Solution of the unsteady Euler equations for fixed and rotor wing configurations
- 1 April 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 23 (4) , 283-289
- https://doi.org/10.2514/3.45301
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Finite Difference Modeling of Rotor Flows Including Wake EffectsJournal of the American Helicopter Society, 1984
- Iterative Lifting Surface Method for Thick Bladed Hovering Helicopter RotorsJournal of Aircraft, 1981
- 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