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Effects of angle of attack and bluntness on the hypersonic flow over a 15 deg semiapex cone in helium

机译：攻角和钝角对氦气中15度半圆锥上高超声速流动的影响

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摘要

Angle of attack and bluntness effects on hypersonic flow over 15 deg semiapex cone in helium

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作者
Cleary, J. W.; Duller, C. E.;
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年度 1970
页码 1-43
总页数 43
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
ANGLE OF ATTACK; CONICAL BODIES; ELLIPTICITY; HYPERSONIC FLOW; WIND TUNNEL STABILITY TESTS; APEXES; HELIUM; PRESSURE DISTRIBUTION; SHADOWGRAPH PHOTOGRAPHY; SHOCK WAVE PROFILES; SPECIFIC HEAT;

机译：攻击角度;圆锥体;椭圆;超音速流动;风洞稳定性试验;茎尖;氦;压力分布; sHaDOWGRapH摄影;冲击波轮廓;特定热量;

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1. Numerical Study of the Effect of Rotation on the Behavior of the Conjugate Heat and Mass Transfer on the Surface of a Spherically Blunted Cone Exposed to a Hypersonic Flow at an Angle of Attack with Ablation from the Surface [J] . Efimov K. N., Ovchinnikov V. A., Yakimov A. S. High temperature: English translation of teplofizika vysokikh temperatur . 2018,第2期

机译：旋转效果对张开锥体表面的缀合物热量和质量传递的作用，其暴露于表面的攻击角度钝化的过度流动
2. Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack [J] . SU Cai-hong, ZHOU Heng 应用数学和力学（英文版） . 2007,第005期

机译：零迎角小鼻钝的钝锥上高超声速边界层的稳定性分析和过渡预测
3. Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number [J] . Gopalan JAGADEESH, Kanderpallt NAGASHETTY, K. P. Jaganntha REDDY, Transactions of the Japan society for aeronautical and space sciences . 2002,第149期

机译：试验气体对高超声速马赫数大角钝锥飞行流场的影响研究
4. Thin-Layer Navier-Stokes Solution for Hypersonic Viscous Flow past a Blunted cone at High Angle of Attack [C] . Cao Ling-Jun, Cao Qi-Peng Numerical Grid Generation in Computational Field Simulations . 1998

机译：高攻角下通过钝锥的高超声速粘性流的薄层Navier-Stokes解决方案
5. Hypersonic crossflow instability and transition on a circular cone at angle of attack. [D] . Ward, Christopher A. C. 2010

机译：高音速横流失稳和在迎角处的圆锥上过渡。
6. Effect of a Roughness Element on the Receptivity of a Hypersonic Boundary Layer over a Blunt Cone Due to Pulse Entropy Disturbance with a Single Frequency [O] . Zhenqing Wang, Mingfang Shi, Xiaojun Tang, 2018

机译：粗糙元件对钝锥体上超声边界层的接受性的影响由于单频脉冲熵干扰
7. Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number. [O] . Gopalan Jagadeesh, Kanderpallt Nagashetty, K. P. Jaganntha Reddy, 2002

机译：超声波马赫数大角度钝锥围绕流域试验气体对流场影响的研究。
8. Effects of Angle of Attack and Bluntness on the Hypersonic Flow over a 15 Deg Semiapex Cone in Helium [R] . Cleary, J. W., Duller, C. E. 1970

机译：攻角和钝角对氦气中15度半球锥上高超声速流动的影响

Effects of angle of attack and bluntness on the hypersonic flow over a 15 deg semiapex cone in helium

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