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Google圖書搜尋
Line-vortex Theory for Calculation of Supersonic Downwash
Harold Mirels
Rudolph C. Haefeli
出版
National Advisory Committee for Aeronautics
, 1949
URL
http://books.google.com.hk/books?id=jRVkbZBtK7sC&hl=&source=gbs_api
EBook
FULL_PUBLIC_DOMAIN
註釋
The perturbation field induced by a line vortex in a supersonic stream and the downwash behind a supersonic lifting surface are examined for the purpose of establishing approximate methods for determining the downwash behind supersonic wings. Lifting-line methods are presented for calculating supersonic downwash.
