Numerical Simulation of Multistream Nozzle Flows
- 1 September 1980
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (9) , 1088-1093
- https://doi.org/10.2514/3.50858
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
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- The general interpolants method - A procedure for generating numerical analogs of the conservation lawsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Numerical solutions of supersonic and hypersonic laminar flows over a two-dimensional compression cornerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Numerical simulation of high Reynolds number transonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Computation of Steady Nozzle Flow by a Time-Dependent MethodAIAA Journal, 1974
- Determination of Internal Gas Flows by a Transient Numerical TechniqueAIAA Journal, 1972
- Computational efficiency achieved by time splitting of finite difference operatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Time-dependent calculations for transonic nozzle flow.AIAA Journal, 1969