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THERMAL PROPERTIES

THERMAL PROPERTIES. ISSUES TO ADDRESS. • How does a material respond to heat ?. • How do we define and measure... --heat capacity --coefficient of thermal expansion --thermal conductivity --thermal shock resistance. • How do ceramics, metals, and polymers rank?. 1.

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THERMAL PROPERTIES

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  1. THERMAL PROPERTIES ISSUES TO ADDRESS... • How does a material respond to heat? • How do we define and measure... --heat capacity --coefficient of thermal expansion --thermal conductivity --thermal shock resistance • How do ceramics, metals, and polymers rank? 1

  2. HEAT CAPACITY • General: The ability of a material to absorb heat. • Quantitative: The energy required to increase the temperature of the material. energy input (J/mol) heat capacity (J/mol-K) temperature change (K) • Two ways to measure heat capacity: -- Cp : Heat capacity at constant pressure. -- Cv : Heat capacity at constant volume. 2

  3. HEAT CAPACITY VS T • Heat capacity... --increases with temperature --reaches a limiting value of 3R Adapted from Fig. 19.2, Callister 6e. • Atomic view: --Energy is stored as atomic vibrations. --As T goes up, so does the avg. energy of atomic vibr. 3

  4. HEAT CAPACITY: COMPARISON • Why is cp significantly larger for polymers? Selected values from Table 19.1, Callister 6e. 4

  5. THERMAL EXPANSION • Materials change size when heating. coefficient of thermal expansion (1/K) • Atomic view: Mean bond length increases with T. Adapted from Fig. 19.3(a), Callister 6e. (Fig. 19.3(a) adapted from R.M. Rose, L.A. Shepard, and J. Wulff, The Structure and Properties of Materials, Vol. 4, Electronic Properties, John Wiley and Sons, Inc., 1966.) 5

  6. THERMAL EXPANSION: COMPARISON • Q: Why does a generally decrease with increasing bond energy? Selected values from Table 19.1, Callister 6e. 6

  7. THERMAL CONDUCTIVITY • General: The ability of a material to transfer heat. • Quantitative: temperature gradient heat flux (J/m2-s) thermal conductivity (J/m-K-s) • Atomic view: Atomic vibrations in hotter region carry energy (vibrations) to cooler regions. 7

  8. THERMAL CONDUCTIVITY: COMPARISON Selected values from Table 19.1, Callister 6e. 8

  9. EX: THERMAL STRESS • Occurs due to: --uneven heating/cooling --mismatch in thermal expansion. • Example Problem 17.1, p. 724, Callister 2e. --A brass rod is stress-free at room temperature (20C). --It is heated up, but prevented from lengthening. --At what T does the stress reach -172MPa? 100GPa 20 x 10-6 /C 20C -172MPa Answer: 106C 9

  10. THERMAL SHOCK RESISTANCE • Occurs due to: uneven heating/cooling. • Ex: Assume top thin layer is rapidly cooled from T1 to T2: Tension develops at surface Critical temperature difference for fracture (set s = sf) Temperature difference that can be produced by cooling: set equal • Result: • Large thermal shock resistance when is large. 10

  11. THERMAL PROTECTION SYSTEM • Application: Space Shuttle Orbiter Fig. 23.0, Callister 5e. (Fig. 23.0 courtesy the National Aeronautics and Space Administration. Fig. 19.2W, Callister 6e. (Fig. 19.2W adapted from L.J. Korb, C.A. Morant, R.M. Calland, and C.S. Thatcher, "The Shuttle Orbiter Thermal Protection System", Ceramic Bulletin, No. 11, Nov. 1981, p. 1189.) • Silica tiles (400-1260C): --large scale application --microstructure: ~90% porosity! Si fibers bonded to one another during heat treatment. Fig. 19.3W, Callister 5e. (Fig. 19.3W courtesy the National Aeronautics and Space Administration. Fig. 19.4W, Callister 5e. (Fig. 219.4W courtesy Lockheed Aerospace Ceramics Systems, Sunnyvale, CA.) 11

  12. SUMMARY • A material responds to heat by: --increased vibrational energy --redistribution of this energy to achieve thermal equil. • Heat capacity: --energy required to increase a unit mass by a unit T. --polymers have the largest values. • Coefficient of thermal expansion: --the stress-free strain induced by heating by a unit T. --polymers have the largest values. • Thermal conductivity: --the ability of a material to transfer heat. --metals have the largest values. • Thermal shock resistance: --the ability of a material to be rapidly cooled and not crack. Maximize sfk/Ea. 12

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