Structure analysis on design and fabrication of UAV capable of carrying maximum payload under given constraints

Please use this identifier to cite or link to this item: https://dr.ddn.upes.ac.in//xmlui/handle/123456789/3202

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DC Field	Value	Language
dc.contributor.author	Gupta, Abhay	-
dc.contributor.author	Takkar, Mangesh	-
dc.date.accessioned	2021-04-20T10:55:41Z	-
dc.date.available	2021-04-20T10:55:41Z	-
dc.date.issued	2013-05	-
dc.identifier.citation	Under the supervision of Prof. Viiav Kumar Patidar	en_US
dc.identifier.uri	http://hdl.handle.net/123456789/3202	-
dc.description	The dissertation report was submitted in partial fulfillment for the requirement of the degree of B. Tech (Aerospace Engineering)	en_US
dc.language.iso	en	en_US
dc.publisher	College of Engineering, UPES, Dehradun	en_US
dc.subject	Dissertation	en_US
dc.subject	Aerospace Engineering	en_US
dc.subject	Aircraft Sizing	en_US
dc.subject	Structural Analysis	en_US
dc.subject	Structural Optimization	en_US
dc.subject	Fabrication Scheduling	en_US
dc.subject	Fabrication Budgeting	en_US
dc.title	Structure analysis on design and fabrication of UAV capable of carrying maximum payload under given constraints	en_US
dc.type	Thesis	en_US
Appears in Collections:	Under Graduate

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