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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    Titel :

    Health Monitoring of RLV Airframe Structures


    Beteiligte:
    Yuan, F. G. (Autor:in) / Peters, K. (Autor:in)

    Erscheinungsdatum :

    10.09.2003


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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