A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70

Falanga, Ralph A
naca-rm-l55l21
March 08, 1956

No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1956/naca-rm-l55l21.pdf