A simplified theory of skin friction and heat transfer for a compressible laminar boundary layer

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dc.contributor.authorLilley, G. M.
dc.date.accessioned2017-03-06T11:10:32Z
dc.date.available2017-03-06T11:10:32Z
dc.date.issued1959-01
dc.description.abstractThe compressible laminar boundary layer equations for a perfect gas in steady flow at arbitrary external Mach number and wall temperature distribution are solved approximately by the combined use of the Stewartson- Illingworth transformation and application of Lighthill's method to yield the shin friction and rate of heat transfer. Appendices are added which give the necessary modifications to the method for the separate cases of very low Prandtl number and for the flow near a separation point. A further appendix describes Spalding's method for improving the accuracy of the wall value of shear stress and rate of heat transfer distributions along a wall having a non-uniform temperature distribution.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/11568
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N-93en_UK
dc.relation.ispartofseries93en_UK
dc.titleA simplified theory of skin friction and heat transfer for a compressible laminar boundary layeren_UK
dc.typeReporten_UK

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CoA. Notes (1952-1969)