Adjoint-Based Constrained Aerodynamic Shape Optimization for Multistage Turbomachines
Author:
Affiliation:
1. Department of Mechanical Engineering, McGill University, Montreal, Quebec H3A 0C3, Canada
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.B35433
Reference39 articles.
1. Optimal Control of Systems Governed by Partial Differential Equations
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4. Control theory based airfoil design using the Euler equations
5. Optimum aerodynamic design using CFD and control theory
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