A lifting surface theory based on an unsteady linearized transonic flow model
- 3 April 1978
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977
- An implicit shock-fitting scheme for unsteady transonic flow computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- On the computation of the transonic perturbation flow field around two- and three-dimensional oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- A perturbation method for transonic flows about oscillating airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A finite difference method for the solution of the transonic flow around harmonically oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- An oscillatory kernel function method for lifting surfaces in mixed transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Numerical lifting-surface theory - Problems and progress.AIAA Journal, 1968