Solution of the unsteady Euler equations for fixed and rotor wing configurations
- 14 January 1985
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Finite Difference Modeling of Rotor Flows Including Wake EffectsJournal of the American Helicopter Society, 1984
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974