Solving Stress Concentration for Elliptical Hole in Square Panel

AI Thread Summary
The discussion focuses on calculating stress concentration at the end of the minor axis of an elliptical hole in a square panel subjected to uniform pressure. The user seeks to determine the correct stress concentration factor (Kt) for the elliptical hole, noting that the typical formula involves the dimensions of the ellipse. There is confusion regarding the correct formula, with references to both Kt = stress x (1 + 2b/a) and Kt = 1 + 2(a/b). The user highlights that as the width decreases or the length increases, the stress concentration increases. The conversation emphasizes the need for clarity on the appropriate equations for elliptical holes in stress analysis.
raunakm
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Homework Statement



Square panel , elliptical hole, uniform pressure p in x direction. calc stress at end of minor axis. pt A

L=40in p=10psi a=1in b=0.5 in t=0.2 in

Homework Equations



i know that stress at end will be max stress multiplied by stress conc. factor.
bt i don't know how to calc stress conc. factor for an elliptical hole

The Attempt at a Solution



Kt = stress x (1 + 2b/a)

is this correct?
 

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Can't read the diagram but it's normally 1+2(a/b) where a is the length and b is the width.
So as the width gets smaller or the length is longer - the concentration gets bigger!

Alternatively it's sqrt(crack_length/radius)
 
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