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.
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
MCB UP Ltd
Copyright © 1934, MCB UP Limited