1[1]MidhaA, Norton TW, Howell LL. On the nomenclature,classification and bstractions of compliant mechanism [J]. Transactions of ASME, Journal of Mechanical Design,1994, 116(1): 270～279.
7[7]http:∥www. seas. upenn. edu/～gksuresh/gooddeform. html
8[8]Howell, Midha. A method for design compliant mechanisms with small-length flexural pivots. Journal of Mechanical Design, Transaction of the ASME 116 (1994): 280～289.
6Matute K, Reich G W. An Aeroelastic Topology Optimization Approach for Adaptive Wing Design [ C ]// 45th AIAA/ASME/ASCE/AHS/ASC Structure Dynamic & Materials Conference 19 - 22 April 2004, Palm Springs, California. AIAA, 2004 - 1805.
7Zhu Z Q, Wang X L, Fu H Y, et al. Aerodynamic Optimization Design of Airfoil and Wing[ C ]//10th AIAA/ ISSMO Multidisciplinary Analysis and Optimization Conference30 Augest- 1 September, 2004, Albany, New York, AIAA, 2004 - 4367.
8Austin F, Van Nostrand W, Structures with Semi-definite Rossi M J. Shape Control of Stiffness Matrices for Adaptive Wings [ C ]// Smart Structures and Intelligent Systems, Proceedings of SPIE, 1993, 1917:419-425.
9Ehlers S M, Weisshaar A. Adaptive Wing Static Aeroelastic Roll Control [ C ]// Smart Structures and Intelligent Systems, Proceedings of SPIE, 1993, 1917:125-134.
10Martin A , Kudva J N, Austin F, et al. Smart Materials and Structures-Smart Wing Volums I, II, III and IV Unclassified [ R ]. Mareials and Manufacturing Directorate: Air Force Research Laboratory, Air Force Material Command, Wright - Patterson AFB, 1998 : 1 - 53.
