AIRCRAFT TURBINE ENGINE LABYRINTH SEAL INTRODUCTION AND CFD CALCULATION
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F20%3A00345880" target="_blank" >RIV/68407700:21220/20:00345880 - isvavai.cz</a>
Result on the web
<a href="https://www.engmech.cz/" target="_blank" >https://www.engmech.cz/</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.21495/5896-3-114" target="_blank" >10.21495/5896-3-114</a>
Alternative languages
Result language
angličtina
Original language name
AIRCRAFT TURBINE ENGINE LABYRINTH SEAL INTRODUCTION AND CFD CALCULATION
Original language description
Abstract: The labyrinth seals are important part of aircraft turbine engine. Primary function of labyrinth seal is elimination air mass flow which is flowing between rotational and non-rotational part. Second function is control air mass in these cavities. In this paper is listen total temperature, static pressure and flow coefficient in typical labyrinth seal geometry
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
20304 - Aerospace 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
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Engineering Mechanics 2020: Book of full texts
ISBN
978-80-214-5896-3
ISSN
1805-8248
e-ISSN
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Number of pages
4
Pages from-to
114-117
Publisher name
Institute of Thermomechanics, AS CR, v.v.i.
Place of publication
Prague
Event location
Brno
Event date
Nov 24, 2020
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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