Experimental and Theoretical Study of Heated Coanda Jet
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24210%2F04%3A24210250" target="_blank" >RIV/46747885:24210/04:24210250 - 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
Experimental and Theoretical Study of Heated Coanda Jet
Original language description
The results of the experimental and analytical study of the effect of temperature and temperature gradient on the stability of the boundary layer of air flow along the curved wall are presented. The transition from laminar to turbulent flow occurs for aertain magnitude of the Reynolds number in the case of plane wall jet as well as curved wall jet. The transition in the case of curved wall jet is well observed owing to the tendency of the laminar flow to separate from the wall. On the other hand the tubulent flow has a strong tendency to remain attached to the surface. The results of the experiments together with the analysis carried out on the basis of the similarity solution show the stabilizing effect of the heated wall on the boundary layer.
Czech name
Experimentální a teoretická studie proudění podél zahřívané stěny
Czech description
Práce přináší výsledky teoretického a experimentálního výzkumu proudění typu Coanda Jet.
Classification
Type
D - Article in proceedings
CEP classification
BK - Liquid mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2004
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
21INTERNATIONAL CONGRESS OF THEORETICAL AND APPLIED MECHANICS
ISBN
83-89687-01-1
ISSN
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e-ISSN
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Number of pages
1
Pages from-to
61
Publisher name
IPPT PAN
Place of publication
Warszawa, Poland
Event location
Warszawa, Poland
Event date
Jan 1, 2004
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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