THE effect of axial constraint on box beams of approximately rectangular section, subject to torsion, is of interest to the aircraft designer in connexion with the stressing of two-spar skin-covered wings. The stresses due to torsion in a uniform box with one end built-in have been investigated by D. Williams, both by rigid methods and using the ordinary “engineer's” theory of bending. Three simple types of loading are considered:—
Torsion in Box Beams
Some Notes on the Effect of End Constraint in Torsion Boxes of Rectangular Section
Aircraft Engineering and Aerospace Technology ; 14 , 1 ; 2-8
01.01.1942
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Engineering Index Backfile | 1942
|Emerald Group Publishing | 1942
Modeling piezoceramic actuation of beams in torsion
AIAA | 1996
|Modeling Piezoceramic Actuation of Beams in Torsion
British Library Conference Proceedings | 1994
|Modeling Piezoceramic Actuation of Beams in Torsion
Online Contents | 1996
|