FLOW OF FLUIDS - Mathematical Models - MATHEMATICAL TECHNIQUES;
D O I:
10.2514/3.23010
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
The extension of a recently developed implicit/explicit approach to analyzing two-dimensional ducted supersonic mixing problems with finite-rate chemistry is presented. The hybrid approach combines a fully implicit parabolic mixing algorithm, an explicit viscous-characteristic-based wave-solver algorithm, and a linearized implicit chemical kinetic solution algorithm. The resultant model provides spatial marching solutions of the parabolized Navier-Stokes (PNS) equations for supersonic combustion problems. Specialized procedures are incorporated to deal with the near-wall sublayer. A parabolic option is available that can be utilized in the direct or inverse mode for design applications. The ability of the model to treat shock waves and wave/mixing layer interactions is assessed via comparisons of predictions with those of well-established, explicit shock-capturing Euler (SCIPPY) and PNS (SCIPVIS) models. Applications to several supersonic combustion flowfield problems are presented that exhibit overall capabilities.
机构:
Science Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USAScience Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USA
Dash, S.M.
Wolf, D.E
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机构:
Science Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USAScience Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USA
Wolf, D.E
Sinha, N.
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h-index: 0
机构:
Science Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USAScience Applications Int Corp,, Princeton, NJ, USA, Science Applications Int Corp, Princeton, NJ, USA