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The fourth part consists of a letter preceded by a hyphen and followed by a number. It indicates the specific condition or temper that the alloy is in. Table 32.12 specifies the symbols that are used for each temper.
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TABLE 32.12 Temper Designation of Magnesium Alloys
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32.1 J. Datsko, Materials in Design and Manufacture, J. Datsko Consultants, Ann Arbor, Mich., 1978. 32.2 Metals and Alloys in the Unified Numbering System, 3d ed., Society of Automotive Engineers, Inc. (SAE), 1983. 32.3 Metals Handbook Desk Edition, American Society for Metals (ASM), Metals Park, Ohio, 1984. 32.4 R. M. Brick, A. W. Pense, and R. B. Gordon, Structure and Properties of Engineering Materials, 4th ed., McGraw-Hill, New York, 1977. 32.5 M. M. Schwartz, Composite Materials Handbook, McGraw-Hill, New York, 1984. 32.6 L. H. Van Vlack, Elements of Materials Science, 4th ed., Addison-Wesley, Reading, Mass., 1980.
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Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.
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Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.
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Source: STANDARD HANDBOOK OF MACHINE DESIGN
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THE STRENGTH OF COLD-WORKED AND HEAT-TREATED STEELS
Charles R. Mischke, Ph.D., P.E.
Professor Emeritus of Mechanical Engineering Iowa State University Ames, Iowa
33.1 33.2 33.3 33.4 33.5
INTRODUCTION / 33.2 STRENGTH OF PLASTICALLY DEFORMED MATERIALS / 33.3 ESTIMATING ULTIMATE STRENGTH AFTER PLASTIC STRAINS / 33.4 ESTIMATING YIELD STRENGTH AFTER PLASTIC STRAINS / 33.8 ESTIMATING ULTIMATE STRENGTH OF HEAT-TREATED PLAIN CARBON STEELS / 33.9 33.6 ESTIMATING ULTIMATE STRENGTH OF HEAT-TREATED LOW-ALLOY STEELS / 33.11 33.7 TEMPERING TIME AND TEMPERATURE TRADEOFF RELATION / 33.29 REFERENCES / 33.31 RECOMMENDED READING / 33.31
GLOSSARY
AR A B d D Dl DH EJD f F H IH Fractional area reduction Area Critical hardness for carbon content and tempering temperature, Rockwell C scale Diameter Tempering decrement, Rockwell C scale; carbon ideal diameter, in Ideal critical diameter, in Distant hardness, Rockwell C scale Equivalent Jominy distance, sixteenths of inch Tempering factor for carbon content and tempering temperature Load, temperature, degrees Fahrenheit Quench severity, in 1 Initial hardness, Rockwell C scale
33.1 Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.
THE STRENGTH OF COLD-WORKED AND HEAT-TREATED STEELS 33.2
PERFORMANCE OF ENGINEERING MATERIALS
m n r Rmax RQ RT Se Su Sy t 0 A o
Strain-strengthening exponent Design factor Radius Maximum hardness attainable, Rockwell C scale As-quenched Jominy test hardness, Rockwell C scale Tempered hardness, Rockwell C scale Engineering endurance limit Engineering ultimate strength in tension Engineering yield strength, 0.2 percent offset Time True strain Factor of safety Strain-strengthening coefficient Normal stress Sum of alloy increments, Rockwell C scale Octahedral shear stress Shearing stress
Subscripts a B c C D e f L R s t u y 0 Axial Long traverse Compression Circumferential Short traverse Endurance Fracture Longitudinal Radial Shear Tension Ultimate Yield No prior strain
33.1 INTRODUCTION
The mechanical designer needs to know the yield strength of a material so that a suitable margin against permanent distortion can be provided. The yield strength provided by a standardized tensile test is often not helpful because the manufactur-
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THE STRENGTH OF COLD-WORKED AND HEAT-TREATED STEELS 33.3
THE STRENGTH OF COLD-WORKED AND HEAT-TREATED STEELS
ing process has altered this property. Hot or cold forming and heat treatment (quenching and tempering) change the yield strength. The designer needs to know the yield strength of the material at the critical location in the geometry and at condition of use. The designer also needs knowledge of the ultimate strength, principally as an estimator of fatigue strength, so that a suitable margin against fracture or fatigue can be provided. Hot and cold forming and various thermomechanical treatments during manufacture have altered these properties too. These changes vary within the part and can be directional. Again, the designer needs strength information for the material at the critical location in the geometry and at condition of use. This chapter addresses the effect of plastic strain or a sequence of plastic strains on changes in yield and ultimate strengths (and associated endurance limits) and gives quantitative methods for the estimation of these properties. It also examines the changes in ultimate strength in heat-treated plain carbon and low-alloy steels.
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