Problems discussed for periods covering pre-1945 and 1945-55; safe life of spars; for immediate future, full scale and ad hoc testing of wings and cabins, and probably tailplanes is necessary; ultimate solution lies in design of structure, fatigue failure of which would be well beyond operational life. 2nd Barnwell Memorial Lecture. (See also Roy Aeronautical Soc -- J v 59 n 533 May 1955 p 339-48; Aeroplane v 88 n 2278 Mar 18 1955 p 357-9)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Outlook on airframe fatigue


    Additional title:

    Flight


    Contributors:
    Tye, W. (author)

    Published in:

    Flight ; 67 , n 2408


    Publication date :

    1955


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Outlook on airframe fatigue

    Tye, W. | Engineering Index Backfile | 1955


    Outlook on airframe fatigue

    Tye, W. | Engineering Index Backfile | 1955


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Trans Tech Publications | 2014


    Helicopter Airframe Fatigue Spectra Generation

    Krake, Luther | Tema Archive | 2014


    Fatigue and fail safe airframe design

    McBrearty, J.F. | Engineering Index Backfile | 1956