首页> 外文会议>International Congress on Sound and Vibration >ANALYSIS OF SYNTHETIC JETS INFLUENCE ON PRES-SURE PULSATIONS AND FLOW IN THREE-DIMENSIONAL CAVITY FOR SUBSONIC AND SUPERSONIC EXTERNAL FLOW USING RANS/ILES METHOD
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ANALYSIS OF SYNTHETIC JETS INFLUENCE ON PRES-SURE PULSATIONS AND FLOW IN THREE-DIMENSIONAL CAVITY FOR SUBSONIC AND SUPERSONIC EXTERNAL FLOW USING RANS/ILES METHOD

机译:使用RANS / ILES方法分析余量和超音速外流的三维腔中的脉冲脉动和流动的影响

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The effect of synthetic jets (SJs) and the influence of an external speed on the flow features were investigated using RANS/ILES method for the cavity M219. The numerical simulations were performed on a grid containing 2.5 million cells at Mach M_0 0.85 and 1.5. The method was approved by the comparison with the experiment and results of other authors. More precisely, the accuracy of the method is comparable to the accuracy of LES for a mesh with the number of cells twice as large. SJs were simulated using the modified boundary wall condition, which is well-proved in the calculations of SJs and permits to avoid time-consuming simulation of flow in the SJ generator. During the calculations there were used various SJ characteristics, such as their number (1 or 4), position (in front of a cavity, inside on the front wall and inside on the back wall), frequency f (100Hz, 200Hz, 300Hz, 1000Hz) and amplitude q (50m/s, 100m/s). It was shown that the jet inside the cavity acts as a turbulator of the flow and the jet in front of the cavity has a barrier character. For a subsonic external flow SJ located in front of a cavity for q=100 m/s and f=200Hz reduce peak pressure pulsations at the cavity back wall by 24%. The same jet located at the back wall increases peak pressure pulsations in 2 times. Spectral characteristics of the flow were obtained for M_0 0.85 and 1.5. Simulation results have shown good agreement with the experimental data and Rossiter's formula. It was found that on the back wall SJs decrease the second and the third modes of pressure fluctuations for subsonic flow and the first, the third and the fourth in the supersonic case.
机译:使用RAN / ILES方法对腔M219的RAN / ILES方法研究了合成射流(SJ)和外部速度对流量特征的影响。在Mach M_0 0.85和1.5的含有250万个细胞的网格上进行数值模拟。该方法通过与其他作者的实验和结果进行批准。更确切地说,该方法的准确性与网格的曲线的精度相当,细胞数量两倍大。 SJS使用修改的边界壁的条件,这是良好的证明SJS和许可证的计算,以在发电机SJ流的避免费时仿真模拟。在计算过程中,使用各种SJ特征,例如它们的数量(1或4),位置(在腔内在前壁上的内部和后壁内部),频率f(100Hz,200Hz,300Hz, 1000Hz)和幅度Q(50m / s,100m / s)。结果表明,腔内的喷射用作流动的湍流器,并且腔前面的射流具有屏障特征。对于位于Q = 100m / s的空腔前面的亚源外流Sj,F = 200Hz将腔体后壁的峰值压力脉动减小24%。位于后壁的相同喷射增加了2次峰值压力脉动。获得流动的光谱特性,用于M_0 0.85和1.5。仿真结果表明了与实验数据和Rossiter的公式吻合良好。发现,在后壁SJ上,在超音速壳体中减少第二和第三种压力波动的压力波动模式,并且第三,第三和第四。

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