Mode II Fatigue Crack Growth Specimen Development

RJ Buzzard; B Gross; JE Srawley

doi:10.1520/STP17405S

SYMPOSIA PAPER Published: 01 January 1986

STP17405S

Mode II Fatigue Crack Growth Specimen Development

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A novel Mode II test specimen has been developed that has potential application in understanding phenomena associated with mixed-mode fatigue failures in high performance aircraft engine bearing races. The attributes of the specimen are as follows: it contains one single-ended notch, which simplifies data gathering and reduction; the fatigue crack grows in-line with the direction of load application; a single axis test machine is sufficient to perform testing; and the Mode I component is vanishingly small.

Author Information

Buzzard, RJ

Structural Materials, NASA Lewis Research Center, Cleveland, OH

Gross, B

Structural Materials, NASA Lewis Research Center, Cleveland, OH

Srawley, JE

NASA Lewis Research Center, Cleveland, OH

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Details

Developed by Committee: E08

Pages: 329–346

DOI: 10.1520/STP17405S

ISBN-EB: 978-0-8031-4972-4

ISBN-13: 978-0-8031-0472-3

Mode II Fatigue Crack Growth Specimen Development

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