In the modeling of a uniformly distributed band heat flux region experiencing constant acceleration from rest over a half-space surface, it is found that the maximum surface temperature at the instantaneous speed and the corresponding Peclet number are already well approximated by the long-established steady-state constant-speed models very soon after the moment the flux region clears the overlap of its original footprint at the initiation of motion. During startup when the flux still overlaps its original footprint, maximum temperature at any instant given the level of flux is well approximated by a simple one-dimensional conduction problem with a correspondingly stationary heat flux initiating at time zero. The above acceleration behaviors are observed regardless of whether the uniform flux is constant or Coulombic (proportional to instantaneous speed as frictional heating), though during the initial startup the maximum temperature rise in the Coulombic case is only two-thirds that of the constant flux case. The case of constant deceleration was additionally modeled, where at the eventual instant of halt, the maximum temperature in the case of constant flux was found to be directly proportional to the rate of deceleration to the 1/4 power, whereas in the case of Coulombic flux it was found that maximum temperature was instead inversely proportional to the rate of deceleration.
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Research-Article
Analysis of Surface Temperatures Within Heat Flux Bands During Constant Acceleration Including Deceleration to Halt
Thierry A. Blanchet,
Thierry A. Blanchet
Department of Mechanical, Aerospace
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
e-mail: blanct@rpi.edu
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
e-mail: blanct@rpi.edu
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Shane P. Lenihan
Shane P. Lenihan
Department of Mechanical, Aerospace
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
Search for other works by this author on:
Thierry A. Blanchet
Department of Mechanical, Aerospace
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
e-mail: blanct@rpi.edu
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
e-mail: blanct@rpi.edu
Shane P. Lenihan
Department of Mechanical, Aerospace
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
and Nuclear Engineering,
Rensselaer Polytechnic Institute,
Troy, NY 12180
1Corresponding author.
Contributed by the Tribology Division of ASME for publication in the JOURNAL OF TRIBOLOGY. Manuscript received May 26, 2016; final manuscript received August 8, 2016; published online January 10, 2017. Assoc. Editor: Sinan Muftu.
J. Tribol. May 2017, 139(3): 031102 (10 pages)
Published Online: January 10, 2017
Article history
Received:
May 26, 2016
Revised:
August 8, 2016
Citation
Blanchet, T. A., and Lenihan, S. P. (January 10, 2017). "Analysis of Surface Temperatures Within Heat Flux Bands During Constant Acceleration Including Deceleration to Halt." ASME. J. Tribol. May 2017; 139(3): 031102. https://doi.org/10.1115/1.4034532
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