The weightshift controlled microlight aeroplane

Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/1234

Full metadata record

DC Field	Value	Language
dc.contributor.author	Gratton, GB	-
dc.coverage.spatial	9	en
dc.date.accessioned	2007-10-15T15:16:53Z	-
dc.date.available	2007-10-15T15:16:53Z	-
dc.date.issued	2001	-
dc.identifier.citation	Proceedings - Institution of Mechanical Engineers Part G, Journal of Aerospace Engineering. 215: 147-154, Aug 2001	en
dc.identifier.issn	0954-4100	-
dc.identifier.uri	http://bura.brunel.ac.uk/handle/2438/1234	-
dc.description.abstract	Microlight aircraft are increasingly becoming the most popular segment of private aviation. In the United Kingdom the majority (about 2500 of a total fleet of 3500) of these aircraft are of the weightshift class, also known as flexwings or trikes. This paper introduces the main issues involved in the design and operation of this class of aeroplane.	en
dc.format.extent	244733 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	Professional Engineering	en
dc.subject	Microlight	en
dc.subject	Weightshift	en
dc.subject	Rogallo	en
dc.subject	Ultralight	en
dc.subject	Flexwing	en
dc.subject	Trike	en
dc.title	The weightshift controlled microlight aeroplane	en
dc.type	Research Paper	en
Appears in Collections:	Aeronautics Mechanical and Aerospace Engineering Brunel Design School Research Papers

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