Load Interaction Effects on Fatigue Crack Growth in A514F Steel Alloy

Load Interaction Effects on Fatigue Crack Growth in A514F Steel Alloy PDF Author: RW. Hertzberg
Publisher:
ISBN:
Category : Closures
Languages : en
Pages : 17

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Book Description
Variable-amplitude fatigue tests of A514F steel alloy were performed within a linear-elastic fracture mechanics framework in order to characterize the retardation response of a cyclic strain softening material. Results of single and multiple overload tests on A514F steel alloy suggested that a material's cyclic properties have little effect on the phenomenology of retardation behavior. For instance, single high load excursions (of different magnitudes and at different baseline ?K levels) in this cyclic strain softening alloy caused fatigue crack growth rate retardation trends comparable to those exhibited by 2024-T3 aluminum, a cyclic strain hardening alloy. In addition, under complex loading conditions, the A514F steel alloy, like the 2024-T3 aluminum alloy, exhibited maximum interaction between single peak load excursions when two peak cycles were separated by a small distance.

Load Interaction Effects on Fatigue Crack Growth in A514F Steel Alloy

Load Interaction Effects on Fatigue Crack Growth in A514F Steel Alloy PDF Author: RW. Hertzberg
Publisher:
ISBN:
Category : Closures
Languages : en
Pages : 17

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Book Description
Variable-amplitude fatigue tests of A514F steel alloy were performed within a linear-elastic fracture mechanics framework in order to characterize the retardation response of a cyclic strain softening material. Results of single and multiple overload tests on A514F steel alloy suggested that a material's cyclic properties have little effect on the phenomenology of retardation behavior. For instance, single high load excursions (of different magnitudes and at different baseline ?K levels) in this cyclic strain softening alloy caused fatigue crack growth rate retardation trends comparable to those exhibited by 2024-T3 aluminum, a cyclic strain hardening alloy. In addition, under complex loading conditions, the A514F steel alloy, like the 2024-T3 aluminum alloy, exhibited maximum interaction between single peak load excursions when two peak cycles were separated by a small distance.

Load Interaction Effects on Fatigue Crack Growth in 2024-T3 Aluminum and A514F Steel Alloys

Load Interaction Effects on Fatigue Crack Growth in 2024-T3 Aluminum and A514F Steel Alloys PDF Author: William J. Mills
Publisher:
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 204

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Load Interaction Effects on Fatigue Crack Growth in Ti-6Al-4V Alloy

Load Interaction Effects on Fatigue Crack Growth in Ti-6Al-4V Alloy PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Cyclic Stress-Strain and Plastic Deformation Aspects of Fatigue Crack Growth

Cyclic Stress-Strain and Plastic Deformation Aspects of Fatigue Crack Growth PDF Author: L. F. Impellizzeri
Publisher: ASTM International
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 242

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Cyclic Stress-Strain and plastic deformation Aspects of fatigue crack growth

Cyclic Stress-Strain and plastic deformation Aspects of fatigue crack growth PDF Author: L. F. Impellizzeri
Publisher: ASTM International
ISBN:
Category : Aluminum alloys
Languages : en
Pages : 234

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Fatigue Crack Growth Under Spectrum Loads

Fatigue Crack Growth Under Spectrum Loads PDF Author: Ralph Ivan Stephens
Publisher: ASTM International
ISBN:
Category : Alloys
Languages : en
Pages : 345

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Fatigue Crack Growth Measurement and Data Analysis

Fatigue Crack Growth Measurement and Data Analysis PDF Author: S. J. Hudak
Publisher: ASTM International
ISBN: 9780803107175
Category : Technology & Engineering
Languages : en
Pages : 384

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On Load-interaction Effects in Fatigue Crack Propagation

On Load-interaction Effects in Fatigue Crack Propagation PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 119

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Book Description
A systematic investigation has been carried out on the mechanisms of the retardation in fatigue crack propagation following either a single overload or a large number of multiple overloads. The results from A1 alloy 6061-T6 and 9Cr-2Mo steel confirmed the observation by Paris and Hermann that during the period of retarded fatigue crack growth subsequent to the application of a single overload, two instead of only one crack opening levels exist.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Load Interaction Effects on Fatigue Crack Propagation in Steels of Varying Strength

Load Interaction Effects on Fatigue Crack Propagation in Steels of Varying Strength PDF Author: Anders F. Blom
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Book Description