FABRICATION, STRUCTURAL INTEGRITY, AND DYNAMIC RESPONSE OF A CARBON FIBER WING WITH STUDY ON MATERIAL PROPERTIES AND VIBRATION CHARACTERIZATION

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dc.contributor.advisorAdhikari, Surya Prasad
dc.contributor.authorShrestha, Bikesh
dc.contributor.authorKarki, Gaurav Jung
dc.contributor.authorShrestha, Manish
dc.contributor.authorParajuli, Utsav
dc.date.accessioned2025-10-15T05:14:59Z
dc.date.available2025-10-15T05:14:59Z
dc.date.issued2025-03
dc.descriptionThis study focuses on the design, fabrication, and analysis of a carbon fiber composite wing for UAV applications, aiming to optimize strength, weight, and durability.
dc.identifier.urihttps://hdl.handle.net/20.500.14540/25275
dc.language.isoen
dc.publisherI.O.E
dc.subjectCarbon Fiber Composite
dc.subjectStructural Integrity
dc.subjectWing Fabrication
dc.subjectAeroelasticity
dc.titleFABRICATION, STRUCTURAL INTEGRITY, AND DYNAMIC RESPONSE OF A CARBON FIBER WING WITH STUDY ON MATERIAL PROPERTIES AND VIBRATION CHARACTERIZATION
dc.typeProject Report
local.academic.levelOther
local.institute.titleInstitute of Engineering

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