DESIGN AND FABRICATION OF ELECTRIC DUCTED FAN FOR Unmanned Aerial Vehicles

dc.contributor.author	Muhammad Abdullah Baig, Anees Hassan Khan ,Syeda Saneeha Naqvi, Bilal Ahmed
dc.date.accessioned	2023-08-29T04:44:43Z
dc.date.available	2023-08-29T04:44:43Z
dc.date.issued	2023
dc.identifier.uri	http://10.250.8.41:8080/xmlui/handle/123456789/37752
dc.description	Supervisor: Dr. Emad ud Din	en_US
dc.description.abstract	This thesis demonstrates the designing and fabricating procedure of electric ducted fans (EDF) used in aerospace and other applications. The primary design parameters include the blade design, duct length, duct shape, duct diameter, and duct clearance. The blade design is critical in determining the thrust, power, and efficiency of the fan. The duct design parameters such as length, shape, diameter, and clearance have significant impacts on the aerodynamics and performance of the fan. It is crucial to optimize these parameters to achieve the desired balance between performance, efficiency, and structural integrity of the fan. Computational fluid dynamics (CFD) simulations and Finite Element Analysis (FEA) are useful tools for optimizing these design parameters.	en_US
dc.language.iso	en	en_US
dc.publisher	School of Mechanical & Manufacturing Engineering (SMME), NUST	en_US
dc.relation.ispartofseries	SMME-FYP-303;
dc.title	DESIGN AND FABRICATION OF ELECTRIC DUCTED FAN FOR Unmanned Aerial Vehicles	en_US
dc.type	Thesis	en_US