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Aeronautical Progress 19301936

Aeronautical Progress 19301936 MUCH has been said earlier concerning the scale effect on drag. A few words must be added on the scale effect on lift near the stall, for it is here that ordinary smallscale wind tunnel tests may be very misleading. The curves of Fig. 9 show the maximum lift coefficient of two wing sections plotted against Reynolds number, and the difference of behaviour is at once apparent. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aircraft Engineering and Aerospace Technology Emerald Publishing

Aeronautical Progress 19301936

Relf, E.F.
Aircraft Engineering and Aerospace Technology , Volume 8 (7): 9 – Jul 1, 1936
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Publisher
Emerald Publishing
Copyright
Copyright © Emerald Group Publishing Limited
ISSN
0002-2667
DOI
10.1108/eb030066
Publisher site
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Abstract

MUCH has been said earlier concerning the scale effect on drag. A few words must be added on the scale effect on lift near the stall, for it is here that ordinary smallscale wind tunnel tests may be very misleading. The curves of Fig. 9 show the maximum lift coefficient of two wing sections plotted against Reynolds number, and the difference of behaviour is at once apparent.

Journal

Aircraft Engineering and Aerospace Technology – Emerald Publishing

Published: Jul 1, 1936

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