Neural network prediction of three-dimensional unsteady separated flowfields
Author:
Affiliation:
1. Frank J. Seller Research Laboratory, U.S. Air Force Academy, Colorado 80840
2. University of Colorado, Boulder, Colorado 80903
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46698
Reference26 articles.
1. Unsteady surface pressure measurements on a pitching rectangular wing
2. 3Schreck, S., and Helin, H. "Unsteady Vortex Dynamics and Surface Pressure Topologies on a Pitching Wing,1' AIAA Paper 93-0435, Jan. 1993.
3. Dynamic stall experiments on a swept three-dimensional wing in compressible flow
4. Neural networks for system identification
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