The longitudinal static stability of tailless aircraft

Show simple item record de Castro, Helena V. en_UK 2001 en_UK 2005-11-23T12:20:10Z 2005-11-23T12:20:10Z 2001 en_UK
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

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