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Modelling of influence of secondary flow on integral parameters of straight blade cascade

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F12%3A%230001474" target="_blank" >RIV/00010669:_____/12:#0001474 - isvavai.cz</a>

  • Result on the web

    <a href="http://www.czaerospace.eu/en/2012-3-45.html" target="_blank" >http://www.czaerospace.eu/en/2012-3-45.html</a>

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    Modelling of influence of secondary flow on integral parameters of straight blade cascade

  • Original language description

    This paper deals with the modelling of the flow through a stright blade cascade. The straight blade cascade is a simplified physical model of an axial blade wheel. Flow in the straight blade cascade is supposed as two-dimensional and periodic. In an experimental investigation, the secondary flow structures are generated due to the limitation of the wind-tunnel test section. It means that the assumption of two-dimensional flow is more or less broken in the experimental investigation. In this paper an efficient method of modelling of the secondary flow through the straight blade cascade is described. This method is applied to calculation of the flow through the real turbine blade cascade. Results are compared with the experimental data.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

  • CEP classification

    BK - Liquid mechanics

  • OECD FORD branch

Result continuities

  • Project

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2012

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Czech Aerospace Proceedings / Letecký zpravodaj

  • ISSN

    1211-877X

  • e-ISSN

  • Volume of the periodical

    3/2012

  • Issue of the periodical within the volume

    3

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    4

  • Pages from-to

    18-21

  • UT code for WoS article

  • EID of the result in the Scopus database