Two‐Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 October 1949
Abstract
Notation. A cross‐section, plan and a perspective view of cell n are given in FIG. 4.
Citation
Goodey, W.J. (1949), "Two‐Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen", Aircraft Engineering and Aerospace Technology, Vol. 21 No. 10, pp. 313-319. https://doi.org/10.1108/eb031816
Publisher
:MCB UP Ltd
Copyright © 1949, MCB UP Limited