WWYK263009_65 Design Analysis_Part16.pdf

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Bomber Agile Common Hangar; 4-Dock Hangar at Tinker Air Force Base
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W912BV25S0014
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This file contains structural analysis calculations and details for concrete grade beams and pier foundations for the Bomber Agile Common Hangar (BACH) at Tinker Air Force Base. The calculations include detailed analysis of three grade beam designs (GB1, GB2, and GB3) using ENERCALC and TEDDS software, with GB1 being 36"x30", GB2 being 36"x30", and GB3 being 36"x36". The documents also contain concrete pier axial capacity calculations and lateral analysis using L-PILE software for various pier diameters ranging from 2' to 7', with depths of 40'-50' and design loads accounting for both end bearing and skin friction resistance.

The foundation design includes detailed calculations for pier capacities ranging from 53,407# for 2' diameter piers to 838,410# for 7' diameter piers, with specific attention to bearing pressure of 23,000 psf and skin friction of 1,100 psf. The foundation reactions sheet shows column base reactions and grade beam reactions for the hangar structure, which inform the sizing and design of these foundation elements. The calculations demonstrate compliance with ACI 318-19 code requirements and include safety factors for various loading conditions including dead loads, live loads, and roof live loads.

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Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 18.43

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

18.43 18.43

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

18.43 18.43 18.43 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.05

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 26.51 [Kip] Ctrl Eq. : D11 at 0.00%

Intermediate results Unit Value Reference

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Ratio : 0.03

Capacity : 395.31 [Kip] Reference : Cl.E3

Demand : 10.95 [Kip] Ctrl Eq. : D6 at 0.00%

Page2

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 395.31 Cl.E3

Compression in the minor axis 22

Ratio : 0.05

Capacity : 224.54 [Kip] Reference : Cl.E3

Demand : 10.95 [Kip] Ctrl Eq. : D6 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 224.54 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 412.55 Cl.E4

Flexural Design

Bending about major axis, M33

Ratio : 0.00

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 0.56 [Kip*ft] Ctrl Eq. : D7 at 100.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength about a geometric axis(φMn): [Kip*ft] 69.38 Cl.F6.1

Shear Design

Shear in major axis 33

Ratio : 0.00

Capacity : 244.04 [Kip] Reference : Cl.G1

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 244.04 Cl.G1

Page3

Shear in minor axis 22

Ratio : 0.00

Capacity : 89.10 [Kip] Reference : Cl.G1

Demand : 0.03 [Kip] Ctrl Eq. : D7 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 89.10 Cl.G1

Combined Actions Design

Combined flexure and axial

Ratio : 0.03

Ctrl Eq. : D11 at 100.00% Reference : Eq.H1-1b

Intermediate results Unit Value Reference

Interaction of flexure and axial force: -- 0.03 Eq.H1-1b

Member : 2 - OK

Section information

Section name: W 8X40 (US)

Dimensions bf = 8.070 [in] Width d = 8.250 [in] Depth k = 0.954 [in] Distance k k1 = 0.813 [in] Distance k1 tf = 0.560 [in] Flange thickness tw = 0.360 [in] Web thickness

Properties Unit Major axis Minor axis

Gross area of the section. (Ag) [in2] 11.700

Moment of Inertia (local axes) (I) [in4] 146.000 49.100

Moment of Inertia (principal axes) (I') [in4] 146.000 49.100

Bending constant for moments (principal axis) (J') [in] 0.000 0.000

Radius of gyration (local axes) (r) [in] 3.533 2.049

Radius of gyration (principal axes) (r') [in] 3.533 2.049

Saint-Venant torsion constant. (J) [in4] 1.120

Section warping constant. (Cw) [in6] 726.000

Distance from centroid to shear center (principal axis) (xo,yo) [in] 0.000 0.000

Top elastic section modulus of the section (local axis) (Ssup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (local axis) (Sinf) [in3] 35.500 12.200

