2 research outputs found
Flight-determined Transonic Lift and Drag Characteristics of the YF-102 Airplane with Two Wing Configurations
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NACA Research Memorandums
Report presenting lift and drag characteristics of the Convair YF-102 airplane for symmetrical wing configuration and for the cambered wing configuration. Data were obtained for a variety of lift coefficients, altitudes, and Mach numbers. Results regarding lift, drag, and some flight-tunnel comparisons are provided