Robust non-reflecting boundary conditions for the simulation of rocket nozzle flow-Reference-Cited by-同舟云学术

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Robust non-reflecting boundary conditions for the simulation of rocket nozzle flow

Published:2010-09 Issue:6 Volume:14 Page:429-441
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Moríñigo José Antonio,Salvá José Juan

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. T. Alziary de Roquefort, Unsteadiness and side loads in overexpanded supersonic nozzles, in: Proc. 4th European Symposium Aerothermodynamics for Space Vehicles, ESA SP-487, Capua, Italy, 2001.

2. Far field boundary conditions for wave-like equations;Bayliss;J. Comput. Phys.,1980

3. Three-dimensional non-reflective boundary conditions for acoustic simulations: Far field formulation and validation test cases;Bogey;Acta Acust. United Acust.,2002

4. Numerical investigation of separated nozzle flows;Chen;AIAA J.,1994

5. Modelling boundary conditions for compressible flow;Colonius;Annu. Rev. Fluid Mech.,2004

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Modeling open boundaries in dissipative MHD simulation;Journal of Computational Physics;2012-04

2. Development of Non-Reflecting Boundary Condition for Application in 3D Computational Fluid Dynamics Codes;Engineering Applications of Computational Fluid Mechanics;2012-01

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