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二元翼型跨音速非定常压力计算
引用本文:顾建农.二元翼型跨音速非定常压力计算[J].海军工程大学学报,1995(2).
作者姓名:顾建农
摘    要:本文描述了用E—O型的ADI隐式差分格式计算二维、无粘、定常与非定常低频小扰动跨音速流的方法。应用附加时间导数项的物面、尾涡面的边界条件及压力系数表达式和远场无反射边界条件,计算翼型绕其1/4弦长处轴作正弦俯仰振动时,翼面上的非定常压力分布。所得结果与文献[1]比较,具有较好的一致性。

关 键 词:跨音速  非定常  小扰动  压力分布  翼型

Computation of Unsteady Pressure Distribution on a Profile in Transonic Flow
Gu Jianlong.Computation of Unsteady Pressure Distribution on a Profile in Transonic Flow[J].Journal of Naval University of Engineering,1995(2).
Authors:Gu Jianlong
Institution:Gu Jianlong
Abstract:In this paper, the Engquist-Osher switch implicit ADI algorithm is quoted to calculate two -dimensional inviscid steady and unsteady small-disturbance transonic flow. The appropriate unsteady terms are added to the boundary conditions on body surface and wake.The nonreflectig far- field boundary conditions are chosen for steady and unsteady cases.The computaional results of unsteady pressure distribution on the profile when the profile is oscillated in pitch about its 1/4 axis are in good agreement with ones in reference 1.
Keywords:Transonic flow  Unsteadiness  Small disturbance  Pressure distribution  Profile
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