Shock reflection and surface effects in the shock tube

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dc.contributor.authorBusing, J. R.
dc.contributor.authorClarke, John F.
dc.date.accessioned2015-09-01T14:29:59Z
dc.date.available2015-09-01T14:29:59Z
dc.date.issued1966
dc.description.abstractA thin-film resistance thermometer, mounted on the end-wall of a shock tube, is used to record surface temperatures and heat transfer rates following reflection of the primary shock wave. This information is combined with the results of theoretical investigations to produce simultaneous information about surface accommodation effects and gas thermal conductivities at high pressures and moderate temperatures.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/9367
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseries101en_UK
dc.relation.ispartofseriesCOA/M-101en_UK
dc.titleShock reflection and surface effects in the shock tubeen_UK
dc.typeReporten_UK

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