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Effects of front-face asymmetry on the aerodynamic characteristics of the Apollo capsule

机译：前脸不对称对阿波罗胶囊气动特性的影响

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Mc Devitt, J. B.; Mellenthin, J. A.;
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年度 1965
页码 1-24
总页数 24
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; AERODYNAMIC CONFIGURATIONS; APOLLO SPACECRAFT; COMMAND MODULES; ASYMMETRY; HYPERVELOCITY WIND TUNNELS; LIFT DRAG RATIO;

机译：空气动力学特征;空气动力学配置; apOLLO spaCECRaFT;命令模块;不对称; HYpERVELOCITY WIND TUNNELs;升降比;

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2. Numerical Modeling of the Effect of Geometric Asymmetry on the Damping Aerodynamic Characteristics of Supersonic Sectional Flight Vehicles [J] . A. V. Antonets Fluid Dynamics . 2006,第3期

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3. High-Altitude Capsule Aerodynamics with Real Gas Effects [J] . M. S. Ivanov, G. N. Markelov, S. F. Gimelshein, Journal of Spacecraft and Rockets . 1998,第1期

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8. Effects of transverse center-of-gravity displacement, afterbody geometry, and front-face curvature on the aerodynamic characteristics of Mercury-type models at a Mach number of 5.5 [R] . Intrieri, P. F. 1961

机译：横向重心位移，后体几何形状和前面曲率对马赫数为5.5的汞型模型气动特性的影响

Effects of front-face asymmetry on the aerodynamic characteristics of the Apollo capsule

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