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The Estimation of the Lift due to Full and Part Span Controls

Published online by Cambridge University Press:  28 July 2016

J. C. Simmons  and
J. A. Dunsby
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Extract

This note describes an investigation of experimental and theoretical data on the lift increment due to the deflection of full and part span controls. For full span controls, existing Data Sheets in the Royal Aeronautical Society Aerodynamics series are found to be inadequate for some of the plan forms currently in use, but the investigation shows that with one additional set of curves the sheets may be applied to almost any plan form. For part span conversion factors, a revision also is proposed.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 60 , Issue 548 , August 1956 , pp. 545 - 549
Copyright
Copyright © Royal Aeronautical Society 1956

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References

1.Royal Aeronautical Society. Aerodynamics Data Sheets.Google Scholar
2. Multhopp, H. (1955). Methods for Calculating the Lift Distribution on Wings (Subsonic Lifting-Surface Theory). A.R.C. R. & M. No. 2884, 1955.Google Scholar
3. Deyoung, J. (1952). Theoretical Symmetric Span Loading Due to Flap Deflection for Wings of Arbitrary Plan Form at Subsonic Speeds. N.A.C.A. Report 1071, 1952.Google Scholar