A heating analysis of the nosecap and leading edges of the X-34 vehicle
- 12 January 1998
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Trajectory based validation of the Shuttle heating environmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- A heating analysis and thermal protection system sizing of a lifting body single-stage-to-orbit vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Numerical benchmarks for Navier-Stokes heating calculations on Access-to-Space vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Multiblock analysis for shuttle orbiter reentry heating from Mach 24 to Mach 12Journal of Spacecraft and Rockets, 1994
- On convergence of computation of chemically reacting flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985