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Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control/

Main Author:	Blair, A. B.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978
Series:	NASA technical paperv 1124
Subjects:	Airplanes > Ramjet engines Spoilers (Airplanes) Rolling (Aerodynamics)

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