Oscillatory supersonic kernel function method for interfering surfaces
- 1 November 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (11), 664-670
- https://doi.org/10.2514/3.44402
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Oscillatory Supersonic Kernel Function Method for Isolated WingsJournal of Aircraft, 1974
- Kernel function for nonplanar oscillating surfaces in supersonic flowJournal of Aircraft, 1971
- A collocation method for predicting oscillatory subsonic pressure distributions on interfering parallel lifting surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971