Three-dimensional hypersonic laminar, transitional and/or turbulent shock-layer flows
- 14 July 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Turbulent viscous-shock-layer solutions with strong vorticity interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Some properties of boundary layer flow during the transition from laminar to turbulent motionJournal of Fluid Mechanics, 1957
- Catholic Counselors BookshelfThe Catholic Counselor and Readings, 1956