Plasma assisted cooling of hot surfaces on hypersonic vehicles

Kyle M. Hanquist, Iain D. Boyd

Research output: Contribution to journalArticlepeer-review

13 Scopus citations

Abstract

Electron transpiration cooling (ETC) is a proposed thermal management approach for the leading edges of hypersonic vehicles that utilizes thermionic emission to emit electrons to carry heat away from the surface. A modeling approach is presented for assessing ETC in a computational fluid dynamics (CFD) framework and is evaluated using previously completed experiments. The modeling approach presented includes developing boundary conditions to account for space-charge-limited emission to accurately determine the level of electron emission from the surface. The effectiveness of ETC for multiple test cases are investigated including sharp leading edges and blunt bodies. For each of these test cases, ETC affects the surface properties, most notably the surface temperature, suggesting that ETC occurs for bodies in thermally intense, ionized flows, no matter the shape of the leading edge. An approximate approach is also presented to assess ETC in an ionized flow and compares its cooling power to radiative cooling.

Original languageEnglish (US)
Article number00009
JournalFrontiers in Physics
Volume7
Issue numberFEB
DOIs
StatePublished - 2019
Externally publishedYes

Keywords

  • Computational fluid dynamics
  • Electron transpiration cooling
  • Hypersonics
  • Plasma sheath
  • Thermionic emission

ASJC Scopus subject areas

  • Biophysics
  • Materials Science (miscellaneous)
  • Mathematical Physics
  • Physics and Astronomy(all)
  • Physical and Theoretical Chemistry

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