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The influence of super gravity on flow and heat transfer characteristics in straight microchannel

  • Beihang University

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

High maneuverability has been a major performance index bf modern military combat flight. Thus, the avionics installed on the flight will frequently suffer the effects of acceleration. The flow and heat dissipation performance of avionics heat Bink will be affected by the super gravity environment. In order to clarify the effects of acceleration, simulative accelerating experiments of flow and heat transfer performance in straight microchannel with rectangular cross section have been conducted. A test piece made of copper is machined. FC-72 is taken as coolant. Simulative accelerating equipment is set up, on which the test piece is installed. Several different acceleration conditions are applied in the experiment. The resulting centripetal acceleration ranged from Og to 15g. Tests are ponducted by varying heat load, flow flux, and microchannel orientation relative to the direction of the accelerating force. In this study, new experimental data is presented. The flow and heat transfer performance in straight microchannel under the effects of acceleration is analyzed. The result shows that the directions and amplitudes of the acceleration have great effects on flow and heat transfer performance in the channel.

Original languageEnglish
Title of host publicationProceedings of the ASME Micro/Nanoscale Heat and Mass Transfer International Conference 2009, MNHMT2009
Pages85-92
Number of pages8
DOIs
StatePublished - 2010
EventASME 2009 Micro/Nanoscale Heat and Mass Transfer International Conference 2009, MNHMT2009 - Shanghai, China
Duration: 18 Dec 2009 → 21 Dec 2009

Publication series

NameProceedings of the ASME Micro/Nanoscale Heat and Mass Transfer International Conference 2009, MNHMT2009
Volume3

Conference

ConferenceASME 2009 Micro/Nanoscale Heat and Mass Transfer International Conference 2009, MNHMT2009
Country/TerritoryChina
CityShanghai
Period18/12/09 → 21/12/09

Keywords

  • Avionics heat sink
  • Experimental study
  • Flow
  • Heat transfer
  • Microchannel
  • Super gravity

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