A field panel/finite difference method for potential unsteady transonic flow
- 1 April 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 23 (4) , 537-545
- https://doi.org/10.2514/3.8948
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- A conservative finite difference algorithm for the unsteady transonic potential equation in generalized coordinatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Calculation of unsteady transonic flows with shocks by field panel methodsAIAA Journal, 1982
- Progress in Finite-Volume Calculations for Wing-Fuselage CombinationsAIAA Journal, 1980
- Transonic flow past lifting wings.AIAA Journal, 1973
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969