Neural Network: A New Prediction Tool for Estimating the Aerodynamic Behavior of a Pitching Delta Wing
Author:
Affiliation:
1. Sharif University of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-3793
Reference16 articles.
1. An experimental investigation of an airfoil undergoing large-amplitude pitching motions
2. Vortex unsteadiness on slender bodies at high incidence
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1. Estimation of aerodynamic coefficients of a non-slender delta wing under ground effect using artificial intelligence techniques;Neural Computing and Applications;2022-02-21
2. Unsteady aerodynamic modeling at high angles of attack using support vector machines;Chinese Journal of Aeronautics;2015-06
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