Design Optimization of a Bendable UAV Wing Under Uncertainty
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Published:2010-04-12
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Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:
Jagdale Vijay,Viana Felipe,Haftka Raphael,Ifju Peter
Publisher
American Institute of Aeronautics and Astronautics
Reference32 articles.
1. Murray,J.,Pahle,J.,Thornton,S.,Frackowiak,T.,Mello,J.,andNorton,B."GroundandFlightEvaluationofaSmall-Scale Inflatable-Winged Aircraft," AIAA 2002-0820, 40th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, Jan.1417,2005. 2. Jacob, J.D., Smith, S.W., Cadogan D., and Scarborough, S. "Expanding the Small UAV Design Space with Inflatable Wings,"07ATC-217,SAE 2007AeroTech CongressandExhibition,Los Angeles, CA,September17-20,2007. 3. Fixed membrane wings for micro air vehicles: Experimental characterization, numerical modeling, and tailoring 4. Albertani, R., Boria, F., Bowman, S., Claxton, D., Crespo, A., Francis, C., Ifju, P., Johnson, B., Lee K., Mortan, M., Systma, M. "Development of Reliable and Mission Capable Micro Air Vehicles," Proc. 9thInternational Micro Air Vehicle Competition,Seoul,SouthKorea,May20and21,2005.
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1 articles.
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