MODEL STUDY OF HELICOPTER DYNAMIC STABILITY AND CONTROL. PHASE 2. COMPARISON OF THEORETICAL AND EXPERIMENTAL RESULTS NEAR HOVERING FLIGHT

1953 ◽  
Author(s):  
R. B. Gray ◽  
A. M. McCaskill ◽  
D. F. Gebhard ◽  
L. Goland
Keyword(s):  
Dynamic Stability ◽  
Experimental Results ◽  
Phase 2 ◽  
Hovering Flight ◽  
Control Phase ◽  
Stability And Control ◽  
Model Study ◽  
And Control

Demonstration of aircraft dynamic stability and response for aeronautical engineering students

1994 ◽  
Vol 98 (975) ◽  
pp. 192-193
Author(s):  
A.W. Bloy
Keyword(s):  
Dynamic Stability ◽  
Degrees Of Freedom ◽  
Engineering Students ◽  
Six Degrees Of Freedom ◽  
Stability And Control ◽  
Good Grasp ◽  
Aircraft Motion ◽  
Aeronautical Engineering ◽  
And Control ◽  
Aircraft Stability And Control

The teaching of aircraft stability and control at university usually progresses to the complexity of six degrees of freedom with a large array of aerodynamic, gravitational and inertial terms. It is therefore essential to ensure that students have a good grasp of fundamental dynamic characteristics such as damping and natural frequency, and any demonstration in which students observe aircraft motion is particularly helpful. At Manchester University this is achieved by a windtunnel demonstration of aircraft dynamic stability and response in pitch to a sinusoidal gust generator.

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