High-Order Spectral/hp-Based Solver for Compressible Navier-Stokes Equations

被引:2
|
作者
Ranjan, Rakesh [1 ]
Catabriga, Lucia [2 ]
Feng, Yusheng [3 ]
机构
[1] Kord Technol, Huntsville, AL 35806 USA
[2] Fed Espirito Santo, Dept Informat, BR-29075910 Vitoria, ES, Brazil
[3] Univ Texas San Antonio, Dept Mech Engn, San Antonio, TX 78249 USA
关键词
COMPUTATIONAL FLUID-DYNAMICS; FINITE-ELEMENT FORMULATION; FLOWS; EULER; FRAMEWORK;
D O I
10.2514/1.J060704
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
High-order spectral element methods are becoming more established for solving problems in computational fluid dynamics. In this paper, we introduce new stabilization parameters for the solution of compressible Navier-Stokes equations in conjunction with high-order spectral element methods. We previously defined a new set of stabilization parameters for Euler equations in a high-order spectral/hp framework. In this paper, we examine the definition of these stabilization parameters in the context of solutions of full Navier-Stokes equations, and we report good agreement with previously published results in the literature. We establish spectral L-2 convergence of errors for Kovasznay flow. We then validate the definition of the stabilization parameter for Couette flow, flat plate, and compression corner problems. In a later example, we solve the flow past a cylinder and benchmark results with previously published results obtained with low-order methods and other approaches in compressible flow computations. We further solve hypersonic flow past a wedge and supersonic flow past a Flight Investigation of Re-Entry program (FIRE) entry capsule. We explore the definition of the shock-capturing parameter delta based on the YZ beta parameter. The introduced definitions are found to provide excellent results for the full Navier-Stokes equations.
引用
收藏
页码:2972 / 2986
页数:15
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