Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F12%3A00376609" target="_blank" >RIV/61388998:_____/12:00376609 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Prediction of Boundary Layer Transition in Transonic Blade Cascade with Sudden Change of Surface Curvature
Original language description
This paper deals with numerical modelling of the development of the boundary layer in transonic turbine blade cascade. The main attention is paid to studying the influence of the supersonic compression on the boundary layer transition to the turbulence.The limiting Reynolds number at which the transition occurs still in region of the supersonic compression was found.
Czech name
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Czech description
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Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year
2012
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
XVIII. International Scientific Conference The Application of Experimental and Numerical Methods in Fluid Mechanics and Energy 2012
ISBN
978-80-554-0516-2
ISSN
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e-ISSN
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Number of pages
8
Pages from-to
261-268
Publisher name
University of Žilina
Place of publication
Žilina
Event location
Demanovská dolina
Event date
Apr 25, 2012
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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