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'.


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    Title :

    Health Monitoring of RLV Airframe Structures


    Contributors:
    Yuan, F. G. (author) / Peters, K. (author)

    Publication date :

    2003-09-10


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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