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TABLAS AISC TABLAS AISC TABLAS AISC, Resúmenes de Ingeniería Civil

TABLAS AISC TABLAS AISC TABLAS AISC TABLAS AISC TABLAS AISC

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2019/2020
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GOP
W, S, M, HP Shapes C, MC Shapes WT, ST, MT Shapes Single Angles Double Angles
Y Y
k1=0.8125 Y Y Y
k=1.02 tf=0.522 tf=0.343 b=3
bf=8.08 t=0.25
y=1.17 x=0.981
x(bar)=0.5 tf=0.64 d=6 t=0.5 X
d=20.8 T X d=6 X X d=4
d=6.1 X y=1.98
tw=0.375 tw=0.314 tw=0.37 b=4
(0, 3/8, or 3/4
bf=8.22 bf=2.03 gap)
W21x55 cm/cm2 C6x10.5 cm/cm2 WT6x25 cm/cm2 L6x4x1/2 cm/cm2 2L4x3x1/4LLBB cm/cm2
16.20 104.52 3.08 19.87 7.30 47.10 615.24 410.16
20.80 52.83 6.000 15.24 6.100 15.49 410.16 37.62
0.375 0.953 0.314 0.798 0.370 0.940 0.5 1.270 0.25 0.635
8.22 20.88 2.030 5.16 8.080 20.52 1.0000 2.54 0.6250 1.59
0.522 1.326 0.343 0.871 0.640 1.626 plf wt./ft. = 16.20 24.11 plf wt./ft. = 11.50 17.11
18-3/8 4-3/8 1.1400 2.90 4.7500 30.6451 3.38 21.81
1.020 2.59 0.8125 2.06 18.70 778 17.30 720.0804 5.49 229
0.813 2.06 1-1/8 3.79 62 4.31 70.6 1.98 32.4
5-1/2 0.500 1.27 1.600 4.06 1.9100 4.8514 1.270 3.23
2.09 5.31 0.486 1.23 1.170 2.97 1.980 5.0292 1.220 3.10
4.85 12.32 8.59 21.82 28.20 1,174 6.22 259 1.150 2.92
1140.00 47,450.383 15.10 629 6.97 114 2.06 33.8 1.270 3.23
110.00 1,803 5.04 83 1.960 4.98 1.1400 2.90 1.410 3.58
8.400 21.34 2.220 5.64 0.855 35.6 0.981 2.49 2.03 5.16
48.40 2,014.560 0.86 36 1.23 330 0.864 2.19 H = 0.710
11.80 193 0.56 91.93 4.90 0.441
1.730 4.39 0.529 1.34 2.67 6.78 0.407000 16.9
126.00 2,065 0.13 5.3 H = 0.899 0.8430000 226 Plates
18.40 302 5.91 1,587 2.32 96.4 Y
1.24 51.6 10.93 27.77 2.91 7.39 t=3
4980 1,337,309 2.48 6.30 H = --- X
101.98 259.02 H = 0.842 b=39.37
41.70 269.0 cm/cm2
44.70 1,861 3 7.62
20.80 341 39.37 100.00
61.80 1,013 plf wt./ft. = 401.90 598.09
118.110 762.00
88.583 3,687.08
59.055 967.74
0.866 2.20
15255.844 634,996
774.998 12,699.9
11.365 28.87
AISC MEMBER DIMENSIONS AND PROPERTIES VIEWER
in^2 A = in^2 A = in^2 A = in d = in d =
in d = in d = in d = in b = in b =
in tw = in tw = in tw = in t = in t =
in bf = in bf = in bf = in k = in k =
in tf = in tf = in tf =
in T = in T = i n k = in^2 A = in^2 A =
in k = in k = in^4 Ix = in^4 Ix = in^4 Ix =
in k1 = in gage = in^3 Sx = in^3 Sx = in^3 Sx =
in gage = in x(bar) = in rx = in rx = in rx =
in rt = in eo = in y = in y = in y =
in d/Af = in d/Af = in^4 Iy = in^4 Iy = in ry(0) =
in^4 Ix = in^4 Ix = in^3 Sy = in^3 Sy = in ry(3/8) =
in^3 Sx = in^3 Sx = in ry = in ry = in ry(3/4) =
in rx = in rx = in^4 J = in x = in ro(bar) =
in^4 Iy = in^4 Iy = in^6 Cw = in r z =
in^3 Sy = in^3 Sy = in a = TAN(a) =
in ry = in ry = in ro(bar) = in^4 J =
in^3 Zx = in^4 J = in^6 Cw =
in^3 Zy = in^6 Cw = in a =
in^4 J = in a = in ro(bar) =
in^6 Cw = in ro(bar) =
in a =
in^2 Wno =
in^4 Sw =
in t =
