By assumption of standard distribution of load, it is possible to calculate rapidly corresponding resultant aerodynamic bending moment at any given fraction of blade radius.
Airscrew blade stressing
Flight
Flight ; 37 , n 1644
1940
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Emerald Group Publishing | 1940
|SLUB | 1937
|Engineering Index Backfile | 1941
|TIBKAT | 1937
|Emerald Group Publishing | 1943
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