Structural characteristics via SLDV for a class of morphing micro-air-vehicles
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Daniel J. Inman | Andrew Kurdila | Onur Bilgen | Joe Vignola | Edward C. Diggs | Kevin Kochersburger | A. Kurdila | D. Inman | J. Vignola | O. Bilgen | Kevin Kochersburger
[1] R. Williams. Nonlinear Mechanical and Actuation Characterization of Piezoceramic Fiber Composites , 1999 .
[2] W. Keats Wilkie,et al. Method of Fabricating NASA-Standard Macro-Fiber Composite Piezoelectric Actuators , 2003 .
[3] Daniel J. Inman,et al. THE USE OF MACRO-FIBER COMPOSITES IN STRUCTURAL VIBRATION APPLICATIONS , 2002 .
[4] N. Hagood,et al. DEVELOPMENT OF PIEZOELECTRIC FIBER COMPOSITES FOR STRUCTURAL ACTUATION , 1993 .
[5] D. Inman,et al. Anisotropic Laminar Piezocomposite Actuator Incorporating Machined PMN–PT Single-crystal Fibers , 2006 .
[6] Mujahid Abdulrahim,et al. ROLL CONTROL FOR A MICRO AIR VEHICLE USING ACTIVE WING MORPHING , 2003 .
[7] Peter Ifju,et al. Experimental Analysis of Deformation for Flexible-Wing Micro Air Vehicles , 2005 .
[8] S. Ettinger,et al. Composite Materials for Micro Air Vehicles , 2001 .
[9] Justin M. Lloyd,et al. Electrical Properties of Macro-Fiber Composite Actuators and Sensors , 2004 .
[10] Michael W. Hyer,et al. A Morphing Concept Based on Unsymmetric Composite Laminates and Piezoceramic MFC Actuators , 2004 .
[11] Paul H. Mirick,et al. Low-cost piezocomposite actuator for structural control applications , 2000, Smart Structures.
[12] T. J. Mueller,et al. Experimental studies of the Eppler 61 airfoil at low Reynolds numbers , 1982 .
[13] Jayanth N. Kudva,et al. Morphing aircraft concepts, classifications, and challenges , 2004, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[14] Daniel J. Inman,et al. Multi-Input Multi-Output Modal Testing Techniques for a Gossamer Structure , 2002 .
[15] Jonathan D. Bartley-Cho,et al. Development, control, and test results of high-rate hingeless trailing edge-control surface for the Smart Wing Phase 2 wind tunnel model , 2002, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[16] Gabriel Eduardo Torres,et al. Aerodynamics of low aspect ratio wings at low Reynolds numbers with applications to micro air vehicle design , 2001 .
[17] M. Schultz,et al. USE OF PIEZOELECTRIC ACTUATORS TO EFFECT SNAP-THROUGH BEHAVIOR OF UNSYMMETRIC COMPOSITE LAMINATES , 2003 .
[18] Thomas J. Mueller,et al. Low Reynolds Number Aerodynamics of Low-Aspect-Ratio, Thin/Flat/Cambered-Plate Wings , 2000 .
[19] W Moses Robert,et al. Evaluation of New Actuators in a Buffet Loads Environment , 2001 .
[20] L Prandtl,et al. Mutual influence of wings and propeller , 1921 .
[21] Dae-Kwan Kim,et al. Smart flapping wing using macrofiber composite actuators , 2006, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[22] Nesbitt W. Hagood,et al. Improving transverse actuation of piezoceramics using interdigitated surface electrodes , 1993, Smart Structures.
[23] Luther N. Jenkins,et al. Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle , 2001 .
[24] Ralph C. Smith,et al. Smart material systems - model development , 2005, Frontiers in applied mathematics.
[25] Daniel J. Inman,et al. Structural and Machine Design Using Piezoceramic Materials: A Guide for Structural Design Engineers , 2000 .
[26] Daniel J. Inman,et al. Morphing wing micro-air-vehicles via macro-fiber-composite actuators , 2007 .
[27] William H. Rae,et al. Low-Speed Wind Tunnel Testing , 1966 .