de Castro, Helena V.2005-11-232005-11-232001http://hdl.handle.net/1826/228This 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-98.1963 bytes1026760 bytestext/plainapplication/pdfen-UKTechnical Report