On the transfer of heat in a cavity at high and low speeds

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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


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