레이저 초음파 기반 구조 건전성 관리 기술

  • 이영준 (한국과학기술원 항공우주공학과) ;
  • 이정률 (한국과학기술원 항공우주공학과)
  • 발행 : 2016.05.20

초록

키워드

참고문헌

  1. Lee, J. R. et al., 2015, Spar Disbond Visualization in In-service Composite UAV with Ultrasonic Propagation Imager, Aerospace Science and Technology, Vol. 45, pp. 180-185. https://doi.org/10.1016/j.ast.2015.05.010
  2. Lee, J. R. et al., 2012, Laser Ultrasonic Anomalous Wave Propagation Imaging Method with Adjacent Wave Subtraction: Application to Actual Damages in Composite Wing, Opt. Laser Technol., Vol. 44, pp. 428-440. https://doi.org/10.1016/j.optlastec.2011.08.007
  3. Shin, H. J. et al., 2015, A Proof-of-concept of Smart Hangar for Composite Aircraft, 20th International Conference on Composite Materials, Copenhagen.
  4. Chia, C. C., 2012, Development of Laser Pyroshock Simulator for Noncontact Characterization and Propagation Mechanism Investigation of Explosive-induces Pyroshock for Space Launcher, CBNU Thesis Paper, pp. 67-70.
  5. Hong, S. C. et al., 2016, Composite NDE using Full-field Pulse-echo Ultrasonic Propagation Imaging System, Proc. SPIE 9799, Active and Passive Smart Structures and Integrated Systems.