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Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet

机译：由于来自具有出口射流的轴对称体的拖尾冲击波，在水平尾部处的马赫数1.9处的干扰效应

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Salmi, Reino J; Klann, John L;
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年度 1956
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Wing-Body and Vertical Tail Interference Effects on Downwash Rate of the Horizontal Tail in Subsonic Flow [J] . Paziresh Ali, Nikseresht Amir Hossein, Moradi Hashem Journal of aerospace engineering . 2017,第4期

机译：亚音速流中机翼和垂直尾翼干扰对水平尾翼下冲率的影响
2. Detection of shock structure around Mach disk in axisymmetric plasma jet [J] . Norifumi Ono, Masami Yamamoto, Kazuo Koike Vacuum: Technology Applications & Ion Physics: The International Journal & Abstracting Service for Vacuum Science & Technology . 2014,第Null期

机译：轴对称等离子体射流马赫盘周围冲击结构的检测
3. irect computation of mach wave radiation in an axisymmetric supersonic jet [J] . Brian E.Mitchell, Sanjiva K.Lele, parviz Moin AIAA Journal . 1997,第10期

机译：轴对称超音速射流中马赫波辐射的直接计算
4. Incident Shock-Transverse Jet Interactions at Mach 1.9: Effect of Shock Impingement Location [C] . H. Zare-Behtash, K.H. Lo, E. Erdem, International Symposium on Shock Waves . 2015

机译：1.9马赫突发冲击横向喷射相互作用：冲击撞击位置的影响
5. An investigation of unsteady pressure and temperature characteristics due to shock-boundary layer interactions in a mach 6 axisymmetric flowfield [D] . Flanagan, Michael John, Jr. 1991

机译：马赫6轴对称流场中由于冲击边界层相互作用而引起的非稳态压力和温度特性的研究
6. Flow behind an exponential shock wave in a rotational axisymmetric perfect gas with magnetic field and variable density [O] . G. Nath, P. K. Sahu -1

机译：具有磁场和可变密度的旋转轴对称完美气体中指数冲击波后的流动
7. Correction: The Effects of Leading Edge Flap and Trailing Edge Flaperon Deflections on Horizontal Tail Optimization [O] . Fazil S. Gomec, Emre C. Unver, Mehmet Z. Arisoy 2020

机译：校正：前沿襟翼和后缘FLAPERON偏转对水平尾优化的影响

Interference effects at Mach 1.9 on a horizontal tail due to trailing shock waves from an axisymmetric body with an exiting jet

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