Three dimensional supersonic inviscid flow field calculations on reentry vehicles with control surfaces
- 24 January 1977
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Phase error and stability of second order methods for hyperbolic problems. IJournal of Computational Physics, 1974
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- A complete numerical technique for the calculation of three-dimensional inviscid supersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- SURFACE PHENOMENAPublished by Elsevier ,1959