steel beam analysis and design...given: yield stress, steel section, loading find: pass/fail of...

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Architecture 324 Structures II Steel Beam Analysis and Design Steel Codes: ASD vs. LRFD Analysis Method Design Method University of Michigan, TCAUP Structures II Slide 1 of 24 Beam Strength vs Unbraced Length University of Michigan, TCAUP Structures II Slide 2 of 24 (for doubly symmetric sections)

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  • Architecture 324

    Structures II

    Steel Beam Analysis and Design

    • Steel Codes: ASD vs. LRFD

    • Analysis Method

    • Design Method

    University of Michigan, TCAUP Structures II Slide 1 of 24

    Beam Strength vs Unbraced Length

    University of Michigan, TCAUP Structures II Slide 2 of 24

    (for doubly symmetric sections)

  • Steel Beams by LRFD

    Yield Stress Values• A36 Carbon Steel Fy = 36 ksi• A992 High Strength Fy = 50 ksi

    Elastic Analysis for Bending

    • Plastic Behavior (zone 1)Mn = Mp = Fy Z < 1.5 My

    • Braced against LTB (Lb < Lp)

    • Inelastic Buckling “Decreased” (zone 2)Mn = Cb(Mp-(Mp-Mr)[(Lb-Lp)/(Lr-Lp)] < Mp

    • Lp < Lb < Lr

    • Elastic Buckling “Decreased Further” (zone 3)Mcr = Cb * π/Lb √(E*Iy*G*J + (π*E/Lb)^2 * IyCw)

    • Lb > Lr

    University of Michigan, TCAUP Structures II Slide 3 of 24

    Lp = 1.76 ry E/FyMp = Fy ZxMr = 0.7 Fy Sx

    Cb is LTB modification factor

    Cb 12.5 Mmax2.5 Mmax 3 MA 4MB 3MC

    Steel Beams by LRFD

    Yield Stress Values

    A36 Carbon Steel Fy = 36 ksiA992 High Strength Fy = 50 ksi

    Analysis for Bending

    • Plastic Behavior (zone 1)Mn = Mp = Fy Z < 1.5 My

    • Braced against LTB (Lb < Lp)

    • Inelastic Buckling “Decreased” (zone 2)Mn = Cb(Mp-(Mp-Mr)[(Lb-Lp)/(Lr-Lp)] < Mp

    • Lp < Lb < Lr

    • Elastic Buckling “Decreased Further” (zone 3) Mcr = Cb * π/Lb √(E*Iy*G*J + (π*E/Lb)^2 * IyCw)

    • Lb > Lr

    University of Michigan, TCAUP Structures II Slide 4 of 24

    AISC 15th ed.

  • Steel Beams by LRFD

    Moment Capacity Graphs

    Analysis for Bending

    • Plastic Behavior (zone 1)Mn = MpBraced against LTB (Lb < Lp)

    • Inelastic Buckling “Decreased” (zone 2)Mn < MpLp < Lb < Lr

    • Elastic Buckling “Decreased Further” (zone 3) Mn = McrLb > Lr

    University of Michigan, TCAUP Structures II Slide 5 of 24

    AISC 15th ed.

    University of Michigan, TCAUP Structures II Slide 6 of 24

    Design for Shear

    Shear stress in steel sections is approximated by averaging the stress in the web:

    Fv = V / AwAw = d * tw

    To adjust the stress a reduction factor of 0.6 is applied to Fy

    Fv = 0.6 Fyso, Vn = 0.6 Fy Aw (Zone 1)

    The equations for the 3 stress zones:( in all cases = 1.0)

  • University of Michigan, TCAUP Structures II Slide 7 of 24

    Design for Shear

    Steel

    Given: yield stress, steel section, loadingFind: pass/fail of section

    1. Calculate the factored design load wuwu = 1.2wDL + 1.6wLL

    2. Determine the design moment Mu.Mu will be the maximum beam moment using the factored loads

    3. Insure that Lb < Lp (zone 1)Lp = 1.76 ry 𝐸/𝐹𝑦

    4. Determine the nominal moment, MnMn = Fy Zx (look up Z for section)

    5. Factor the nominal momentøMn = 0.90 Mn

    6. Check that Mu < øMn

    7. Check shear

    8. Check deflection

    Pass/Fail Analysis of Steel Beams – for Zone 1 Lb < Lp

    University of Michigan, TCAUP Structures II Slide 8 of 24

  • Example:

    Given: yield stress, steel section, loading, braced @ 24” o.c.

