Investigation carried out to determine stress distribution in stiffened conical and orthogonal cylindrical shells cut by planes and subjected to torsional moments; such shells are frequently encountered in aircraft design; for example, cockpit enclosure trays and floors in fuselages, sloping frames and spars in wings; diagrams presented.
Torsion in conical and cylindrical shells intersected by planes
Aircraft Eng
Aircraft Engineering ; 18 , n 208
1946
6 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Torsion in Conical and Cylindrical Shells Intersected by Planes
Emerald Group Publishing | 1946
|