Euler solutions for wing and wing-body combination at supersonic speeds with leading-edge separation
- 14 January 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971