Primitive numerical simulation of circular Couette flow

dc.contributor.advisor James D. Iversen
dc.contributor.author Hasiuk, Jan
dc.contributor.department Department of Aerospace Engineering
dc.date 2018-08-16T17:16:52.000
dc.date.accessioned 2020-07-02T06:12:53Z
dc.date.available 2020-07-02T06:12:53Z
dc.date.copyright Fri Jan 01 00:00:00 UTC 1988
dc.date.issued 1988
dc.description.abstract <p>The azimuthal-invariant, 3-d cylindrical, incompressible Navier-Stokes equations are solved to steady state for a finite-length, physically realistic model. The numerical method relies on an alternating-direction implicit (ADI) scheme that is formally second-order accurate in space and first-order accurate in time. The equations are linearized and uncoupled by evaluating variable coefficients at the previous time iteration. Wall grid clustering is provided by a Roberts transformation in radial and axial directions. A vorticity-velocity formulation is found to be preferable to a vorticity-streamfunction approach. Subject to no-slip, Dirichlet boundary conditions, except for the inner cylinder rotation velocity (impulsive start-up) and zero-flow initial conditions, nonturbulent solutions are obtained for sub- and supercritical Reynolds numbers of 100 to 400 for a finite geometry where R[subscript] outer/R[subscript] inner = 1.5, H/R[subscript] inner = 0.73 and H/[delta]R = 1.5. An axially-stretched model solution is shown to asymptotically approach the 1-d analytic Couette solution at the cylinder midheight. Flowfield change from laminar to Taylor-vortex flow is discussed as a function of Reynolds number. Three-dimensional velocities, vorticity and streamfunction are presented via 2-d graphs and 3-d surface and contour plots. A Prandtl-Van Driest turbulence model based on an effective isotropic eddy viscosity hypothesis was applied resulting in accurate 1-d turbulent flow solutions assuming long cylinders. A small aspect ratio correction factor was empirically determined. Comparisons to experiment are very good. Extending the nonturbulent analysis, 3-d turbulent flow equations are developed for Prandtl-Van Driest and energy-dissipation turbulence models. The energy-dissipation model includes corrections for streamline curvature, system rotation and low-Re effects. Solutions of the 3-d equations involve current work in progress.</p>
dc.format.mimetype application/pdf
dc.identifier archive/lib.dr.iastate.edu/rtd/9349/
dc.identifier.articleid 10348
dc.identifier.contextkey 6356003
dc.identifier.doi https://doi.org/10.31274/rtd-180813-11111
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath rtd/9349
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/82438
dc.language.iso en
dc.source.bitstream archive/lib.dr.iastate.edu/rtd/9349/r_8825399.pdf|||Sat Jan 15 02:31:51 UTC 2022
dc.subject.disciplines Aerospace Engineering
dc.subject.keywords Aerospace engineering
dc.title Primitive numerical simulation of circular Couette flow
dc.type dissertation
dc.type.genre dissertation
dspace.entity.type Publication
relation.isOrgUnitOfPublication 047b23ca-7bd7-4194-b084-c4181d33d95d
thesis.degree.level dissertation
thesis.degree.name Doctor of Philosophy
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