A kernel function method for computing steady and oscillatory supersonic aerodynamics with interference
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis 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