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Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail

Alan B Kehlet

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Key concepts: Airplane, Lift (data mining), Mach number, Range (aeronautics), Lift coefficient, Aeronautics, Aerospace engineering, Mathematics

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Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail — Research Paper | ScholarLens