONCENTRATED LOAD. (AISC 360-05, J10.2)R = P = 0.00 kipsN = 0 in, bearing length, point.
0.87 in1.5
0.00 < [Satisfactory]
Mmax =
Mallowable =
Vmax =
Vallowable =
in4
w =
wmin = in, < w
wmax = in, > wW =
Vmax =
Q = Af(d - y - 0.5 tf,top) = in3
vmax = Vmax Q / I =
1. BEARING STIFFENERS ARE REQUIRED AT EACH END SUPPORT. (AISC 360-05, J10.8)
k = tf,top + w =W =
Fy / W
-160-140-120-100
-80-60-40-20
0
BENDING LOADS & CAPACITY
Length
Mo
me
nts
-68.00-67.50-67.00-66.50-66.00-65.50
SHEAR LOADS & CAPACITY
Length
Sh
ea
r F
orc
es
4
3/ 2225 0.06415
384DL
w PbLbL
EI EIL
4
3/ 2225 0.06415
384LL
w PbLbL
EI EIL
0.6 0.707
max
EXX w AFB
v
W
,5
,2.5
Rfor c d
N kt wR
for c dN kt w
(cont'd)3. CHECK WEB CRIPPLING FOR THE CONCENTRATED LOAD. (AISC 360-05, J10.3)
2.0
85.01 > P [Satisfactory]
(Note : If item 2, local web yielding is Satisfactory, this item does not need to be checked.)
4. CHECK SIDESWAY WEB BUCKING FOR THE CONCENTRATED LOAD. (AISC 360-05, J10.4)
8.37 in
960000 ksi
1.261.76
171.48 > P [Satisfactory]
(Note : If item 2, local web yielding is Satisfactory, this item does not need to be checked.)
5. DETERMINE STIFFENER SIZE.
1/3 4 in
12.80[Satisfactory]
4.14 15
R = 0.4 kips
1.67 , (AISC 365-05 E1)
3.5
113
23867.77 ksi
123.9 kips, (AISC 360-05 E2)
> R [Satisfactory]
Techincal Reference: 1. AISC: "Steel Construction Manual 13th Edition", American Institute of Steel Construction, 2005.
W =
dc = d - 2k =
Cr =
(dc / tw ) / (l / bf) =W =
tw = in , bst =
bst / tw = < 0.56 (E / Fy)0.5 , (AISC 360-05 Table B4.1)
Ag = in2 , I = in4
Wc =
K l / r = 0.75 h / ( I / Aeff)0.5 =
Cc = 4.71 (E/ Fy)0.5 =
1.5
2
1.5
2
0.80 1 3 , 0.5
/ 1 /
0.40 1 3 , 0.5
yw fww
f w
yw fww
f w
tEFN t for c dtd t t
RntEFN t for c dt
d t t
W W
33
2
33
2
/ /0.4 , 1.7
/ /
/ // 1 / 1 0.4 , 1.7 2.3
/ /
/, 2.3
/
r w f c w c w
f f
r w f c w c w
f f
c w
f
C t t d t d tforl lb bh
C t t d t d tforRnl lb bh
d tP forl b
W W W
/ /
,0.658
0.877 ,
F yy cFe
R An c g c
e c
klfor CF
r
klfor CF
r
W W
2
2/
FeE
kl r
PROJECT : PAGE :
CLIENT : DESIGN BY : JOB NO. : DATE : REVIEW BY :
WF Simply Supported Beam Design with Torsional Loading Based on AISC Manual 9th
INPUT DATA & DESIGN SUMMARY
BEAM SECTION = > W10X54 = > A dGRAVITY DISTRIBUTED LOAD w = 1.15 kips / ft 15.8 10.1 4.38 2.55 303 60
LATERAL POINT LOAD AT MID F = 5 kips lTORSION AT MID SPAN T = 5.1 ft-kips 103 20.6 0.01744 0.37 10.00 0.62
AXIAL LOAD P = 96 kips
BEAM LENGTH 15 ft
BEAM YIELD STRESS 50 ksi
VERTICAL BENDING UNBRACED LENGTH 15 ft
AXIAL VERTICAL UNBRACED LENGTH 15 ft
AXIAL HORIZONTAL UNBRACED LENGTH 7.5 ft
ANALYSIS
CHECK LOCAL BUCKLING (AISC-ASD Tab. B5.1)
