dc.contributor.author |
R. D. Mills |
en_US |
dc.date.accessioned |
2014-10-21T15:56:26Z |
|
dc.date.available |
2014-10-21T15:56:26Z |
|
dc.date.issued |
1964 |
en_US |
dc.identifier.other |
ARC/R&M-3428 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4012 |
|
dc.description.abstract |
The transfer of heat between a fluid and a cavity in a solid surface over which it flows is discussed from the viewpoint of the closed 'inner boundary layer'. A (constant pressure) integral condition is derived from the energy equation which specifies the net flux of heat through the cavity at all Mach numbers. For a simplified viscosity-temperature function, velocity and temperature profiles are obtained as functions of Mach number and Prandtl number, while heat-transfer coefficients are developed in terms of these parameters. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
On the transfer of heat in a cavity at high and low speeds |
en_US |