Unsteady aerodynamic modeling of a fighter wing in transonic flow
- 25 June 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Numerical simulation of 2-D unsteady transonic flows using the full-potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A conservative finite difference algorithm for the unsteady transonic potential equation in generalized coordinatesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- An implicit conservative algorithm for steady and unsteady three-dimensional transonic potential flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A strongly implicit procedure for steady three-dimensional transonic potential flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Numerical solution of three-dimensional unsteady transonic flow overswept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A CONSERVATIVE IMPLICIT FINITE DIFFERENCE ALGORITHEM FOR THE UNSTEADY TRANSONIC FULL POTENTIAL EQUATIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Implicit computations of unsteady transonic flow governed by the full-potential equation in conservation formPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A finite volume method for transonic potential flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977