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Google圖書搜尋
An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90°
David E. Fetterman
Luther Neal
出版
National Aeronautics and Space Administration
, 1963
URL
http://books.google.com.hk/books?id=OQMLl13-KyIC&hl=&source=gbs_api
EBook
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