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7/21/2019 Member Detail
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M2M12
M38
M39
M29
Detail member
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Design Of Member No. 2 As Per AISC
Input Parameters
Member Section H300X300X10
Cross Sectional Area Ax (m
2
) 0.01Net section factor 1.00
Net Effective Sectional Area Anet (m2) 0.01
Shear Area Along Y Axis Ay (m2) 0.00
rz (m ) 0.13
ry (m ) 0.08
Section Modulus About Z Axis - Tension Edge Stz (m3) 0.00
Section Modulus About Z Axis - Compression Edge Szz (m3) 0.00
Section Modulus About Y Axis - Tension Edge Sty (m3) 0.00
Section Modulus About Y Axis - Compression Edge Syy (m3) 0.00
Unsupported Length - Z Axis For Slenderness Check Lz (m ) 1.70
Unsupported Length - Y Axis For Slenderness Check Ly (m ) 1.70
Effective Length For Allowable Bending Stress Calculation Unl (m )1.70
Yield Stress fy (MPa) 248.00
Ultimate tensile strength fu (MPa) 400.00
Allowable Ratio For Interaction Check 1.50
Design Forces
Combined Axial Force & Bi-axial momentAxial Load Fx (kg ) -1.#J
Torsion Mx (kg m ) -1.#J
Z Axis Moment Mz (kg m ) 1.#J
Y Axis Moment My (kg m ) -1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 2
No Shear Force Developed Along Z Axis
Shear Along Y Axis
Shear Along Y Axis Fy (kg ) 1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 2
Details Of Calculation
Slenderness Checking
Lez (m ) 1.70
Ley (m ) 1.70
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Lez / rz 13.02
Ley / ry 22.51
Actual Slenderness Ratio 22.51
Allowable Slenderness Ratio 300.00
Status SAFE
Check Against Axial Tension And Bi-Axial Bending
No Warping Tensile Normal Stress Developed, Ws is 0.0 ksi
T1 (kg )
=Fx / ( Ax0.60fy ) 1.#INF
T2 (kg )
=Fx / ( Anet0.60fu ) 1.#INF
Actual Tensile Stress ft (MPa)
=Fx / Ax + Ws 0.08
Allowable Tensile Stress ft_allowable
(MPa)
=0.60fy 99.97
Bending Tension Governs For AISC H2-1
Actual Bending Tensile Stress - Z Axis ftz (MPa)
=Mz / Stz 29.12
No Bending Moment Developed Along Y Axis
Calculation Of Allowable Bending Stresses
Calculation of Allowable Bending Tensile Stress About Z and Y Axis :
Limiting Width - Thickness Ratio = 0.5 * bf / tf 10.00
Lc
=Min ( 76bf / fy0.5, 20000 / (( d / Af ) fy )) (in) 149.61
Interaction Checking
Factor by which all allowable stresses/capacities to be multiplied2.00
Interaction ratio
=ft / ft_allowable + ftz / ftz_allowable + fty / fty_allowable 0.09
Status SAFE
Check Against Shear
Shear Stress Along Y Axis Vy (MPa)
=Fy / Ay 10.62
Vf (MPa)
=0.4fy 99.28
f
=( d w - 2t
f ) / t
w*f
y
0.5 162.00
f is less than 380.
