Shape optimization of supersonic turbines using response surface and neural network methods
Author:
Affiliation:
1. Florida, Univ., Gainesville
2. NASA, Marshall Space Flight Center, Huntsville, AL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-1065
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1. Design Optimization of Axial Flow Compressor Blades With Three-Dimensional Navier-Stokes Solver
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