Stowability Constraint Within a Two-Dimensional Aerodynamic Optimization Method
Author:
Affiliation:
1. Ryerson University, Toronto, Ontario M5M 2K3, Canada
2. Bombardier Aerospace, Downsview, Ontario M3K 1Y5, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34863
Reference17 articles.
1. Towards efficient aerodynamic shape optimization based on the Navier-Stokes equations
2. Newton-Krylov Algorithm for Aerodynamic Design Using the Navier-Stokes Equations
3. Nemec, M. "Optimal Shape Design of Aerodynamic Configurations: A Newton-Krylov Approach," Ph.D. Thesis,Univ. of Toronto, Toronto, 2003.
4. Optimal airfoil design
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