A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50

Falanga, Ralph A
naca-rm-l55f09a
August 18, 1955


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-l55f09a.pdf