Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3

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dc.contributor.author P. R. Guyett en_US
dc.contributor.author J. K. Curran en_US
dc.date.accessioned 2014-10-21T15:54:58Z
dc.date.available 2014-10-21T15:54:58Z
dc.date.issued 1958 en_US
dc.identifier.other ARC/R&M-3171 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3740
dc.description.abstract A complete set of oscillatory aerodynamic stiffness and damping derivatives has been determined for a rectangular wing for rigid-wing modes of normal translation, pitch, and roll, in the range of frequency parameter 0.4 to 1.3, at low subsonic wind speeds. Each available comparison shows that the results are in satisfactory agreement with theoretical derivatives calculated by W. P. Jones and by Lawrence and Gerber. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title Aerodynamic derivative measurements on a rectangular wing of aspect ratio 3.3 en_US


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