<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-09-22T14:55:16Z</responseDate><request verb="GetRecord" identifier="oai:www.repository.cam.ac.uk:1810/271753" metadataPrefix="uketd_dc">https://api.repository.cam.ac.uk/server/oai/request</request><GetRecord><record><header><identifier>oai:www.repository.cam.ac.uk:1810/271753</identifier><datestamp>2024-06-26T13:54:25Z</datestamp><setSpec>com_1810_213729</setSpec><setSpec>com_1810_256065</setSpec><setSpec>col_1810_219485</setSpec></header><metadata><uketd_dc:uketddc xmlns:uketd_dc="http://naca.central.cranfield.ac.uk/ethos-oai/2.0/" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:dcterms="http://purl.org/dc/terms/" xmlns:uketdterms="http://naca.central.cranfield.ac.uk/ethos-oai/terms/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://naca.central.cranfield.ac.uk/ethos-oai/2.0/ http://naca.central.cranfield.ac.uk/ethos-oai/2.0/uketd_dc.xsd">
   <dc:title>Large Eddy Simulation of Labyrinth Seals and Rib Shapes for Internal Cooling Passges</dc:title>
   <dc:identifier xsi:type="dcterms:DOI">10.17863/CAM.18745</dc:identifier>
   <dc:creator>Dai, Yushuang</dc:creator>
   <uketdterms:advisor>Tucker, Paul</uketdterms:advisor>
   <dcterms:abstract>The turbine is one of the key components in gas turbine engines. To prevent the turbine
blades from being badly damaged by their harsh working environment, it is necessary to
keep them cool. This can be achieved by enhancement of the heat transfer performance
through internal cooling passages. However, the large quantity of flow within this internal
cycle inevitably results in mass flow loss, which is a major source of loss in turbomachinery.
Therefore labyrinth seals are also investigated in this study, attempting to reduce the flow
leakage and further increase the turbine efficiency.

Large Eddy Simulation ( LES ) is used for its capability to capture the complex unsteady
flow features in this study. Different rib shapes in a fully developed ribbed channel are
investigated, aiming to improve the heat transfer performance. An immersed boundary
method ( IBM ) is used with LES to generate complex geometries. With the use of IBM , the
range of geometries can be represented on a background Cartesian grid.

To obtain the best sealing performance, an investigation is undertaken into the possibility
of optimising labyrinth seal planforms using a genetic algorithm ( GA ). By making use
of the large number of populations, a much faster calculation can be achieved toward the
objective function. Three hundred LES calculations are carried out, and an optimised design
is generated that maximises the sealing effectiveness. The optimised design shows a leakage
reduction of about 27.6% compared to the baseline geometry.

The optimisation process employing a GA will be continued. It is expected that automated
optimisation as presented will become increasingly important in the design process of future
turbomachines, particularly for flows with strong parameter interactions, with an aim to
further improve the overall efficiency of gas turbines.</dcterms:abstract>
   <uketdterms:institution>University of Cambridge</uketdterms:institution>
   <dcterms:issued>2018-04-28</dcterms:issued>
   <dc:type>Thesis</dc:type>
   <uketdterms:qualificationlevel>Doctoral</uketdterms:qualificationlevel>
   <uketdterms:qualificationname>Doctor of Philosophy (PhD)</uketdterms:qualificationname>
   <dc:language>en</dc:language>
   <uketdterms:sponsor>CSC</uketdterms:sponsor>
   <dcterms:isReferencedBy xsi:type="dcterms:URI">https://www.repository.cam.ac.uk/handle/1810/271753</dcterms:isReferencedBy>
   <dcterms:license>https://apollo8-f-pro.lib.cam.ac.uk/bitstreams/9b66b61f-36a7-4dbf-9680-90c18d3f4d35/download</dcterms:license>
   <uketdterms:checksum xsi:type="uketdterms:MD5">87eda9de84448d1f82354d60eee3eb5f</uketdterms:checksum>
   <dc:identifier xsi:type="dcterms:URI">https://apollo8-f-pro.lib.cam.ac.uk/bitstreams/fd82d3c4-3398-4cdd-bce1-91a88ab9eba6/download</dc:identifier>
   <uketdterms:checksum xsi:type="uketdterms:MD5">674125a8418e1c884696fecfcf56da96</uketdterms:checksum>
   <dc:rights>https://www.rioxx.net/licenses/all-rights-reserved/</dc:rights>
   <dc:subject>LES</dc:subject>
   <dc:subject>GA</dc:subject>
   <dc:subject>turbomachinary</dc:subject>
</uketd_dc:uketddc>
</metadata></record></GetRecord></OAI-PMH>