Page4

Top elastic section modulus of the section (principal axis) (S'sup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (principal axis) (S'inf) [in3] 35.500 12.200

Plastic section modulus (local axis) (Z) [in3] 39.800 18.500

Plastic section modulus (principal axis) (Z') [in3] 39.800 18.500

Polar radius of gyration. (ro) [in] 4.084

Area for shear (Aw) [in2] 9.040 2.970

Torsional constant. (C) [in3] 1.901

Material : A992 Gr50

Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 17.90

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

17.90 17.90

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

17.90 17.90 17.90 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.00

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 2.60 [Kip] Ctrl Eq. : D11 at 0.00%

Page5

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Ratio : 0.02

Capacity : 401.78 [Kip] Reference : Cl.E3

Demand : 8.79 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 401.78 Cl.E3

Compression in the minor axis 22

Ratio : 0.04

Capacity : 235.65 [Kip] Reference : Cl.E3

Demand : 8.79 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 235.65 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 414.06 Cl.E4

Flexural Design

Bending about major axis, M33

Ratio : 0.01

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 1.74 [Kip*ft] Ctrl Eq. : D11 at 100.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength about a geometric axis(φMn): [Kip*ft] 69.38 Cl.F6.1

Page6

Shear Design

Shear in major axis 33

Ratio : 0.00

Capacity : 244.04 [Kip] Reference : Cl.G1

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 244.04 Cl.G1

Shear in minor axis 22

Ratio : 0.00

Capacity : 89.10 [Kip] Reference : Cl.G1

Demand : 0.07 [Kip] Ctrl Eq. : D11 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 89.10 Cl.G1

Combined Actions Design

Combined flexure and axial

Ratio : 0.02

Ctrl Eq. : D3 at 100.00% Reference : Eq.H1-1b

Intermediate results Unit Value Reference

Interaction of flexure and axial force: -- 0.02 Eq.H1-1b

Member : 3 - OK

Section information

Section name: W 8X40 (US)

Dimensions bf = 8.070 [in] Width d = 8.250 [in] Depth k = 0.954 [in] Distance k k1 = 0.813 [in] Distance k1 tf = 0.560 [in] Flange thickness tw = 0.360 [in] Web thickness

Page7

Properties Unit Major axis Minor axis

Gross area of the section. (Ag) [in2] 11.700

Moment of Inertia (local axes) (I) [in4] 146.000 49.100

Moment of Inertia (principal axes) (I') [in4] 146.000 49.100

Bending constant for moments (principal axis) (J') [in] 0.000 0.000

Radius of gyration (local axes) (r) [in] 3.533 2.049

Radius of gyration (principal axes) (r') [in] 3.533 2.049

Saint-Venant torsion constant. (J) [in4] 1.120

Section warping constant. (Cw) [in6] 726.000

Distance from centroid to shear center (principal axis) (xo,yo) [in] 0.000 0.000

Top elastic section modulus of the section (local axis) (Ssup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (local axis) (Sinf) [in3] 35.500 12.200

Top elastic section modulus of the section (principal axis) (S'sup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (principal axis) (S'inf) [in3] 35.500 12.200

Plastic section modulus (local axis) (Z) [in3] 39.800 18.500

Plastic section modulus (principal axis) (Z') [in3] 39.800 18.500

Polar radius of gyration. (ro) [in] 4.084

Area for shear (Aw) [in2] 9.040 2.970

Torsional constant. (C) [in3] 1.901

Material : A992 Gr50

Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 10.20

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

10.20 10.20

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

10.20 10.20 10.20 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Page8

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.00

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Ratio : 0.01

Capacity : 482.25 [Kip] Reference : Cl.E3

Demand : 3.35 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 482.25 Cl.E3

Compression in the minor axis 22

Ratio : 0.01

Capacity : 405.54 [Kip] Reference : Cl.E3

Demand : 3.35 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 405.54 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 450.96 Cl.E4

