Investigation into the use of Segmented Control Surfaces in Aircrafts

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dc.contributor.advisorAbdullah, Masuk
dc.contributor.authorBawa, Asulada
dc.contributor.departmentDE--Műszaki Kar
dc.date.accessioned2025-03-04T09:59:16Z
dc.date.available2025-03-04T09:59:16Z
dc.date.created2024-11-22
dc.description.abstractThis thesis explores the use of segmented control surfaces in modern aircraft for improved aerodynamic performance, redundancy, and adaptability. Using computational and experimental approaches, it demonstrates higher efficiency and structural benefits, particularly for UAV flights and high-performance aircraft. The research addresses challenges in actuation, integration, and certification, focusing on advanced materials and modular design for scalability. Future applications include military, UAV, and commercial aviation, offering advantages like noise reduction, acoustic performance, passenger comfort, and environmental sustainability.
dc.description.courseVehicle Engineering
dc.description.degreeBSc/BA
dc.format.extent49
dc.identifier.urihttps://hdl.handle.net/2437/387817
dc.language.isoen
dc.rights.accessHozzáférhető a 2022 decemberi felsőoktatási törvénymódosítás értelmében.
dc.subjectFlow Dynamics
dc.subjectSegmented Control Surfaces
dc.subjectFlight Optimization
dc.subjectWing Segmentation
dc.subject.dspaceEngineering Sciences
dc.titleInvestigation into the use of Segmented Control Surfaces in Aircrafts
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