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Flight Investigation of the Low-speed Characteristics of a 45° Swept-wing Fighter-type Airplane with Blowing Boundary-layer Control Applied to the Leading- and Trailing-edge Flaps
出版National Aeronautics and Space Administration, 1960
URLhttp://books.google.com.hk/books?id=_rHjMQEACAAJ&hl=&source=gbs_api