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The induced drag on a rolling wing

Published online by Cambridge University Press:  04 July 2016

G. J. Hancock
G. J. Hancock*
Affiliation:
Department of Aeronautical Engineering, Queen Mary College, University of London
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Extract

In a recent paper Garner discusses, among other topics, the induced (inviscid) drag or lift dependent drag, on finite wings which have effective antisymmetric incidence distributions. One example concerns a finite wing whose incidence varies linearly in the spanwise direction as

This wing experiences an overall induced drag which is made up from two contributions.

Type
Technical notes
Information
The Aeronautical Journal , Volume 76 , Issue 742 , October 1972 , pp. 617 - 620
Copyright
Copyright © Royal Aeronautical Society 1972 

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References

1. Garner, H. C. Theoretical lift-dependent yawing moment on a swept wing in subsonic flow with spanwise asymmetry NPL Aero Note 1084. January 1970.Google Scholar