Labyrinth seal total temperature investigation
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F21%3A00353233" target="_blank" >RIV/68407700:21220/21:00353233 - isvavai.cz</a>
Result on the web
<a href="https://doi.org/10.14311/TPFM.2021.003" target="_blank" >https://doi.org/10.14311/TPFM.2021.003</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.14311/TPFM.2021.003" target="_blank" >10.14311/TPFM.2021.003</a>
Alternative languages
Result language
angličtina
Original language name
Labyrinth seal total temperature investigation
Original language description
This article presents the labyrinth seal thermal energy investigation in an aircraft turbine engine application. It starts by describing the CFD calculation with three critical radial clearance variants and three variants of the number of labyrinth seal teeth. The calculation result of the aircraft turbine engine boundary conditions is shown. The CFD, verification experiment and comparison with current labyrinth seal design are presented.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
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OECD FORD branch
20104 - Transport engineering
Result continuities
Project
<a href="/en/project/EF16_019%2F0000826" target="_blank" >EF16_019/0000826: Center of Advanced Aerospace Technology</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2021
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Topical Problems of Fluid Mechanics 2021
ISBN
978-80-87012-76-5
ISSN
2336-5781
e-ISSN
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Number of pages
9
Pages from-to
16-24
Publisher name
Institute of Thermomechanics, AS CR, v.v.i.
Place of publication
Prague
Event location
Praha
Event date
Feb 17, 2021
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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