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Low-lift Flight Tests of Four-engine Delta Wing Configurations to Obtain Wing Pressure and Aerodynamic Coefficients Including Some Jet Effects from Mach Number 0.5 to 1.5

Ralph A. Falanga

出版	NASA, 1960
URL	http://books.google.com.hk/books?id=r14hyAEACAAJ&hl=&source=gbs_api