Predicted on assumption of certain normal conditions, for engine and propeller, simple expressions for static and dynamic stresses of propeller blade roots are evolved. English translation of paper indexed in Engineering Index 1941 p 59, from Luftfahrtforschung Apr 22 1941.
Design of propeller blade roots
Nat Advisory Committee Aeronautics -- Tech Memo
1942
14 pages
4 Supp plates
Report
English
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