NONREFLECTING BOUNDARY-CONDITIONS FOR JET FLOW COMPUTATIONS

被引:24
作者
HAYDER, ME
TURKEL, E
机构
[1] Institute for Computational Mechanics in Propulsion, NASA Lewis Research Center, Cleveland, OH
[2] Department of Mathematics, Tel-Aviv University, Tel-Aviv
关键词
D O I
10.2514/3.12978
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, we examine the effect of boundary conditions, both inflow and outflow, on the predicted flow fluctuations in a supersonic Set entering into a subsonic outer flow. Various boundary conditions are used to compute the flowfield of a laminar axisymmetric jet excited at the inflow by a disturbance given by the corresponding eigenfunction of the linearized stability equations. Our goal is to determine the suitability of these conditions for computations of time-dependent flows. We solve the full time-dependent Navier-Stokes equations by a high-order numerical scheme. For very small excitations, the computed growth of the modes closely corresponds to that predicted by the linear theory. We then vary the excitation level and examine the effect of the boundary conditions in the nonlinear flow regime.
引用
收藏
页码:2264 / 2270
页数:7
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