The present paper treats less of the effect of the union (of spars and ribs, namely, the reduction of the bending moment at the fixed ends of the spars) than of its influence on the torsional rigidity of the wing. The calculations are carried out for a two-spar wing of constant cross section, in which the ribs are replaced by a continuous member of constant rigidity.
Torsional rigidity of cantilever wings with constant spar and rib sections
1929-07-01
Miscellaneous
No indication
English
Torsional rigidity in cantilever wings
Engineering Index Backfile | 1931
|Engineering Index Backfile | 1936
|Frequencies of cantilever wings in beam and torsional vibrations
Engineering Index Backfile | 1940
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