DocumentCode :
572476
Title :
Numerical study of the drag coefficient of air cushion craft´s bow skirt based on Virtual Experiment
Author :
Fu, Ming-yu ; Zhang, Li-na ; Wang, Cheng-long ; Song, Da-cheng
Author_Institution :
Dept. of Autom., Univ. of Harbin Eng., Harbin, China
fYear :
2012
fDate :
15-17 Aug. 2012
Firstpage :
567
Lastpage :
572
Abstract :
The basic model for computing resistance of air cushion craft bow skirt is established, simulations are carried out in finite element analysis software ANSYS CFX to compute the coefficient of bow skirt resistance. According to the results, the law of the effect of skirt finger inclination angle on skirt resistance coefficient is showed, and which provides a reference for hovercraft hull design.
Keywords :
aerodynamics; aerospace components; aerospace engineering; aircraft; computational fluid dynamics; design engineering; drag; finite element analysis; hovercraft; ANSYS CFX; air cushion craft bow skirt; bow skirt resistance coefficient; drag coefficient; finite element analysis software; hovercraft hull design; numerical study; skirt finger inclination angle law; virtual experiment; Computational modeling; Drag; Fingers; Immune system; Resistance; Vehicles; ANSYS CFX; bow skirt resistance; hovercraft; numerical simulation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Automation and Logistics (ICAL), 2012 IEEE International Conference on
Conference_Location :
Zhengzhou
ISSN :
2161-8151
Print_ISBN :
978-1-4673-0362-0
Electronic_ISBN :
2161-8151
Type :
conf
DOI :
10.1109/ICAL.2012.6308142
Filename :
6308142
Link To Document :
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