Oscillatory Supersonic Kernel Function Method for Isolated Wings
- 1 October 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (10) , 609-615
- https://doi.org/10.2514/3.60397
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Kernel function for nonplanar oscillating surfaces in supersonic flowJournal of Aircraft, 1971
- Unsteady aerodynamic distributions for harmonically deforming wings in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968