[1] Yang N B, Zhang Y N. Design of composite aircraft structure. Beijing: Aviation Industry Press, 2002: 1-19. 杨乃宾, 章怡宁. 复合材料飞机结构设计. 北京: 航空工业出版社, 2002: 1-19. (in Chinese) [2] Yuan S F. Structural health monitoring and damage control. Beijing: National Defense Industry Press, 2007: 1-23. 袁慎芳. 结构健康监测. 北京: 国防工业出版社, 2007: 1-23. (in Chinese) [3] Boller C. Next generation structural health monitoring and its integration into aircraft design. International Journal of Systems Science, 2000, 31(11): 1333-1349. [4] Yuan S, Xu Y, Peng G. New developments in structural health monitoring based on diagnostic Lamb wave. Journal of Material Science and Technology, 2004, 20(5): 490-496. [5] Deng M X, Wang Q, Giurgiutiu V. Structural health monitoring using active sensors and wavelet transforms. Proceedings of the SPIE, Smart Structures and Materials, 1999 [6] Jeong H, Jang Y S. Wavelet analysis of plate wave propagation in composite laminates. Composite Structures, 2000, 49(4): 443-450. [7] ViktorovI A. Rayleigh and Lamb waves. New York: Plenum Press, 1967: 67-117. [8] Ihn J B, Chang F K. Pitch-catch active sensing methods in structural health monitoring for aircraft structures. SAGE, 2008, 7(1): 5-15. [9] Ihn J B, Chang F K. Detection and monitoring of hidden fatigue crack growth using a built-in piezoelectric sensor/actuator network: II, validation using riveted joints and repair patches. Smart Materials and Structures, 2004, 13(3): 621-630 [10] Ihn J B, Chang F K. Detection and monitoring of hidden fatigue crack growth using a built-in piezoelectric sensor/actuator network: I, diagnostics. Smart Materials and Structures, 2004, 13(3): 609-620. [11] Wang L, Yuan F G. Damage identification in a composite plate using prestack reverse-time migration technique. Structural Health Monitoring, 2005, 4(3): 195-211. [12] Wang Q, Yuan S F, Qiu L, et al. Image representation based on time reversal theory for structure health monitoring. Chinese Journal of Scientific Instrument, 2008, 29(9): 1816-1821.(in Chinese) 王强, 袁慎芳, 邱雷, 等. 基于时间反转理论的结构损伤图像表征方法. 仪器仪表学报, 2008, 29(9): 1816-1821. [13] Wang Q, Yuan S F. Amplifying signal and imaging damage method for active Lamb wave structure health monitoring. Acta Aeronautica et Astronautica Sinica, 2008, 29(4): 1062-1067.(in Chinese) 王强, 袁慎芳. 主动Lamb波结构健康监测中信号增强与损伤成像方法. 航空学报, 2008, 29(4): 1062-1067. [14] Wang Q, Yuan S F. Time reversal imaging method for composite delamination monitoring. Acta Materiae Compositae Sinica, 2009, 26(3): 99-104.(in Chinese) 王强, 袁慎芳. 复合材料板脱层损伤的时间反转成像监测. 复合材料学报, 2009, 26(3): 99-104. [15] Zhang H Y, Ta D A, Liu Z Q. Lamb wave in layered anisotropic composite plate. Beijing: Science Press, 2008: 138-157.(in Chinese) 张海燕, 他得安, 刘镇清. 层状各向异性复合板中的兰姆波. 北京: 科学出版社, 2008: 138-157. |