A flight investigation to determine the effectiveness of Mach number 1.0, 1.2, and 1.41 fuselage indentations for reducing the pressure drag of a 45 degree sweptback wing configuration at transonic and low supersonic speeds

Blanchard, Willard S , Jr Hoffman, Sherwood
naca-rm-l57b27
May 16, 1957


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1957/naca-rm-l57b27.pdf