Some experimental and theoretical studies in aircraft stability at high angles of attack
A review of techniques for stability and response investigations is presented and the averaging technique of Beecham- Titchener-Simpson is applied to the lateral equations of. motion for two combat aircraft. The analytic technique predicts oscillation amplitudes and frequencies accurately, for non-l...
| Main Author: | |
|---|---|
| Other Authors: | |
| Language: | en |
| Published: |
Cranfield University
2009
|
| Online Access: | http://hdl.handle.net/1826/3673 |