Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53

Hoffman, Sherwood
naca-rm-l56b27
April 26, 1956


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1956/naca-rm-l56b27.pdf