Implicit Finite-Difference Computations of Unsteady Transonic Flows about Airfoils
- 1 December 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (12), 1728-1735
- https://doi.org/10.2514/3.60838
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Computation of unsteady transonic flows by the indicial methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- 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