Free-flight investigation at Mach numbers between 0.5 and 1.7 of the zero-lift rolling effectiveness and drag of various surface, spoiler, and jet controls on an 80 degree delta-wing missile

Schult, Eugene D
naca-rm-l56h29
November 29, 1956


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1956/naca-rm-l56h29.pdf