Derivation of Aerodynamic Kernel Functions
Author:
Affiliation:
1. Princeton University, Princeton, N.J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference12 articles.
1. Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutter
2. Fluctuating lift and moment coefficients for cascaded airfoils in a nonuniform compressible flow.
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3. Derivation by a Transform Method of Integral Equations of Unsteady Lifting Surface Theory in Subsonic and Supersonic Flow;Aeronautical Quarterly;1979-11
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