Please use this identifier to cite or link to this item: https://scholarhub.balamand.edu.lb/handle/uob/7513
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dc.contributor.advisorSabat, Macoleen_US
dc.contributor.authorBassil, Charbelen_US
dc.date.accessioned2024-09-17T12:29:03Z-
dc.date.available2024-09-17T12:29:03Z-
dc.date.issued2024-
dc.identifier.urihttps://scholarhub.balamand.edu.lb/handle/uob/7513-
dc.descriptionIncludes bibliographical references (p. 42-43)en_US
dc.description.abstractA 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.en_US
dc.description.statementofresponsibilityby Charbel Bassilen_US
dc.format.extent1 online resource (xi, 43 pages) : ill., tablesen_US
dc.language.isoengen_US
dc.publisher[Kalhat, Lebanon] : [University of Balamand], 2024en_US
dc.rightsThis 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 holderen_US
dc.subjectTubercles; Aspect ratio; Stall; Coefficient of lift; Leading edge; Laminar separation bubbleen_US
dc.subject.lcshUniversity of Balamand--Dissertationsen_US
dc.subject.lcshDissertations, Academicen_US
dc.titleStudy of the effect of leading-edge tubercles on the aerodynamics performance of an airfoilen_US
dc.typeThesisen_US
dc.contributor.corporateUniversity of Balamanden_US
dc.contributor.departmentDepartment of Mechanical Engineeringen_US
dc.contributor.facultyFaculty of Engineeringen_US
dc.contributor.institutionUniversity of Balamanden_US
dc.date.catalogued2024-09-17-
dc.description.degreeMS in Mechanical Engineeringen_US
dc.description.statusUnpublisheden_US
dc.relation.ispartofbookseriesUniversity of Balamand. Thesis. Mecen_US
dc.rights.accessrightsThis item is not approved for publicationen_US
Appears in Collections:UOB Theses and Projects
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