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Published: 01 March 2002
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Published: 01 March 2006
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Macrograph of an AISI/SAE 1035 steel showing surface cracking due to a hot-...
Available to Purchase
in Alteration of Microstructure
> Metallographer’s Guide: Practices and Procedures for Irons and Steels
Published: 01 March 2002
Fig. 3.39 Macrograph of an AISI/SAE 1035 steel showing surface cracking due to a hot-shortness condition caused by copper. 2×
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Example of PP surface cracking for AISI type 304 stainless steel at 650 °C ...
Available to Purchase
in Strain-Range Partitioning—Concepts and Analytical Methods
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
Fig. 3.5 Example of PP surface cracking for AISI type 304 stainless steel at 650 °C (1200 °F). Source: Ref 3.3
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Liquid penetrant test for surface cracks. (a) An open crack draws in penetr...
Available to PurchasePublished: 01 October 2011
Fig. 7.26 Liquid penetrant test for surface cracks. (a) An open crack draws in penetrant liquid by capillary action. (b) Excess surface penetrant is removed. (c) Developer draws out penetrant liquid and forms a visible indication of the surface crack.
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Surface cracks in a flux-cored arc weld highlighted by dye penetrant inspec...
Available to PurchasePublished: 01 July 1997
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Forging laps detected by surface crack examinations. Extensive decarburizat...
Available to PurchasePublished: 01 August 2018
Fig. 11.58 Forging laps detected by surface crack examinations. Extensive decarburization of the lap region can be noticed when observing the reduction of the pearlite volume fraction. Etchant: nital 2%. Courtesy of M.M. Souza, Neumayer-Tekfor, Jundiaí, SP, Brazil.
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Published: 01 September 2008
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Fully pearlitic steel fatigue fracture surfaces. Crack growth direction is ...
Available to PurchasePublished: 01 August 2005
Fig. 3.19 Fully pearlitic steel fatigue fracture surfaces. Crack growth direction is from left to right in both images. (a) Intermediate crack growth rate (~0.1 μm/cycle), and (b) low crack growth rate (~0.001 μm/cycle). No fatigue striations were resolved by scanning electron microscopy (SEM
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Configuration of a semielliptical surface crack. The C-tip is at either end...
Available to PurchasePublished: 01 August 2005
Fig. 5.16 Configuration of a semielliptical surface crack. The C-tip is at either end of the major axis (along the surface). The A-tip is at the maximum depth of the minor axis. In this book, C-tips are always on the surface; the A-tip is always at the maximum depth, whether c is greater
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in Partitioning of Hysteresis Loops and Life Relations
> Fatigue and Durability of Metals at High Temperatures
Published: 01 July 2009
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Published: 30 April 2025
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Published: 30 April 2025
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Surface area of thermal cracking as a function of thermal cycles for H13 st...
Available to PurchasePublished: 01 January 1998
Fig. 13-26 Surface area of thermal cracking as a function of thermal cycles for H13 steel austenitized and heat treated to various levels of hardness. Source Ref 19 , as reproduced in Ref 6
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Hot cracking network on the working surface of a tapered extrusion mandrel ...
Available to PurchasePublished: 01 December 2006
Fig. 7.119 Hot cracking network on the working surface of a tapered extrusion mandrel in the hot working steel 1.2367 for the production of copper tubes, resulting from the fluctuating tensile and compressive stresses. Copper that has welded to the mandrel surface can be seen in the lower
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Surface profile adjacent to the cracking. Evidence of high-temperature grai...
Available to Purchase
in Steel Heat Treatment Failures due to Quenching
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 46 Surface profile adjacent to the cracking. Evidence of high-temperature grain-boundary oxidation. Etched with 2% nital. Original magnification: 400×
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Thermal-mechanical fatigue cracking on internal surface of a nickel-base su...
Available to PurchasePublished: 01 March 2002
Fig. 14.18 Thermal-mechanical fatigue cracking on internal surface of a nickel-base superalloy forward liner of a gas turbine combustor. Note: One crack extends from a keyhole slot (right), while another can be seen in the area adjacent to an airhole (left). 1.5×
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in Failure of a Tail Rotor Blade in a Helicopter
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
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in Cracking in the Wing Root Fitting in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
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in Cracking in the Wing Root Fitting in an Aircraft
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
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