PZT behavior in cyclic strain environments
暂无分享,去创建一个
[1] Christian Boller,et al. Ways and options for aircraft structural health management , 2001 .
[2] Jeffrey T. Chambers,et al. Durability Assessment of Lamb Wave-Based Structural Health Monitoring Nodes , 2006 .
[3] Eric D. Swenson,et al. Structural health monitoring of aerospace applications with restricted geometry , 2008, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[4] Christian Boller,et al. Next generation structural health monitoring and its integration into aircraft design , 2000, Int. J. Syst. Sci..
[5] Jan Drewes Achenbach. On the road from schedule-based nondestructive inspection to structural health monitoring , 2007 .
[6] V. Giurgiutiu. Tuned Lamb Wave Excitation and Detection with Piezoelectric Wafer Active Sensors for Structural Health Monitoring , 2005 .
[7] Wei Zhao,et al. Piezoelectric wafer active sensor embedded ultrasonics in beams and plates , 2003 .
[8] James L. Blackshire,et al. Characterization of Bonded Piezoelectric Sensor Performance and Durability in Simulated Aircraft Environments , 2006 .
[9] James L. Blackshire,et al. Effect of adhesive properties on elastic wave generation by bonded sensors , 2007, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[10] Xinlin Qing,et al. SMART Layer and SMART Suitcase for structural health monitoring applications , 2001, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[11] Fu-Kuo Chang,et al. Structural Health Monitoring 2007: Quantification, Validation and Implementation , 2007 .
[12] Roy Ikegami,et al. Structural health management for aging aircraft , 2001, SPIE Smart Structures and Materials + Nondestructive Evaluation and Health Monitoring.
[13] J. Rose. Ultrasonic Waves in Solid Media , 1999 .