A computational procedure is presented for calculating the response of building components to acoustic loads due to spacecraft launch. The methodology described is in-built as routines into a software module &&ACOUP'' which forms part of the OSTA software package for o!-shore and on-shore structural
RESPONSE OF AEROSPACE SANDWICH PANELS TO LAUNCH ACOUSTIC ENVIRONMENT
β Scribed by A. Paolozzi; I. Peroni
- Publisher
- Elsevier Science
- Year
- 1996
- Tongue
- English
- Weight
- 414 KB
- Volume
- 196
- Category
- Article
- ISSN
- 0022-460X
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β¦ Synopsis
The response prediction of aerospace sandwich panels is studied through a numerical simulation based on Statistical Energy Analysis. The influence on the structural response to the launch acoustic environment of the design parameters, such as core type, thickness and number of ribs, is examined. The numerical results show a great sensitivity of the panel response to parameter variations and can be used for design selection.
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