Campion, B. S.2012-09-132012-09-131954-01http://dspace.lib.cranfield.ac.uk/handle/1826/7579The effects if distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers) are considered on a quasi-static basis. The method employed is based on the theory of Gates and Lyon but involves some extension of this theory.enReport