PIV analysis of near-wake flow patterns of an ice-accreted bridge cable in low and moderately turbulent wind
Identifikátory výsledku
Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68378297%3A_____%2F19%3A00505717" target="_blank" >RIV/68378297:_____/19:00505717 - isvavai.cz</a>
Nalezeny alternativní kódy
RIV/68407700:21110/19:00333725
Výsledek na webu
<a href="https://doi.org/10.1016/j.jweia.2019.06.011" target="_blank" >https://doi.org/10.1016/j.jweia.2019.06.011</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.1016/j.jweia.2019.06.011" target="_blank" >10.1016/j.jweia.2019.06.011</a>
Alternativní jazyky
Jazyk výsledku
angličtina
Název v původním jazyce
PIV analysis of near-wake flow patterns of an ice-accreted bridge cable in low and moderately turbulent wind
Popis výsledku v původním jazyce
The study contributes to the explanation of flow behaviour and the basis of phenomena existing during two dimensional airflow around an ice-accreted cylinder, representing the section model of a bridge cable. The geometrical features and flow characteristics of the near-wake flow patterns of the iced cable were investigated within the Reynolds number range of 2.2⋅10^4–6.4⋅10^4 in low and moderately turbulent flow. The experimental procedure was conducted to create ice accretion on the cylindrical model. The shape of the ice was registered using a photogrammetry method. For the aerodynamic investigations the ice-accreted model was reproduced at a smaller scale by means of 3D printing. Representative snapshots of the flow field behind the stationary horizontal simulated iced cable were digitally analyzed by the Particle Image Velocimetry technique. The flow visualization provided quantitative data about the velocity and the direction of flow streams within both the near-wake and the sidewise regions of distributed flow around the model. Evidence of the existence of the vortex excitation proces was obtained at three principal angles of attack. The characteristics of the vortex street and the location of the flow boundary layer separation points were recognized. The obtained results were compared with results for a smooth cylinder.
Název v anglickém jazyce
PIV analysis of near-wake flow patterns of an ice-accreted bridge cable in low and moderately turbulent wind
Popis výsledku anglicky
The study contributes to the explanation of flow behaviour and the basis of phenomena existing during two dimensional airflow around an ice-accreted cylinder, representing the section model of a bridge cable. The geometrical features and flow characteristics of the near-wake flow patterns of the iced cable were investigated within the Reynolds number range of 2.2⋅10^4–6.4⋅10^4 in low and moderately turbulent flow. The experimental procedure was conducted to create ice accretion on the cylindrical model. The shape of the ice was registered using a photogrammetry method. For the aerodynamic investigations the ice-accreted model was reproduced at a smaller scale by means of 3D printing. Representative snapshots of the flow field behind the stationary horizontal simulated iced cable were digitally analyzed by the Particle Image Velocimetry technique. The flow visualization provided quantitative data about the velocity and the direction of flow streams within both the near-wake and the sidewise regions of distributed flow around the model. Evidence of the existence of the vortex excitation proces was obtained at three principal angles of attack. The characteristics of the vortex street and the location of the flow boundary layer separation points were recognized. The obtained results were compared with results for a smooth cylinder.
Klasifikace
Druh
J<sub>imp</sub> - Článek v periodiku v databázi Web of Science
CEP obor
—
OECD FORD obor
20101 - Civil engineering
Návaznosti výsledku
Projekt
<a href="/cs/project/GA19-04695S" target="_blank" >GA19-04695S: Aerodynamická odezva válce s povrchovou drsností v kritickém a přechodovém režimu Reynoldsova čísla</a><br>
Návaznosti
I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace
Ostatní
Rok uplatnění
2019
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Údaje specifické pro druh výsledku
Název periodika
Journal of Wind Engineering and Industrial Aerodynamics
ISSN
0167-6105
e-ISSN
—
Svazek periodika
191
Číslo periodika v rámci svazku
August
Stát vydavatele periodika
NL - Nizozemsko
Počet stran výsledku
15
Strana od-do
297-311
Kód UT WoS článku
000474561600023
EID výsledku v databázi Scopus
2-s2.0-85068217962