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Static Wing‐Rib Tests: A Method of Calculating Approximate Values for the Loads to be Applied

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1934

Abstract

THE strength of main plane ribs for use on all British aircraft is determined by static tests of single representative ribs under conditions of loading determined from the characteristics of the aerofoil.

Citation

Clegg, A.W. (1934), "Static Wing‐Rib Tests: A Method of Calculating Approximate Values for the Loads to be Applied", Aircraft Engineering and Aerospace Technology, Vol. 6 No. 11, pp. 301-301. https://doi.org/10.1108/eb029871

Publisher

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MCB UP Ltd

Copyright © 1934, MCB UP Limited