Rocket-model investigation to determine the lift and pitching effectiveness of small pulse rockets exhausted from the fuselage over the surface of an adjacent wing at Mach numbers from 0.9 to 1.8

Martz, C William
naca-rm-l58g29
September 30, 1958


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1958/naca-rm-l58g29.pdf