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On the Suitability of Direct Application of Acoustic Theory to Time- Resolved Tomographic PIV Tested by DNS for Low Mach Number Jet Flows

机译：关于将声学理论直接应用到DNS测试的低马赫数射流的时间分辨断层成像PIV中的适用性

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《AIAA/CEAS Aeroacoustics Conference》|2010年|P.1-13|共13页
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P. Moore; D. Violato; K. Bryon; F. Scarano;
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中图分类气体动力学（可压缩流体力学）;声的传播;
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机译：使用高时间分辨PIV技术的封闭侧分支系统中流致声共振和流场的实验研究
2. Integrating Mach-Zehnder interferometry with TPIV to measure the time-resolved deformation of a compliant wall along with the 3D velocity field in a turbulent channel flow [J] . Zhang Cao, Miorini Rinaldo, Katz Joseph Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2015,第11期

机译：将Mach-Zehnder干涉仪与TPIV集成在一起以测量湍流通道中顺应壁的时间分辨变形以及3D速度场
3. Experiments on the Flow Field and Acoustic Properties of a Mach number 0·75 Turbulent Air Jet at a Low Reynolds Number [J] . Harmen J. Slot, Peter Moore, René Delfos, Flow, Turbulence and Combustion . 2009,第4期

机译：低雷诺数马赫数0·75湍流射流的流场和声学特性实验
4. On the Suitability of Direct Application of Acoustic Theory to Time- Resolved Tomographic PIV Tested by DNS for Low Mach Number Jet Flows [C] . P. Moore, D. Violato, K. Bryon, AIAA/CEAS Aeroacoustics Conference . 2010

机译：关于声学理论直接应用的适用性，DNS用于低马赫数喷射流动测试的断层扫描PIV
5. MACH REFLECTION, MACH DISC, AND THE ASSOCIATED NOZZLE FREE-JET FLOWS. [D] . CHANG, I-SHIH. 1973

机译：Mach反射，Mach光盘和相关的喷嘴自由流动。
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. On the suitability of direct application of acoustic theory to time-resolved tomographic PIV tested by DNS for low Mach number jet flows [O] . Moore, P., Violato, D., Bryon, K., 2010

机译：关于将声学理论直接应用于DNS测试的低马赫数射流的时间分辨断层成像PIV的适用性
8. High-Energy, High-Pulse-Rate Light Sources for Enhanced Time-Resolved Tomographic PIV of Unsteady and Turbulent Flows. [R] . Schatz, M., Grigoriev, R., Sponberg, S. 2017

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On the Suitability of Direct Application of Acoustic Theory to Time- Resolved Tomographic PIV Tested by DNS for Low Mach Number Jet Flows

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