21.09.2015 Views

Course No Course Title Credits

Heat & Mass Transfer - acharya ng ranga agricultural university

Heat & Mass Transfer - acharya ng ranga agricultural university

SHOW MORE
SHOW LESS
  • No tags were found...

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

μ = absolute or dynamic viscosity (kg/m. s, cP)<br />

c p = specific heat capacity (J/kg K,)<br />

k = thermal conductivity (W/m K)<br />

The Prandtl Number is often used in heat transfer and free and forced<br />

convection calculations.<br />

<strong>No</strong>te that whereas the Reynolds number and Grashof number are<br />

subscripted with a length scale variable, Prandtl number contains no such<br />

length scale in its definition and is dependent only on the fluid and the fluid<br />

state. As such, Prandtl number is often found in property tables alongside<br />

other properties such as viscosity and thermal conductivity.<br />

Typical values for Pr are:<br />

• around 0.015 for mercury<br />

• around 0.16-0.7 for mixtures of noble gases or noble gases with<br />

hydrogen<br />

• around 0.7-0.8 for air and many other gases,<br />

• between 4 and 5 for R-12 refrigerant<br />

• around 7 for water (At 20 degrees Celsius)<br />

• between 100 and 40,000 for engine oil<br />

• around 1 × 10 25 for Earth's mantle.<br />

For mercury, heat conduction is very effective compared to convection:<br />

thermal diffusivity is dominant. For engine oil, convection is very effective in<br />

transferring energy from an area, compared to pure conduction: momentum<br />

diffusivity is dominant.<br />

In heat transfer problems, the Prandtl number controls the relative<br />

thickness of the momentum and thermal boundary layers. When Pr is small, it<br />

means that the heat diffuses very quickly compared to the velocity<br />

(momentum). This means that for liquid metals the thickness of the thermal<br />

boundary layer is much bigger than the velocity boundary layer.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!