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Ashok Saxena, Christopher L. Muhlstein
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in Modeling of Quenching, Residual-Stress Formation, and Quench Cracking
> Metals Process Simulation
Published: 01 November 2010
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Published: 30 November 2018
Book Chapter
Fatigue Crack Growth Testing
Available to PurchaseBook: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002360
EISBN: 978-1-62708-193-1
... Abstract This article describes the fracture mechanics in fatigue. It discusses the fatigue crack growth rate (FCGR) testing that consists of several steps, beginning with selecting the specimen size, geometry, and crack length measurement technique. The two major aspects of FCGR test analysis...
Abstract
This article describes the fracture mechanics in fatigue. It discusses the fatigue crack growth rate (FCGR) testing that consists of several steps, beginning with selecting the specimen size, geometry, and crack length measurement technique. The two major aspects of FCGR test analysis are to ensure suitability of the test data and to calculate growth rates from the data. The article presents an analysis of the crack growth data. Optical, compliance, and electric potential difference are the most common laboratory techniques, and the article reviews their merits and limitations. Forced-displacement, forced-vibration, rotational-bending, resonance, and servomechanical systems for various loading conditions are also discussed.
Book Chapter
Fatigue Crack Growth Testing
Available to PurchaseSeries: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003317
EISBN: 978-1-62708-176-4
... Abstract Testing and characterization of fatigue crack growth are used extensively to predict the rate at which subcritical cracks grow due to fatigue loading. ASTM standard E 647 is the accepted guideline for fatigue crack growth testing (FCGR) and is applicable to a wide variety of materials...
Abstract
Testing and characterization of fatigue crack growth are used extensively to predict the rate at which subcritical cracks grow due to fatigue loading. ASTM standard E 647 is the accepted guideline for fatigue crack growth testing (FCGR) and is applicable to a wide variety of materials and growth rates. The two most widely used types of specimens are the middle-crack tension and compact-type specimens. This article describes the factors affecting the selection of appropriate geometries of these specimens: consideration of material availability and raw form, desired loading condition, and equipment limitations. Various crack measurement techniques, including optical, ultrasonic, acoustic emission, electrical, and compliance methods, are also reviewed. The article discusses the two major aspects of FCGR test analysis: to ensure suitability of the test data and to calculate growth rates from the data.
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003307
EISBN: 978-1-62708-176-4
... Abstract Predicting the service life of structural components involves creep-fatigue crack growth (CFCG) testing under pure creep conditions. This article provides a discussion on the loading condition and the type of ductile and brittle material showing creep behavior. It focuses...
Abstract
Predicting the service life of structural components involves creep-fatigue crack growth (CFCG) testing under pure creep conditions. This article provides a discussion on the loading condition and the type of ductile and brittle material showing creep behavior. It focuses on a description of the experimental method that should be followed in conducting tests of CFCG with various hold times. The article describes the testing conditions, definitions, and the necessary calculations of various crack-tip parameters considered during static and cyclic loading in time-dependent fracture mechanics. The parameters considered for static loading are C*, C(t), C*(t), C*h, Ct, and Cst(t). For cyclic loading, the parameters are delta Jc and (Ct)avg. An overview of life-prediction models is also provided.
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Method of plotting results of sulfide stress cracking tests. Open symbols i...
Available to PurchasePublished: 01 January 2003
Fig. 51 Method of plotting results of sulfide stress cracking tests. Open symbols indicate failure; closed symbols indicate runouts. Source: Ref 120
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Published: 01 January 1993
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Boeing wedge test (ASTM D 3762) (a) Test specimen. (b) Typical crack propag...
Available to PurchasePublished: 01 January 2000
Fig. 8 Boeing wedge test (ASTM D 3762) (a) Test specimen. (b) Typical crack propagation behavior at 49 °C (120 °F) and 100% relative humidity. a , distance from load point to initial crack tip; Δ a , growth during exposure. Source: Ref 49
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Published: 01 January 2000
Fig. 1 Fatigue crack growth rate test specimens; a , crack length, a n , notch length, B , thickness, D , diameter, W , width, W 1 , length, W 2 , notch-to-diameter width, W 3 , notch-to-outside width. (a) Compact-type specimen. (b) Center-cracked tension specimen
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Effect of test orientation and stress ratio ( R ), on the fatigue crack gro...
Available to Purchase
in Aluminum-Lithium Alloys
> Properties and Selection: Nonferrous Alloys and Special-Purpose Materials
Published: 01 January 1990
Fig. 25 Effect of test orientation and stress ratio ( R ), on the fatigue crack growth rates of 8090-T81 and clad 2024-T3 sheet. L-T, crack plane and direction perpendicular to the principal direction of rolling; T-L, crack plane and direction parallel to the principal direction of rolling
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Destructive inspection with proof test. (a) Crack growth. (b) Detection of ...
Available to PurchasePublished: 01 January 1996
Fig. 5 Destructive inspection with proof test. (a) Crack growth. (b) Detection of cracks equal to or greater than proof size. (c) Lower proof load with cooling
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Crack closure measurements during a flight simulation test and different no...
Available to PurchasePublished: 01 January 1996
Fig. 36 Crack closure measurements during a flight simulation test and different nonlinearities for two peak loads in 2024-T3. Truncation level 9; a = 13.5 mm. Source: Ref 72
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Plastic zones in crack growth test with blocks of overload cycles. Source: ...
Available to PurchasePublished: 01 January 1996
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Comparison between test results and predictions of fatigue crack growth lif...
Available to PurchasePublished: 01 January 1996
Fig. 45 Comparison between test results and predictions of fatigue crack growth life under flight simulation loading in 2024-T3 ( t = 2 mm). S, severe; N normal; L, light. Source: Ref 87
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Bolt-on attachment of crack-opening displacement transducer to fatigue test...
Available to PurchasePublished: 01 January 1996
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Published: 01 January 1996
Fig. 18 Comparison of da / dN calculation methods. (a) Crack length test data. (b) Plot of calculated da / dN rates from the data in (a). Source: Metals Handbook , 9th ed., Vol 8, p 679–680
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Effect of test temperature on stage II crack growth rates for 18Ni(250) mar...
Available to PurchasePublished: 01 January 1990
Fig. 46 Effect of test temperature on stage II crack growth rates for 18Ni(250) maraging steel in gaseous hydrogen at different pressures (133, 57, 28, and 11.5 kpa, or 1000, 430, 210, and 86 torr). Source: Ref 274
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Published: 01 January 2000
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Bolt-on attachment of crack-opening displacement transducer to fatigue test...
Available to PurchasePublished: 01 January 2000
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Published: 01 January 2000
Fig. 19 Comparison of da / dN calculation methods. (a) Crack length test data. (b) Plot of calculated da / dN rates from the data in (a)
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