Tapered Beams: Suggested Solutions for Some Typical Aircraft Cases

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