Study on the effect of raindrops on the dynamic stall of a NACA-0012 airfoil

In this study the pure effect of raindrops on dynamic stall of a pitching airfoil has been investigated. The simulation was performed at Reynolds number of 10 6 with raindrop diameter equal to 10 - 5m. A couple of multiphase models based on Eulerian and Lagrangian frames of reference have been imple...

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Bibliographic Details
Main Authors: Salavatidezfouli, S. (Author), Schito, P. (Author), Sheidani, A. (Author)
Format: Article
Language:English
Published: Springer Science and Business Media Deutschland GmbH 2022
Subjects:
Online Access:View Fulltext in Publisher
LEADER 02391nam a2200409Ia 4500
001 10.1007-s40430-022-03498-8
008 220510s2022 CNT 000 0 und d
020 |a 16785878 (ISSN) 
245 1 0 |a Study on the effect of raindrops on the dynamic stall of a NACA-0012 airfoil 
260 0 |b Springer Science and Business Media Deutschland GmbH  |c 2022 
856 |z View Fulltext in Publisher  |u https://doi.org/10.1007/s40430-022-03498-8 
520 3 |a In this study the pure effect of raindrops on dynamic stall of a pitching airfoil has been investigated. The simulation was performed at Reynolds number of 10 6 with raindrop diameter equal to 10 - 5m. A couple of multiphase models based on Eulerian and Lagrangian frames of reference have been implemented to simulate the raindrops. In the first step the accuracy of each multiphase model has been appraised. As a result, the Lagrangian multiphase model, which is called Discrete Phase Model, has been proven to be of better accuracy. It has been concluded that in general raindrops has negative effects on the lift coefficient of the pitching airfoil. In addition, a lead in aerodynamic phenomena has been observed due to the presence of water drops. This phenomenon has also been observed in the formation and separation of Leading Edge and Trailing Edge vortices which come to existence in advance of the dry case. Finally, it has been illustrated that the main effect of raindrops is on the phase of force oscillation rather than the force amplitude. © 2022, The Author(s). 
650 0 4 |a Aerodynamic stalling 
650 0 4 |a Airfoils 
650 0 4 |a Discrete phase model 
650 0 4 |a Discrete phase model (DPM) 
650 0 4 |a Discrete phase modeling 
650 0 4 |a Dispersed multiphase 
650 0 4 |a Dispersed multiphase (DMP) 
650 0 4 |a Drops 
650 0 4 |a Dynamic stall 
650 0 4 |a Dynamic stalls 
650 0 4 |a Lagrange multipliers 
650 0 4 |a Model-based OPC 
650 0 4 |a Multiphase modeling 
650 0 4 |a Multiphases 
650 0 4 |a ON dynamics 
650 0 4 |a Pitching airfoil 
650 0 4 |a Pitching airfoils 
650 0 4 |a Rain 
650 0 4 |a Reynold number 
650 0 4 |a Reynolds number 
650 0 4 |a Vortex flow 
700 1 |a Salavatidezfouli, S.  |e author 
700 1 |a Schito, P.  |e author 
700 1 |a Sheidani, A.  |e author 
773 |t Journal of the Brazilian Society of Mechanical Sciences and Engineering