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Allowable Shear Stress V_allowable
(MPa)
=0.4fy 99.28
Interaction ratio (Along Y Axis)
=Vy / V _allowable 0.11
Status SAFE
Deflection Checking Ignored
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Design Of Member No. 12 As Per AISC
Input Parameters
Member Section 2XL100X100X10
- 0.000000 mm short leg back-to-back
Cross Sectional Area Ax (m
2
) 0.00Shear Area Along Y Axis Ay (m
2) 0.00
rz (m ) 0.03
ry (m ) 0.04
Section Modulus About Z Axis - Tension Edge Stz (m3) 0.00
Section Modulus About Z Axis - Compression Edge Szz (m3) 0.00
Section Modulus About Y Axis - Tension Edge Sty (m3) 0.00
Section Modulus About Y Axis - Compression Edge Syy (m3) 0.00
Unsupported Length - Z Axis For Slenderness Check Lz (m ) 1.70
Unsupported Length - Y Axis For Slenderness Check Ly (m ) 1.70
Effective Length For Allowable Bending Stress Calculation Unl (m )1.70
Yield Stress fy (MPa) 248.00
Ultimate tensile strength fu (MPa) 400.00
Allowable Ratio For Interaction Check 1.50
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx (kg ) 1.#J
Torsion Mx (kg m ) -1.#JZ Axis Moment Mz (kg m ) 1.#J
Y Axis Moment My (kg m ) -1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 12
No Shear Force Developed Along Z Axis
Shear Along Y Axis
Shear Along Y Axis Fy (kg ) 1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 12
Details Of Calculation
Slenderness Checking
Lez (m ) 1.70
Ley (m ) 1.70
Lez / rz 55.23
Ley / ry 55.03
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Actual Slenderness Ratio 55.23
Allowable Slenderness Ratio 200.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc (MPa)=Fx / Ax 13.64
Calculation Of Allowable Axial Compressive Stress :
L / r ( Critical Value ) 55.23
E (MPa) 205000.78
Cc
2E / ( Qs fy )
0.5127.68
L / r is less than Cc
F1a(Ksi)
=Q s fy( 1 - 0.5*( L / r * Cc )2 ) 32.63
F2a
=1.667 + 0.375 * L / r * Cc - 0.125 * ( L / r * Cc )3
1.82
Allowable Axial Compressive Stress fc_allowable
(MPa)
=F1a / F2a 123.68
Bending about Z Axis :
Actual Bending Compressive Stress - Z Axis fcz (MPa)=Mz / Szz 78.97
No Bending Moment Developed Along Y Axis
Calculation of Allowable Bending Compressive Stress About Z and Y Axis :
Allowable Bending Compressive Stress - Z Axis fcz_allowable (MPa) 163.82
Allowable Bending Compressive Stress - Y Axis fcy_allowable (MPa) 148.93
Interaction Checking
Factor by which all allowable stresses/capacities to be multiplied2.00
Interaction ratio
=fc / fc_allowable + fcz / fcz_allowable + fcy / fcy_allowable 0.30
Status SAFE
Check Against Shear
Shear Stress Along Y Axis Vy (MPa)
=Fy / Ay 4.83
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 198.57
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Interaction ratio (Along Y Axis)
=Vy / V _allowable 0.02
Status SAFE
Deflection Checking Ignored
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Design Of Member No. 38 As Per AISC
Input Parameters
Member Section 2XL200X200X20
- 0.000000 mm short leg back-to-back
Cross Sectional Area Ax (m
2
) 0.02Shear Area Along Y Axis Ay (m
2) 0.00
rz (m ) 0.06
ry (m ) 0.08
Section Modulus About Z Axis - Tension Edge Stz (m3) 0.00
Section Modulus About Z Axis - Compression Edge Szz (m3) 0.00
Section Modulus About Y Axis - Tension Edge Sty (m3) 0.00
Section Modulus About Y Axis - Compression Edge Syy (m3) 0.00
Unsupported Length - Z Axis For Slenderness Check Lz (m ) 1.05
Unsupported Length - Y Axis For Slenderness Check Ly (m ) 18.10
Effective Length For Allowable Bending Stress Calculation Unl (m )18.10
Yield Stress fy (MPa) 248.00
Ultimate tensile strength fu (MPa) 400.00
Allowable Ratio For Interaction Check 1.50
