Boundary layer transition due to isolated roughness - Shuttle results from the LaRC 20-inch Mach 6 tunnel
- 6 January 1997
- proceedings article
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Isolated roughness induced boundary-layer transition - Shuttle Orbiter ground tests and flight experiencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Aerothermodynamic measurement and prediction for a modified orbiter at Mach 6 and 10 in airPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Surface temperature/heat transfer measurement using a quantitative phosphor thermography systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Spreading of a Turbulent DisturbanceAIAA Journal, 1972