Unsteady Supersonic Aerodynamic Theory by the Method of Potential Gradient
- 1 January 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (1) , 59-65
- https://doi.org/10.2514/3.60603
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A finite element method for potential aerodynamics around complex configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A kernel function method for computing steady and oscillatory supersonic aerodynamics with interferencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Development and applications of supersonic unsteady consistent aerodynamics for interfering parallel wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Kernel function for nonplanar oscillating surfaces in supersonic flowJournal of Aircraft, 1971
- Kinematically consistent unsteady aerodynamic coefficients in supersonic flowInternational Journal for Numerical Methods in Engineering, 1970
- Improved numerical procedure for harmonically deforming lifting surfaces from the supersonic kernel function method.AIAA Journal, 1966