Mass-flux fraction

Ratio of mass-flux of chemical species to total mass flux

The mass-flux fraction (or Hirschfelder-Curtiss variable or Kármán-Penner variable) is the ratio of mass-flux of a particular chemical species to the total mass flux of a gaseous mixture. It includes both the convectional mass flux and the diffusional mass flux. It was introduced by Joseph O. Hirschfelder and Charles F. Curtiss in 1948[1] and later by Theodore von Kármán and Sol Penner in 1954.[2][3] The mass-flux fraction of a species i is defined as[4]

ϵ i = ρ i ( v + V i ) ρ v = Y i ( 1 + V i v ) {\displaystyle \epsilon _{i}={\frac {\rho _{i}(v+V_{i})}{\rho v}}=Y_{i}\left(1+{\frac {V_{i}}{v}}\right)}

where

  • Y i = ρ i / ρ {\displaystyle Y_{i}=\rho _{i}/\rho } is the mass fraction
  • v {\displaystyle v} is the mass average velocity of the gaseous mixture
  • V i {\displaystyle V_{i}} is the average velocity with which the species i diffuse relative to v {\displaystyle v}
  • ρ i {\displaystyle \rho _{i}} is the density of species i
  • ρ {\displaystyle \rho } is the gas density.

It satisfies the identity

i ϵ i = 1 {\displaystyle \sum _{i}\epsilon _{i}=1} ,

similar to the mass fraction, but the mass-flux fraction can take both positive and negative values. This variable is used in steady, one-dimensional combustion problems in place of the mass fraction.[5] For one-dimensional ( x {\displaystyle x} direction) steady flows, the conservation equation for the mass-flux fraction reduces to

d ϵ i d x = w i ρ v {\displaystyle {\frac {d\epsilon _{i}}{dx}}={\frac {w_{i}}{\rho v}}} ,

where w i {\displaystyle w_{i}} is the mass production rate of species i.

References

  1. ^ Hirschfelder, J. O., & Curtiss, C. F. (1948, January). Theory of propagation of flames. Part I: General equations. In Symposium on Combustion and Flame, and Explosion Phenomena (Vol. 3, No. 1, pp. 121-127). Elsevier.
  2. ^ von Karman, T., & Penner, S. S. (1954). Fundamental approach to laminar flame propagation.
  3. ^ von Karman, T., & Penner, S. S. (1954). The thermal theory of constant-pressure deflagration for first-order global reactions.
  4. ^ Williams, F. A. (2018). Combustion theory. CRC Press.
  5. ^ Penner, S. S. (1957). Chemistry problems in jet propulsion (Vol. 1). Pergamon Press.