Computation of underexpanded solid rocket plume and its effects on the mated Shuttle configuration
- 22 June 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Multizonal Navier-Stokes solutions for the multibody Space Shuttle configurationJournal of Spacecraft and Rockets, 1992
- Computation of supersonic turbulent shear layer mixing with mild compressibility effectsAIAA Journal, 1991