In the foregoing remarks I have made an attempt to touch on some of the structural problems met with in cantilever wings, and dealt rather fully with a certain type of single-spar construction. The experimental test wing was a first attempt to demonstrate the principles of this departure from orthodox methods. The result was a wing both torsionally stiff and of light weight - lighter than a corresponding biplane construction.
Cantilever Wings for Modern Aircraft: Some Aspects of Cantilever Wing Construction with Special Reference to Weight and Torsional Stiffness
01.11.1929
Sonstige
Keine Angabe
Englisch
Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Cantilever Wings for Modern Aircraft
Emerald Group Publishing | 1929
|Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|Cantilever wings for modern aircraft
Engineering Index Backfile | 1929
|