1-20 of 2381

Search Results for crack test

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Image
Published: 01 November 2010
Fig. 89 Crack test specimen geometry and dimensions. Source: Ref 185 More
Image
Published: 30 November 2018
Fig. 20 Permanent mold hot crack test casting More
Book Chapter

By Ashok Saxena, Christopher L. Muhlstein
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...
Book Chapter

By Ashok Saxena, Christopher L. Muhlstein
Series: 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...
Book Chapter

By B.E. Gore, W. Ren, P.K. Liaw
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...
Image
Published: 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 More
Image
Published: 01 January 1993
Fig. 9 Specifications for cruciform cracking test specimens. Source: Ref 8 More
Image
Published: 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 More
Image
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 More
Image
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 More
Image
Published: 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 More
Image
Published: 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 More
Image
Published: 01 January 1996
Fig. 38 Plastic zones in crack growth test with blocks of overload cycles. Source: Ref 75 More
Image
Published: 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 More
Image
Published: 01 January 1996
Fig. 12 Bolt-on attachment of crack-opening displacement transducer to fatigue test specimen More
Image
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 More
Image
Published: 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 More
Image
Published: 01 January 2000
Fig. 36 Definition of crack opening displacement for a double cantilever beam test More
Image
Published: 01 January 2000
Fig. 12 Bolt-on attachment of crack-opening displacement transducer to fatigue test specimen More
Image
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) More