A computational study of the flowfield surrounding the Aeroassist Flight Experiment vehicle
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- The rationale for an aeroassist flight experimentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Nonequilibrium radiation during re-entry at 10 km/sPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Enhancements to Program LAURA for computation of three-dimensional hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Application of program LAURA to three-dimensional AOTV flowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Three-dimensional AOTV flowfields in chemical nonequilibriumPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981