dc.contributor.advisor | Cizmas, Paul G. A. | |
dc.creator | Carpenter IV, Forrest Lafon | |
dc.date.accessioned | 2016-09-22T19:48:04Z | |
dc.date.available | 2018-08-01T05:58:16Z | |
dc.date.created | 2016-08 | |
dc.date.issued | 2016-07-15 | |
dc.date.submitted | August 2016 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/158055 | |
dc.description.abstract | The following dissertation examines several aspects of numerical simulations for turbomachinery flows modeled with an in-house Reynolds-averaged Navier-Stokes solver. The impact of the turbulence model on the solution is also explored in this work. Additionally, the effects of different solution limiters, including both a new and modified limiter, are examined.
This dissertation also presents a new grid generator that was tailored for turbomachinery geometries. The grid generator uses a combination of structured grid blocks to discretize a single blade passage domain. Structured grid blocks can also be placed at the blade tip, allowing for the modelling of tip leakage flows.
A number of canonical cases were used to validate the additions and modifications to the flow solver. Among these cases were the inviscid flow through a convergent-divergent nozzle and a turbulent flat plate. It is shown that the new and modified limiters perform similarly to the existing limiter functions, and in some cases, out-perform their predecessors.
The flow solver is further validated against two turbomachinery cases: an annular turbine vane and a transonic fan. Comparisons with experimental data are made in both cases. The effects of turbulent inlet conditions and the under-relaxation of the turbulence equations are examined for the turbine vane geometry. Two novel rubbing configurations are presented and examined in the turbulent transonic fan case. Additionally, a transonic fan case, which includes the tip leakage flow, is also presented and compared against the rubbing cases. | en |
dc.format.mimetype | application/pdf | |
dc.language.iso | en | |
dc.subject | Computational Fluid Dynamcs | en |
dc.subject | Turbomachinery | en |
dc.title | Practical Aspects of Computational Fluid Dynamics for Turbomachinery | en |
dc.type | Thesis | en |
thesis.degree.department | Aerospace Engineering | en |
thesis.degree.discipline | Aerospace Engineering | en |
thesis.degree.grantor | Texas A & M University | en |
thesis.degree.name | Doctor of Philosophy | en |
thesis.degree.level | Doctoral | en |
dc.contributor.committeeMember | Rediniotis, Othon | |
dc.contributor.committeeMember | Carlson, Leland | |
dc.contributor.committeeMember | Guermond, Jean-Luc | |
dc.type.material | text | en |
dc.date.updated | 2016-09-22T19:48:05Z | |
local.embargo.terms | 2018-08-01 | |
local.etdauthor.orcid | 0000-0002-9336-8669 | |