Transonic panel method for the full potential equation applied to multicomponent airfoils
- 1 September 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (9) , 1327-1334
- https://doi.org/10.2514/3.9088
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- Method of calculating the compressible flow round an aerofoil or a cascade up to the shockfree transonic rangeComputers & Fluids, 1977
- A finite volume method for transonic potential flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977