Acoustic Analysis of Spacecraft Cavities using the Boundary Element Method
Spacecraft structures are subject to a series of load environments during their service life, with the most severe of these occurring during the spacecraft's launch and ascension through the atmosphere. In particular, acoustic loads imposed on stowed satellites within the launch vehicle fairing...
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| Format: | Others |
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Virginia Tech
2018
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| Online Access: | http://hdl.handle.net/10919/83460 |