HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 10. STABILITY AND CONTROL

1965 ◽  
Author(s):  
HILLER AIRCRAFT CORP PALO ALTO CA
Keyword(s):  
Rotor System ◽  
Stability And Control ◽  
Heavy Lift ◽  
And Control ◽  
System Volume

The Helicopter Association of Great Britain

1961 ◽  
Vol 65 (601) ◽  
pp. 51-58
Author(s):  
J. W. Richardson
Keyword(s):  
Great Britain ◽  
Rotor System ◽  
Missing Link ◽  
Stability And Control ◽  
Rapid Sequence ◽  
Air Speed ◽  
And Control

It is reasonable to date the prehistory of the Helicopter Association from the arrival in this country of Juan de la Cierva in 1925, at the invitation of lames Weir and his Associates.The helicopter idea had intrigued designers from the earliest days of aeronautical experiment but, so far, often to their detriment and the derision of their contemporaries. Cierva had been first in translating the theory of auto-rotation into practical terms and had proved that both stability and control in flight could be achieved regardless of forward air speed. The freely rotating rotor system of the Cierva Autogiro and other early gyroplanes, such as those of Kay and Hafner, provided the missing link which all had been seeking and from this point development proceeded by logical rapid sequence to the flight of the first potentially safe and controllable helicopter in Germany in 1937.

HEAVY-LIFT TIP TURBOJET ROTOR SYSTEM. VOLUME 1

1965 ◽  
Author(s):  
HILLER AIRCRAFT CORP PALO ALTO CA
Keyword(s):  
Rotor System ◽  
Heavy Lift ◽  
System Volume

Stability and Control Characteristics of the Aerocrane Hybrid Heavy-Lift Vehicle

1980 ◽  
Vol 17 (10) ◽  
pp. 719-726 ◽  
Author(s):  
W. F. Putman ◽  
H. C. Curtiss
Keyword(s):  
Stability And Control ◽  
Heavy Lift ◽  
And Control

Nonlinear analysis of stability and control for an F-16 configuration

1997 ◽  
Author(s):  
Zhongjun Wang ◽  
Zhidai He ◽  
C. Lan ◽  
Zhongjun Wang ◽  
Zhidai He ◽  
...  
Keyword(s):  
Nonlinear Analysis ◽  
Stability And Control ◽  
Analysis Of Stability ◽  
And Control
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