8.13 < 9.19
[Satisfactory]
27.30 < 90.51 THE BEAM DESIGN IS ADEQUATE.[Satisfactory]
DETERMINE GOVERNING MOMENTS AT MIDDLE OF SPAN
32.3 ft-kips
18.8 ft-kips
22.7 ft-kips 0.584 ,(Philip page 101)
13.3 ft-kips
DETERMINE GOVERNING UNBALANCED SEGMENT LENGTH (AISC-ASD F1)
8.96 ft
20.30 ft
22.39 ft
Where 1.64
2.66
1.00
DETERMINE ALLOWABLE BENDING STRESSES (AISC-ASD F1)
= = N/A
= = 30.00
= = N/A
= = N/A
Where 25.85 ksi
16.67 ksi
30.00 ksi
CHECK VERTICAL FLEXURAL CAPACITY (AISC-ASD F & Philip page 100)
0.73 < 1.00 [Satisfactory]
Where 21.93 ksi
rx ry Ix Sx
Iy Sy tw bf tf
L =
Fy =
Lb =
Lx =
Ly =
bf / (2tf ) = 65 / (Fy)0.5 =
d / tw = 640 / (Fy)0.5 =
Mx = w L2/ 8 =
My = F L / 4 =
M0 = T L / (4d) =
MT = bM0 =
Lc = MIN[76bf/(Fy)0.5 , 20000/(d/Af)Fy] =
Lu = MAX[rT(102000Cb/Fy)0.5 , 12000Cb/(d/Af)0.6Fy] =
L3 = rT(510000Cb/Fy)0.5 =
(d/Af) = in-1
rT =
Cb =
Fbx = {0.66Fy ksi, for Lb @ [0, Lc]
0.60Fy ksi, for Lb @ (Lc, Lu]
MAX(Fb1, Fb3) ksi, for Lb @ (Lu, L3]
MAX(Fb2, Fb3) ksi, for Lb @ (L3, Larger)
Fb1 = MIN{[2/3 - Fy(L/rT)2/(1530000Cb)]Fy , 0.6Fy} =
Fb2 = MIN[170000Cb/(L/rT)2, Fy/3] =
Fb3 = MIN[12000Cb/(Ld/Af), 0.6Fy] =
fbx / Fbx =
fbx = Mx / Sx + 2MT / Sy =
24 sinh
2sinh
L
L L
l
bl l
(cont'd)CHECK COMPRESSION CAPACITY (AISC-ASD E2)
0.24 < 1.33 [Satisfactory]
Where 6.08 ksi
K = 1.0
29000 ksi 25.68
107 N/A
41.10 < 200 [Satisfactory]
0.38
CHECK COMBINED STRESS (AISC-ASD H1)
0.24 > 0.15
1.33 < 1.33
Where 1.00
10.92 ksi
37.50 ksi
88.39 ksi 120.18 ksi
1.22 < 1.33
1.26 < 1.33 <== Not applicable.
[Satisfactory]
DETERMINE DEFLECTIONS
0.22127
Where 11200 ksi
J = 1.82
0.15 in = L / 1207 , vertical deflection at middle
Where 303
0.20 in = L / 885 , horizontal deflection at middle
Where 103
Technical References: 1. AISC: "Manual of Steel construction 9th", American Institute of Steel Construction, 1990. 2. Philip H. Lin: "Simplified Design for Torsional Loading of Rolled Steel Members", Engineering Journal, AISC, 1977.
fa / Fa =
fa = P / A =
Es =Fa = {
(1-F2/2)Fy / (5/3+3F/8-F3/8) = ksi, for Cc > (Kl/r)
Cc = (22Es/Fy)0.5 = 122Es/[23(KL/r)2] = ksi, for Cc < (Kl/r)
KL/r = MAX(KLx/rx, KLy/ry) =
F = (KL/ r) / Cc =
fa / Fa =
Cm =
fby = My / Sy =
Fby = 0.75 Fy =
o , max twist angle at middle (Philip page 100)
G =
in4
I3 = Ix sin2(90-) + Iy cos2(90-) = in4 , (AISC-ASD Page 6-23)
I4 = Ix cos2(90-) + Iy sin2(90-) = in4 , (AISC-ASD Page 6-23)
1 1' '
fCf f myC bymxa bxfF a fa aFbx FbyFex Fey
212'2
23
EFex
K l xr x
212'2
23
EFey
K l yr y
0.6
ff f bya bxF F Fbx byy
ff f bya bxF F Fa bx by
2sinh
2 sinh2 22 sinh
LT LL
GJ L
lll l l
4
3
5384
wLvert E I
3
448
F Lhoriz E I