FOR the past fifteen years nearly all aircraft structures have been of the shell or stressed-skin type and problems pertaining to this type of structure have been steadily tackled and finally solved for practical use by the designers.
A Solution to the Problem of Torsion-Flexure
A Method of Using the Principle of Least Work and Calculus of Variations to Establish the Potential Energy Integrals
Aircraft Engineering and Aerospace Technology ; 22 , 11 ; 335-337
1950-11-01
3 pages
Article (Journal)
Electronic Resource
English
Solution to problem of torsion-flexure
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1939
|Emerald Group Publishing | 1939
|On flexure-torsion flutter criteria
Online Contents | 1999
|Flexure-Torsion Failure of Panels
Emerald Group Publishing | 1954
|