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dc.contributor.advisorLigrani, Phillip M.
dc.contributor.advisorSubramanian, Chelakara S.
dc.contributor.authorMitchell, Stephen W.
dc.date1990
dc.date.accessioned2013-12-16T23:09:54Z
dc.date.available2013-12-16T23:09:54Z
dc.description.abstractThe effects of embedded longitudinal vortices on film cooling injectant from one row and two rows of holes with compound angles are investigated. Holes are designed such that their angle from the test surface is 30 degrees in a spanwise/normal plane projection, and 35 degrees in a streamwise/normal plane projection. A blowing ratio of 0.5, non-dimensional injection temperature parameters of 1.29 to 1.38, and freestream velocity of 10 m/s are employed. As the spanwise position of the vortex is altered. Stanton Numbers change considerably depending upon which portion of each vortex is proximate to film injection holes. These variations are vastly different depending on whether or nor spanwise components of vortex secondary flows are opposed or aligned with the spanwise direction of the injectant. Mean velocity surveys, injection distribution surveys, and flow visualization results are also discussed.en_US
dc.description.urihttp://archive.org/details/theeffectsofembe1094537993
dc.format.extentxviii, 237 p.: ill.en_US
dc.language.isoen_US
dc.publisherMonterey, California. Naval Postgraduate Schoolen_US
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleThe Effects of Embedded Vortices on Heat Transfer in a Turbulent Boundary Layer with Film Cooling from Holes with Compound Anglesen_US
dc.typeThesisen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentMechanical Engineering
dc.subject.authorCompound Angle Injectionen_US
dc.subject.authorEmbedded Vorticesen_US
dc.subject.authorFilm-coolingen_US
dc.subject.authorTurbulent Boundary Layeren_US
dc.subject.authorMechanical engineeringen_US
dc.subject.authorAerial reconnaissanceen_US
dc.description.serviceLieutenant, United States Navyen_US
etd.thesisdegree.nameM.S. in Mechanical Engineeringen_US
etd.thesisdegree.levelMastersen_US
etd.thesisdegree.grantorNaval Postgraduate Schoolen_US
dc.description.distributionstatementApproved for public release; distribution is unlimited.


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