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二维非均匀超音来流下最有利压缩面型面的随机选取法数值研究
引用本文:张堃元.二维非均匀超音来流下最有利压缩面型面的随机选取法数值研究[J].推进技术,1994,15(5):9-15.
作者姓名:张堃元
作者单位:南京航空航天大学动力工程系
摘    要:采用近年发展起来的随机选取法,研究非均匀二维超音来流流过6种不同形状的楔型压缩面时的波后非均匀超音流场。结果表明来流的非均匀性对下游流场具有重大影响,对6种不同形状楔型压缩面流场的计算表明,单纯用改变压缩面型面的办法难以减少来流的非均匀性,但是可以部分改善下游流场的非均匀程度,在研究的6种型面中,凹圆弧压缩面及等熵压缩面在本文限定的非均匀来流下,其性能优于其它4种型面的压缩面。

关 键 词:非均匀流动  超音速流动  进气道  航空发动机

A STUDY ON OPTIMUM COMPRESSION SURFACE UNDER NON-UNIFORM 2-D SUPERSONIC FLOW CONDITION USING R. C.METHOD
Zhang Kunyuan.A STUDY ON OPTIMUM COMPRESSION SURFACE UNDER NON-UNIFORM 2-D SUPERSONIC FLOW CONDITION USING R. C.METHOD[J].Journal of Propulsion Technology,1994,15(5):9-15.
Authors:Zhang Kunyuan
Institution:Department of Power Engineering, Naming University of Aeronautics and Astronautics, Nanjing, 210016
Abstract:A newly developed Random-(choice Method is used to study a two dimensional non-uniform supersonic flow field create when incoming flows passthrough six shock generators with different wedges. The numerical results strongly show the influence of incoming flow non-unifomity on downstream flow field. The computations for compression surfaces reveal that there is nearly no possible to crease incoming flow distorting, or say non-uniformity, but possible to expand it by simply changing the geometry of compression surfaces slightly of the studied six shock generators, these with concave circle configuration and isotropic configuration have better properties in non-uniformity streamwise propagation.
Keywords:Non-uniform flow  Supersonic flow  Two dimensional flow  Supersonic inlet  Flow field simulation  Numerical calculation
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