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Series: ASM Technical Books
Publisher: ASM International
Published: 30 November 2013
DOI: 10.31399/asm.tb.uhcf3.t53630063
EISBN: 978-1-62708-270-9
...Abstract Abstract From a fundamental standpoint, there are only two modes, or ways, in which metals can fracture under single, or monotonic, loads: shear and cleavage. There are fracture modes other than shear and cleavage. These include intergranular and quasi-cleavage fracture modes...
Series: ASM Technical Books
Publisher: ASM International
Published: 30 November 2013
DOI: 10.31399/asm.tb.uhcf3.t53630071
EISBN: 978-1-62708-270-9
...Abstract Abstract In order to understand how various types of single-load fractures are caused, one must understand the forces acting on the metals and also the characteristics of the metals themselves. All fractures are caused by stresses. Stress systems are best studied by examining free-body...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 February 2005
DOI: 10.31399/asm.tb.chffa.t51040185
EISBN: 978-1-62708-300-3
...Abstract Abstract This chapter presents a relatively simple method for estimating forging loads and flow stresses. The method uses the slab analysis technique and accounts for material properties, friction and heat transfer, press ram speed, forging geometry, and billet and die temperatures...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1988
DOI: 10.31399/asm.tb.eihdca.t65220027
EISBN: 978-1-62708-341-6
...Abstract Abstract This chapter focuses on the transfer of energy between the power supply and the induction heating coil. The most efficient transfer requires that the induction heated load and coil be matched to the power supply and that the electrical circuit containing these elements...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.cfap.t69780216
EISBN: 978-1-62708-281-5
...Abstract Abstract This article discusses the material and engineering issues associated with plastic components subjected to impact. The first part covers the effects of loading rate, temperature, and state of stress on both deformation and mode of failure. It discusses standard impact tests...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060155
EISBN: 978-1-62708-343-0
... by multiaxial loading and set practical limits on the problem they intend to treat. low-cycle fatigue multiaxial loading strain-range partitioning torsional creep-fatigue life analysis PRACTICAL DESIGN SITUATIONS invariably involve biaxial (or occasionally triaxial) stresses. Therefore...
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Published: 01 December 2006
Fig. 3.26 Principal variation of the stem load F St and the deformation load F U = F M over the stem length s St for the direct hot extrusion with a shell for the initial billet temperature ϑ B that is significantly above the container temperature ϑ R , which is the case for direct More
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Published: 01 December 2006
Fig. 3.30 Principal variation in the stem load F St and the deformation load F U over the stem displacement for direct hot extrusion with a lubricant and without a shell (e.g., steel) More
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Published: 01 December 2006
Fig. 6.6 Load diagram of a prestressed and non-prestressed press frame at a load of 31.5 MN. g , platen; h , column; i , inboard nut; j , outboard nut; k , tension element; l , compression element; m , cyclindar housing More
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Published: 01 October 2011
Fig. 7.6 Rockwell hardness indentations. (a) Minor load. (b) Major load More
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Published: 01 September 2008
Fig. 16 Fatigue fracture surface. (a) High applied load. (b) Low applied load More
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Published: 01 December 2004
Fig. 9 Load cell and digital load indicator used to calibrate a 200,000 lbf hydraulic testing machine More
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Published: 01 September 2005
Fig. 7 Load cycles diagram constructed from STF data. See Table 2 for load-cycles relationship for data More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060001
EISBN: 978-1-62708-343-0
... of creep strain and strain rate equations, explains how to determine creep constants, and reviews the findings of several studies on cyclic loading. It also discusses the development of a novel test that measures the cyclic creep-rupture resistance of materials in tension and compression. activation...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.tt2.t51060013
EISBN: 978-1-62708-355-3
... for the specification of materials. In this test procedure, a specimen is subjected to a continually increasing uniaxial load (force), while simultaneous observations are made of the elongation of the specimen. In this chapter, emphasis is placed on the interpretation of these observations rather than on the procedures...
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Published: 30 November 2013
Fig. 2 Tube of ordinary typing paper supporting a balanced load. As additional weight is added to the column, the tube will eventually collapse, or buckle. More
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Published: 30 November 2013
Fig. 10 Origin (at arrow) of a single-load brittle fracture that initiated at a small weld defect. Note also a fatigue fracture in the upper right corner. Radial ridges emanate from the origin in a fan-shaped pattern. The brittle part of the fracture is bright and sparkling, in contrast More
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Published: 01 March 2006
Fig. 4 Indentation in a workpiece made by application of (a) the minor load and (b) the major load, on a diamond Brale indenter in Rockwell hardness testing. The hardness value is based on the difference in depths of indentation produced by the minor and major loads. Source: Ref 1 More
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Published: 01 March 2006
Fig. 10 Relationship of Knoop hardness number and load. Note the increase in Knoop hardness for hardened steel with decreasing load. Source: Ref 8 More
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Published: 01 March 2002
Fig. 3.57 Microstructure of a Ni-Cr-Mo steel held at 565 °C (1050 °F) under a load of 210 MPa (30 ksi), showing (a) initial void formation at the austenite grain boundaries, (b) void linkup, and (c) separation of an austenite grain boundary. 4% picral and HCl etch. 500× More