Computation of viscous transonic flow over porous airfoils
- 1 December 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (12), 1067-1075
- https://doi.org/10.2514/3.45882
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Porous aerofoil analysis using viscous-inviscid coupling at transonic speedsInternational Journal for Numerical Methods in Fluids, 1987
- Passive shockwave boundary layer control experiments on a circular arc modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90Published by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Effects of suction on shock/boundary-layer interaction and shock-induced separationJournal of Aircraft, 1985
- A new consistent spatial differencing scheme for the transonic full-potential equationAIAA Journal, 1984
- Porous Airfoils in Transonic FlowAIAA Journal, 1984
- Porosity effect on supercritical airfoil drag reduction by shock wave/boundary layer controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- A diagonal form of an implicit approximate-factorization algorithmJournal of Computational Physics, 1981
- Implicit Algorithm for the Conservative Transonic Full-Potential Equation Using an Arbitrary MeshAIAA Journal, 1979
- Analysis of Turbulent Boundary LayersJournal of Applied Mechanics, 1976