首页> 美国政府科技报告 >Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations
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Pitching-Moment Derivatives Cmq and Cma at Supersonic Speeds for a Slender-Delta-Wing and Slender-Body Combination and Approximate Solutions for Broad-Delta-Wing and Slender-Body Combinations

机译:纵摆力矩衍生CmQ和Cma以超音速为广泛,三角翼和细长型体组合一个苗条,三角翼和修长的身组合体和近似解

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The pitching-moment derivatives Cmq and Cma at supersonic speeds are developed for a slender-delta-wing and slender-body combination having no afterbody. By drawing an analogy between the aerodynamics of the wing-body section of the combination and the aerodynamics of a delta wing alone, the results for the slender-delta-wing and slender-body combination are modified to the extent that approximate solutions for Cmq and for broad-delta-wing and slender-body combinations can be obtained.

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