Numerical issues in computing inviscid supersonic flow over conical delta wings
- 6 January 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Computation of three-dimensional, inviscid supersonic flowsPublished by Springer Nature ,2008
- Efficient computation of volume in flow predictionsAIAA Journal, 1983
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981