Neural network prediction and control of three-dimensional unsteady separated flowfields
- 1 November 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 32 (6) , 1213-1220
- https://doi.org/10.2514/3.46866
Abstract
No abstract availableKeywords
This publication has 16 references indexed in Scilit:
- Dynamic reattachment on a downward pitching finite wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Tip vortex, stall vortex, and separation observations on pitching three-dimensional wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Unsteady vortex dynamics and surface pressure topologies on a pitching wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Reattachment studies of an oscillating airfoil dynamic stall flow fieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Dynamic stall experiments on a swept three-dimensional wing in compressible flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Lift Force of Delta WingsApplied Mechanics Reviews, 1990
- Unsteady surface pressure measurements on a pitching rectangular wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Progress in analysis and prediction of dynamic stallJournal of Aircraft, 1988
- Unsteady AirfoilsAnnual Review of Fluid Mechanics, 1982
- The 1976 Freeman Scholar Lecture: Some Current Research in Unsteady Fluid DynamicsJournal of Fluids Engineering, 1977