ICF13B

References [1] S.S. Kessler. “Certifying a Structural Health Monitoring System: Characterizing Durability, Reliability and Longevity”. In Proceedings of the 1st International Forum on Integrated Systems Health Engineering and Management in Aerospace, Napa, CA, 7-10 November 2005. [2] S.S. Kessler and D.J. Shim. “Validation of a Lamb Wave-Based Structural Health Monitoring for Aircraft Applications”. In Proceedings of the SPIE’s 12th International Symposium on Smart Structures and Materials, pages 293-301, San Diego, CA, 7-10 March 2005. [3] F-K Chang. “Structural Health Monitoring: A Summary Report”. In Proceedings of the 2nd International Workshop on Structural Health Monitoring, Stanford, CA, 8-10 September 1999. [4] V. Giurgiutiu. “Tuned Lamb-Wave Excitation and Detection with Piezoelectric Wafer Active Sensors for Structural Health Monitoring”. Journal of Intelligent Material Systems and Structures, v.16:291-306, 16 April 2005. [5] D.Cope, J.Cronenberger, K.Schrader, L.Smith and C.Thwing, Integration of Remote Sensing and Risk Analysis for Airframe Structural Integrity Assessment, 2010 Aircraft Airworthiness & Sustainment Conference ,Austin, TX , May 10-20, 2010 [6] H. Speckmann, International Maintenance Review Board Policy Board (IMRBPB) Meeting, EASA, April 22, 2007, Cologne 2007. [7] B.P.Y. Tang, M. Martinez, T. Marincak, T. Benak and N.C. Bellinger, PROTOTYPE INSTALLATION OF A SURFACE MOUNTABLE CRACK SENSOR, Presented in the 11th Joint NASA/FAA/DOD Conference on Aging Aircraft ,Phoenix, Arizona, April 21-24, 2008, [8] Z. Lü, M. Liu, China Patent, No.200610104559.4. [9] Z. Lü, M. Liu, China Patent, No.200620079776.8. [10] Feng Hu, Mabao Liu, Zhigang Lü. “The flaw-detected coating and its applications in R&M of aircrafts”, Proc. of SPIE, Vol. 7493, 2009, Page(s):1-7

RkJQdWJsaXNoZXIy MjM0NDE=