Aileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristics

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dc.contributor.authorRadok, J. R. M.
dc.date.accessioned2012-07-25T14:27:42Z
dc.date.available2012-07-25T14:27:42Z
dc.date.issued1952-03
dc.description.abstractUsing oblique coordinates, the static problems of Aero-elasticity for swept wings are reduced to the solution of integral – or matrix equations, which may be solved by iteration. The present treatment also indicates the suitability of integral equations for fundamental aero-elastic investigations. Continues …en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/7420
dc.language.isoenen_UK
dc.publisherCollege of Aeronautics, Cranfielden_UK
dc.relation.ispartofseriesCollege Reporten_UK
dc.relation.ispartofseries55en_UK
dc.titleAileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristicsen_UK
dc.typeReporten_UK

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