Micro Measurements FM Fatigue Sensors were installed on A-37 aircraft at three CONUS bases to determine the longevity and suitability of this device for field installation. A similar installation on an A-37B full scale fatigue test provided base line data for relative severity comparisons of accumulated fatigue. The sensor is shown to be practical for field installation and this report recommends field installations designed for more advanced data analysis methods. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    A-37B Fatigue Sensor Evaluation Program - Full Scale Test and Field Aircraft Instrumentation


    Contributors:

    Publication date :

    1977


    Size :

    122 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    An Inexpensive, Full-Scale Aircraft Fatigue Test System

    Simmons, John H. | SAE Technical Papers | 1973


    Full-scale structural fatigue test program

    Ketola, R.N. | Engineering Index Backfile | 1965