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Effects of a Single Blade Incidence Angle Offset on Adjacent Blades in a Linear Cascade

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24220%2F21%3A00008995" target="_blank" >RIV/46747885:24220/21:00008995 - isvavai.cz</a>

  • Alternative codes found

    RIV/61388998:_____/21:00549596 RIV/68407700:21220/21:00352658

  • Result on the web

    <a href="https://doi.org/10.3390/pr9111974" target="_blank" >https://doi.org/10.3390/pr9111974</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.3390/pr9111974" target="_blank" >10.3390/pr9111974</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Effects of a Single Blade Incidence Angle Offset on Adjacent Blades in a Linear Cascade

  • Original language description

    The paper presents a numerical and experimental investigation of the effect of incindence angle offset in a two-dimensional section of a flat blade cascade in a high-speed wind tunnel. The aim of the current work is tp determine the aerodynamic excitation forces and approximation of the unsteady blade-loading function using a quasi-stationary approach. The numerical simulations were performed with an in-house finite-volume code built on the top of the OpenFOAM framework. The experimental data were acquired for regimes corresponding to the numerical setup. The comparison of the computational and experimental results is shown for the static pressure distributions on three blades and upstream and downstream of the cascade. The plot of the aerodynamic moments acting on all five blades shows that the adjacent blades are significantly influenced by the angular offset of the middle blade.

  • Czech name

  • Czech description

Classification

  • Type

    J<sub>imp</sub> - Article in a specialist periodical, which is included in the Web of Science database

  • CEP classification

  • OECD FORD branch

    20402 - Chemical process engineering

Result continuities

  • Project

    <a href="/en/project/GA20-11537S" target="_blank" >GA20-11537S: Experimental research on flutter excitation function in turbomachinery</a><br>

  • Continuities

    P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)<br>S - Specificky vyzkum na vysokych skolach

Others

  • Publication year

    2021

  • Confidentiality

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

Data specific for result type

  • Name of the periodical

    Processes

  • ISSN

    2227-9717

  • e-ISSN

  • Volume of the periodical

    9

  • Issue of the periodical within the volume

    11

  • Country of publishing house

    CH - SWITZERLAND

  • Number of pages

    14

  • Pages from-to

  • UT code for WoS article

    000726839400001

  • EID of the result in the Scopus database

    2-s2.0-85119070052