Effect of compressive force on strut-braced wing response
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/10.2514/6.2001-1611
Reference27 articles.
1. Multidisciplinary design optimization of a strut-braced wing transonic transport
2. Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing
3. Naghshineh-Pour, A. "Structural Optimization and Design of a Strut-Braced Wing Aircraft," MS Thesis,Virginia Tech,November 1998.
4. Flexible wing model for structural wing sizing and multidisciplinary design optimization of a strut-braced wing
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4. Effect of Compressive Force on Flutter Speed of a Strut-Braced Wing;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07
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