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dc.contributor.advisorNorton, D. J.
dc.creatorWhite, Robert Earl
dc.date.accessioned2020-08-21T22:03:59Z
dc.date.available2020-08-21T22:03:59Z
dc.date.issued1977
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-624014
dc.descriptionVita.en
dc.description.abstractAn experimental study was conducted using a plate test bed having a turbulent boundary layer to determine the momentum transfer to the faces of step/cavity excrecences on the plate. Tested configurations include an isolated excrecence and an array of blocks in tile patterns. A momentum transfer correlation model of pressure forces on an isolated step/cavity was developed with experimental results to relate flow and geometry parameters. Results of the experiments reveal that isolated step/cavity excrecences do not have a unique and unifying parameter group due in part to cavity depth effects and in part to width parameter scale effects. Drag predictions for tile patterns by a kinetic pressure empirical method predict experimental results w ell. Trends were not, however, predicted by a method of variable roughness density phenomenology. Data presented will be helpful in testing formal numerical solutions over a step/cavity excrecence, and correlations permit drag predictions on like configurations.en
dc.format.extentxv, 247 leavesen
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectAerodynamicsen
dc.subjectCavities (Airplanes)en
dc.subjectDrag (Aerodynamics)en
dc.subjectTurbulent boundary layeren
dc.subjectMajor aerospace engineeringen
dc.subject.classification1977 Dissertation W587
dc.subject.lcshTurbulent boundary layeren
dc.subject.lcshCavities (Airplanes)en
dc.subject.lcshAerodynamicsen
dc.subject.lcshDrag (Aerodynamics)en
dc.titleThe momentum transfer of incompressible turbulent separated flow due to cavities with stepsen
dc.typeThesisen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
dc.type.genredissertationsen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen
dc.publisher.digitalTexas A&M University. Libraries
dc.identifier.oclc4087493


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