SIMILITUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE

机译：一个微小的超音速喷嘴中气体流动的相似定律

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Flow in an ideal nozzle.n2.tFlow in a boundary layer.n3.tSimilitude law for flow of gas in dyadic-like nozzles.n4.tCalculation of real processes in a boundary layer.

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Yu. L. Zhilin;
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年度 1965
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Investigation of hypersonic nozzle flow uniformity using NO fluorescence [J] . OByrne S, Danehy PM, Houwing AFP Shock Waves . 2006,第2期

机译：使用NO荧光研究高超声速喷嘴的流量均匀性
2. On nitrogen condensation in hypersonic nozzle flows: numerical method and parametric study [J] . L. Lin, W. Cheng, X. Luo, Shock Waves . 2014,第2期

机译：关于高超声速喷嘴流中的氮冷凝：数值方法和参数研究
3. Numerical flow visualization of a single expansion ramp nozzle with hypersonic external flow [J] . Thiagarajan V, Panneerselvam S, Rathakrishnan E Journal of visualization . 2006,第1期

机译：具有高超声速外流的单膨胀斜面喷嘴的数值流可视化
4. Experimental analysis of the flow of exhaust gas in a hypersonic nozzle [C] . H.Weisgerber, M.Fischer, E.Magens, AIAA international space planes and hypersonic systems and technologies conference . 1998

机译：高超声速喷嘴中废气流动的实验分析
5. An experimental and computational investigation on the effect of transonic flow in hypersonic wind tunnel nozzles, including filtered Rayleigh scattering measurements. [D] . Boyd, Robert Raymond. 1996

机译：对高超声速风洞喷嘴中跨音速流动的影响进行实验和计算研究，包括滤波瑞利散射测量。
6. Numerical Study on the Gas–Solid Flow in aSpouted Bed Installed with a Controllable Nozzle and a Swirling FlowGenerator [O] . Feng Wu, Xinxin Che, Zhenyu Huang, 2020

机译：气固两相流动的数值研究喷水床安装有可控的喷嘴和旋流发电机
7. Part I. The effect of a simple throat distortion on the downstream flow in a hypersonic wind tunnel nozzle. Part II. An experimental investigation of flow over simple blunt bodies at a nominal Mach number of 5.8 [O] . Oliver Robert E. 1957

机译：第一部分。高超声速风洞喷嘴中简单喉部扭曲对下游流动的影响。第二部分。标称马赫数为5.8的简单钝体流动的实验研究
8. SIMILITUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE [R] . Yu. L. Zhilin 1965

机译：一个微小的超音速喷嘴中气体流动的相似定律

SIMILITUDE LAWS FOR A FLOW OF GAS IN A THIN HYPERSONIC NOZZLE

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