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Experimental Investigation of the Unsteady Stator/Rotor Wake Characteristics Downstream of an Axial Air Turbine

The result's identifiers

  • Result code in IS VaVaI

    <a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61388998%3A_____%2F21%3A00545831" target="_blank" >RIV/61388998:_____/21:00545831 - isvavai.cz</a>

  • Alternative codes found

    RIV/49777513:23210/21:43962488 RIV/00010669:_____/21:N0000073

  • Result on the web

    <a href="https://www.mdpi.com/2504-186X/6/3/22/htm" target="_blank" >https://www.mdpi.com/2504-186X/6/3/22/htm</a>

  • DOI - Digital Object Identifier

    <a href="http://dx.doi.org/10.3390/ijtpp6030022" target="_blank" >10.3390/ijtpp6030022</a>

Alternative languages

  • Result language

    angličtina

  • Original language name

    Experimental Investigation of the Unsteady Stator/Rotor Wake Characteristics Downstream of an Axial Air Turbine

  • Original language description

    A feasibility study of velocity field measurements using the Particle Image Velocimetry (PIV) method in an axial air turbine model is presented. The wakes past the blades of the rotor wheel were observed using the PIV technique. Data acquisition was synchronized with the shaft rotation, thus, the wakes were phase averaged for statistical analysis. The interaction of the rotor blade wakes with the stator ones was investigated by changing the stator wheel’s angle. The measurement planes were located just behind the rotor blades, covering approximately 3 cm x 3 cm in axial x tangential directions. The spatial correlation function suggests that the resolution used is sufficient for the large-scale flow-patterns only, but not for the small ones. The scales of fluctuations correspond to the shear layer thickness at the mid-span plane but, close to the end-wall, they contain larger structures caused by the secondary flows. The length-scales of the fluctuations under off-design conditions display a dependence on the area of the stator and rotor wakes cross-sections, which, in turn, depend on their angle. The obtained experimental data are to be used for the validation of mathematical simulation results in the future.

  • 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

    20302 - Applied mechanics

Result continuities

  • Project

    <a href="/en/project/TN01000007" target="_blank" >TN01000007: National Centre for Energy</a><br>

  • Continuities

    I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

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

    International Journal of Turbomachinery, Propulsion and Power

  • ISSN

    2504-186X

  • e-ISSN

    2504-186X

  • Volume of the periodical

    6

  • Issue of the periodical within the volume

    3

  • Country of publishing house

    CH - SWITZERLAND

  • Number of pages

    23

  • Pages from-to

    22

  • UT code for WoS article

    000700698300001

  • EID of the result in the Scopus database

    2-s2.0-85110477662