DocumentCode :
2042391
Title :
Numerical and experimental investigation of the hydrodynamics of flapping foil added in-line motion
Author :
Fujuan Liu ; Weishan Chen ; Kai Zhou
Author_Institution :
Dept. of Mech. & Electron. Eng., Harbin Inst. of Technol., Harbin, China
fYear :
2015
fDate :
2-5 Aug. 2015
Firstpage :
976
Lastpage :
981
Abstract :
The flapping foil based on bionics is a sort of simplified model which imitates the motion of the wings or fins of animals. Based on the backgrounds of underwater vehicle with high capabilities of propulsion, the hydrodynamics of flapping foil added in-line motion is numerical and experimental investigated in this paper. We simulate this 3 DOF motion in the method of computational fluid dynamics. The synthetic effect of the heave amplitude, Strouhal number, attack angle, and the stroke angle on the propulsive efficiency are investigated by the response surface methodology (RSM). We obtain a prediction model of the propulsive efficiency depended on the four parameters and design a 3 DOF experimental setup with the aim of investigating the propulsion mechanism of the flapping hydrofoils and analysis the hydrodynamic forces generated on the hydrofoils.
Keywords :
hydrodynamics; propulsion; response surface methodology; 3 DOF motion; RSM; Strouhal number; animals; attack angle; bionics; computational fluid dynamics; fins; flapping foil added in-line motion; flapping hydrofoils; heave amplitude; hydrodynamic forces; hydrodynamics; propulsion mechanism; propulsive efficiency; response surface methodology; stroke angle; underwater vehicle; wings; Encoding; Force; Hydrodynamics; Mathematical model; Predictive models; Propulsion; Response surface methodology; Propulsion; experimental setup; flapping foil; response surface methodology;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2015 IEEE International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4799-7097-1
Type :
conf
DOI :
10.1109/ICMA.2015.7237618
Filename :
7237618
Link To Document :
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