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Simple approach to thermal vacuum testing of spacecraft equipment

✍ Scribed by J.F. Farquhar; J.D. Nuttall


Publisher
Elsevier Science
Year
1988
Tongue
English
Weight
414 KB
Volume
38
Category
Article
ISSN
0042-207X

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The aim of the present paper is to propose a simple method to investigate the vibratory behaviour of laminated composite structures subjected to large thermal loads (may be beyond critical temperature T cr ). von Karman type non-linear strain-displacement relationships are employed to derive non-lin