Inviscid analysis of two-dimensional airfoils in unsteady motion using conformal mapping
Author:
Affiliation:
1. Korea Advanced Institute of Science and Technology, Seoul, Korea
2. University of Iowa, Iowa City, Iowa
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10518
Reference18 articles.
1. The unsteady motion of a two-dimensional aerofoil in incompressible inviscid flow
2. Application of continuous vorticity panels to general unsteady incompressible two-dimensional lifting flows
3. Computation of the potential flow over airfoils with cusped or thin trailing edges
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1. Lift Enhancement in a Flapping Airfoil by an Attached Free Vortex and Sink;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
2. A simple model of propulsive oscillating foils;Ocean Engineering;2004-05
3. Propulsive efficiency of oscillating foils;European Journal of Mechanics - B/Fluids;2004-03
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