Numerical Analysis of High Aspect Ratio Flexible Wings in Flapping Motion

Numerical Analysis of High Aspect Ratio Flexible Wings in Flapping Motion

Wing geometry, kinematics and flexibility are the fundamental components which contribute towards the aerodynamics performance of micro aerial vehicles. This research focuses on determining the role of isotropic flexibility in the aerodynamic performance of high aspect ratio (AR = 6.0) wings with di...

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Bibliographic Details
Main Authors:	A. Shahzad, M. N. Mumtaz Qadri, S. Ahmad
Format:	Article
Language:	English
Published:	Isfahan University of Technology 2019-01-01
Series:	Journal of Applied Fluid Mechanics
Subjects:	Flapping wings; Wing shape; Aspect ratio; Fluid-structure interaction; Micro aerial vehicle.
Online Access:	http://jafmonline.net/JournalArchive/download?file_ID=50122&issue_ID=1003

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