Heat flux correlation for high-speed flow in the transitional regime

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Abstract

An analytical correlation is developed for stagnation-point heat flux on spherical objects travelling at high velocity which is accurate for conditions ranging from the continuum to the free-molecular flow regime. Theoretical analysis of the Burnett and super-Burnett equations is performed using simplifications from shock-wave and boundary-layer theory to determine the relative contribution of higher-order heat flux terms compared with the Fourier heat flux (assumed in the Navier-Stokes equations). A rarefaction parameter (Wr = M / Re), based on the free-stream Mach number (M), the Reynolds number (Re) and the viscosity-temperature index (ω), is identified as a better correlating parameter than the Knudsen number in the transition regime. By studying both the Burnett and super-Burnett equations, a general form for the entire series of higher-order heat flux contributions is obtained. The resulting heat flux expression includes terms with dependence on gas properties, stagnation to wall-temperature ratio and a main dependence on powers of the rarefaction parameter Wr. The expression is applied as a correction to the Fourier heat flux and therefore can be combined with any continuum-based correlation of choice. In the free-molecular limit, a bridging function is used to ensure consistency with well-established free-molecular flow theory. The correlation is then fitted to direct simulation Monte Carlo (DSMC) solutions for stagnation-point heat flux in high-speed nitrogen flows. The correlation is shown to accurately capture the variation in heat flux predicted by the DSMC method in the transition flow regime, while limiting to both continuum and free-molecular values.

Original languageEnglish (US)
Pages (from-to)981-996
Number of pages16
JournalJournal of Fluid Mechanics
Volume792
DOIs
StatePublished - Apr 10 2016

Keywords

  • aerodynamics
  • compressible flows
  • rarefied gas flow

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