Applications of dynamic stability parametes to problems in aircraft dynamics
Abstract
The application and analysis of dynamic stability parameters were examined. The effects of wing leading edge modifications on the stalling and spinning characteristics of a single engine general aviation research airplane are evaluated. It is illustrated how dynamic stability parameters measured in wind tunnel tests are used to predict the spin resistance of this class of aircraft, and that autorotation criteria are derived from the relationships which exist between static and dynamic aerodynamic characteristics.
- Publication:
-
In AGARD Dyn. Stability Parameters 12 p (SEE N81-31105 22-01
- Pub Date:
- May 1981
- Bibcode:
- 1981dsp..agar.....C
- Keywords:
-
- Aircraft Performance;
- Dynamic Stability;
- Dynamic Tests;
- Flight Characteristics;
- Parameter Identification;
- Stability Derivatives;
- Aerodynamic Configurations;
- Aircraft Spin;
- Angle Of Attack;
- Mathematical Models;
- Wind Tunnel Tests;
- Instrumentation and Photography