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Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1983
DOI: 10.31399/asm.tb.mlt.t62860047
EISBN: 978-1-62708-348-5
... Abstract Specific heat is a fundamental property that relates the total heat per unit mass added to a system to the resultant temperature change of the system. This chapter begins with the definition and historical development of specific heat. Thermodynamic and solid state relationships...
Abstract
Specific heat is a fundamental property that relates the total heat per unit mass added to a system to the resultant temperature change of the system. This chapter begins with the definition and historical development of specific heat. Thermodynamic and solid state relationships are presented which include discussions about lattice specific heat and the effects of magnetic and superconducting transitions. Data sources for practical applications and methods of estimating specific heat for materials are also included. The chapter concludes with a section concerning the measurement of specific heat at low temperatures.
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Published: 01 June 1983
Figure 2.3 Specific heat of diamond calculated using (a) Einstein’s specific heat function and θ E = 1326 K, (b) Debye’s specific heat function and θ D = 2050 K, and (c) experimental data (o— Desnoyers and Morrison, 1958 ). Dashed lines indicate a T 3 temperature dependence
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Published: 01 July 2009
Fig. 4.21 Specific heat of beryllium as a function of temperature. Results from two different sources. Dashed line is for a brake grade of normal-purity block. Source: Pinto 1979b
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Published: 01 July 2009
Fig. 4.22 Specific heat of beryllium (per gram) as a function of temperature. Source: Lillie 1955
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Published: 01 July 2009
Fig. 4.23 Specific heat of beryllium as a function of temperature from four different sources for both solid and liquid regions. Source: Touloukian 1967
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Published: 01 July 2009
Fig. 4.24 Specific heat of beryllium covering a wide temperature range, from 40 to 2200 K. 1: 0 to 300 K, 99.5% Be, high-temperature extrusion of powder; 2: 600 to 2200 K, 99.8% Be, pulverized and tightly filled into ampoules; 3: 323 to 773 K, 99.8% Be, history not given. Source: Touloukin
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Published: 01 July 2009
Fig. 13.1 Specific heat of beryllium, titanium, magnesium, aluminum, and steel, plotted as a function of temperature. Source: Greenfield 1971
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in Fundamentals of Steel Heat Treatment[1]
> Practical Heat Treating<subtitle>Basic Principles</subtitle>
Published: 31 December 2020
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Published: 01 August 2015
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Published: 01 June 1983
Figure 2.1 Specific heat as a function of temperature for several types of material. Typical behaviors are illustrated for metals (aluminum, beryllium, and copper), semiconductors (carbon and silicon), an amorphous inorganic (Pyrex glass) ( Corruccini and Gniewek, 1960 ), and for an organic
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Published: 01 June 1983
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Published: 01 June 1983
Figure 2.10 Specific heat of NiSO 4 ·6H 2 O (Δ— Stout and Hadley, 1964 ) and holmium (▪— Lounasmaa, 1962 and □— van Kemper, Miedema, and Huiskamp, 1964 ) as a function of temperature. The observed Schottky effect is a result of cooperative electronic spin alignment in the case of NiSO 4 ·6H 2
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Published: 01 June 1983
Figure 2.12 Electronic specific heat for superconducting vanadium expressed as C ES / γT C vs. T C / T . Experimental data ( Corak, Goodman, Satterthwaite, and Wexler, 1954 ) are well represented by the energy-gap formula (---) over the entire temperature range whereas the T 3
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Published: 01 June 1983
Figure 2.13 Ratio of specific heat to molar volume and temperature as a function of T 2 for a composite of niobium wires. These data include the specific heat of the addenda. The specimen was cooled prior to application of a 0.1-T field ( McConville and Serin, 1964 ).
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Published: 01 June 1983
Figure 2.15 Components of total specific heat in copper. The cubic lattice term is dominate except at very low temperatures.
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Published: 01 June 1983
Figure 2.19 Specific heat of copper calculated using θ D = 310 K and θ D = 348 K. Experimental points (□— Sandenaw, 1959 ) are included for comparison. The electronic contribution (see Fig. 2.15 ) has been removed from the 5-K experimental point.
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Published: 01 June 1983
Figure 2.20 Specific heat as a function of temperature for five composite materials. The true shapes of the fiber-reinforced composite curves are somewhat uncertain because of the widely spaced data points. The calculated values for the polystyrene foam are based on 98 wt.% polystyrene and 2
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Published: 01 June 1983
Figure 3.26 Temperature dependence of the constant, Q 0 , relating specific heat to volume expansivity for the Cu-Ni system.
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Published: 01 June 1983
Figure 3.27 Dependence on composition of the constant Qo relating specific heat to volume expansivity for the Cu-Ni system.
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Published: 01 June 1983
Figure 9.16 Specific heat, C p , variations when cooling to 20 K and subsequently warming to higher temperatures. Total heat content of anomalous Δ C p ( C p dT ) is 39.3 kJ/kg for lithium and 38.9 kJ/kg for Li–0.95 at.% Mg. ( Martin 1960a , 1960b .)
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