首页> 美国政府科技报告 >Calculated Pressure Distributions and Components of Total-Drag Coefficients for 18 Constant-Volume, Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, WITH Experimental Aerodynamic Characteristics for Three of the Bodies
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Calculated Pressure Distributions and Components of Total-Drag Coefficients for 18 Constant-Volume, Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2.0 to 12.0, WITH Experimental Aerodynamic Characteristics for Three of the Bodies

机译:计算压力分布和总阻力系数的组成部分为18个恒定体积,零点处的细长旋转体,马赫数从2.0到12.0,具有三个实体的实验空气动力学特性

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