Kinematic Coupling Analysis of Autorotation Flying Body
The kinematic coupling dynamic stability has been analyzed .The Laplace transformation and the coefficient matrix determinant are used to find the rolling stability characteristic equation. The effect of parameters is investigated with different value of roll rate . It is found that the kinematics c...
Saved in:
| Published in | Engineering and Technology Journal Vol. 29; no. 10; pp. 2013 - 2025 |
|---|---|
| Main Author | |
| Format | Journal Article |
| Language | English |
| Published |
Unviversity of Technology- Iraq
01.07.2011
|
| Online Access | Get full text |
Cover
Loading…
| Summary: | The kinematic coupling dynamic stability has been analyzed .The Laplace transformation and the coefficient matrix determinant are used to find the rolling stability characteristic equation. The effect of parameters is investigated with different value of roll rate . It is found that the kinematics coupling or autorotation is critical at flying regime of low and high .The results can be used as real design requirements for further configuration improvements of the airplane. |
|---|---|
| ISSN: | 1681-6900 2412-0758 |
| DOI: | 10.30684/etj.29.10.13 |