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”

TANDEM BLADE CENTRIFUGAL COMPRESSOR IMPELLER DESIGN

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21260%2F05%3A06146286" target="_blank" >RIV/68407700:21260/05:06146286 - isvavai.cz</a>

  • Alternative codes found

    RIV/68407700:21260/05:06148413

  • Result on the web

  • DOI - Digital Object Identifier

Alternative languages

  • Result language

    angličtina

  • Original language name

    TANDEM BLADE CENTRIFUGAL COMPRESSOR IMPELLER DESIGN

  • Original language description

    In the article an innovative design of the centrifugal compressor rotor tandem cascade is described. The new design approach is based on the analysis of the flow characteristics in the rotating working channels within the turbo-machines as one of the results of the arising from previous systematical research of the flow phenomena in the curved channels of turbo-machines carried out at the of Aerospace Research Center. The new design of the impeller flow passage geometry has been made in the form of re-engineering of the existing newly designed centrifugal compressor stage in the Walter Engines a. s. The rotor tandem blade concept lies in the separation of the impeller blades into two parts. First part is formed by the axial-diagonal flow inducer section of the rotor. This flow part is designed as a highly aerodynamic loaded axial flow compressor cascade. The second part of the impeller cascade is designed with double number of blades as in the first part of the impeller.

  • Czech name

    Návrh odstředivého kompresoru s tandemovým lopatkováním rotoru

  • Czech description

    Návrh odstředivého kompresoru s tandemovým lopatkováním rotoru

Classification

  • Type

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

  • CEP classification

    JU - Aeronautics, aerodynamics, aeroplanes

  • OECD FORD branch

Result continuities

  • Project

  • Continuities

    S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2005

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Letecký zpravodaj

  • ISSN

    1211-877X

  • e-ISSN

  • Volume of the periodical

    2005

  • Issue of the periodical within the volume

    -

  • Country of publishing house

    CZ - CZECH REPUBLIC

  • Number of pages

    1

  • Pages from-to

  • UT code for WoS article

  • EID of the result in the Scopus database