in^3 Qf = in b =
in^3 Qw =
in^2 A =
in^4 Ix =
in^3 Sx =
in rx =
in^4 Iy =
in^3 Sy =
in ry =
pf3
pf4
pf5
pf8
pf9
pfa
pfd
pfe
pff
pf12
pf13
pf14
pf15
pf16
pf17
pf18
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GOP W, S, M, HP Shapes C, MC Shapes WT, ST, MT Shapes Single Angles Double Angles Y Y k1=0.8125 Y^ Y^ Y k=1.02 tf=0.522 tf=0.343 b= bf=8.08 (^) t=0. y=1.17 x=0. x(bar)=0.5 (^) tf=0.64 d=6 t=0.5 (^) X d=20.8 T^ X^ d=6^ X^ X^ d= d=6.1 X^ y=1. tw=0.375 tw=0.314 tw=0.37 b= (0, 3/8, or 3/ bf=8.22 bf=2.03 (^) gap) W21x55 cm/cm2 C6x10.5 cm/cm2 WT6x25 cm/cm2 L6x4x1/2 cm/cm2 2L4x3x1/4LLBB cm/cm 16.20 104.52^ 3.08 19.87^ 7.30 47.10^ 6 15.24^ 4 10. 20.80 52.83 6.000 15.24 6.100 15.49 4 10.16 3 7. 0.375 0.953 0.314 0.798 0.370 0.940 0.5 1.270 0.25 0. 8.22 20.88 2.030 5.16 8.080 20.52 1.0000 2.54 0.6250 1. 0.522 1.326 0.343 0.871 0.640 1.626 plf wt./ft. = 16.20 24.11 plf wt./ft. = 11.50 17. 18-3/8 4-3/8 1.1400 2.90 4.7500 30.6451 3.38 21. 1.020 2.59 0.8125 2.06 18.70 778 17.30 720.0804 5.49 229 0.813 2.06 1-1/8 3.79 62 4.31 70.6 1.98 32. 5-1/2 0.500 1.27 1.600 4.06 1.9100 4.8514 1.270 3. 2.09 5.31^ 0.486 1.23^ 1.170 2.97^ 1.980 5.0292^ 1.220 3. 4.85 12.32^ 8.59 21.82^ 28.20 1,174^ 6.22^259 1.150 2. 1140.00 47,450.383^ 15.10^629 6.97^114 2.06 33.8^ 1.270 3. 110.00 1,803 5.04 83 1.960 4.98 1.1400 2.90 1.410 3. 8.400 21.34 2.220 5.64 0.855 35.6 0.981 2.49 2.03 5. 48.40 2,014.560 0.86 36 1.23 330 0.864 2.19 H = 0. 11.80 193 0.56 9 1.93 4.90 0. 1.730 4.39 0.529 1.34 2.67 6.78 0.407000 16. 126.00 2,065^ 0.13 5.3^ H = 0.899 0.8430000^226 Plates 18.40^302 5.91 1,587^ 2.32 96.4^ Y 1.24 51.6 10.93 27.77 2.91 7.39 t= 4980 1,337,309 2.48 6.30 H = --- X 101.98 259.02 H = 0.842 b=39. 41.70 269.0 cm/cm 44.70 1,861^ 3 7. 20.80 341 39.37 100. 61.80 1,013^ plf wt./ft. = 401.90 598. 118.110 762. 88.583 3,687. 59.055 967. 0.866 2. 15255.844 634, 774.998 12,699. 11.365 28. AISC MEMBER DIMENSIONS AND PROPERTIES VIEWER in^2 A = in^2 A = in^2 A = (^) in d = in d = in d = in d = in d = in b = in b = in tw = in tw = in tw = in t = in t = in bf = in bf = in bf = in k = in k = in tf = in tf = in tf = in T = in T = in k = in^2 A = in^2 A = in k = in k = in^4 Ix = in^4 Ix = in^4 Ix = in k1 = in gage = in^3 Sx = in^3 Sx = in^3 Sx = in gage = in x(bar) = in rx = in rx = in rx = in rt = in eo = in y = in y = in y = in d/Af = in d/Af = in^4 Iy = in^4 Iy = in ry(0) = in^4 Ix = in^4 Ix = (^) in^3 Sy = in^3 Sy = in ry(3/8) = in^3 Sx = in^3 Sx = in ry = in ry = in ry(3/4) = in rx = in rx = in^4 J = in x = in ro(bar) = in^4 Iy = in^4 Iy = in^6 Cw = in r z = in^3 Sy = in^3 Sy = in a = TAN(a) = in ry = in ry = in ro(bar) = in^4 J = in^3 Zx = in^4 J = in^6 Cw = in^3 Zy = in^6 Cw = in^ a = in^4 J = in a = in ro(bar) = in^6 Cw = in ro(bar) = in a = in^2 Wno = in^4 Sw = in t = in^3 Qf = in b = in^3 Qw = in^2 A = in^4 Ix = in^3 Sx = in rx = in^4 Iy = in^3 Sy = in ry =

