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Tests at a Mach Number of 2.0 on a Rectangular, Twin-duct Air Intake with Variable Geometry, Situated in the Flow Field of a Slender Wing
M. D. Dobson
出版H.M. Stationery Office, 1968
ISBN01147031089780114703103
URLhttp://books.google.com.hk/books?id=1ZGPoAEACAAJ&hl=&source=gbs_api