Neural net-based redesign of a gas generator turbine for improved unsteady aerodynamic performance
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. Riverbend Design Services, Palm Beach Gardens, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2522
Reference20 articles.
1. Unsteady Aerodynamic and Heat Transfer Processes in a Transonic Turbine Stage
2. Fully Scaled Transonic Turbine Rotor Heat Transfer Measurements
3. Stator/rotor interaction in a transonic turbine
4. Comparison of Time-Resolved Turbine Rotor Blade Heat Transfer Measurements and Numerical Calculations
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