Implementation and futher application of refined transition prediction methods for turbomachinery and other aerodynamics flows. /Z - 1307/.
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F01%3A51010126" target="_blank" >RIV/61388998:_____/01:51010126 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Implementation and futher application of refined transition prediction methods for turbomachinery and other aerodynamics flows. /Z - 1307/.
Original language description
The report deals with mathematical modelling and experimental investigation of the bypass transition in boundary-layer flows. The modelling of bypass transition is based on two-layer turbulence models and an algebraic intermittency model. The effect o
Czech name
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Czech description
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Classification
Type
V<sub>x</sub> - Unclassified - Research report containing classified information
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
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)
Others
Publication year
2001
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Number of pages
45
Place of publication
Praha
Publisher/client name
Ústav termomechaniky AV ČR
Version
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