An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : force characteristics of the complete configuration and its various components at Mach numbers of 1.40 and 1.59

Smith, Norman F Marte, Jack E
naca-rm-l50k14
January 22, 1951


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l50k14.pdf