Supersonic three-dimensional oscillatory piecewise continuous kernelfunction method
- 1 August 1983
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 20 (8) , 674-681
- https://doi.org/10.2514/3.44928
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Three-Dimensional Oscillatory Piecewise Continuous-Kernel Function Method-Part II: Geometrically Continuous WingsJournal of Aircraft, 1981
- Three-Dimensional Oscillatory Piecewise Continuous-Kernel Function Method-Part I: Basic ProblemsJournal of Aircraft, 1981
- Three-dimensional oscillatory piecewise continuous-kernel function method. I - Basic problems. II - Geometrically continuous wings. III - Wings with geometrical discontinuitiesJournal of Aircraft, 1981
- Numerical application of Evvard's supersonic wing theory to flutter analysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Oscillatory Subsonic Piecewise Continuous Kernel Function MethodJournal of Aircraft, 1977
- AN IMPROVED MACH-BOX APPROACH FOR THE CALCULATION OF SUPERSONIC OSCILLATORY PRESSURE DISTRIBUTIONSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Oscillatory Supersonic Kernel Function Method for Isolated WingsJournal of Aircraft, 1974
- Application of the Doublet-Lattice Method to Nonplanar Configurations in Subsonic FlowJournal of Aircraft, 1971
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic EdgesJournal of the Aeronautical Sciences, 1955