homework3

homework3 - = αβ ¯ ¯ ¯ ¯ N ¯ ¯ ¯ ¯ N Given a and...

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2.081J/16.230J Plates and Shells Homework #3 Due date: c lass on Monday March 6 PROBLEM 1 A simply-supported square ( a × a ) plate is subjected to biaxial compression of the intensity N . N N x 0 y (a) Prove that the following pre-buckling solution satisfy all equations in the in- plane direction: N
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Unformatted text preview: = αβ ¯ ¯ ¯ ¯ N ¯ ¯ ¯ ¯ N Given a and D , fi nd the buckling load using: (b) Finite di f erence method with 4 and 16 elements (c) Raleigh-Ritz quotient and compare the results. 1...
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This note was uploaded on 11/07/2011 for the course AERO 16.21 taught by Professor Dffs during the Fall '10 term at MIT.

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