Application of computational aerodynamics to airplane design
- 1 June 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (6) , 355-370
- https://doi.org/10.2514/3.44974
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- PAN AIR - A higher order panel method for predicting subsonic or supersonic linear potential flows about arbitrary configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Transfinite mesh generation and damped Euler equation algorithm for transonic flow around wing-body configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- An implicit marching procedure for the treatment of supersonic flow fields using the conservative full potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Progress in Finite-Volume Calculations for Wing-Fuselage CombinationsAIAA Journal, 1980
- Shock-Free Wing DesignAIAA Journal, 1980
- New Method for Designing Shock-Free Transonic ConfigurationsAIAA Journal, 1979
- The Prediction of Clmax Using a Separated Flow ModelJournal of the American Helicopter Society, 1978
- A numerical technique for subsonic flows past three dimensional canard-wing configurations with edge separationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- A General Three-Dimensional Potential-Flow Method Applied to V/STOL AerodynamicsSAE International Journal of Advances and Current Practices in Mobility, 1968
- A unified approach to the analysis and design of wing-body combinations at subsonic and supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968