Computation of the Shuttle solid booster nozzle start-up transient flow
- 1 September 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 1 (5), 321-328
- https://doi.org/10.2514/3.22804
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Computation of the Space Shuttle solid rocket booster nozzle start-up transient flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Computation of high Reynolds number internal/external flowsAIAA Journal, 1983
- VNAP2: a computer program for computation of two-dimensional, time-dependent, compressible, turbulent flowPublished by Office of Scientific and Technical Information (OSTI) ,1981
- A nonreflecting outflow boundary condition for subsonic navier-stokes calculationsJournal of Computational Physics, 1980
- Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner FlowsAIAA Journal, 1976
- Starting Transient of Solid-Propellant ocket Motors with High Internal Gas VelocitiesAIAA Journal, 1973
- The calculation of low-Reynolds-number phenomena with a two-equation model of turbulenceInternational Journal of Heat and Mass Transfer, 1973
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Transient pressures caused by rocket start and shutdown in ducted launchers.Journal of Spacecraft and Rockets, 1967