    Find: pass/fail of section

    1. Calculate the factored design load wuwu = 1.2wDL + 1.6wLL

    2. Determine the design moment Mu.Mu will be the maximum beam moment using the factored loads.

    Pass/Fail Analysis of Steel Beams – for Zone 1 Lb < Lp

    University of Michigan, TCAUP Structures II Slide 9 of 24

    Example:Pass/Fail Analysis of Steel Beams – for Zone 1 Lb < Lp

    University of Michigan, TCAUP Structures II Slide 10 of 24

    3. Insure that Lb < Lp (zone 1)Lp = 1.76 ry 𝐸/𝐹𝑦Lp = 1.76 (1.26) 29000/50Lp = 53.4 in. = 4.45 ft > 2 ft ok

    3. Determine the nominal moment, MnMn = Mp = Fy Zx (look up Z for section)

    4. Factor the nominal momentøMn = 0.90 Mn

    5. Check that Mu < øMn

  • Analysis of Steel Beam – Lb < LpW21x44

    University of Michigan, TCAUP Structures II Slide 11 of 24

    7. Check shear

    Example cont.:Pass/Fail Analysis of Steel Beam – Lb < Lp

    University of Michigan, TCAUP Structures II Slide 12 of 24

    Check shear:

    Therefore, pass.7. Check shear

    8. Check deflection

  • Given: yield stress, steel sectionFind: moment or load capacity

    1. Determine the unbraced length of the compression flange (Lb).

    2. Find the Lp and Lr values from the AISC properties table 3-6

    3. Compare Lb to Lp and Lr and determine which equation for Mn or Mcr to be used.

    4. Determine the beam load equation for maximum moment in the beam. Solve for Mn.

    5. Calculate load based on maximum moment. Mu = b Mn

    Capacity Analysis of Steel Beam

    University of Michigan, TCAUP Structures II Slide 13 of 24

    Find applied live load capacity, wLL in KLFwu = 1.2wDL + 1.6wLLwDL = beam + floor = 44plf + 1500plf

    Fy = 50 ksi, Fully BracedMy = Fy * Sx = 50 ksi x 81.6 in^3 = 340 k-ft

    1. Find the Plastic Modulus (Zx) and Section Modulus (Sx) for the given section from the AISC table 1-1

    2. Determine 1.5 My (limit of Mp)

    3. Determine Mp = Fy Zx

    4. Compare Mp and 1.5 My, and choose the lesser of the two for Mn

    5. Calculate Mu: = b Mnb = 0.90

    Example – Capacity Analysis of Steel Beam

    University of Michigan, TCAUP Structures II Slide 14 of 24

  • 6. Using the maximum moment equation, solve for the factored distributed loading, wu

    7. The applied (unfactored) loadw = wu / (g factors)wu = 1.2wDL + 1.6wLL

    Example – Load Analysis cont.W21x44

    University of Michigan, TCAUP Structures II Slide 15 of 24

    Braced Beam Design with Plastic Modulus Table

    Procedure• Calculate Required Moment • Determine Mn

    Mu = b MnMn = Mu / b

    • Determine Minimum Zx requiredMn = Fy Zx = MpZx > Mn / Fy

    • Choose a section based on Z from the AISC table. Bold faced sections are lighter

    • Check Shear

    If h/tw < 59Vn = 0.6 * Fy * AwVu < v * Vn

    v = 1.0

    University of Michigan, TCAUP Structures II Slide 16 of 24

    AISC 16th ed.

  • 1. Use the maximum moment equation, and solve for the ultimate moment, Mu.

    2. Solve for Mn

    Design of Steel BeamExample - Bending

    University of Michigan, TCAUP Structures II Slide 17 of 24

    3. Determine Zx required

    4. Select the lightest beam with a Zx greater than the Zxrequired from AISC table

    Design of Steel BeamExample - Bending

    University of Michigan, TCAUP Structures II Slide 18 of 24

  • 5. Determine if h/tw < 59 (case 1, most common)

    6. Determine Aw: Aw = d * tw

    7. Calculate Vn: Vn = 0.6*Fy*Aw

    8. Calculate Vu for the given loadingVu = wu L / 2 (unif. load)

    9. Check Vu < v Vnv = 1.0

    Design of Steel BeamExample - Shear

    University of Michigan, TCAUP Structures II Slide 19 of 24

    Steel Beam Deflection

    Deflection limits by applicationIBC Table 1604.3

    Secondary roof structural members formed metal roofing – LL L/150

    For steel structural members, the DL can be taken as zero (note g)

    DL deflection can be compensated for by beam camber

    University of Michigan, TCAUP Structures II Slide 20 of 24

  • Beam without Camber

    University of Michigan, TCAUP Structures II Slide 21 of 24

    Developed by Scott CivjanUniversity of Massachusetts, AmherstFor AISC

    Results in deflection in floor under Dead Load.This can affect thickness of slab and fit of non-structural components.

    University of Michigan, TCAUP Structures II Slide 22 of 24

    Developed by Scott CivjanUniversity of Massachusetts, AmherstFor AISC

  • Results in deflection in floor under Dead Load.This can affect thickness of slab and fit of non-structural components.

    Beam with Camber

    University of Michigan, TCAUP Structures II Slide 23 of 24

    Developed by Scott CivjanUniversity of Massachusetts, AmherstFor AISC

    Results in deflection in floor under Dead Load.This can affect thickness of slab and fit of non-structural components.

    Cambered beam counteracts service dead load deflection.

    University of Michigan, TCAUP Structures II Slide 24 of 24

    Developed by Scott CivjanUniversity of Massachusetts, AmherstFor AISC