Calculation of High-speed Inlet Flows Using the Navier-Stokes Equations
- 1 September 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (9) , 748-754
- https://doi.org/10.2514/3.57557
Abstract
No abstract availableKeywords
This publication has 22 references indexed in Scilit:
- Numerical solution of the interaction of a shock wave with a laminar boundary layerPublished by Springer Nature ,2008
- Flow oscillations of spike-tipped bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Calculation of the three-dimensional flow field in supersonic inlets at angle of attack using a bicharacteristic method with discrete shock wave fittingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Effects of airframe-inlet integration on half-axisymmetric and two-dimensional supersonic inlet performancePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical Simulation of Realistic High-speed Inlets Using the Navier-Stokes EquationsAIAA Journal, 1977
- Numerical Solution for Supersonic Turbulent Flow over a Compression RampAIAA Journal, 1975
- Numerical Simulation of High Reynolds Number Transonic FlowsAIAA Journal, 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
- Advanced supersonic inlet technology.Journal of Aircraft, 1973
- Combined Viscous-Inviscid Analysis of Supersonic Inlet FlowfieldsJournal of Aircraft, 1972