Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/7513
Title: Study of the effect of leading-edge tubercles on the aerodynamics performance of an airfoil
Authors: Bassil, Charbel
Advisors: Sabat, Macole 
Keywords: Tubercles; Aspect ratio; Stall; Coefficient of lift; Leading edge; Laminar separation bubble
Subjects: University of Balamand--Dissertations
Dissertations, Academic
Issue Date: 2024
Publisher: [Kalhat, Lebanon] : [University of Balamand], 2024
Abstract: 
A bumpy anatomy characterizes the flippers of the humpback whales, basically described by
its tubercle structures. Inspired by this, innovative airfoil designs have been introduced to
enhance aerodynamic performance. In the present work, biomechanics of flippers from
humpback whales were analyzed and applied to improve airfoil design in lift performance.
This Thesis examines flow characteristics around an airfoil with leading-edge tubercles
through a combination of computational fluid dynamics simulations. The results that were
obtained show that airfoils with tubercles delayed the stall compared to conventional airfoils.
Thus that applying some of the biomimetic features of flippers from humpback whales to an
airfoil design may improve its aerodynamic performance, with possible applications in
aeronautics, wind energy, and undersea vehicle propulsion.
Description: 
Includes bibliographical references (p. 42-43)
URI: https://scholarhub.balamand.edu.lb/handle/uob/7513
Rights: This object is protected by copyright, and is made available here for research and educational purposes. Permission to reuse, publish, or reproduce the object beyond the personal and educational use exceptions must be obtained from the copyright holder
Type: Thesis
Appears in Collections:UOB Theses and Projects

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