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Aerodynamic Investigation at Mach Number 1.92 of a Rectangular Wing and Tail and Body Configuration and Its Components

Macon C. Ellis

出版	National Advisory Committee for Aeronautics, 1950
URL	http://books.google.com.hk/books?id=9KpTmQR-B3EC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

An investigation at Mach number 1.92 in the Langley 9-inch supersonic tunnel of a variable body-wing-tail configuration has been made in order to determine and to isolate the aerodynamic effects on each other of the components of the configuration.