Improved Calculation of High Speed Inlet Flows. Part II: Results
- 1 February 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (2) , 172-179
- https://doi.org/10.2514/3.50939
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Improved Calculation of High Speed Inlet Flows: Part I. Numerical AlgorithmAIAA Journal, 1981
- Calculation of high speed inlet flows using the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- The performance of a vectorized 3-D Navier-Stokes code on the CRAY-1 computerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computation of three-dimensional turbulent separated flows at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical Solution of Three-Dimensional Shock Wave and Turbulent Boundary-Layer InteractionAIAA Journal, 1978
- Numerical Simulation of Realistic High-speed Inlets Using the Navier-Stokes EquationsAIAA Journal, 1977
- Numerical Simulation of Shock Wave - Turbulent Boundary-Layer InteractionAIAA Journal, 1976
- Numerical Solution for Supersonic Turbulent Flow over a Compression RampAIAA Journal, 1975
- Numerical solution of the interaction of a strong shock wave with a hypersonic turbulent boundary layerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974