A recently developed Shastry formalism for energy transport is used to analyze the temporal behavior of the energy and heat transport in metals. Comparison with Cattaneo’s equation is performed. Both models show the transition between ballistic and diffusive regimes. Furthermore, because the new model considers the discrete character of the lattice, it highlights some new phenomena such as oscillations in the energy transport at very short time scales. The energy relaxation of the conduction band electrons in metals is considered to be governed by the electron-phonon scattering, and the scattering time is taken to be averaged over the Fermi surface. Using the new formalism, one can quantify the transfer from ballistic modes to diffusive ones as energy propagates in the material and it is transformed into heat. While the diffusive contribution shows an almost exponentially decaying behavior with time, the non-diffusive part shows a damped oscillating behavior. The origin of this oscillation will be discussed as well as the effect of temperature on the dynamics of the energy modes transport.
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ASME 2009 Heat Transfer Summer Conference collocated with the InterPACK09 and 3rd Energy Sustainability Conferences
July 19–23, 2009
San Francisco, California, USA
Conference Sponsors:
- Heat Transfer Division
ISBN:
978-0-7918-4357-4
PROCEEDINGS PAPER
Transient Energy and Heat Transport in Metals Available to Purchase
Y. Ezzahri,
Y. Ezzahri
University of California at Santa Cruz, Santa Cruz, CA
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A. Shakouri
A. Shakouri
University of California at Santa Cruz, Santa Cruz, CA
Search for other works by this author on:
Y. Ezzahri
University of California at Santa Cruz, Santa Cruz, CA
A. Shakouri
University of California at Santa Cruz, Santa Cruz, CA
Paper No:
HT2009-88280, pp. 217-226; 10 pages
Published Online:
March 12, 2010
Citation
Ezzahri, Y, & Shakouri, A. "Transient Energy and Heat Transport in Metals." Proceedings of the ASME 2009 Heat Transfer Summer Conference collocated with the InterPACK09 and 3rd Energy Sustainability Conferences. Volume 2: Theory and Fundamental Research; Aerospace Heat Transfer; Gas Turbine Heat Transfer; Computational Heat Transfer. San Francisco, California, USA. July 19–23, 2009. pp. 217-226. ASME. https://doi.org/10.1115/HT2009-88280
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