Numerical and experimental investigations of supersonic turbine cascade flow
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F11%3A00358774" target="_blank" >RIV/61388998:_____/11:00358774 - 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
Numerical and experimental investigations of supersonic turbine cascade flow
Original language description
This paper presents results of the experimental and numerical investigations of the validation of the aerodynamic performance of the supersonic tip section airfoil cascade. The tip section airfoil design respects the supersonic inlet and outlet conditions of the ultra long bucket. The paper is organized into two main chapters: 1. the description of the experimental set up and obtained xperimental data by optical and pneumatic methods, 2. the comparison of the results of numerical and experimental investigations.
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
Ninth European Conference on Turbomachinery
ISBN
978-975-561-389-5
ISSN
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e-ISSN
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Number of pages
9
Pages from-to
547-554
Publisher name
Local Organising Committee
Place of publication
Istanbul
Event location
Istanbul
Event date
Mar 21, 2011
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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