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Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects

机译：两个钝锥再入配置的纵向气动特性，马赫数从17.6到22.2，包括一些雷诺数效应

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摘要

Longitudinal aerodynamic characteristics of blunted cone reentry vehicle configurations at high Mach numbers, including Reynolds number effect

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作者
Maddalon, D. V.;
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年度 1966
页码 1-33
总页数 33
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; BLUNT BODIES; CONICAL BODIES; MACH NUMBER; REENTRY VEHICLES; REYNOLDS NUMBER; AERODYNAMIC CHARACTERISTICS; BLUNT BODY; MACH NUMBER; REENTRY VEHICLE; REYNOLDS NUMBER EFFECT;

机译：空气动力学特征;空气动力学配置; BLUNT BODIEs;圆锥体;马赫数; REENTRY车辆; REYNOLDs NUmBER;空气动力学特征; BLUNT BODY;马赫数; REENTRY VEHICLE;雷诺数量效应;

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1. Effects of flap on the reentry aerodynamics of a blunt cone in the supersonic flow [J] . International Journal of Mechanical Sciences . 2020,第期

机译：翻盖对超声波流动钝锥体再入空气动力学的影响
2. Studies on the Effects of the Plasma Wake Flow Fields of Hypersonic Reentry Blunt Cone on Electromagnetic Wave [J] . Yuxin Wang, Song Liu, Shuangying Zhong IEEE Transactions on Plasma Science . 2019,第8期

机译：高超声速折返钝角等离子体尾流场对电磁波影响的研究
3. Effects of wall temperature on boundary layer stability over a blunt cone at Mach 7.99 [J] . Xian Liang, Xinliang Li, Dexun Fu, Computers & Fluids . 2010,第2期

机译：壁温对7.99马赫钝锥上边界层稳定性的影响
4. Effects of Flap on the Reentry Aerodynamics of a Blunt Cone [C] . Senthil Kumar Raman, Kexin Wu, Heuy Dong Kim Asian Joint Workshop on Thermophysics and Fluid Science . 2020

机译：襟翼对钝锥再入空气动力学的影响
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. Distinct Adsorption Configurations and Self-Assembly Characteristics of Fibrinogen on Chemically Uniform and Alternating Surfaces including Block Copolymer Nanodomains [O] . Sheng Song, Kristina Ravensbergen, Anginelle Alabanza, -1

机译：纤维蛋白原在包括嵌段共聚物纳米域在内的化学均匀和交替表面上的独特吸附构型和自组装特征
7. 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/
8. Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17.6 to 22.2 Including Some Reynolds Number Effects [R] . Maddalon, D. V. 1966

机译：两个钝体锥再入构型在17.6至22.2马赫数下的纵向气动特性，包括一些雷诺数效应

Longitudinal aerodynamic characteristics of two blunted cone reentry configurations at Mach numbers from 17.6 to 22.2 including some Reynolds number effects

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