Počet záznamů: 1  

Hot-Wire Investigation of Turbulence Topology behind Blades at Different Shape Qualities

  1. 1.
    SYSNO ASEP0556228
    Druh ASEPJ - Článek v odborném periodiku
    Zařazení RIVJ - Článek v odborném periodiku
    Poddruh JČlánek ve WOS
    NázevHot-Wire Investigation of Turbulence Topology behind Blades at Different Shape Qualities
    Tvůrce(i) Yanovych, Vitalii (UT-L)
    Duda, D. (CZ)
    Uruba, Václav (UT-L) RID, ORCID
    Tomášková, T. (CZ)
    Číslo článku522
    Zdroj.dok.Processes. - : MDPI
    Roč. 10, č. 3 (2022)
    Poč.str.22 s.
    Forma vydáníOnline - E
    Jazyk dok.eng - angličtina
    Země vyd.CH - Švýcarsko
    Klíč. slovaasymmetric airfoil ; hot-wire ; shape inaccuracies ; the structure of turbulent ; wake topology ; aerodynamic characteristics
    Vědní obor RIVBK - Mechanika tekutin
    Obor OECDApplied mechanics
    Způsob publikováníOpen access
    Institucionální podporaUT-L - RVO:61388998
    UT WOS000774237400001
    EID SCOPUS85126518599
    DOI10.3390/pr10030522
    AnotaceThe scope of this paper is to perform a detailed experimental investigation of the shape error effect on the turbulence evolution behind NACA 64-618 airfoil. This airfoil is 3D-printed with predefined typical shape inaccuracies. A high-precision optical 3D scanner was used to assess the shape and surface quality of the manufactured models. The turbulent flow was studied using hot-wire anemometry. The developed force balance device was provided to measure the aerodynamic characteristics of the airfoil. Experimental studies were carried out for three angles of attack, +10°, 0°, −10°, and different chord-based Reynolds numbers from 5.3 × 104 to 2.1 × 105. The obtained results show that the blunt trailing edge and rough surface decline the aerodynamic performance of the blades. In addition, the experimental results revealed a strong sensitivity of the Taylor microscale Reynolds number to the type of shape inaccuracy, especially at Re ≈ 1.7 × 105. We also discuss the evolution of the Reynolds stress components, the degree of flow anisotropy, and the power spectrum distributions depending on the airfoil inaccuracies. © 2022 by the authors. Licensee MDPI, Basel, Switzerland.
    PracovištěÚstav termomechaniky
    KontaktMarie Kajprová, kajprova@it.cas.cz, Tel.: 266 053 154 ; Jana Lahovská, jaja@it.cas.cz, Tel.: 266 053 823
    Rok sběru2023
    Elektronická adresahttps://mdpi-res.com/d_attachment/processes/processes-10-00522/article_deploy/processes-10-00522-v3.pdf?version=1646878698
Počet záznamů: 1  

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