DESIGN, FABRICATION AND BENCH TEST OF FLAPPING WING AERIAL VEHICLE

Simple item page
dc.contributor.advisorKayastha, Rajesh Kaji
dc.contributor.authorYadav, Anil Kumar
dc.contributor.authorTimsina, Ashmit
dc.contributor.authorMagar, Gopal Thada
dc.contributor.authorThapa, Santosh
dc.date.accessioned2024-08-13T07:03:27Z
dc.date.available2024-08-13T07:03:27Z
dc.date.issued2024-03-13
dc.descriptionThis project presents the comprehensive development and completion of a flapping wing mechanism, encompassing critical aspects including CAD modeling, gearbox design, wing structure design, tail design and overall body fabrication.
dc.description.abstractThis project presents the comprehensive development and completion of a flapping wing mechanism, encompassing critical aspects including CAD modeling, gearbox design, wing structure design, tail design and overall body fabrication. Our efforts have culminated in the successful realization of a large-scale ornithopter, colloquially termed the flapping wing bird, intended to serve as a platform for the study of flapping wing flight control. On moving forward, our project has successfully performed bench tests including wind tunnel experiments for lift analysis through the load cell, smoke flow visualization and tuft flow analysis to validate the functionality, performance and aerodynamics of the developed flapping wing mechanism. The successful completion of this project marks a significant milestone in the advancement of flapping wing technology, demonstrating its potential for various applications in aerodynamics, bio-mimicry, and unmanned aerial vehicles
dc.identifier.urihttps://hdl.handle.net/20.500.14540/22682
dc.language.isoen
dc.publisherI.O.E
dc.subjectOrnithopter
dc.subjectFlapping wing mechanism
dc.subjectWind tunnel experiment
dc.subjectAerodynamics
dc.titleDESIGN, FABRICATION AND BENCH TEST OF FLAPPING WING AERIAL VEHICLE
dc.typeTechnical Report
local.academic.levelOther
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
Yadav, Anil K et al. 076 mechanical and aero project report March 2024.pdf
Size:
21.75 MB
Format:
Adobe Portable Document Format
Download
License bundle
Now showing 1 - 1 of 1
No Thumbnail Available
Name:
license.txt
Size:
1.71 KB
Format:
Item-specific license agreed upon to submission
Description:
Download
Collections
Mechanical and Aerospace Engineering