Numerical Aerodynamic Optimization Incorporating Laminar-Turbulent Transition Prediction
Author:
Affiliation:
1. University of Toronto, Toronto, Ontario M3H 5T6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.23569
Reference24 articles.
1. Aerodynamic design via control theory
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4. Comparison of Evolutionary (Genetic) Algorithm and Adjoint Methods for Multi-Objective Viscous Airfoil Optimizations
5. Optimum Aerodynamic Design Using the Navier-Stokes Equations
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