Author:
Barrett R,Gross R,Brozoski F
Publisher
American Institute of Aeronautics and Astronautics
Cited by
4 articles.
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1. Gust load alleviation of an unmanned aerial vehicle wing using variable camber;Journal of Intelligent Material Systems and Structures;2013-11-07
2. Magnification of Work Output in PBP Class Actuators Using Buckling/Converse Buckling Techniques;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07
3. Improvements to Commercial and General Aviation via Adaptive Aerostructures;7th AIAA ATIO Conf, 2nd CEIAT Int'l Conf on Innov and Integr in Aero Sciences,17th LTA Systems Tech Conf; followed by 2nd TEOS Forum;2007-09-18
4. (Student paper) Nonlinear Semi-Analytical Modeling of Post-Buckled Precompressed (PBP) Piezoelectric Actuators for UAV Flight Control;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05