Rocket-model investigation to determine the force and hinge-moment characteristics of a half-Delta tip control on a 59 degree sweptback delta wing between Mach numbers of 0.55 and 1.43

Martz, C William Church, James D Goslee, John W
naca-rm-l52h06
October 06, 1952


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-l52h06.pdf