Show simple item record

dc.contributor.authorMoses, Hal Lynwooden_US
dc.contributor.authorChappell, John R.en_US
dc.contributor.authorGoldberger, Tomasen_US
dc.contributor.otherDavid W. Taylor Model Basinen_US
dc.contributor.otherUnited States. Navy Department. Bureau of Ships. Fundamental Hydromechanics Research Programen_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:21:55Z
dc.date.available2016-10-06T21:21:55Z
dc.date.issued1965en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104679
dc.descriptionSeptember 1965en_US
dc.descriptionIncludes bibliographical referencesen_US
dc.description.abstractAn investigation of incompressible turbulent boundary layer separation in internal flow is presented with experimental results for a variable geometry, two-dimensional diffuser and two conical diffusers. A simple analytical model is adopted, which consists of wall boundary layers and a one-dimensional, inviscid core. Several approximate boundary layer methods and the possibility of extending them into the separated region are examined. With a limited amount of separated flow, the calculated pressure agrees reasonably well with the experimental results and gives a fair indication of maximum diffuser performance. The limitations of the model to the more general problem, as well as the problem of singularities and downstream stability, are discussed.en_US
dc.description.sponsorship"Research was carried out under the Bureau of Ships Fundamental Hydromechanics Research Program, and administered by the David Taylor Model Basin Contract S-R009 01 01 Nonr-1841(91)."en_US
dc.format.extent1 volume ([68] pages in various pagings)en_US
dc.publisherCambridge, Mass. : Gas Turbine Laboratory, Massachusetts Institute of Technology, [1965]en_US
dc.relation.ispartofseriesGTL report #81en_US
dc.subject.lccTJ267.A1 M37 no.81en_US
dc.subject.lccTL574.B6 M67 1964en_US
dc.subject.lcshBoundary layeren_US
dc.subject.lcshDiffusersen_US
dc.titleBoundary layer separation in internal flowen_US
dc.typeTechnical Reporten_US
dc.identifier.oclc09165401en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record