Research program undertaken to locate origin of fatigue following loss, due to engine trouble, of number of Douglas B.66 bomber aircraft of United States Air Force in Europe; technique and equipment used successfully to carry out ultrasonic inspection of compressor rotor blades of Allison J.71 turbojet while still installed in engine; Rayleigh wave mode was chosen as most suitable for detection of fatigue cracks.


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    Title :

    Ultrasonic testing of B.66 compressor blades


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1963


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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