Numerical solution of three-dimensional unsteady transonic flow overswept wings
- 14 July 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Role of Shocks in the "Sub-Transonic" Flutter PhenomenonJournal of Aircraft, 1980
- Simulated transonic flows for aircraft with nacelles, pylons, and wingletsPublished 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 fast, conservative algorithm for solving the transonic full-potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- A numerical three-dimensional viscous transonic wing-body analysis and design toolPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977
- A finite difference method for the solution of the transonic flow around harmonically oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Calculation of plane steady transonic flowsAIAA Journal, 1971