Study of sweep angle effect on thrust generation of oscillatory pectoral fins

Author(s):  
C.-M. Chew ◽  
S. Arastehfar ◽  
G. Gunawan ◽  
K. S. Yeo
2018 ◽  
Vol 11 (1) ◽  
Author(s):  
Soheil Arastehfar ◽  
Chee-Meng Chew ◽  
Athena Jalalian ◽  
Gunawan Gunawan ◽  
Khoon Seng Yeo

Propulsive capability of manta rays' flapping pectoral fins has inspired many to incorporate these fins as propulsive mechanisms for autonomous underwater vehicles. In particular, geometrical factors such as sweep angle have been postulated as being influential to these fins' propulsive capability, specifically their thrust generation. Although effects of sweep angle on static/flapping wings of aircrafts/drones have been widely studied, little has been done for underwater conditions. Furthermore, the findings from air studies may not be relatable to the underwater studies on pectoral fins because of the different Reynolds number (compared to the flapping wings) and force generation mechanism (compared to the static wings). This paper aims to establish a relationship between the sweep angle and thrust generation. An experiment was conducted to measure the thrust generated by 40 fins in a water channel under freestream and still water conditions for chord Reynolds number between 2.2 × 104 and 8.2 × 104. The fins were of five different sweep angles (0 deg, 10 deg, 20 deg, 30 deg, and 40 deg) that were incorporated into eight base designs of different flexibility characteristics. The results showed that the sweep angle (within the range considered) may have no significant influence on these fins' thrust generation, implying no significant effects on thrust under uniform flow condition and on the maximum possible thrust under still water. Overall, it can be concluded that sweep angle may not be a determinant of thrust generation for flapping pectoral fins. This knowledge can ease the decision-making process of design of robots propeled by these fins.


2020 ◽  
Vol 162 ◽  
pp. 1087-1103
Author(s):  
Mabrouk Mosbahi ◽  
Ahmed Ayadi ◽  
Youssef Chouaibi ◽  
Zied Driss ◽  
Tullio Tucciarelli

2017 ◽  
Vol 30 (4) ◽  
pp. 04017005 ◽  
Author(s):  
Masoud Kharati-Koopaee ◽  
Mojtaba Mohammadpour-Shoorbakhloo

Acoustics ◽  
2020 ◽  
Vol 2 (4) ◽  
pp. 812-832
Author(s):  
Alessandro Zarri ◽  
Julien Christophe ◽  
Stéphane Moreau ◽  
Christophe Schram

The low-speed fans used for automotive engine cooling contribute to a significant part of the global noise emitted by the vehicle. A low-order sound-prediction methodology is developed considering the blade sweep-angle effect on the acoustic predictions of the turbulence-impingement and the trailing-edge noise-generating mechanisms. We modeled these through the application of a semianalytical method based on Amiet’s airfoil theory, appropriately adapted via a strip-theory approach accounting for rotation and modified to include the blades forward curvature. Sweep was already shown in the literature to reduce the noise emitted by isolated airfoils, but its effect on rotating machines was not yet well understood. In this study, we show that the effect of the sweep-angle is to globally reduce the emitted noise by the fan and to change the sound distribution of the sources along the blade span. Thus, the sweep-angle must be considered not only because it yields a better comparison with experimental results but also because wrong conclusions on the dominating noise-generating mechanisms can be drawn when this effect is not taken into account. The investigation is finally complemented by a sensitivity analysis focusing on some of the key parameters characterizing the acoustic prediction.


2021 ◽  
Vol 1909 (1) ◽  
pp. 012005
Author(s):  
Alessandro Zarri ◽  
Julien Christophe ◽  
Stéphane Moreau ◽  
Christophe Schram
Keyword(s):  

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