New approach to calculation of bending strength of semi-monocoque (and possibly fully monocoque) fuselage shells; method uses directly load deflection graphs obtained from laboratory compression tests on panels representative of shell at section under consideration, and is analogous to calculation of form factor for solid beam section.
Bending of fuselage shells
Aircraft Eng
Aircraft Engineering ; 21 , n 243
1949
6 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
The Bending of Fuselage Shells
Emerald Group Publishing | 1949
|Engineering Index Backfile | 1944
|Integral Solutions for Fuselage Shells
British Library Conference Proceedings | 2001
|FRAME FOR FUSELAGE SHELLS OF AN AIRCRAFT AND FUSELAGE SHELL
European Patent Office | 2020
|Frame for fuselage shells of an aircraft and fuselage shell
European Patent Office | 2022
|