THE methods and formula outlined below are applicable to any shape of fuselage, but an elliptical one is assumed to serve as an illustration.
Tapered Spar Frames
An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage
Aircraft Engineering and Aerospace Technology ; 13 , 4 ; 90-94
1941-04-01
5 pages
Article (Journal)
Electronic Resource
English
Engineering Index Backfile | 1941
|Emerald Group Publishing | 1941
Stiffness matrix for a tapered spar element
TIBKAT | 1970
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