Condition for best thrust distribution with least losses is fulfilled by arrangement in which induced efficiency of annular parts varies within internal and external limit; thrust and performance of this propeller are compared with ideal machine. Bibliography. English translation of paper indexed in Engineering Index 1941 p 59, from Luftfahrtforschung Apr 22 1941.
Contribution to ideal efficiency of screw propellers
Nat Advisory Committee Aeronautics -- Tech Memo
1942
25 pages
3 Supp plates
Report
English
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