Semi-Inverse Design Optimization Method for Film-Cooling Arrangement of High-Pressure Turbine Vanes
Author:
Affiliation:
1. Shanghai Jiao Tong University, 200240 Shanghai, People’s Republic of China
2. Chinese Academy of Sciences, 201210 Shanghai, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B35747
Reference24 articles.
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5. Aerodynamic shape design and optimization - Status and trends
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