Improvements to an Euler aerodynamic method for transonic flow analysis
- 1 January 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 26 (1) , 13-20
- https://doi.org/10.2514/3.45717
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Application of Runge-Kutta scheme for high-speed inviscid internal flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Computation of flow around wings based on the Euler equationsJournal of Fluid Mechanics, 1984
- A multi-grid method for transonic wing analysis and designJournal of Aircraft, 1984
- Free vortex flows - Recent encounters with an Euler codePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Solution of the Euler equations for complex configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Numerical solution of transonic wing flowfieldsAIAA Journal, 1983
- Transonic wing-body calculations using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Damped Euler-equation method to compute transonic flow around wing-body combinationsAIAA Journal, 1982
- Reynolds Averaged Navier-Stokes Computations of Transonic Flows-the State-of-the-ArtPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Progress in Finite-Volume Calculations for Wing-Fuselage CombinationsAIAA Journal, 1980