All

What are you looking for?

All
Projects
Results
Organizations

Quick search

  • Projects supported by TA ČR
  • Excellent projects
  • Projects with the highest public support
  • Current projects

Smart search

  • That is how I find a specific +word
  • That is how I leave the -word out of the results
  • “That is how I can find the whole phrase”

3D Flow Past Transonic Turbine Cascade SE 1050-Experiment and Numerical Simulations

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F13%3A00394705" target="_blank" >RIV/61388998:_____/13:00394705 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21220/13:00206638

  • Result on the web

    <a href="http://dx.doi.org/10.1007/s11630-013-0629-7" target="_blank" >http://dx.doi.org/10.1007/s11630-013-0629-7</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.1007/s11630-013-0629-7" target="_blank" >10.1007/s11630-013-0629-7</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    3D Flow Past Transonic Turbine Cascade SE 1050-Experiment and Numerical Simulations

  • Original language description

    The paper is concerned with experimental and numerical research on 3D flow past prismatic turbine cascade SE1050 (known in QNET network as open test case SE1050). The primary goal was to assess the influence of the inlet velocity profile on the flow structures in the interblade channel and on the flow field parameters at the cascade exit and to compare these findings to results of numerical simulations. Investigations of 3D flow past the blade cascade with non-uniform inlet velocity profile were carriedout both experimentally and numerically at subsonic (M2is = 0.8) and at transonic (M2is = 1.2) regime at design angle of incidence. Experimental data was obtained using a traversing device with a five-hole conical probe. Numerically, the 3D flow was simulated by open source code OpenFOAM and in-house code. Analyses of experimental data and CFD simulations have revealed development of distinctive vortex structures resulting from non-uniform inlet velocity profile. Origin of these structu

  • 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

    <a href="/en/project/GAP101%2F10%2F1329" target="_blank" >GAP101/10/1329: Numerical and experimental research on the flow in axial turbine cascades</a><br>

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Others

  • Publication year

    2013

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Journal of Thermal Science

  • ISSN

    1003-2169

  • e-ISSN

  • Volume of the periodical

    22

  • Issue of the periodical within the volume

    4

  • Country of publishing house

    CN - CHINA

  • Number of pages

    9

  • Pages from-to

    311-319

  • UT code for WoS article

    000321724900004

  • EID of the result in the Scopus database