System consists of freely rotating rotor in which opposite blades are rigidly connected and allowed to rotate freely about their span axis; equations for lift, lift-drag ratio, angle of attack, feathering angles, and rolling and pitching moments of gyroplane rotor in terms of its basic parameters; investigation discloses that aerodynamic principles of gyroplane are sound.
Aerodynamic analysis of gyroplane rotating-wing system
Nat Advisory Committee Aeronautics -- Tech Note
1934
6 Supp plates
Report
English
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Aerodynamic Characteristics of a Gyroplane Configuration
AIAA | 1998
|Aerodynamic Characteristics of a Gyroplane Configuration
Online Contents | 1998
|Engineering Index Backfile | 1938
|Engineering Index Backfile | 1937