轴对称偏转板上超音速射流冲击的CFD分析

A. Ahmed, A. Baig, S. Bilal, S. Zahir
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引用次数: 2

摘要

利用商业CFD程序对轴对称偏转板上的射流冲击进行了研究。分析了射流冲击问题,将超声速喷管流动发展为自由膨胀流,并首先捕捉其射流对平板和偏转板的冲击效应。通过改变喷嘴出口平面与导流板顶点之间的距离,对导流板进行了优化设计。CFD解是时变的,但射流羽流形成现象在一段时间间隔后稳定下来,之后的影响以偏转板上的压力分布的形式被捕获。
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CFD analysis of supersonic jet impingement on axisymmetric deflector plate
The study of jet impingement on axisymmetric deflector plate is done using commercial CFD code. The problem of jet impingement was analyzed by developing a supersonic nozzle flow as free expansion and then capturing the effects of its jet impinging upon flat plate first and then deflector plate. The deflector plate was optimized for its design by varying distance between nozzle exit plane and deflector plate apex. The CFD solutions were time-variant but phenomenon of jet plume formation stabilizes after a time interval after which the effects were captured in form of pressure distribution on deflector plate.
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