Aerodynamic mechanism of forces generated by twisting model-wing in bat flapping flight
The aerodynamic mechanism of the bat wing membrane Mong the lateral border of its body is studied. The twist-morphing that alters the angle of attack （AOA） along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along th...
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| Published in | Applied mathematics and mechanics Vol. 35; no. 12; pp. 1607 - 1618 |
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| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
Heidelberg
Shanghai University
01.12.2014
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| Subjects | |
| Online Access | Get full text |
| ISSN | 0253-4827 1573-2754 |
| DOI | 10.1007/s10483-014-1882-6 |
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| Abstract | The aerodynamic mechanism of the bat wing membrane Mong the lateral border of its body is studied. The twist-morphing that alters the angle of attack （AOA） along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along the span-wise direction. The plate with the aspect ratio of 3 is used to model a bat wing. A three-dimensional （3D） unsteady panel method is used to predict the aerodynamic forces generated by the flapping plate with leading edge separation. It is found that, relative to the rigid wing flapping, twisting motion can increase the averaged lift by as much as 25% and produce thrust instead of drag. Furthermore, the aerodynamic forces （lift/drag） generated by a twisting plate-wing are similar to those of a pitching rigid-wing, meaning that the twisting in bat flight has the same function as the supination/pronation motion in insect flight. |
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| AbstractList | The aerodynamic mechanism of the bat wing membrane Mong the lateral border of its body is studied. The twist-morphing that alters the angle of attack （AOA） along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along the span-wise direction. The plate with the aspect ratio of 3 is used to model a bat wing. A three-dimensional （3D） unsteady panel method is used to predict the aerodynamic forces generated by the flapping plate with leading edge separation. It is found that, relative to the rigid wing flapping, twisting motion can increase the averaged lift by as much as 25% and produce thrust instead of drag. Furthermore, the aerodynamic forces （lift/drag） generated by a twisting plate-wing are similar to those of a pitching rigid-wing, meaning that the twisting in bat flight has the same function as the supination/pronation motion in insect flight. The aerodynamic mechanism of the bat wing membrane along the lateral border of its body is studied. The twist-morphing that alters the angle of attack (AOA) along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along the span-wise direction. The plate with the aspect ratio of 3 is used to model a bat wing. A three-dimensional (3D) unsteady panel method is used to predict the aerodynamic forces generated by the flapping plate with leading edge separation. It is found that, relative to the rigid wing flapping, twisting motion can increase the averaged lift by as much as 25% and produce thrust instead of drag. Furthermore, the aerodynamic forces (lift/drag) generated by a twisting plate-wing are similar to those of a pitching rigid-wing, meaning that the twisting in bat flight has the same function as the supination/pronation motion in insect flight. O351.2%O355; The aerodynamic mechanism of the bat wing membrane along the lateral border of its body is studied. The twist-morphing that alters the angle of attack (AOA) along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along the span-wise direction. The plate with the aspect ratio of 3 is used to model a bat wing. A three-dimensional (3D) unsteady panel method is used to predict the aerodynamic forces generated by the flapping plate with leading edge separation. It is found that, relative to the rigid wing flapping, twisting motion can increase the averaged lift by as much as 25% and produce thrust instead of drag. Furthermore, the aerodynamic forces (lift/drag) generated by a twisting plate-wing are similar to those of a pitching rigid-wing, meaning that the twisting in bat flight has the same function as the supination/pronation motion in insect flight. |
| Author | 管子武 余永亮 |
| AuthorAffiliation | Department of Modern Mechanics, University of Science and Technology of China, Hefei 230027, P. R. China; The Laboratory for Biomechanics of Animal Locomotion,University of Chinese Academy of Sciences, Beijing 100049, P. R. China |
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| Cites_doi | 10.1146/annurev-fluid-121108-145456 10.1016/j.jtbi.2008.06.011 10.1242/jeb.02704 10.1242/bio.20122964 10.1088/1748-3182/1/4/S02 10.1088/1748-3182/8/1/016009 10.1242/jeb.029777 10.1007/BF02484543 10.1126/science.1142281 10.1126/science.284.5422.1954 10.1242/jeb.02446 10.2514/1.J051593 10.1038/321162a0 10.2514/3.13250 10.1242/jeb.00739 10.2514/1.J050827 10.1016/S0029-8018(98)00018-3 10.1016/j.jfluidstructs.2012.12.005 10.1017/S002211200200143X 10.1017/CBO9780511810329 10.1126/science.1153019 10.1063/1.4794753 10.1242/jeb.008649 10.1007/s10409-005-0032-z 10.1242/jeb.205.1.55 10.1242/jeb.59.1.169 10.1242/jeb.65.1.179 10.1242/jeb.126.1.479 10.1242/jeb.65.2.459 10.1242/jeb.199.5.1073 |
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| Copyright | Shanghai University and Springer-Verlag Berlin Heidelberg 2014 Copyright © Wanfang Data Co. Ltd. All Rights Reserved. |
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| Notes | Zi-wu GUAN , Yong-liang YU The aerodynamic mechanism of the bat wing membrane Mong the lateral border of its body is studied. The twist-morphing that alters the angle of attack （AOA） along the span-wise direction is observed widely during bat flapping flight. An assumption is made that the linearly distributed AOA is along the span-wise direction. The plate with the aspect ratio of 3 is used to model a bat wing. A three-dimensional （3D） unsteady panel method is used to predict the aerodynamic forces generated by the flapping plate with leading edge separation. It is found that, relative to the rigid wing flapping, twisting motion can increase the averaged lift by as much as 25% and produce thrust instead of drag. Furthermore, the aerodynamic forces （lift/drag） generated by a twisting plate-wing are similar to those of a pitching rigid-wing, meaning that the twisting in bat flight has the same function as the supination/pronation motion in insect flight. 31-1650/O1 bat wing, twisting, panel method, aerodynamic mechanism ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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| PublicationTitle | Applied mathematics and mechanics |
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| PublicationYear | 2014 |
| Publisher | Shanghai University |
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| Snippet | The aerodynamic mechanism of the bat wing membrane Mong the lateral border of its body is studied. The twist-morphing that alters the angle of attack （AOA）... The aerodynamic mechanism of the bat wing membrane along the lateral border of its body is studied. The twist-morphing that alters the angle of attack (AOA)... O351.2%O355; The aerodynamic mechanism of the bat wing membrane along the lateral border of its body is studied. The twist-morphing that alters the angle of... |
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| SubjectTerms | Aerodynamics Applications of Mathematics Bats Classical Mechanics Drag Flapping wings Fluid- and Aerodynamics Lift Mathematical Modeling and Industrial Mathematics Mathematical models Mathematics Mathematics and Statistics Partial Differential Equations Three dimensional Twisting Wings (aircraft) 动力学机理 扑翼 扭动 昆虫飞行 机制 模型 空气动力 蝙蝠 |
| Title | Aerodynamic mechanism of forces generated by twisting model-wing in bat flapping flight |
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