Maximum Lift Data for Symmetrical Wings
- 1 January 1955
- journal article
- Published by Emerald Publishing in Aircraft Engineering and Aerospace Technology
- Vol. 27 (1) , 2-8
- https://doi.org/10.1108/eb032510
Abstract
We shall attempt here to summarize the existing data on the values of the low‐speed CLmax. of wings, in the absence of a fuselage, and without including information on stalling incidence or pitching moment. The summary is limited to the consideration of unswept wings, and those of delta plan form, which have symmetrical sections: there is some discussion of the maximum lift increments due to the use of flaps of various kinds.Keywords
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