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Please use this identifier to cite or link to this item: http://dspace.lib.cranfield.ac.uk/handle/1826/7579

Document Type: Report
Title: Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)
Authors: Campion, B. S.
Issue Date: Jan-1954
Abstract: The 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.
URI: http://dspace.lib.cranfield.ac.uk/handle/1826/7579
Appears in Collections:College of Aeronautics Reports

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