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx (kg ) 1.#J
Torsion Mx (kg m ) -1.#JZ Axis Moment Mz (kg m ) 1.#J
Y Axis Moment My (kg m ) -1.#J
Critical Loadcase No. 3
Critical Section (m ) 1.00
Beam No. 48
No Shear Force Developed Along Z Axis
No Shear Force Developed Along Y Axis
Details Of Calculation
Slenderness Checking
Lez (m ) 1.05
Ley (m ) 18.10
Lez / rz 17.06
Ley / ry 216.15
Actual Slenderness Ratio 216.15
Allowable Slenderness Ratio 200.00
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Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc (MPa)
=Fx / Ax 36.63
Calculation Of Allowable Axial Compressive Stress :
L / r ( Critical Value ) 216.15
E (MPa) 205000.78
Cc
2E / ( Qs fy )
0.5127.68
Allowable Axial Compressive Stress fc_allowable
(MPa)
=F1a / F2a 22.59
Bending about Z Axis :
Actual Bending Compressive Stress - Z Axis fcz (MPa)
=Mz / Szz 18.64
No Bending Moment Developed Along Y Axis
Calculation of Allowable Bending Compressive Stress About Z and Y Axis :
Allowable Bending Compressive Stress - Z Axis fcz_allowable (MPa) 163.82
Allowable Bending Compressive Stress - Y Axis fcy_allowable (MPa) 148.93
Interaction Checking
Factor by which all allowable stresses/capacities to be multiplied2.00
E (MPa) 205000.78
C mz 0.62
C my 0.60
fez
=12*2*E / ( 23*Lez / rz
2 ) 1052.52
fffz
=1 - fc / fez 1.00
fey=12*2*E / ( 23*Ley / ry
2 ) 6.55
fffy
=1 - fc / fey 0.81
Interaction ratio
=fc / fc_allowable + C mzfcz / ( fffz fcz_allowable ) +
C myfcy / ( fffy fcy_allowable ) 0.83
Status SAFE
Check Against Shear
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Shear Stress Along Y Axis Vy (MPa)
=Fy / Ay 18.09
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 198.57
Interaction ratio (Along Y Axis)
=Vy / V _allowable 0.09
Status SAFE
Deflection Checking Ignored
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Design Of Member No. 39 As Per AISC
Input Parameters
Member Section 2XL200X200X25
- 0.000000 mm short leg back-to-back
Cross Sectional Area Ax (m
2
) 0.02Shear Area Along Y Axis Ay (m
2) 0.00
rz (m ) 0.06
ry (m ) 0.08
Section Modulus About Z Axis - Tension Edge Stz (m3) 0.00
Section Modulus About Z Axis - Compression Edge Szz (m3) 0.00
Section Modulus About Y Axis - Tension Edge Sty (m3) 0.00
Section Modulus About Y Axis - Compression Edge Syy (m3) 0.00
Unsupported Length - Z Axis For Slenderness Check Lz (m ) 1.05
Unsupported Length - Y Axis For Slenderness Check Ly (m ) 18.10
Effective Length For Allowable Bending Stress Calculation Unl (m )18.10
Yield Stress fy (MPa) 248.00
Ultimate tensile strength fu (MPa) 400.00
Allowable Ratio For Interaction Check 1.50
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx (kg ) 1.#J
Torsion Mx (kg m ) -1.#JZ Axis Moment Mz (kg m ) -1.#J
Y Axis Moment My (kg m ) -1.#J
Critical Loadcase No. 3
Critical Section (m ) 1.00
Beam No. 73
No Shear Force Developed Along Z Axis
Shear Along Y Axis
Shear Along Y Axis Fy (kg ) 1.#J
Critical Loadcase No. 3
Critical Section (m ) 1.00
Beam No. 73
Details Of Calculation
Slenderness Checking
Lez (m ) 1.05
Ley (m ) 18.10
Lez / rz 17.24
Ley / ry 213.83
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Actual Slenderness Ratio 213.83
Allowable Slenderness Ratio 200.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc (MPa)=Fx / Ax 42.56
Calculation Of Allowable Axial Compressive Stress :
L / r ( Critical Value ) 213.83
E (MPa) 205000.78
Cc
2E / ( Qs fy )
0.5127.68
Allowable Axial Compressive Stress fc_allowable
(MPa)
=F1a / F2a 23.09
Bending about Z Axis :
Actual Bending Compressive Stress - Z Axis fcz (MPa)
=Mz / Szz 50.14
No Bending Moment Developed Along Y Axis
Calculation of Allowable Bending Compressive Stress About Z and Y Axis :
