Show simple item record

dc.contributor.authorNice, George Rolanden_US
dc.contributor.authorTseng, W.-Y. (Wu-Yang)en_US
dc.contributor.authorMoses, Hal Lynwooden_US
dc.contributor.otherMassachusetts Institute of Technology. Gas Turbine Laboratoryen_US
dc.date.accessioned2016-10-06T21:22:19Z
dc.date.available2016-10-06T21:22:19Z
dc.date.issued1966en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/104740
dc.descriptionOctober 1966en_US
dc.descriptionIncludes bibliographical referencesen_US
dc.description.abstractAn experimental investigation of turbulent, incompressible flow separation over curved and sharp, backward-facing steps is presented with results for various step heights. Mean velocities in the separating boundary layer as well as the downstream shear layer were recorded. The static pressure in the separated region was determined with a spherical probe. With the curved step, the boundary layer separated at approximately 28 degrees: the reattachment lengths were somewhat less and the base pressures slightly higher than those with the sharp step.en_US
dc.description.sponsorshipResearch carried out under Bureau of Ships General Hydromechanics Research Program, administered by the David Taylor Model Basin contract S-R009 01 01 Nonr 1841(91)en_US
dc.format.extent[43] pages in various pagingsen_US
dc.publisherCambridge, Mass. : Massachusetts Institute of Technology, Gas Turbine Laboratory, [1966]en_US
dc.relation.ispartofseriesGTL report #87en_US
dc.subject.lccTJ267.A1 M37 no.87en_US
dc.subject.lcshTurbulenceen_US
dc.subject.lcshBoundary layeren_US
dc.subject.lcshPressureen_US
dc.titleSeparation of turbulent, incompressible flow from a curved, backward-facing stepen_US
dc.typeTechnical Reporten_US
dc.identifier.oclc227430185en_US
dc.identifier.oclc09165611en_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record