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Investigation of Inlet Condition Effect on Flow and Turbulence Characteristics in Subsonic Jets from Conical and Chevron Nozzles Using RANS/ILES High Resolutions Method

机译：利用RaNs / ILEs高分辨率法研究进口条件对锥形和雪佛龙喷嘴亚音速射流流动和湍流特性的影响

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L. A. Benderskiy; D. A. Lyubimov;
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1. INVESTIGATION OF NOZZLE GEOMETRY AND OUTFLOW REGIME EFFECT ON FLOW PARAMETERS AND TURBULENT JET NOISE BY THE HIGH-RESOLUTION RANS/ILES METHOD [J] . L. A. Bendersky, D. A. Lyubimov TsAGI science journal . 2016,第2期

机译：高分辨率Rans / Iles法研究喷嘴几何形状及出流方式对流动参数和湍流射流噪声的影响
2. The Application of Hybrid RANS/ILES Approach for the Investigation of the Effect of Nozzle Geometry and Mode of Efflux on the Characteristics of Turbulence of Exhaust Jets [J] . D. A. Lyubimov High temperature: English translation of teplofizika vysokikh temperatur . 2009,第3期

机译：混合RANS / ILES方法在研究喷嘴几何形状和排气模式对排气射流湍流特性的影响中的应用
3. RANS/ILES Analysis of the Flow Pattern and the Acoustic Characteristics of a Supersonic Off-Design Jet at Large Nozzle Pressure Ratios [J] . Ayupov R. Sh., Benderskii L. A., Lyubimov D. A. Fluid Dynamics . 2019,第1期

机译：大型喷嘴压力比的超音速设计射流的流动模式和流量图案的rans / iles分析
4. INVESTIGATION OF FLOW PARAMETERS AND NOISE OF SUBSONIC AND SUPERSONIC JETS USING RANS/ILES HIGH RESOLUTION METHOD [C] . L.A. Benderskiy, D.A. Lyubimov Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：用Rans / Iles高分辨率方法研究亚音速和超音速飞行器的流动参数和噪声
5. Supersonic jet noise prediction and noise source investigation for realistic baseline and chevron nozzles based on hybrid RANS/LES simulations. [D] . Du, Yongle. 2011

机译：基于混合RANS / LES模拟的逼真的基线和V形喷嘴的超音速喷气噪声预测和噪声源研究。
6. Investigation of Synthetic Jets Efficiency to Control Cavity Flotation with Subsonic External Flow by High-Resolution RANS / ILES Method [O] . D. A. Lyubimov, A. E. Fedorenko 2015

机译：用高分辨率RaNs / ILEs方法研究合成射流控制亚音速外流空穴浮选的效率

Investigation of Inlet Condition Effect on Flow and Turbulence Characteristics in Subsonic Jets from Conical and Chevron Nozzles Using RANS/ILES High Resolutions Method

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