Optimization Strategy for a Shrouded Turbine Blade Using Variable-Complexity Modeling Methodology
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
2. Aviation Industry Corporation of China, 100028 Beijing, People’s Republic of China
3. McGill University, Montreal, Quebec H3A 0C5, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054742
Reference55 articles.
1. Coupled Multidisciplinary Optimization of Engine Structural Performance
2. Multidisciplinary turbomachinery blade design optimization
3. Blading Aerodynamics Design Optimization With Mechanical and Aeromechanical Constraints
4. Multiobjective Optimization Approach to Multidisciplinary Design of a Three-Dimensional Transonic Compressor Blade
5. Aerostructural Optimization of a Transonic Compressor Rotor
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