Numerical Solution of Space Shuttle Orbiter Flowfield
- 1 January 1984
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 21 (1) , 9-15
- https://doi.org/10.2514/3.57695
Abstract
No abstract availableKeywords
This publication has 21 references indexed in Scilit:
- Numerical Simulation of Steady Supersonic Viscous FlowAIAA Journal, 1980
- Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical Computation of Space Shuttle Laminar Heating and Surface StreamlinesJournal of Spacecraft and Rockets, 1977
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- Inviscid Supersonic/Hypersonic Body Flowfield and Aerodynamicsfrom Shock-Capturing Technique CalculationsJournal of Spacecraft and Rockets, 1976
- Calculation of the flow on a blunted cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Calculation of the Flow on a Cone at High Angle of AttackAIAA Journal, 1974
- Computation of Three Dimentional Flows about aircraft configurationsComputers & Fluids, 1973
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973