Flexural Design

Bending about major axis, M33

Ratio : 0.01

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 1.74 [Kip*ft] Ctrl Eq. : D11 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Page9

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength about a geometric axis(φMn): [Kip*ft] 69.38 Cl.F6.1

Shear Design

Shear in major axis 33

Ratio : 0.00

Capacity : 244.04 [Kip] Reference : Cl.G1

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 244.04 Cl.G1

Shear in minor axis 22

Ratio : 0.00

Capacity : 89.10 [Kip] Reference : Cl.G1

Demand : 0.17 [Kip] Ctrl Eq. : D11 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 89.10 Cl.G1

Combined Actions Design

Combined flexure and axial

Ratio : 0.01

Ctrl Eq. : D7 at 0.00% Reference : Eq.H1-3a(H1-1b)

Intermediate results Unit Value Reference

Interaction for doubly symmetric members for in-plane bending: -- 0.01 Eq.H1-3a(H1-1b)

Interaction for doubly symmetric members for out-of-plane bending: -- 0.01 Eq.H1-3b

Member : 4 - OK

Section information

Section name: W 8X40 (US)

Page10

Dimensions bf = 8.070 [in] Width d = 8.250 [in] Depth k = 0.954 [in] Distance k k1 = 0.813 [in] Distance k1 tf = 0.560 [in] Flange thickness tw = 0.360 [in] Web thickness

Properties Unit Major axis Minor axis

Gross area of the section. (Ag) [in2] 11.700

Moment of Inertia (local axes) (I) [in4] 146.000 49.100

Moment of Inertia (principal axes) (I') [in4] 146.000 49.100

Bending constant for moments (principal axis) (J') [in] 0.000 0.000

Radius of gyration (local axes) (r) [in] 3.533 2.049

Radius of gyration (principal axes) (r') [in] 3.533 2.049

Saint-Venant torsion constant. (J) [in4] 1.120

Section warping constant. (Cw) [in6] 726.000

Distance from centroid to shear center (principal axis) (xo,yo) [in] 0.000 0.000

Top elastic section modulus of the section (local axis) (Ssup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (local axis) (Sinf) [in3] 35.500 12.200

Top elastic section modulus of the section (principal axis) (S'sup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (principal axis) (S'inf) [in3] 35.500 12.200

Plastic section modulus (local axis) (Z) [in3] 39.800 18.500

Plastic section modulus (principal axis) (Z') [in3] 39.800 18.500

Polar radius of gyration. (ro) [in] 4.084

Area for shear (Aw) [in2] 9.040 2.970

Torsional constant. (C) [in3] 1.901

Material : A992 Gr50

Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 9.70

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

9.70 9.70

Page11

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

9.70 9.70 9.70 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.00

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Ratio : 0.01

Capacity : 486.32 [Kip] Reference : Cl.E3

Demand : 3.35 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 486.32 Cl.E3

Compression in the minor axis 22

Ratio : 0.01

Capacity : 415.79 [Kip] Reference : Cl.E3

Demand : 3.35 [Kip] Ctrl Eq. : D3 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 415.79 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 454.65 Cl.E4

Flexural Design

Page12

Bending about major axis, M33

Ratio : 0.01

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 1.83 [Kip*ft] Ctrl Eq. : D7 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength about a geometric axis(φMn): [Kip*ft] 69.38 Cl.F6.1

Shear Design

Shear in major axis 33

Ratio : 0.00

Capacity : 244.04 [Kip] Reference : Cl.G1

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 244.04 Cl.G1

Shear in minor axis 22

Ratio : 0.00

Capacity : 89.10 [Kip] Reference : Cl.G1

Demand : 0.19 [Kip] Ctrl Eq. : D7 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 89.10 Cl.G1

Combined Actions Design

Combined flexure and axial

Ratio : 0.01

Ctrl Eq. : D7 at 0.00% Reference : Eq.H1-3a(H1-1b)

