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Page 1: 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