The effect of sweepback on the fundamental derivative coefficient for flexural motion

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dc.contributor.author J. B. Bratt en_US
dc.contributor.author K. C. Wight en_US
dc.date.accessioned 2014-10-21T15:52:47Z
dc.date.available 2014-10-21T15:52:47Z
dc.date.issued 1950 en_US
dc.identifier.other ARC/R&M-2774 en_US
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/3327
dc.description.abstract Measurements have been made with new equipment designed for derivative tests in a 9 x 7 ft tunnel, to determine the effect of sweepback on the derivatives for a rectangular aerofoil of aspect ratio 6. Some difficulty was experienced in the interpretation of the measurements on the swept aerofoil due to distortion of the model during oscillation. The effect is examined in detail in an appendix and a method of correction devised. A comparison between measurements for the unswept aerofoil and earlier measurements made with the same model by the method of decaying oscillations gives satisfactory agreement. en_US
dc.relation.ispartofseries Aeronautical Research Council Reports & Memoranda en_US
dc.title The effect of sweepback on the fundamental derivative coefficient for flexural motion en_US


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