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Member 1 Design Report Page 1 of 6 REFERENCES CALCULATIONS RESULTS Code: AISC 360-16 LRFD MEMBER #1 DESIGN REPORT Project details Project Name: Project ID: Company: Designer: Client: Project Notes: Project Units: imperial General member design information Section Name: W8x58 Shape: I-Beam (Rolled) Dimensions: Height Web Thick Top Flange Width Top Flange Thick Bottom Flange Width Bottom Flange Thick Fillet Properties: Area Moment of Inertia about the z-axis Moment of Inertia about the y-axis Plastic Section Modulus about the z-axis Plastic Section Modulus about the y-axis Torsion Contant Warping Contant Material properties: Material Name: Structural Steel Modulus of Elasticity Yield Strength Ultimate Tensile Strength Design parameters: Member length Length between braced points Effective Length factor for flexural buckling about y-axis Effective Length factor for flexural buckling about z-axis Load case Axial Force Major Banding Moment Minor Banding Moment Shear Force Shear Force CHECK AXIAL STRENGTH (axial compression member) Check slenderness ratio of axial compression member (AISC E2) Slenderness ratio z-axis Slenderness ratio y-axis

MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

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Page 1: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage1of6

REFERENCES CALCULATIONS RESULTS

Code:AISC360-16LRFD

MEMBER#1DESIGNREPORT

Projectdetails

ProjectName:ProjectID:Company:Designer:Client:ProjectNotes:ProjectUnits: imperial

Generalmemberdesigninformation

SectionName: W8x58Shape: I-Beam (Rolled)

Dimensions:HeightWebThickTopFlangeWidthTopFlangeThickBottomFlangeWidthBottomFlangeThickFillet

Properties:AreaMomentofInertiaaboutthez-axisMomentofInertiaaboutthey-axisPlasticSectionModulusaboutthez-axisPlasticSectionModulusaboutthey-axisTorsionContantWarpingContant

Materialproperties:MaterialName:StructuralSteelModulusofElasticityYieldStrengthUltimateTensileStrength

Designparameters:MemberlengthLengthbetweenbracedpointsEffectiveLengthfactorforflexuralbucklingabouty-axisEffectiveLengthfactorforflexuralbucklingaboutz-axis

Loadcase

AxialForceMajorBandingMomentMinorBandingMomentShearForceShearForce

CHECKAXIALSTRENGTH(axialcompressionmember)

Checkslendernessratioofaxialcompressionmember(AISCE2)Slendernessratioz-axis

Slendernessratioy-axis

Page 2: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage2of6

Maximumslendernessratio

STATUSOK!

Checkwidth-thicknessratioofflange(B4.TableB4.1a)

CalculateFlexuralBucklingStress

Calculatetheelasticcriticalbucklingstress .

Calculatetheflexuralbucklingstress .

Because:

NominalCompressiveStrength .

Calculateaxialcompressivestrength.

Calculatetheflexuralbucklingstress .

Because:

Checkratioofaxialstrength

Page 3: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage3of6

STATUSOK!

CHECKFLEXURALSTRENGTHABOUTMAJORAXIS

Calculatelimitingwidth-thicknessratioofflangeforflexure(AISCB4.TableB4.1b)

Calculatelimitingwidth-thicknessratioofwebforflexure

Calculatelateral-torsionalbucklingmodificationfactor

YieldingCalculatenominalflexuralstrengthforYielding(AISCF2.1(F2-1))

Lateral-TorsionalBucklingComputelimitinglaterallyunbracedlengthforthelimitstateofyieldingF2.2(F2-5)

Laterallyunbracedlengthforthelimitstateofinelasticlateral-torsionalbucklingF2.2(F2-6)FordoublysymmetricI-shapesF2-8a

Distancebetweentheflangecentroid

Page 4: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage4of6

CalculatenominalflexuralstrengthforLateral-torsionalbucklingF2.2(F2-2)Because:

then

Nominalflexuralstrengthaboutmajoraxis .

Calculateflexuralstrengthaboutmajoraxis

Checkratioofshearstrength

STATUSOK!

CHECKFLEXURALSTRENGTHABOUTMINORAXIS

Calculatelimitingwidth-thicknessratioofflangeforflexure(AISCB4.TableB4.1b)

Calculatelimitingwidth-thicknessratioofwebforflexure

YieldingCalculatenominalflexuralstrengthforYielding(AISCF6.1(F6-1))

М

М

М

Page 5: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage5of6

Nominalflexuralstrengthaboutminoraxis .

Calculateflexuralstrengthaboutminoraxis

Checkratioofshearstrength

STATUSOK!

CHECKSHEARSTRENGTHY-AXIS

Nominalshearstrengthy-axis .

Calculateshearstrengthy-axis

Checkratioofshearstrength

STATUSOK!

CHECKSHEARSTRENGTHZ-AXIS

Calculatethewebplatebucklingcoefficient(AISCG2.1).

Calculatethewebshearcoefficient(AISCG2.1)

Nominalshearstrengthz-axis .

Calculateshearstrengthz-axis

Checkratioofshearstrength

STATUSOK!

М

М

М

Page 6: MEMBER #1 DESIGN REPORT - skyciv.com SkyCiv AISC 360 Design... · Member 1 Design Report Page 2 of 6 Maximum slenderness ratio STATUS OK! Check width-thickness ratio of flange (B4

Member1DesignReportPage6of6

CHECKINTERACTIONOFCOMBINEDSTRENGTH

BecausePr/Pc<0.2:

STATUSOK!


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