Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases
Aircraft Engineering and Aerospace Technology
ISSN: 0002-2667
Article publication date: 1 December 1938
Abstract
PART III.—Taper Beams with uniform thin webs and concentrated booms of constant cross‐sectional area. This type of girder is shown in Fig. 1.
Citation
Atkin, E.H. (1938), "Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases", Aircraft Engineering and Aerospace Technology, Vol. 10 No. 12, pp. 371-374. https://doi.org/10.1108/eb030409
Publisher
:MCB UP Ltd
Copyright © 1938, MCB UP Limited