Samiksha Jaiswal (Editor)

Stanton number

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The Stanton number, St, is a dimensionless number that measures the ratio of heat transferred into a fluid to the thermal capacity of fluid. The Stanton number is named after Thomas Edward Stanton (1865–1931). It is used to characterize heat transfer in forced convection flows.

Contents

S t = h G c p = h ρ u c p

where

  • h = convection heat transfer coefficient
  • ρ = density of the fluid
  • cp = specific heat of the fluid
  • u = speed of the fluid
  • It can also be represented in terms of the fluid's Nusselt, Reynolds, and Prandtl numbers:

    S t = N u R e P r

    where

  • Nu is the Nusselt number;
  • Re is the Reynolds number;
  • Pr is the Prandtl number.
  • The Stanton number arises in the consideration of the geometric similarity of the momentum boundary layer and the thermal boundary layer, where it can be used to express a relationship between the shear force at the wall (due to viscous drag) and the total heat transfer at the wall (due to thermal diffusivity).

    Mass Transfer

    Using the heat-mass transfer analogy, a mass transfer St equivalent can be found using the Sherwood number and Schmidt number in place of the Nusselt number and Prandtl number, respectively.

    S t m = S h R e S c

    S t m = h m ρ m u

    where

  • St_m is the mass Stanton number;
  • Sh is the Sherwood number;
  • Re is the Reynolds number;
  • Sc is the Schmidt number;
  • h m is defined based on a concentration difference (kg s−1 m−2);
  • ρ m is the component density of the species in flux.
  • Boundary Layer Flow

    The Stanton number is a useful measure of the rate of change of the thermal energy deficit (or excess) in the boundary layer due to heat transfer from a planar surface. If the enthalpy thickness is defined as

    Δ 2 = 0 ρ u ρ u T T T s T d y

    Then the Stanton number is equivalent to

    S t = d Δ 2 d x

    for boundary layer flow over a flat plate with a constant surface temperature and properties.

    Correlations using Reynolds-Colburn Analogy

    Using the Reynolds-Colburn analogy for turbulent flow with a thermal log and viscous sub layer model, the following correlation for turbulent heat transfer for is applicable

    S t = C f / 2 1 + 12.8 ( P r 0.68 1 ) C f / 2

    where

    C f = 0.455 [ l n ( 0.06 R e x ) ] 2

    References

    Stanton number Wikipedia