X-34 experimental aeroheating at Mach 6 and 10
- 12 January 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- Reduction and analysis of phosphor thermography data with the IHEAT software packagePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Computational aeroheating predictions for X-34Published by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Aeroheating predictions for X-34 using an inviscid-boundary layer methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Engineering aerothermal analysis for X-34 thermal protection designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Single-stage-to-orbit — Meeting the challengeActa Astronautica, 1996
- Pioneering industry/government partnerships - X-34Published by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center - Aerothermodynamic Facilities ComplexPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- 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
- Aerothermodynamic measurements on a proposed assured crew return vehicle (ACRV) lifting-body configuration at Mach 6 and 10 in airPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990