Stalling speeds and determination of manoeuver speed for Rogallo-winged microlight airplanes

Please use this identifier to cite or link to this item: http://bura.brunel.ac.uk/handle/2438/2139

Full metadata record

DC Field	Value	Language
dc.contributor.author	Gratton, GB	-
dc.coverage.spatial	3	en
dc.date.accessioned	2008-05-02T10:52:37Z	-
dc.date.available	2008-05-02T10:52:37Z	-
dc.date.issued	2008	-
dc.identifier.citation	Journal of Aircraft 45(2): 723-725, Mar 2008	en
dc.identifier.issn	0021-8669	-
dc.identifier.uri	http://bura.brunel.ac.uk/handle/2438/2139	-
dc.description.abstract	Rogallo-winged airplanes can display a non-square law of stall speed versus loading. This Note shows, from experimental data, the form of this relationship and how this has been used during the certification of such airplanes, through operating data and modification of either maneuver speed or the normal acceleration limits	en
dc.format.extent	2275482 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	American Institute of Aeronautics and Astronautics	en
dc.subject	Rogallo	en
dc.subject	Microlight	en
dc.subject	Aeroelasticity	en
dc.subject	Flexwing	en
dc.title	Stalling speeds and determination of manoeuver speed for Rogallo-winged microlight airplanes	en
dc.type	Research Paper	en
Appears in Collections:	Mechanical and Aerospace Engineering Brunel Design School Research Papers

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