Hypersonic boundary layer transition for X-33 Phase II vehicle
- 12 January 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Three-dimensional boundary-layer transition on a swept wing at Mach 3.5AIAA Journal, 1995
- Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center - Aerothermodynamic Facilities ComplexPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Data-parallel lower-upper relaxation method for reacting flowsAIAA Journal, 1994
- Approximate method for calculating heating rates on three-dimensional vehiclesJournal of Spacecraft and Rockets, 1994
- Surface temperature/heat transfer measurement using a quantitative phosphor thermography systemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Computer graphic visualization of orbiter lower surface boundary-layer transitionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984