STP216

    Fatigue Testing of Airframe Structural Components

    Published: Jan 1958


      Format Pages Price  
    PDF Version (1.2M) 22 $25   ADD TO CART
    Complete Source PDF (6.6M) 22 $55   ADD TO CART


    Abstract

    A brief discussion is presented of some important points to be considered in laying out simulated service fatigue tests of components. Typical airframe component tests that are illustrated and discussed include tests of primary wing surface structure, landing gear, and secondary and equipment structure subjected to very high cycle loadings. Some discussion is also presented on the reliability of data which may be obtained from tests of a single component.


    Author Information:

    Foster, H. W.
    Department Manager, Lockheed Aircraft Corp., Burbank, Calif.


    Paper ID: STP45763S

    Committee/Subcommittee: E08.03

    DOI: 10.1520/STP45763S


    CrossRef ASTM International is a member of CrossRef.