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Volume 12, Issue 2
1 February 1940
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 12, Issue 2
Review Article| February 01 1940

Aerofoil Sections and Torsion: Geometrical Properties of Symmetrical N.A.C.A. Aerofoils for use in Torsional Calculations

Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1940
Aircraft Engineering (1940) 12 (2): 44.
https://doi.org/10.1108/eb030608

The chart accompanying this note refers to symmetrical aerofoils of the N.A.C.A. family, but the ordinary magnitude of the mean camber will have no practical influence on the results if it is also used for non‐symmetrical aerofoils.

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© MCB UP Limited
1940
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