Numerical simulation by TVD schemes of complex shock reflections from airfoils at high angle of attack
- 24 March 1987
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Self adjusting grid methods for one-dimensional hyperbolic conservation lawsJournal of Computational Physics, 1983
- High resolution schemes for hyperbolic conservation lawsJournal of Computational Physics, 1983
- On the Construction and Comparison of Difference SchemesSIAM Journal on Numerical Analysis, 1968