Rectangular HSS Y t=0. H=14 X B= HSS14x14x1/2 cm/cm 14 35. 14 35. 0.465 1. plf wt./ft. = 89.60 133. 24.60 158. 743.00 30, 106.00 1, 5.490 13. 743.00 30, 106.00 1, 5.490 13. 124.00 2, 124.00 2, 1170.00 48, Round HSS & Pipes Y t=0. O.D.=1.32 X I.D.=0. PIPE1XS cm/cm in O.D. = 1.32 3. in I.D. = 0.957 2. 0.179 0. plf wt./ft. = 2.17 plf. 0.64 4. 0.11 4 0.16 3 0.407 1. in d = in b = in t = in^2 A = in^4 Ix = in^3 Sx = in rx = in^4 Iy = in^3 Sy = in ry = in^3 Zx = in^3 Zy = in^4 J = in t = in^2 A = in^4 Ix = in^3 Sx = in rx =

Pd = 120 kip Pu = 518.4 kip Pw = 288 kip Pa = 408 kip DISEÑO DE PERFIL W A TRACCION CON CONECTORES EN ALAS SELECCIONAR PERFIL W W21x Ag = 16. r = 1. tf = 0. bf = 8. d = 20. Fy = 50 Fu = 65 Diseño por fluencia Pn = 810 kip LRFD ASD 729 Pn/rho = 486 Diseño por rotura

Agujeros: 4

tamaño perno: 0. An = 14.373 in^ Selección WT = WT6x

espac. Entre conectores: 3 in

de tornillos por linea: 3

U (caso 2) 0. U (caso 7) 0. U = 0. Pn = 794.10825 kip LRFD ASD 595.58 Pn/rho = 397. ФPn = ФPn =

X ̅

Resistencia de diseño LRFD ASD 595.58 397.

Fcr 268. ar 0. m 1. Rpg 1. Re 1 Mn 467475748.2 N mm 47.68 t m Mn 363914165.4 N mm 37.12 t m

pies Cuando Lb > Lp Mn 44.17 t m bf 300

φb Mn 39.75 t m h 268

tf 16 t DE LA SECCION h 268.00 mm tw 6 mm h/tw 44.67 ok

SECCION NO COMPACTA

φv 0.

Aw 1608.00 mm pies 59. Calculo del Cortante nominal

φv Vn 299344.637 N

30.53 t pies Estado limite de pandeo local del ala

λp = 9.

