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Pressure distribution induced on a flat plate by a supersonic and sonic jet exhaust at a free-stream Mach number of 1.80

机译：通过超音速和声波喷射排气在平板上引起的压力分布，自由流马赫数为1.80

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Leiss, Abraham; Bressette, Walter E;
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年度 1957
页码 1-62
总页数 62
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Wall-pressure fluctuations induced by a compressible jet flow over a flat plate at different Mach numbers [J] . Meloni S., Di Marco A., Mancinelli M., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2019,第3期

机译：在不同马赫数的平板上通过压缩射流诱导的壁压波动
2. Pressure measurements on the impingement surface of sonic and sub-sonic jets impinging onto a flat plate at inclined angles [J] . Jim Crafton, Campbell Carter, John Sullivan, Experiments in Fluids . 2006,第5期

机译：以倾斜角度撞击平板的音速和亚音速射流的撞击表面上的压力测量
3. Pressure measurements on the impingement surface of sonic and sub-sonic jets impinging onto a flat plate at inclined angles [J] . Crafton J, Carter C, Sullivan J, Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2006,第5期

机译：以倾斜角度撞击平板的音速和亚音速射流的撞击表面上的压力测量
4. An experimental investigation of the wall pressure field induced by a low and moderate Mach numbers jet on a tangential flat plate [C] . Matteo Mancinelli, Roberto Camussi AIAA/CEAS aeroacoustics conference;AIAA aviation forum . 2018

机译：切向平板上低和中等马赫数射流引起壁压力场的实验研究
5. The impingement of sonic and sub-sonic jets onto a flat plate at inclined angles. [D] . Crafton, Jimmy Wayne. 2004

机译：将声波和次声波射流以倾斜角度撞击到平板上。
6. Penetration Characteristics of Air Carbon Dioxide and Helium Transverse Sonic Jets in Mach 5 Cross Flow [O] . Erinc Erdem, Konstantinos Kontis, Selvaraj Saravanan 2014

机译：空气二氧化碳和氦气横向声速射流在5马赫错流中的渗透特性
7. Coupled CFD-CAA Simulation of the Noise Generated by a Hot Supersonic Jet Impinging on a Flat Plate with Exhaust Hole [O] . Julien N. Troyes, Francois Vuillot, Adrien Langenais, 2019

机译：耦合CFD-CAA仿真由热超声波喷射产生的噪声，其撞击带有排气孔的平板

Pressure distribution induced on a flat plate by a supersonic and sonic jet exhaust at a free-stream Mach number of 1.80

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