Affiliation:
1. Istanbul Technical University
Publisher
American Institute of Aeronautics and Astronautics
Reference56 articles.
1. Navier-Stokes Optimization of Supersonic Wings with Four Objectives Using Evolutionary Algorithm
2. 5Nikbay, M., Coupled Sensitivity Analysis by Discrete-Analytical Direct and Adjoint Methods with Applications to Aeroelastic Optimization and Sonic Boom Minimization, Ph.D. thesis,University of Coloradoat Boulder, USA,2002.
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2 articles.
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