Study of dynamic stability of helicopter with hinged rotor blades under hovering conditions; possibility of controlled stability is proved by successful flights of various helicopters, particularly of universally known Focke. From Ingenieur-Archiv Dec 1938.
Dynamic stability of helicopter with hinged rotor blades
Nat Advisory Committee Aeronautics -- Tech Memo
1939
17 pages
1 Supp plate
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Stability and Control of Single Rotor Helicopter with Hinged Blades
Emerald Group Publishing | 1949
|Engineering Index Backfile | 1955
|Engineering Index Backfile | 1955
|The Stiff-hinged Helicopter Rotor
Emerald Group Publishing | 1955
|