An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : aerodynamic characteristics of the configuration equipped with a canard control surface at a Mach number of 1.89

Spearman, M Leroy Plazzo, Edward B
naca-rm-l54h19
October 18, 1954


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1954/naca-rm-l54h19.pdf