Experimental Data on High-Speed Flow Past the Root Blade Cascade
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F11%3A00361182" target="_blank" >RIV/61388998:_____/11:00361182 - 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 Data on High-Speed Flow Past the Root Blade Cascade
Original language description
The paper deals with experimental results of high-speed aerodynamic research on a blade cascade. The blade cascade represents root section of the last stage rotor blades of large output steam turbine. Basic aerodynamic characteristics of the blade cascade are presented together with photographs of flow fields in the range of transonic flow regimes. Results are analysed and discussed to provide a new knowledge on design and operation of the last rotor at the region of the blade root.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
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)<br>Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Současné trendy při návrhu a výpočtu turbostrojů
ISBN
978-80-254-9934-4
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
119-124
Publisher name
Technologické inovační centrum ČKD Praha
Place of publication
Praha
Event location
Praha
Event date
May 31, 2011
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
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