Allowable Bending Compressive Stress - Z Axis fcz_allowable (MPa) 163.82
Allowable Bending Compressive Stress - Y Axis fcy_allowable (MPa) 148.93
Interaction Checking
Factor by which all allowable stresses/capacities to be multiplied2.00
E (MPa) 205000.78
C mz 0.58
C my 0.60
fez
=12*2*E / ( 23*Lez / rz
2 ) 1029.76
fffz
=1 - fc / fez 1.00
fey=12*2*E / ( 23*Ley / ry
2 ) 6.70
fffy
=1 - fc / fey 0.69
Interaction ratio
=fc / fc_allowable + C mzfcz / ( fffz fcz_allowable ) +
C myfcy / ( fffy fcy_allowable ) 1.01
Status SAFE
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Check Against Shear
Shear Stress Along Y Axis Vy (MPa)
=Fy / Ay 12.99
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 198.57
Interaction ratio (Along Y Axis)=Vy / V _allowable 0.07
Status SAFE
Deflection Checking Ignored
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Design Of Member No. 29 As Per AISC
Input Parameters
Member Section 2XL100X100X13
- 0.000000 mm short leg back-to-back
Cross Sectional Area Ax (m
2
) 0.00Shear Area Along Y Axis Ay (m
2) 0.00
rz (m ) 0.03
ry (m ) 0.04
Section Modulus About Z Axis - Tension Edge Stz (m3) 0.00
Section Modulus About Z Axis - Compression Edge Szz (m3) 0.00
Section Modulus About Y Axis - Tension Edge Sty (m3) 0.00
Section Modulus About Y Axis - Compression Edge Syy (m3) 0.00
Unsupported Length - Z Axis For Slenderness Check Lz (m ) 1.97
Unsupported Length - Y Axis For Slenderness Check Ly (m ) 1.97
Effective Length For Allowable Bending Stress Calculation Unl (m )1.97
Yield Stress fy (MPa) 248.00
Ultimate tensile strength fu (MPa) 400.00
Allowable Ratio For Interaction Check 1.50
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx (kg ) 1.#J
Torsion Mx (kg m ) -1.#JZ Axis Moment Mz (kg m ) 1.#J
Y Axis Moment My (kg m ) -1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 29
No Shear Force Developed Along Z Axis
Shear Along Y Axis
Shear Along Y Axis Fy (kg ) 1.#J
Critical Loadcase No. 3
Critical Section (m ) 0.00
Beam No. 29
Details Of Calculation
Slenderness Checking
Lez (m ) 1.97
Ley (m ) 1.97
Lez / rz 64.92
Ley / ry 51.19
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Actual Slenderness Ratio 64.92
Allowable Slenderness Ratio 200.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc (MPa)=Fx / Ax 122.74
Calculation Of Allowable Axial Compressive Stress :
L / r ( Critical Value ) 64.92
E (MPa) 205000.78
Cc
2E / ( Qs fy )
0.5127.68
L / r is less than Cc
F1a(Ksi)
=Q s fy( 1 - 0.5*( L / r * Cc )2 ) 31.35
F2a
=1.667 + 0.375 * L / r * Cc - 0.125 * ( L / r * Cc )3
1.84
Allowable Axial Compressive Stress fc_allowable
(MPa)
=F1a / F2a 117.38
Bending about Z Axis :
Actual Bending Compressive Stress - Z Axis fcz (MPa)=Mz / Szz 30.95
No Bending Moment Developed Along Y Axis
Calculation of Allowable Bending Compressive Stress About Z and Y Axis :
Allowable Bending Compressive Stress - Z Axis fcz_allowable (MPa) 163.82
Allowable Bending Compressive Stress - Y Axis fcy_allowable (MPa) 148.93
Interaction Checking
Factor by which all allowable stresses/capacities to be multiplied2.00
E (MPa) 205000.78
C mz 0.61
C my 0.60
fez
=12*2*E / ( 23*Lez / rz
2 ) 72.65
fffz
=1 - fc / fez 0.92
fey=12*2*E / ( 23*Ley / ry
2 ) 116.87
fffy=1 - fc / fey 0.95
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Interaction ratio
=fc / fc_allowable + C mzfcz / ( fffz fcz_allowable ) +
C myfcy / ( fffy fcy_allowable ) 0.60
Status SAFE
Check Against Shear
Shear Stress Along Y Axis Vy (MPa)
=Fy / Ay 1.03
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 198.57
Interaction ratio (Along Y Axis)
=Vy / V _allowable 0.01
Status SAFE
Deflection Checking Ignored
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