Numerical Simulation of Realistic High-speed Inlets Using the Navier-Stokes Equations
- 1 November 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (11) , 1583-1589
- https://doi.org/10.2514/3.60825
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner FlowsAIAA Journal, 1976
- Numerical simulation of shock wave-turbulent boundary layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Numerical simulation of nonchemically reacting radial supersonic diffusion laserPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Numerical Solution for Supersonic Turbulent Flow over a Compression RampAIAA Journal, 1975
- Numerical Simulation of High Reynolds Number Transonic FlowsAIAA Journal, 1975
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974
- Hypersonic flows in large-scale inlet models.Journal of Aircraft, 1973
- Calculation of Compressible Turbulent Boundary Layers with Heat and Mass TransferAIAA Journal, 1971
- Calculation of compressible adiabatic turbulent boundary layersAIAA Journal, 1970