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Postbuckling response of antisymmetric angle-ply laminates to uniform temperature loading

✍ Scribed by N. N. Huang; T. R. Tauchert

Book ID
112492663
Publisher
Springer Vienna
Year
1988
Tongue
English
Weight
498 KB
Volume
72
Category
Article
ISSN
0001-5970

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The purpose of this investigation is to study the random vibration behavior (including snap-through) of a thermally buckled composite plate. Five different time domain simulation methods and two equivalent linearization solutions were used to determine the mean-square response for a single-degree-of