| 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 |