Theoretical studies have predicted that it is desirable to design rotors for operation close to limits imposed by blade stalling; experimental investigation was needed to determine whether, in actual practice, stall did occur and spread as predicted and to establish amount of stalling that could be present without severe vibration or control difficulties being introduced.
Stalling of helicopter blades
Nat Advisory Committee Aeronautics -- Report
1946
6 pages
Results
Report
Englisch
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NTRS | 1946
|NTRS | 1946
|Engineering Index Backfile | 1946
|TIBKAT | 1946
|The Stalling of Airscrew Blades
Emerald Group Publishing | 1945
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