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Numerical Simulation on the Flow Fields Downstream Nozzles with Tabs by Modified Turbulent Model

机译:改进湍流模型的带突片的下游喷嘴流场数值模拟。

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Firstly, the flow fields downstream one axisymmetric nozzles and a nozzle with four tabs were simulated with four different turbulent models, and the results were compared with experimental data. Then the flow fields downstream nozzles with tabs of varied orientation angles were predicted for different orientation angles of the tabs while the projected blockage of tabs was kept unchanged. The predictions were also compared with that of the nozzle without tabs. The decrease of potential core length was remarkable when tabs were affixed. As the orientation angle increased, the potential core length decreased firstly and then increased. The streamwise vortices strength increased straightly with the orientation angle. Both entrainment gain and thrust losses of the nozzles decreased as the orientation angle increased.
机译:首先,用四种不同的湍流模型模拟了一个轴对称喷嘴和一个带有四个翼片的喷嘴下游的流场,并将其与实验数据进行了比较。然后,针对翼片的不同定向角度,预测了翼片具有不同取向角的下游喷嘴的流场,而翼片的预计阻塞保持不变。还将预测结果与不带凸耳的喷嘴的预测结果进行了比较。固定翼片后,潜在的铁心长度减少明显。随着取向角的增加,潜在的铁芯长度先减小然后增加。流向涡流强度随取向角的增加而直线增加。随着定向角的增加,喷嘴的夹带增益和推力损失均减小。

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