Flexible wing model for structural wing sizing and multidisciplinary design optimization of a strut-braced wing
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
2. Florida, Univ., Gainesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1327
Reference18 articles.
1. AIRCRAFT LAMINAR FLOW CONTROL
2. Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes.
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2. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11
3. Wing weight estimation in conceptual design: a method for strut-braced wings considering static aeroelastic effects;CEAS Aeronautical Journal;2016-08-02
4. Multilevel Structural Optimization for Preliminary Wing-Box Weight Estimation;Journal of Aircraft;2010-03
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