The role of constraints in the MDO of a cantilever and strut-braced wing transonic commercial transport aircraft
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/10.2514/6.2000-5609
Reference31 articles.
1. Wing Planform Geometry Effects on Large Subsonic Military Transport Airplanes.
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