λr = 25.

Cpg = 108143.

Cb 1

Estado Limite de pandeo lateral torsional

bfc 300

Viga W21x Lb 6300 mm 20. Fy 344.74 Mpa E 200000 Mpa

φb 0.

ry 80.1524 mm

G 77200 Mpa

J 810698.7 mm

A 11208 mm

Sx 1356024.1 mm

Cw 7.23521E+12 mm

Iy 72004824 mm

Fr 115 Mpa 70 Mpa para Laminados, 115 para soldados

FL 229.74 Mpa

Zx 1470936 mm

My 467475748.2 N mm

Mp 507090476.6 N mm 51.72 t m

φb Mn 46.

  1. Definir si es compacta o no compacta kc 0.455 INGRESAR b y t DE LA SECCION

λp = 9.16 b = 296

λr = 18.92 Patines de secciòn laminada t = 16

para el patin λ =^ 18.

  1. Definir Lp y Lr Lp 3401.707048 mm Lp 3.40 m 11. X1 19403. X2 0. Lr 14054.76116 mm Lr 14.05 m 46. Mr 311532976.7 N mm 31.78 t m Si Lb > Lr Mcr = 1229918244 N mm 125.45 t m

φb Mn 112.91 t m

pies Cuando Lb > Lp Mn 46.30 t m b 300

φb Mn 41.67 t m h 634

tf 16 t DE LA SECCION h 618.00 mm tw 8 mm h/tw 77.

SECCION NO COMPACTA λr = 137.

φv 0.

Aw 4944.00 mm pies 59. Calculo del Cortante nominal

φv Vn 920373.062 N

93.88 t pies

Viga HSS14x14x1/ Lb 3800 mm Fy 344.74 Mpa E 200000 Mpa

φb 0.

ry 139.45 mm

G 77200 MPa

J ### mm

A 15870.94 mm

Sx 1,737,029 mm

Cw

Iy

Fr 70 MPa

FL 274.74 MPa

Zx 2031995.94 mm

My 598823303 Nmm

Mp 700510279 Nmm 71.45 t m

b/t 28.

  1. Definir si es compacta o no compacta

λp =

λr = 33.

  1. Definir Lp y Lr Lp 14388.8648 mm Lp 14.39 m X X Lr Lr Mr Si Lb > Lr Mcr =

Secciones Cuadradas kl 275.52 in ry 5.49 in E 29000 ksi Fy 50 ksi 344.7 Mpa Cc 322. A 24.60 in kl/ry 50. c 7 IN I 743.00 in Fa 30.2386606 ksi 0. b/t 28.

150.812517 in Fbx,y 30 ksi M 10 T M 867.96 kip pulg fbx,y 8.18 ksi P 10 T 22.04 kip fa 0.89593496 ksi h/tw 30.1075269 53. Fv 20 ksi Vv 492 kips 223.2 t

Viga W300X650X16X Lb 6300 mm 20. Fy 344.74 Mpa E 200000 Mpa

φb 0.

ry 73.5603 mm

G 77200 Mpa

J 835898.7 mm

A 13308 mm

Sx 3332042 mm

Cw 7.23521E+12 mm

Iy 72011124 mm

Fr 115 Mpa 70 Mpa para Laminados, 115 para soldados

FL 229.74 Mpa

Zx 3332042 mm

My 1148688159 N mm

Mp 1148688159 N mm 117.17 t m

φb Mn 105.

  1. Definir si es compacta o no compacta kc 0.394 INGRESAR b y t DE LA SECCION

λp = 9.16 b = 147

λr = 17.60 Patines de secciòn fabricada t = 16

para el patin λ =^ 9.

  1. Definir Lp y Lr Lp 3121.9351 mm Lp 3.12 m 10. X1 8737. X2 0. Lr 8197.7502 mm Lr 8.20 m 26. Mr 765503329.1 N mm 78.08 t m Si Lb > Lr Mcr = 1232801105 N mm 125.75 t m

φb Mn 113.17 t m