A harmonic gradient method for unsteady supersonic flow calculations
- 1 May 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (5) , 371-379
- https://doi.org/10.2514/3.45134
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Transonic kernel function method for unsteady flow calculations using a unified linear pressure panel procedurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- A new unified approach for analyzing wing-body-tail configurations with control surfacesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Oscillatory supersonic kernel function method for interfering surfacesJournal of Aircraft, 1974
- Oscillatory Supersonic Kernel Function Method for Isolated WingsJournal of Aircraft, 1974
- Kernel function for nonplanar oscillating surfaces in supersonic flowJournal of Aircraft, 1971