Transsonic Flow in RS0 Direct Cascades - Experiment and Computing Solution

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F03%3A02090559" target="_blank" >RIV/68407700:21220/03:02090559 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

čeština

Original language name

Transsonické proudění v přímé lopatkové mříži RS0 - experiment a numerické řešení

Original language description

The article describes experimental research in the RS0 turbine cascades aerodynamic characteristics based on presure and optical measurement and numeric simulation of flow. Pressure distribution in one blade canal is acoompanied with an optical record ofthe flow field using the schlieren visualisation. The flow loss factor and exit angle are evaluated. Numerical solution is based on the system of Euler equations. The problem is solved by the finite volume method on a nonstructural triangle mesh.

Czech name

Transsonické proudění v přímé lopatkové mříži RS0 - experiment a numerické řešení

Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

BK - Liquid mechanics

OECD FORD branch

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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)

Publication year

2003

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

6

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

6

Pages from-to

21-26

UT code for WoS article

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EID of the result in the Scopus database

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