Page13

Interaction for doubly symmetric members for in-plane bending: -- 0.01 Eq.H1-3a(H1-1b)

Interaction for doubly symmetric members for out-of-plane bending: -- 0.01 Eq.H1-3b

Member : 5 - OK

Section information

Section name: W 8X40 (US)

Dimensions bf = 8.070 [in] Width d = 8.250 [in] Depth k = 0.954 [in] Distance k k1 = 0.813 [in] Distance k1 tf = 0.560 [in] Flange thickness tw = 0.360 [in] Web thickness

Properties Unit Major axis Minor axis

Gross area of the section. (Ag) [in2] 11.700

Moment of Inertia (local axes) (I) [in4] 146.000 49.100

Moment of Inertia (principal axes) (I') [in4] 146.000 49.100

Bending constant for moments (principal axis) (J') [in] 0.000 0.000

Radius of gyration (local axes) (r) [in] 3.533 2.049

Radius of gyration (principal axes) (r') [in] 3.533 2.049

Saint-Venant torsion constant. (J) [in4] 1.120

Section warping constant. (Cw) [in6] 726.000

Distance from centroid to shear center (principal axis) (xo,yo) [in] 0.000 0.000

Top elastic section modulus of the section (local axis) (Ssup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (local axis) (Sinf) [in3] 35.500 12.200

Top elastic section modulus of the section (principal axis) (S'sup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (principal axis) (S'inf) [in3] 35.500 12.200

Plastic section modulus (local axis) (Z) [in3] 39.800 18.500

Plastic section modulus (principal axis) (Z') [in3] 39.800 18.500

Polar radius of gyration. (ro) [in] 4.084

Area for shear (Aw) [in2] 9.040 2.970

Torsional constant. (C) [in3] 1.901

Material : A992 Gr50

Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Page14

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 18.40

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

18.40 18.40

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

18.40 18.40 18.40 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.00

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Ratio : 0.03

Capacity : 395.67 [Kip] Reference : Cl.E3

Demand : 11.95 [Kip] Ctrl Eq. : D8 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 395.67 Cl.E3

Compression in the minor axis 22

Page15

Ratio : 0.05

Capacity : 225.16 [Kip] Reference : Cl.E3

Demand : 11.95 [Kip] Ctrl Eq. : D8 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 225.16 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 412.63 Cl.E4

Flexural Design

Bending about major axis, M33

Ratio : 0.01

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 1.83 [Kip*ft] Ctrl Eq. : D7 at 100.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength about a geometric axis(φMn): [Kip*ft] 69.38 Cl.F6.1

Shear Design

Shear in major axis 33

Ratio : 0.00

Capacity : 244.04 [Kip] Reference : Cl.G1

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored shear capacity(φVn): [Kip] 244.04 Cl.G1

Shear in minor axis 22

Ratio : 0.00

Capacity : 89.10 [Kip] Reference : Cl.G1

Demand : 0.08 [Kip] Ctrl Eq. : D7 at 0.00%

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Factored shear capacity(φVn): [Kip] 89.10 Cl.G1

Combined Actions Design

Combined flexure and axial

Ratio : 0.04

Ctrl Eq. : D8 at 100.00% Reference : Eq.H1-1b

Intermediate results Unit Value Reference

Interaction of flexure and axial force: -- 0.04 Eq.H1-1b

Member : 6 - OK

Section information

Section name: W 8X40 (US)

Dimensions bf = 8.070 [in] Width d = 8.250 [in] Depth k = 0.954 [in] Distance k k1 = 0.813 [in] Distance k1 tf = 0.560 [in] Flange thickness tw = 0.360 [in] Web thickness

