Rocket-model investigation to determine the hinge-moment and normal-force properties of a full-span, constant-chord, partially balanced trailing-edge control on a 60 degree clipped delta wing between Mach numbers of 0.50 and 1.26

Martz, C William Goslee, John W
naca-rm-l53i04
October 30, 1953


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1953/naca-rm-l53i04.pdf