Multilevel decomposition approach to the preliminary sizing of a transport aircraft wing
Author:
Affiliation:
1. PRC Kentron, Inc., Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45634
Reference21 articles.
1. 2Vanderplaats, G. N., Numerical Optimization Techniques for Engineering Design with Applications, McGraw-Hill, New York, 1984, pp.217-225.
2. Sensitivity of Optimum Solutions of Problem Parameters
3. SYSTEMATIC CONTROL DESIGN BY OPTIMIZING A VECTOR PERFORMANCE INDEX
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