Properties Unit Major axis Minor axis

Gross area of the section. (Ag) [in2] 11.700

Moment of Inertia (local axes) (I) [in4] 146.000 49.100

Moment of Inertia (principal axes) (I') [in4] 146.000 49.100

Bending constant for moments (principal axis) (J') [in] 0.000 0.000

Radius of gyration (local axes) (r) [in] 3.533 2.049

Radius of gyration (principal axes) (r') [in] 3.533 2.049

Saint-Venant torsion constant. (J) [in4] 1.120

Section warping constant. (Cw) [in6] 726.000

Distance from centroid to shear center (principal axis) (xo,yo) [in] 0.000 0.000

Top elastic section modulus of the section (local axis) (Ssup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (local axis) (Sinf) [in3] 35.500 12.200

Top elastic section modulus of the section (principal axis) (S'sup) [in3] 35.500 12.200

Bottom elastic section modulus of the section (principal axis) (S'inf) [in3] 35.500 12.200

Plastic section modulus (local axis) (Z) [in3] 39.800 18.500

Plastic section modulus (principal axis) (Z') [in3] 39.800 18.500

Polar radius of gyration. (ro) [in] 4.084

Area for shear (Aw) [in2] 9.040 2.970

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Torsional constant. (C) [in3] 1.901

Material : A992 Gr50

Properties Unit Value

Yield stress (Fy): [Kip/in2] 50.00

Tensile strength (Fu): [Kip/in2] 65.00

Elasticity Modulus (E): [Kip/in2] 29000.00

Shear modulus for steel (G): [Kip/in2] 11153.85

Design Criteria

Description Unit Value

Length for tension slenderness ratio (L) [ft] 18.43

Distance between member lateral bracing points

Length (Lb) [ft]

Top Bottom

18.43 18.43

Laterally unbraced length

Length [ft] Effective length factor

Major axis(L33) Minor axis(L22) Torsional axis(Lt) Major axis(K33) Minor axis(K22) Torsional axis(Kt)

18.43 18.43 18.43 1.0 1.0 1.0

Additional assumptions

Continuous lateral torsional restraint No

Tension field action No

Continuous flexural torsional restraint No

Effective length factor value type None

Major axis frame type Sway

Minor axis frame type Sway

Design Checks

Axial Tension Design

Axial tension

Ratio : 0.00

Capacity : 526.50 [Kip] Reference : Cl.D2

Demand : 0.00 [Kip] Ctrl Eq. : D1 at 0.00%

Intermediate results Unit Value Reference

Factored axial tension capacity(φPn): [Kip] 526.50 Cl.D2

Axial Compression Design

Compression in the major axis 33

Page18

Ratio : 0.09

Capacity : 395.31 [Kip] Reference : Cl.E3

Demand : 36.14 [Kip] Ctrl Eq. : D7 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn33): [Kip] 395.31 Cl.E3

Compression in the minor axis 22

Ratio : 0.16

Capacity : 224.54 [Kip] Reference : Cl.E3

Demand : 36.14 [Kip] Ctrl Eq. : D7 at 0.00%

Intermediate results Unit Value Reference

Section classification

Factored flexural buckling strength(φPn22): [Kip] 224.54 Cl.E3

Factored torsional or flexural-torsional buckling strength(φPn11): [Kip] 412.55 Cl.E4

Flexural Design

Bending about major axis, M33

Ratio : 0.00

Capacity : 149.25 [Kip*ft] Reference : Cl.F2.1

Demand : 0.41 [Kip*ft] Ctrl Eq. : D11 at 100.00%

Intermediate results Unit Value Reference

Section classification

Factored yielding strength(φMn): [Kip*ft] 149.25 Cl.F2.1

Factored lateral-torsional buckling strength(φMn): [Kip*ft] 149.25 Cl.F2.2

Bending about minor axis, M22

Ratio : 0.00

Capacity : 69.38 [Kip*ft] Reference : Cl.F6.1

Demand : 0.00 [Kip*ft] Ctrl Eq. : D1 at 0.00%

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