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Effect of Nose Bluntness and Controlled Roughness on the Flow on Two Hypersonic Inlet Center Bodies Without Cowling at Mach 5.98

机译：鼻子钝度和控制粗糙度对5.98马赫时没有整流罩的两个高超声速进气道中心流动的影响

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作者
Cubbage, J. M.;
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年度 1965
页码 1-6
总页数 6
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Flow characteristics ; Hypersonic inlet ; Nose inlet ; Bluntness ; Characteristics ; Compression ; Flow ; Hypersonic ; Inlet ; Nose ; Roughness;

机译：流动特性;高超声速入口;鼻子入口;钝化;特征;压缩;流动;高超音速;入口;鼻子;粗糙度;

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1. TURBULIZATION OF THE WAKE BEHIND A SINGLE ROUGHNESS ELEMENT ON A BLUNTED BODY AT A HYPERSONIC MACH NUMBER [J] . Polivanov P. A., Gromyko Yu V., Sidorenko A. A., Journal of Applied Mechanics and Technical Physics . 2017,第5期

机译：超音速数下钝体上单一粗糙度元素后的尾迹化
2. General Reynolds Analogy for Blunt-Nosed Bodies in Hypersonic Flows [J] . Chen Xing-Xing, Wang Zhi-Hui, Yu Yong-Liang AIAA Journal . 2015,第8期

机译：雷诺的通用类比在超音速流中的钝头物体
3. A hybrid CFD/characteristics method for fast characterization of hypersonic blunt forebody/inlet flow [J] . GAO WenZhi, LI ZhuFei, YANG JiMing 中国科学:物理学力学天文学（英文版） . 2015,第010期

机译：快速表征超声波钝头体/入口流动的混合CFD /特征方法
4. Pulsating Flow Investigation for Spiked Blunt-Nose Body in Hypersonic Flow and its Control [C] . Ashish Vashishtha, Shashank Khurana AIAA SciTech Forum and Exposition . 2021

机译：超声波流动中尖刺钝鼻体的脉动流动研究及对照
5. Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows. [D] . Singh, Dal Jeet. 1989

机译：鼻子过钝和电击-相互作用对粘性高超声速流动中钝体的影响。
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. An experimental investigation by hypersonic flow over blunt nosed cones at a mach number of 5.8. [O] . Machell Reginald M. 1956

机译：高超声速流过钝头锥的马赫数为5.8的实验研究。
8. Effect of nose bluntness and controlled roughness on the flow on two hypersonic inlet center bodies without cowling at mach 5.98 [R] . Cubbage, J. M. 1965

机译：鼻子钝度和受控粗糙度对在5.98机器上没有整流罩的两个高超声速入口中心体的流动的影响

Effect of Nose Bluntness and Controlled Roughness on the Flow on Two Hypersonic Inlet Center Bodies Without Cowling at Mach 5.98

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