notes_31_Ult_str_stf_

# notes_31_Ult_str_stf_ - Section 14.2 Ultimate Strength of...

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Section 14.2 Ultimate Strength of Stiffened Panels three failure types compression in flange of stiffener (negative bending moment) Mode I compression in plate (positive bending moment) Mode II tension in flange of stiffener (high positive moment) Mode III b HSF γ C := 1.5 σ C := input b p := input σ ax := σ C t p j = 5, PS 6, stiffener #6 from catalog BSF := 3.94 SDEPTH := 7.89 TSF := 0.205 TSW := .17SCG := 5.35 a plate a := 8 12 b := 23.844 t := .375 N := 1 L := a material υ := 0.3 E := 29.6 10 6 D := Et 3 allowing for different yield stresses 12 ( 1 − υ 2 ) plate stiffener general parameters: σ Yp := 47 10 3 σ Ys := 47 10 3 HSW := SDEPTH TSF A w := (SDEPTH TSF) TSW A f := BSF TSF A s := A w + A f HSW = 7.685 A w = 1.306 A f = 0.808 A s = 2.114 TSF t A s ⋅σ Ys + σ Yp A p d := SDEPTH + B := (N + 1) b A p := bt A := A s + A p σ Y_bar := A 2 2 d = 7.975 B = 47.688 A p = 8.942 A = 11.056 σ Y_bar = 47000 1 notes_31_Ult_str_stf_panels.mcd

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For later use and to set the scale on plots, calculate M p , plastic moment of section if Ap>Aw+Af; i.e. Ap>At/2 => g is in plate g := A p A w A f g = 0.143 2b centroid of upper half centroid of lower half bg 2 + A w HSW + g + A f (g) + HSW + TSF y 2 := t g y 2 = 0.116 y 1 := 2 2  2 2 A y 1 = 2.145 2 plastic section modulus, if Ap>At/2 Z P1 := A ⋅( y 1 + y 2 ) Z P1 = 12.498 TSF = 0.205 2 ______________________________________________________ if Ap<Aw+Af; i.e. Ap<At/2 => g is is web g := A f + A w A p g = − 20.08 2 TSW centroid of upper half centroid of lower half A f HSW g + TSF + TSW (HSW g) 2 A p g + 2 t + TSW g 2 2 2 2 y 1 := y 2 := A f + A w g TSW A p + g TSW y 1 = 15.926 y 2 = − 25.977 plastic section modulus, if Ap<At/2 Z P2 := A y 1 + y 2 ) Z P2 = − 55.562 2 Z P := if A p > A , Z P1 , Z P2 Z P = 12.498 2 M P := σ Y_bar Z P M P = 587397 2 notes_31_Ult_str_stf_panels.mcd
a. Compression failure of stiffener (flange): Mode I (Point E figure 14.2) and curve - PCSF - Panel Collapse Stiffener Flexure. (Mode I). geometry of panel Combination of plate and stiffeners (from p287, equation 8.3.6 in text): A A w A w A w A w + A f A p + A p + A p d C 1 := 3 4 I := A () 2 C 1 y f := d 2 A y p := d1 2 A A 2 C 1 = 0.095 I = 66.789

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## This note was uploaded on 02/24/2012 for the course MECHANICAL 2.082 taught by Professor Davidburke during the Spring '03 term at MIT.

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notes_31_Ult_str_stf_ - Section 14.2 Ultimate Strength of...

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