A new boundary-layer inviscid iteration technique for separated flow
- 23 July 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- An inverse boundary-layer method for compressible laminar and turbulent boundary layersJournal of Aircraft, 1976
- New Approach to Inviscid Flow/ Boundary-Layer MatchingAIAA Journal, 1975
- Supercritical Wing Sections IIPublished by Springer Nature ,1975
- RELAXATION SOLOTIONS FOR INVISCID AXISYMMETRIC TRANSOlOiC FLOW OVER BLUNT OR POINTED BODIESPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- The law of the wake in the turbulent boundary layerJournal of Fluid Mechanics, 1956