Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6

Strass, H Kurt Stephens, Emily W Fields, E M Schult, Eugene D
naca-rm-l55f14
September 02, 1955


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-l55f14.pdf