Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch
- 2 May 1983
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Static and unsteady pressure measurements on a 50 degree clipped delta wing at M = 0.9Published by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Transonic Unsteady Airloads on an Energy Efficient Transport Wing with Oscillating Control SurfacesJournal of Aircraft, 1981
- Remarks on the Suitability of Various Transonic Small Perturbation Equations to Describe Three-Dimensional Transonic Flow; Examples of Computations Using a Fully-Conservative Rotated Difference SchemePublished by Springer Nature ,1976