Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness
- 1 May 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 35 (3) , 241-248
- https://doi.org/10.2514/2.3327
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Boundary layer transition due to isolated roughness - Shuttle results from the LaRC 20-inch Mach 6 tunnelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- 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 modified orbiter at Mach 6 and 10Journal of Spacecraft and Rockets, 1995
- Computation of inviscid flowfield around 3-D aerospace vehicles and comparison with experimental and flight dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Surface temperature/heat transfer measurement using a quantitative phosphor thermography systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Langley hypersonic aerodynamic/aerothermodynamic testing capabilities - Present and futurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Spreading of a Turbulent DisturbanceAIAA Journal, 1972