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Please use this identifier to cite or link to this item: http://arks.princeton.edu/ark:/88435/dsp013r074v10j
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dc.contributor.advisorSmits, Alexander Jen_US
dc.contributor.authorVallikivi, Margiten_US
dc.contributor.otherMechanical and Aerospace Engineering Departmenten_US
dc.date.accessioned2014-06-05T19:46:48Z-
dc.date.available2014-06-05T19:46:48Z-
dc.date.issued2014en_US
dc.identifier.urihttp://arks.princeton.edu/ark:/88435/dsp013r074v10j-
dc.description.abstractMeasurements are reported that give new insight into the behavior of turbulent wall-bounded flows at high Reynolds number. Turbulent pipe and boundary layer flows are examined experimentally over a wide range of Reynolds numbers - up to Re&tau;=100,000 (ReD=6&times;10<super>6</super>) in pipe flow, and up to Re&tau;=73,000 (ReD=235&times;10<super>3</super>) in a flat plate zero pressure gradient boundary layer. A Nano-Scale Thermal Anemometry Probe (NSTAP) was developed for very high spatial and temporal resolution measurements. Sensors with wire lengths 30 and 60 &mu;m were fabricated, tested and validated in known flows, and then used to obtain single-point measurements at high Reynolds numbers in pipe and boundary layers. The mean velocity data together with data from previous studies and extensive error analysis showed that the von K´arm´an's constant in the log-law is &kappa;=0.40&plusmn;0.02. It was shown that the streamwise Reynolds stress exhibits a logarithmic behavior in the inertial sublayer for Re&tau;&ge;20,000, in both pipes and boundary layers. Variances as well as higher order even moments were compared for pipes and boundary layers and it was shown that all even moments have a logarithmic behavior in the inertial sublayer, suggesting a true scale separation. Streamwise turbulent spectra showed a clear k<super>-5/3</super> region for up to two decades in wavenumber. No k<super>-1</super> region was found to be present in any of the cases in the pipe or the boundary layer. The location of the outer spectral peak, associated with very large scale motions, was found to have only a weak dependence on Reynolds number. The loci of these peak occur at the same wall-normal distance where the streamwise stresses establish a logarithmic behavior and where the amplitude modulation coefficient has a zero value. This suggests that with Reynolds number increasing to infinity most of the energy is contained within a diminishing wall-layer in physical coordinates.en_US
dc.language.isoenen_US
dc.publisherPrinceton, NJ : Princeton Universityen_US
dc.relation.isformatofThe Mudd Manuscript Library retains one bound copy of each dissertation. Search for these copies in the <a href=http://catalog.princeton.edu> library's main catalog </a>en_US
dc.subjectanemometryen_US
dc.subjectboundary layersen_US
dc.subjecthigh Reynolds numbersen_US
dc.subjectpipe flowen_US
dc.subjectsensorsen_US
dc.subjectturbulenceen_US
dc.subject.classificationAerospace engineeringen_US
dc.subject.classificationMechanical engineeringen_US
dc.subject.classificationElectrical engineeringen_US
dc.titleWall-bounded turbulence at high Reynolds numbersen_US
dc.typeAcademic dissertations (Ph.D.)en_US
pu.projectgrantnumber690-2143en_US
Appears in Collections:Mechanical and Aerospace Engineering

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