Finite-difference analysis of the three-dimensional turbulent boundary layer on a sharp cone at angle of attack in a supersonic flow
- 17 January 1972
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Calculation of three-dimensional turbulent boundary layersJournal of Fluid Mechanics, 1971
- Turbulent boundary-layer flow over a rotating flat-plate bladeAIAA Journal, 1971
- The calculation of three-dimensional turbulent boundary layers in incompressible flowJournal of Fluid Mechanics, 1969
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- Recent Developments in Calculation Methods for Turbulent Boundary Layers With Pressure Gradients and Heat TransferJournal of Applied Mechanics, 1966