Drag Estimation in the Near Wake of the NREL's Airfoils Based on Hot-Wire Data
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F49777513%3A23210%2F22%3A43968057" target="_blank" >RIV/49777513:23210/22:43968057 - isvavai.cz</a>
Výsledek na webu
<a href="https://www.matec-conferences.org/articles/matecconf/pdf/2022/16/matecconf_aenmmte2022_02012.pdf" target="_blank" >https://www.matec-conferences.org/articles/matecconf/pdf/2022/16/matecconf_aenmmte2022_02012.pdf</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1051/matecconf/202236902012" target="_blank" >10.1051/matecconf/202236902012</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
Drag Estimation in the Near Wake of the NREL's Airfoils Based on Hot-Wire Data
Popis výsledku v původním jazyce
This paper presents the results of the drag coefficient estimations for different types of NREL airfoils based on the experimental data. Namely, it was S803, S807, S813, and S817 profiles with the same chord length. The investigations were conducted at three angles of attack α=0°, α=±5°, different chord-based Reynolds numbers 0.6×105, 1.3×105 and 2.6×105. While, measuring cross-sections were placed behind the trailing edge at x∙c−1≈0.2, 0.4 and 1.0. Experimental data were collected using a hot-wire split fiber probe 55R55, which allowed us to estimate the characteristics of turbulent flow in stream-wise and crosswise directions. According to the obtained results, the highest and lowest Cd values correspond to profiles S817 and S803, respectively. Moreover, the results show that more asymmetric profiles S803 and S807 have the lowest resistance at zero angles of attack.Research background: Application of Antonia and Rajagopalan methodology to drag assessment of various stream bodies.Purpose of the article: Comparative evaluation of the drag coefficients of the NREL airfoils based on instantaneous velocity distribution behind.Methods: Hot-wire anemometry with split fiber probe 55R55.Findings & Value added: The highest drag coefficient corresponds to the S817 profile. The asymmetry of the airfoil shape has a significant impact on its drag characteristics.
Název v anglickém jazyce
Drag Estimation in the Near Wake of the NREL's Airfoils Based on Hot-Wire Data
Popis výsledku anglicky
This paper presents the results of the drag coefficient estimations for different types of NREL airfoils based on the experimental data. Namely, it was S803, S807, S813, and S817 profiles with the same chord length. The investigations were conducted at three angles of attack α=0°, α=±5°, different chord-based Reynolds numbers 0.6×105, 1.3×105 and 2.6×105. While, measuring cross-sections were placed behind the trailing edge at x∙c−1≈0.2, 0.4 and 1.0. Experimental data were collected using a hot-wire split fiber probe 55R55, which allowed us to estimate the characteristics of turbulent flow in stream-wise and crosswise directions. According to the obtained results, the highest and lowest Cd values correspond to profiles S817 and S803, respectively. Moreover, the results show that more asymmetric profiles S803 and S807 have the lowest resistance at zero angles of attack.Research background: Application of Antonia and Rajagopalan methodology to drag assessment of various stream bodies.Purpose of the article: Comparative evaluation of the drag coefficients of the NREL airfoils based on instantaneous velocity distribution behind.Methods: Hot-wire anemometry with split fiber probe 55R55.Findings & Value added: The highest drag coefficient corresponds to the S817 profile. The asymmetry of the airfoil shape has a significant impact on its drag characteristics.
Klasifikace
Druh
D - Stať ve sborníku
CEP obor
—
OECD FORD obor
20304 - Aerospace engineering
Návaznosti výsledku
Projekt
—
Návaznosti
S - Specificky vyzkum na vysokych skolach
Ostatní
Rok uplatnění
2022
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název statě ve sborníku
MATEC Web of Conferences
ISBN
—
ISSN
2261-236X
e-ISSN
2261-236X
Počet stran výsledku
9
Strana od-do
—
Název nakladatele
EDP Sciences
Místo vydání
Les Ulis
Místo konání akce
Piešťany
Datum konání akce
12. 9. 2022
Typ akce podle státní příslušnosti
EUR - Evropská akce
Kód UT WoS článku
—