A Coupled Aeroelastic Model for Launch Vehicle Stability Analysis
Keyword(s):
Keyword(s):
2013 ◽
Vol 2013
◽
pp. 1-9
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2009 ◽
Vol 37
(6)
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pp. 537-544
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2006 ◽
Vol 120
(5)
◽
pp. 3372-3372