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dc.rights.licenseCC 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.contributorShephard, M. S. (Mark S.)
dc.contributorHicken, Jason
dc.contributor.advisorSahni, Onkar
dc.contributor.authorTam, Isaac
dc.date.accessioned2022-09-15T22:08:06Z
dc.date.available2022-09-15T22:08:06Z
dc.date.issued2021-05
dc.identifier.urihttps://hdl.handle.net/20.500.13015/6174
dc.descriptionMay 2021
dc.descriptionSchool of Engineering
dc.description.abstractWithin 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.languageENG
dc.language.isoen_US
dc.publisherRensselaer Polytechnic Institute, Troy, NY
dc.relation.ispartofRensselaer Theses and Dissertations Online Collection
dc.rightsAttribution-NonCommercial-NoDerivs 3.0 United States*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectAeronautical engineering
dc.titleCoping with shock : numerical procedure for the detection and sorting of shocks in fluid flows
dc.typeElectronic thesis
dc.typeThesis
dc.date.updated2022-09-15T22:08:08Z
dc.rights.holderThis electronic version is a licensed copy owned by Rensselaer Polytechnic Institute (RPI), Troy, NY. Copyright of original work retained by author.
dc.description.degreeMS
dc.relation.departmentDept. of Mechanical, Aerospace, and Nuclear Engineering


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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.
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.