Coping with shock : numerical procedure for the detection and sorting of shocks in fluid flows
dc.rights.license | CC BY-NC-ND. Users may download and share copies with attribution in accordance with a Creative Commons Attribution-Noncommercial-No Derivative Works 3.0 license. No commercial use or derivatives are permitted without the explicit approval of the author. | |
dc.contributor | Shephard, M. S. (Mark S.) | |
dc.contributor | Hicken, Jason | |
dc.contributor.advisor | Sahni, Onkar | |
dc.contributor.author | Tam, Isaac | |
dc.date.accessioned | 2022-09-15T22:08:06Z | |
dc.date.available | 2022-09-15T22:08:06Z | |
dc.date.issued | 2021-05 | |
dc.identifier.uri | https://hdl.handle.net/20.500.13015/6174 | |
dc.description | May 2021 | |
dc.description | School of Engineering | |
dc.description.abstract | Within computational fluid dynamics (CFD) simulations, many complex flow phenomena can emerge. Accurately modeling these phenomena is often a primary motivating factor behind these simulations, and shocks are some of the most challenging phenomena to either model or resolve. However, once a shock is identified and well defined within a flow, there are many proven tools available to both improve the resolution of a given shock, and to efficiently propagate it through space. These methods often rely upon key geometric and/or mesh information related to the shocks, but such knowledge is non-trivial to obtain apriori. This thesis presents a numerical procedure to efficiently detect shocks, filter them to eliminate noise, and sort them into separate shocks or individual shock segments for further analysis. The resulting information could be used for shock fitting, anisotropic layered meshing, or analysis of complex shocks. A combination of numerical simulation data and manufactured data is used to demonstrate the performance of the current procedure. Overall, the novelprocedure developed in this work is robust, and results obtained thus far demonstrate its efficacy. | |
dc.language | ENG | |
dc.language.iso | en_US | |
dc.publisher | Rensselaer Polytechnic Institute, Troy, NY | |
dc.relation.ispartof | Rensselaer Theses and Dissertations Online Collection | |
dc.rights | Attribution-NonCommercial-NoDerivs 3.0 United States | * |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/3.0/us/ | * |
dc.subject | Aeronautical engineering | |
dc.title | Coping with shock : numerical procedure for the detection and sorting of shocks in fluid flows | |
dc.type | Electronic thesis | |
dc.type | Thesis | |
dc.date.updated | 2022-09-15T22:08:08Z | |
dc.rights.holder | This electronic version is a licensed copy owned by Rensselaer Polytechnic Institute (RPI), Troy, NY. Copyright of original work retained by author. | |
dc.description.degree | MS | |
dc.relation.department | Dept. of Mechanical, Aerospace, and Nuclear Engineering |
Files in this item
This item appears in the following Collection(s)
-
RPI Theses Online (Complete)
Rensselaer theses from 2006; many restricted to current RPI Students, Faculty and Staff -
RPI Theses Open Access
Rensselaer Theses and Dissertations with Creative Commons Licenses
Except where otherwise noted, this item's license is described as CC BY-NC-ND. Users may download and share copies with attribution in accordance with a Creative Commons
Attribution-Noncommercial-No Derivative Works 3.0 license. No commercial use or derivatives
are permitted without the explicit approval of the author.