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Cyclic Fatigue Damage Characteristics Observed for Simple Loadings Extended to Multiaxial Life Prediction

AUTHOR Nasa, National Aeronautics and Space Adm
PUBLISHER Independently Published (11/07/2018)
PRODUCT TYPE Paperback (Paperback)

Description
Fully reversed uniaxial strain controlled fatigue tests were performed on smooth cylindrical specimens made of 304 stainless steel. Fatigue life data and cracking observations for uniaxial tests were compared with life data and cracking behavior observed in fully reversed torsional tests. It was determined that the product of maximum principle strain amplitude and maximum principle stress provided the best correlation of fatigue lives for these two loading conditions. Implementation of this parameter is in agreement with observed physical damage and it accounts for the variation of stress-strain response, which is unique to specific loading conditions. Biaxial fatigue tests were conducted on tubular specimens employing both in-phase and out-of-phase tension torsion cyclic strain paths. Cracking observations indicated that the physical damage which occurred in the biaxial tests was similar to the damage observed in uniaxial and torsional tests. The Smith, Watson, and Topper parameter was then extended to predict the fatigue lives resulting from the more complex loading conditions. Jones, David J. and Kurath, Peter Unspecified Center CRACK INITIATION; CYCLIC LOADS; FATIGUE LIFE; METAL FATIGUE; S-N DIAGRAMS; AXIAL STRAIN; DAMAGE; FATIGUE TESTS; STAINLESS STEELS; STRESS-STRAIN RELATIONSHIPS...
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Product Details
ISBN-13: 9781730988264
ISBN-10: 1730988261
Binding: Paperback or Softback (Trade Paperback (Us))
Content Language: English
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Page Count: 104
Carton Quantity: 39
Product Dimensions: 8.50 x 0.22 x 11.02 inches
Weight: 0.58 pound(s)
Country of Origin: US
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BISAC Categories
Science | Space Science - General
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Fully reversed uniaxial strain controlled fatigue tests were performed on smooth cylindrical specimens made of 304 stainless steel. Fatigue life data and cracking observations for uniaxial tests were compared with life data and cracking behavior observed in fully reversed torsional tests. It was determined that the product of maximum principle strain amplitude and maximum principle stress provided the best correlation of fatigue lives for these two loading conditions. Implementation of this parameter is in agreement with observed physical damage and it accounts for the variation of stress-strain response, which is unique to specific loading conditions. Biaxial fatigue tests were conducted on tubular specimens employing both in-phase and out-of-phase tension torsion cyclic strain paths. Cracking observations indicated that the physical damage which occurred in the biaxial tests was similar to the damage observed in uniaxial and torsional tests. The Smith, Watson, and Topper parameter was then extended to predict the fatigue lives resulting from the more complex loading conditions. Jones, David J. and Kurath, Peter Unspecified Center CRACK INITIATION; CYCLIC LOADS; FATIGUE LIFE; METAL FATIGUE; S-N DIAGRAMS; AXIAL STRAIN; DAMAGE; FATIGUE TESTS; STAINLESS STEELS; STRESS-STRAIN RELATIONSHIPS...
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Paperback