Dimensional static stability derivatives with respect to forward speed(u) and aerodynamic incidence (w) for the three locusts,resolved in the stability axes
| . | ue . | Xu . | Zu . | Mu . | Xw . | Zw . | Mw . |
|---|---|---|---|---|---|---|---|
| Locust . | (m s−1) . | (10−3 N m−1 s) . | (10−3 N m−1 s) . | (10−6 N s) . | (10−3 N m−1 s) . | (10−3 N m−1 s) . | (10−6 N s) . |
| `R' | 5.45 | −7.8 | −1.4 | −416 | −1.8 | −58 | −170 |
| `G' | 2.82 | −8.3 | 0.53 | −461 | −8.0 | −9.0 | −520 |
| `B' | 5.04 | −9.0 | 0.050 | −492 | −0.31 | −6.7 | −147 |
| . | ue . | Xu . | Zu . | Mu . | Xw . | Zw . | Mw . |
|---|---|---|---|---|---|---|---|
| Locust . | (m s−1) . | (10−3 N m−1 s) . | (10−3 N m−1 s) . | (10−6 N s) . | (10−3 N m−1 s) . | (10−3 N m−1 s) . | (10−6 N s) . |
| `R' | 5.45 | −7.8 | −1.4 | −416 | −1.8 | −58 | −170 |
| `G' | 2.82 | −8.3 | 0.53 | −461 | −8.0 | −9.0 | −520 |
| `B' | 5.04 | −9.0 | 0.050 | −492 | −0.31 | −6.7 | −147 |
The estimated equilibrium flight speed (ue) is also given.