Aerostructural Optimization of a Transonic Compressor Rotor
Author:
Affiliation:
1. Ohio Aerospace Institute, Cleveland, Ohio, 44142
2. NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135
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/10.2514/1.15397
Reference26 articles.
1. Transonic Axial-Flow Blade Optimization: Evolutionary Algorithms/Three-Dimensional Navier-Stokes Solver
2. Three-Dimensional Multi-Objective Design Optimization of a Transonic Compressor Rotor
3. Single and Multipoint Shape Optimization of Gas Turbine Blade Cascades
4. Coupled Multidisciplinary Optimization of Engine Structural Performance
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