Three-dimensional oscillatory piecewise continuous-kernel function method. I - Basic problems. II - Geometrically continuous wings. III - Wings with geometrical discontinuities
- 1 May 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (5) , 356-363
- https://doi.org/10.2514/3.44709
Abstract
No abstract availableKeywords
This publication has 4 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
- Oscillatory Subsonic Piecewise Continuous Kernel Function MethodJournal of Aircraft, 1977
- General Reverse Flow and Variational Theorems in Lifting-Surface TheoryJournal of the Aeronautical Sciences, 1952