TY - GEN
T1 - The biomimetic propulsion of two tandem foils with different sizes
AU - Chao, Liming
AU - Fan, Guang
AU - Zhang, Dong
N1 - Publisher Copyright:
© 2017 IEEE.
PY - 2017/10/25
Y1 - 2017/10/25
N2 - With numerical studies of two tandem foils, the effect of size gaps and distance between two tandem foils on reducing drag is presented. A symmetric 4-digit NACA0012 foil has been used as the outline of leading foil, while the trailing foil has been redesigned as multiple of scale down of leading one, by which the size gaps between two tandem foil can be non-dimensionalized as a parameter Sg. Moreover, the ratios of the spatial gaps between two tandem foils to the length of leading foil have been used as another non-dimensionalized parameter Dg to describe the effect of distance gaps on drag reduce. As a result, it is found that the leading foil would enjoy the biggest drag reduction at Sg = 1 and Dg = 0.3, as 24%. It is also revealed that the trailing foils would also enjoy an drag reduction or thrust increase, and the biggest drag reduction of trailing foils has been observed as 67%, moreover, the trailing foil would increase thrust when Sg = 2, as the biggest value is 37%.
AB - With numerical studies of two tandem foils, the effect of size gaps and distance between two tandem foils on reducing drag is presented. A symmetric 4-digit NACA0012 foil has been used as the outline of leading foil, while the trailing foil has been redesigned as multiple of scale down of leading one, by which the size gaps between two tandem foil can be non-dimensionalized as a parameter Sg. Moreover, the ratios of the spatial gaps between two tandem foils to the length of leading foil have been used as another non-dimensionalized parameter Dg to describe the effect of distance gaps on drag reduce. As a result, it is found that the leading foil would enjoy the biggest drag reduction at Sg = 1 and Dg = 0.3, as 24%. It is also revealed that the trailing foils would also enjoy an drag reduction or thrust increase, and the biggest drag reduction of trailing foils has been observed as 67%, moreover, the trailing foil would increase thrust when Sg = 2, as the biggest value is 37%.
UR - http://www.scopus.com/inward/record.url?scp=85044753196&partnerID=8YFLogxK
U2 - 10.1109/OCEANSE.2017.8084704
DO - 10.1109/OCEANSE.2017.8084704
M3 - 会议稿件
AN - SCOPUS:85044753196
T3 - OCEANS 2017 - Aberdeen
SP - 1
EP - 4
BT - OCEANS 2017 - Aberdeen
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - OCEANS 2017 - Aberdeen
Y2 - 19 June 2017 through 22 June 2017
ER -