The laminar boundary layer in slip flow

dc.contributor.authorNonweiler, T.
dc.date.accessioned2012-07-27T14:48:45Z
dc.date.available2012-07-27T14:48:45Z
dc.date.issued1952-11
dc.description.abstractThis report discusses the effects of the existence of a small, but finite, molecular mean-free-path on the steady air flow in the laminar boundary later. The boundary conditions at the exposed surface are modified by the existence of a slip velocity and temperature-jump between the air and the surface, and a theory of first-order approximation is developed to account for the consequent modification to the shear stress and heat flux to the surface. Continues…en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7446
dc.language.isoenen_UK
dc.publisherCollege of Aeronuatics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries62en_UK
dc.titleThe laminar boundary layer in slip flowen_UK
dc.typeReporten_UK

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