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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