The longitudinal static stability of tailless aircraft

de Castro, Helena V.

dc.contributor.author	de Castro, Helena V.	en_UK
dc.date	2001	en_UK
dc.date.accessioned	2005-11-23T12:20:10Z
dc.date.available	2005-11-23T12:20:10Z
dc.date.issued	2001	en_UK
dc.identifier.uri	http://hdl.handle.net/1826/228
dc.description.abstract	This paper describes the development of a simple theory of the longitudinal controls fixed static stability of tailless aeroplanes. The classical theory, as developed for the conventional aircraft, is modified to accommodate the particular features of the tailless aeroplanes. The theory was then applied to a particular blended-wing-body tailless civil transport aircraft, BWB-98.	en_UK
dc.description.sponsorship	Cranfield University	en_UK
dc.format.extent	1963 bytes
dc.format.extent	1026760 bytes
dc.format.mimetype	text/plain
dc.format.mimetype	application/pdf
dc.language.iso	en_UK	en_UK
dc.relation.ispartofseries	College of Aeronautics Report;2001/0018/1	en_UK
dc.relation.ispartofseries	CU/CoA;2001/0018/1	en_UK
dc.title	The longitudinal static stability of tailless aircraft	en_UK
dc.type	Technical Report	en_UK