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Aerodynamic investigation of sharp cone- cylinder spikes on 120 degree blunted cones at Mach numbers of 3.00, 4.50, and 6.00

机译：在马赫数为3.00,4.50和6.00的120度钝锥上的尖锥筒尖峰的空气动力学研究

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摘要

Aerodynamic investigation of sharp cone-cylinder spikes on 120 degree blunted cones at Mach numbers of 3, 4.5, and 6

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作者
Mc Ghee, R. J.; Staylor, W. F.;
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年度 1969
页码 1-42
总页数 42
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CHARACTERISTICS; BLUNT BODIES; MACH NUMBER; BOW WAVES; HYPERVELOCITY WIND TUNNELS; PRESSURE DISTRIBUTION; SHOCK WAVES; SPIKES (AERODYNAMIC CONFIGURATIONS);

机译：空气动力学特征; BLUNT BODIEs;马赫数;弓波; HYpERVELOCITY WIND TUNNELs;压力分布;冲击波; spIKEs（空气动力学配置）;

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专利

1. Numerical simulation of a pulsating flow arising over an axisymmetric spiked blunt body at Mach 2.21 and Mach 6.00 [J] . Feszty D., Badcock KJ., Woodgate MA., Shock Waves . 2000,第5期

机译：轴对称尖刺钝体在2.21马赫和6.00马赫处产生脉动流的数值模拟
2. Measured aerodynamic coefficients of without and with spiked blunt body at Mach 6 [J] . R. Kalimuthu, R. C. Mehta, E. Rathakrishnan Advances in Aircraft and Spacecraft Science . 2019,第3期

机译：在6马赫速度下不带钝顶体和带尖顶钝体的空气动力学系数
3. Measured aerodynamic coefficients of without and with spiked blunt body at Mach 6 [J] . R. Kalimuthu, R. C. Mehta, E. Rathakrishnan Advances in Aircraft and Spacecraft Science . 2019,第3期

机译：测量的空气动力学系数没有和在马赫6的尖刺钝体
4. Nonlinear stability of straight cones with sharp and blunt noses at Mach 6 [C] . Arham Amin Khan, Armani Batista, Joseph Kuehl AIAA SciTech forum and exposition . 2020

机译：鼻尖尖钝的直锥的非线性稳定性为6马赫
5. Hot-wire measurements of instability waves on sharp and blunt cones at Mach 6. [D] . Rufer, Shann J. 2005

机译：在6马赫速度下对尖锐和钝锥上的不稳定性波进行热线测量。
6. A compilation of longitudinal aerodynamic characteristics including pressure information for sharp-and blunt-nose cones having flat and modified bases / [O] . Foster, A. D.,, compiler., U.S. Atomic Energy Commission., 1965

机译：纵向空气动力学特征的汇编，包括具有平坦和修改基部的尖锐和钝鼻锥的压力信息/
7. Aerodynamic Investigation of Sharp Cone- Cylinder Spikes on 120 Degree Blunted Cones at Mach Numbers of 3.00, 4.50, AND 6.00 [R] . Mc Ghee, R. J., Staylor, W. F. 1969

机译：在马赫数为3.00,4.50和6.00的120度钝锥上尖锐圆柱钉的气动研究

Aerodynamic investigation of sharp cone- cylinder spikes on 120 degree blunted cones at Mach numbers of 3.00, 4.50, and 6.00

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