Transonic pressure distributions on a rectangular supercritical wingoscillating in pitch
- 1 August 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (8), 576-582
- https://doi.org/10.2514/3.45026
Abstract
No abstract availableKeywords
This 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