Aerothermodynamic environment definition for an X-23/X-24A derived assured crew return vehicle
- 17 June 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- HL-20 computational fluid dynamics analysisJournal of Spacecraft and Rockets, 1993
- 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
- High angle of attack inviscid flow calculations over a Shuttle-like vehicle with comparisons to flight dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983