Multidisciplinary optimization on an advanced composite wing
Author:
Affiliation:
1. McDonnell Douglas Aerospace, Long Beach, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-4003
Reference11 articles.
1. Integrated aerodynamic-structural design of a transport wing
2. A General Approach to Multiple Lifting Surface Design and Analysis
3. Spanload optimization for strength designed lifting surfaces
4. McGeer, T., Wing Designfor Minimum Drag with Practical Constraints, Ph.D. Dissertation,Stanford University Department of Aeronautics and Astronautics, Stanford, Dec. 1983.
5. Wing design for minimum drag with practical constraints
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