This report deals with an investigation carried out in the Civil Engineering Laboratory of the University of California, to determine the accuracy of existing methods of computing the stresses in an airplane fuselage when subjected to torsion, and to derive a simple approximate formula for the rapid calculation of these stresses.
A Short Method of Calculating Torsional Stresses in an Airplane Fuselage
1924-09-01
Sonstige
Keine Angabe
Englisch
A short method of calculating torsional stresses in an airplane fuselage
Engineering Index Backfile | 1924
|Torsional stresses in the fuselage of an aeroplane
TIBKAT | 1921
|Torsional stresses in the fuselage of an aeroplane
SLUB | 1921
|Analysis of torsional stresses in airplane wings
Engineering Index Backfile | 1929
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