To read the full version of this content please select one of the options below:

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

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 February 1940

Abstract

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.

Citation

David, F. (1940), "Aerofoil Sections and Torsion: Geometrical Properties of Symmetrical N.A.C.A. Aerofoils for use in Torsional Calculations", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 2, pp. 44-44. https://doi.org/10.1108/eb030608

Publisher

:

MCB UP Ltd

Copyright © 1940, MCB UP Limited