Three-Dimensional Oscillatory Piecewise Continuous-Kernel Function Method-Part II: Geometrically Continuous Wings
- 1 May 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (5) , 352-355
- https://doi.org/10.2514/3.57500
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- 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
- Oscillatory Subsonic Piecewise Continuous Kernel Function MethodJournal of Aircraft, 1977
- A Quasi-Vortex-Lattice Method in Thin Wing TheoryJournal of Aircraft, 1974
- On the singularity method of subsonic lifting- surface theoryJournal of Aircraft, 1969
- Die kreisförmige Tragfläche auf potentialtheoretischer GrundlageArchive of Applied Mechanics, 1937