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A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

机译：一种计算超音速下细长开口旋转体外部升力，力矩和压力阻力的方法

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Parker, Hermon M;
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年度 1946
页码 1-34
总页数 34
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Minimization of body of revolution aerodynamic drag at supersonic speeds [J] . Ageev Nikita, Pavlenko Alexander Aircraft engineering . 2016,第2期

机译：以超音速降低旋转体的空气阻力
2. Calculation of Hydrodynamic Drag Force Exerted on a Supercavitating Slender Body Using Boundary Element Method [J] . N. M. NOURI, A. ESLAMDOOST, A. SHIENEJAD, WSEAS Transactions on Fluid Mechanics . 2006,第6期

机译：用边界元法计算超空泡细长体的水动力阻力。
3. Supersonic scattering of a wing-induced incident shock by a slender body of revolution [J] . Fedorov AV, Malmuth ND, Soudakov VG Journal of Fluid Mechanics . 2007,第0期

机译：细长旋转体对机翼引起的入射冲击的超音速散射
4. Pressures and Drag Characteristics of Bodies of Revolution at Near Sonic Speeds Including the Effects of Viscosity and Wind Tunnel Walls [C] . B. Kulfan, J. Bussoletti, C. Hilmes AIAA Aerospace Sciences Meeting and Exhibit . 2007

机译：接近声速时旋转体的压力和阻力特性，包括粘度和风洞壁的影响
5. BASE DRAG EFFECTS ON MAXIMUM LIFT-TO-DRAG RATIO AIRFOILS AT MODERATE SUPERSONIC SPEEDS [D] . PRITCHARD, ROBERT EMLYN -1

机译：在中等超声速下最大升降比比翼型上的基本拉力效应
6. Method for the calculation of velocity rate of flow and viscous drag in arteries when the pressure gradient is known [O] . J. R. Womersley 1955

机译：已知压力梯度时计算动脉速度流速和粘滞阻力的方法
7. Note on the results of some profile drag calculations for a particular body of revolution at supersonic speeds [O] . Wedderspoon J. R. 1954

机译：请注意在超音速速度下特定旋转体的一些轮廓阻力计算结果
8. Method for the Calculation of External Lift, Moment, and Pressure Drag of Slender Open-Nose Bodies of Revolution at Supersonic Speeds [R] . 1946

机译：对外电梯，片刻，以超音速革命瘦开放式鼻机构的压力阻力的计算方法

A method for the calculation of external lift, moment, and pressure drag of slender open-nose bodies of revolution at supersonic speeds

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