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Table 7.

Dimensional static stability derivatives with respect to forward speed(u) and aerodynamic incidence (w) for the three locusts,resolved in the stability axes

ueXuZuMuXwZwMw
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 
ueXuZuMuXwZwMw
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.

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