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Numerical Simulation of Subsonic Diffuser for Supersonic Air-Intake (Effects of Blowing on Diffuser Performance)

机译:超音速进气的亚音速扩散器的数值模拟(吹气对扩散器性能的影响)

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摘要

The effects of tangential blowing on the performance of subsonic diffuser for supersonic air- intakes are numerically investigated in order to develop a high performance subsonic diffuser with short length. Using a k-εturbulence model, numerical simulation is performed on five types of diffuser configurations with and without tangential blowing. The results show that our calculation reproduces the qualitative features of the flow, and remarkable improvement of diffuser performance can be achieved by tangential blowing into the separation region. Moreover, it is suggested that tuning a model constant has possibility to predict the flow more reasonably.
机译:数值研究了切向吹气对超音速进气口亚音速扩散器性能的影响,以开发出短长度的高性能亚音速扩散器。使用k-ε湍流模型,对有和没有切向吹气的五种扩散器配置进行了数值模拟。结果表明,我们的计算再现了流的定性特征,并且通过切向吹入分离区域可以实现扩压器性能的显着提高。此外,建议调整模型常数有可能更合理地预测流量。

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