Kernel function for nonplanar oscillating surfaces in supersonic flow
Author:
Affiliation:
1. The MacNeal-Schwendler Corporation, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44292
Reference9 articles.
1. Kernel Function for Nonplanar Oscillating Surfaces in a Subsonic Flow
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1. Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method;International Journal for Numerical Methods in Fluids;2003
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3. Continuity of Lifting Surface Theory in Subsonic and Supersonic Flow;AIAA Journal;1998-10
4. Ein Abriß der Aeroelastizität;Computerdynamik der Tragwerke;1997
5. An Expansion Series for Solving Improper Cylindrical Functions Occurring in Subsonic, Supersonic and Transonic Kernel Formulations;Contemporary Research in Engineering Science;1995
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