Two-dimensional impervious sails: experimental results compared with theory

Author:

Newman B. G.,Low H. T.

Abstract

Experiments have been made on quasi two-dimensional sails of small camber and at small incidence. Four excess-length ratios have been tested at a Reynolds number of 1.2 x 105. The results for lift, tension, centre of lift, maximum camber and its position, and leading- and trailing-edge membrane angles have been compared with existing inviscid theories and show poor agreement in general. This is attributed to leading- and trailing-edge flow separations as indicated by supplementary flow-visualization experiments. The optimum incidences in particular are much greater than the theoretical value of 0°. Luffing occurs at slightly negative incidences and appears to be a dynamic instability. The highest lift-to-drag ratio obtained was 16.5 on a membrane with an excess-length ratio of 0.03.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference24 articles.

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4. Murai, H. & Maruyama, S. 1980 Theoretical investigation of the aerodynamics of double membrane sailwing aerofoil sections.J. Aircraft 17,294–299.

5. Milgram, J. H. 1971 Sail force coefficients for systematic rig variations.Soc. Nav. Arch. and Mar. Engng T. & R. Rep. R-10.

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