Supersonic theory for oscillating wings of any plan form

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dc.contributor.author W. P. Jones en_US
dc.date.accessioned 2014-10-21T15:52:10Z
dc.date.available 2014-10-21T15:52:10Z
dc.date.issued 1948 en_US
dc.identifier.other ARC/R&M-2655 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3195
dc.description.abstract Summary.--A theory for thin wings of any plan form describing simple harmonic oscillations of small amplitude in a supersonic air stream is developed. It is based on the use of the generalised Green\\'s Theorem in conjunction with particular solutions which vanish over the charadteristic cone with vertex at any point in the field of flow. The theory can be used to calculate tile aerodynamic forces acting on fluttering wings when the modes of distortion are known. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Supersonic theory for oscillating wings of any plan form en_US


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