This final report is divided into three sections on health monitoring technologies: 1) Analysis of Optical Fiber Bragg Grating Sensor Data from Composite Wing Box Experiment; 2) Current Optical Fiber Bragg Grating Sensor Data Acquisition Design; and 3) Damages Identification of a Composite Plate by Prestack Reverse-Time Migration Technique. The report also includes an appendix, 'Group Velocities of Flexural Waves in a Composite Plate'.
Health Monitoring of RLV Airframe Structures
2003-09-10
Report
No indication
English
A robust structural health monitoring technique for airframe structures
Tema Archive | 2009
|M.A.H.S. (Monitoring of Airframe Health Systems)
AIAA | 2024
|