[1]Rodriguez A R. Morphing Aircraft Technology Survey[C]//45th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: AIAA,2007:1-16.
[2]杨智春[1],解江[1].自适应机翼技术的分类和实现途径[J].飞行力学,2008,26(5):1-4.
[3]Bowman J, Sanders B, Cannon B. Development of Next Generation Morphing Aircraft Structures [C]//48th AIAA/ASME/ASCE/ASC Structures, Structural Dynamics and Materials Conference. Honolulu, Hawaii: AIAA, 2007: 1-10.
[4]杨士斌[1],徐敏[1].智能蒙皮飞行器的飞行控制研究[J].飞行力学,2007,25(1):39-42.
[5]Perkins D A, Reed J L, Havens E. Morphing Wing Structures for Loitering Air Vehicles [ C]//45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Material Conference. Palm Springs, California : AIAA, 2004 : 1-10.
[6]Bartley--Cho J D,Wang D P,Martin C A,et al. De velopment of High-- rate, Adaptive Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel Model[J]. Intelligent Material System and Structures,2004,15(4) :279-291.
[7]Prock B C,Weisshaar T A,Crossley W A. Morphing Airfoil Shape Change Optimization with Minimum Actuator Energy As An Objective[C]//9th AIAA/ SSMO Symposiym on Multidisciplinary Analysis and Optimization. Atlanta, Georgia: AIAA 2005 : 1 - 13.
[8]Aboura A,Talbi N, Allaoui S, et al. Elastic Behavior of Corrugated Cardboard Experiments and Modeling [J].Composite Structures, 2004,63 ( 1 ) : 53-62.
[9]Buannic N,Cartraud P, Quesnel T. Homogenization of Corrugated Core Sandwich Panels[J]. Composite Structures, 2003,59 (3) :299-312.
[10]刘鸿文.材料力学[M].3版.北京:高等教育出版社,2002. |