Fatigue Testing of Airframe Structural Components

H. Foster

doi:10.1520/STP45763S

SYMPOSIA PAPER Published: 01 January 1958

STP45763S

Fatigue Testing of Airframe Structural Components

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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.

Lockheed Aircraft Corp., Burbank, Calif.

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Details

Developed by Committee: E08

Pages: 37–58

DOI: 10.1520/STP45763S

ISBN-EB: 978-0-8031-6716-2

ISBN-13: 978-0-8031-6553-3

Fatigue Testing of Airframe Structural Components

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