Nonplanar, subsonic, three-dimensional oscillatory piecewise continuous kernel function method
- 1 December 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (12) , 1043-1048
- https://doi.org/10.2514/3.45247
Abstract
No abstract availableKeywords
This publication has 9 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
- Refinement of the nonplanar aspects of the subsonic doublet-lattice lifting surface method.Journal of Aircraft, 1972
- Wing-Body Aerodynamic InteractionAnnual Review of Fluid Mechanics, 1972
- Numerical lifting-surface theory - Problems and progress.AIAA Journal, 1968
- Kernel Function for Nonplanar Oscillating Surfaces in a Subsonic FlowAIAA Journal, 1967
- UNSTEADY AERODYNAMICS FOR ADVANCED CONFIGURATIONS. PART I. APPLICATION OF THE SUBSONIC KERNEL FUNCTION TO NONPLANAR LIFTING SURFACESPublished by Defense Technical Information Center (DTIC) ,1965
- Das Potential und das Geschwindigkeitsfeld der harmonisch schwingenden tragenden Fläche bei UnterschallströmungZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 1963