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Prandtl number

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Pr \equiv \frac{\mu C_p}{k}
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Pr = \frac{\mu C_p}{k}
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* <math>C_p</math> is the specific heat at constant pressure
* <math>C_p</math> is the specific heat at constant pressure
* <math>k</math> is the coefficient of thermal conduction
* <math>k</math> is the coefficient of thermal conduction
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It is the ratio of momentum diffusivity (kinematic viscosity) to thermal diffusivity. It can be related to the thickness of the thermal and velocity boundary layers. It is actually the ratio of velocity boundary layer to thermal boundary layer. When Pr=1, the boundary layers coincide. When Pr is small, it means that heat diffuses very quickly compared to the velocity (momentum). This means the thickness of the thermal boundary layer is much bigger than the velocity boundary layer for liquid metals.
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[[Category: Dimensionless parameters]]
[[Category: Dimensionless parameters]]

Revision as of 06:03, 20 December 2005

The Prandtl number is defined as


Pr = \frac{\mu C_p}{k}

where

  • \mu is the dynamic viscosity coefficient
  • C_p is the specific heat at constant pressure
  • k is the coefficient of thermal conduction


It is the ratio of momentum diffusivity (kinematic viscosity) to thermal diffusivity. It can be related to the thickness of the thermal and velocity boundary layers. It is actually the ratio of velocity boundary layer to thermal boundary layer. When Pr=1, the boundary layers coincide. When Pr is small, it means that heat diffuses very quickly compared to the velocity (momentum). This means the thickness of the thermal boundary layer is much bigger than the velocity boundary layer for liquid metals.

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