A panel method to determine loads on oscillating airfoils in transonic flow with embedded shock waves
- 12 May 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Linearization of Unsteady Transonic Flows Containing ShocksAIAA Journal, 1979
- Implicit Finite-Difference Computations of Unsteady Transonic Flows about AirfoilsAIAA Journal, 1977
- A Theory of Transonic Aileron Buzz, Neglecting Viscous EffectsJournal of the Aerospace Sciences, 1962