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Effect of thrust on the aeroelastic instability of a composite swept wing with two engines in subsonic compressible flow

✍ Scribed by Firouz-Abadi, R.D.; Askarian, A.R.; Zarifian, P.


Book ID
119297172
Publisher
Elsevier Science
Year
2013
Tongue
English
Weight
707 KB
Volume
36
Category
Article
ISSN
0889-9746

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