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The momentum transfer of incompressible turbulent separated flow due to cavities with steps
dc.contributor.advisor | Norton, D. J. | |
dc.creator | White, Robert Earl | |
dc.date.accessioned | 2020-08-21T22:03:59Z | |
dc.date.available | 2020-08-21T22:03:59Z | |
dc.date.issued | 1977 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/DISSERTATIONS-624014 | |
dc.description | Vita. | en |
dc.description.abstract | An 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.extent | xv, 247 leaves | en |
dc.format.medium | electronic | en |
dc.format.mimetype | application/pdf | |
dc.language.iso | eng | |
dc.rights | This 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.uri | http://rightsstatements.org/vocab/InC/1.0/ | |
dc.subject | Aerodynamics | en |
dc.subject | Cavities (Airplanes) | en |
dc.subject | Drag (Aerodynamics) | en |
dc.subject | Turbulent boundary layer | en |
dc.subject | Major aerospace engineering | en |
dc.subject.classification | 1977 Dissertation W587 | |
dc.subject.lcsh | Turbulent boundary layer | en |
dc.subject.lcsh | Cavities (Airplanes) | en |
dc.subject.lcsh | Aerodynamics | en |
dc.subject.lcsh | Drag (Aerodynamics) | en |
dc.title | The momentum transfer of incompressible turbulent separated flow due to cavities with steps | en |
dc.type | Thesis | en |
thesis.degree.grantor | Texas A&M University | en |
thesis.degree.name | Doctor of Philosophy | en |
dc.type.genre | dissertations | en |
dc.type.material | text | en |
dc.format.digitalOrigin | reformatted digital | en |
dc.publisher.digital | Texas A&M University. Libraries | |
dc.identifier.oclc | 4087493 |
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