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Table 5.

Measurements of mean relative lift Lr,ref, mean relative thrust-drag Tr,refand mean relative pitching moment Mr,refat the reference flight condition (Uref=3.50 m s−1; αb,ref=7°),together with their partial derivatives with respect to tunnel speed U and body angle αb, and the calculated pseudo-equilibria for tunnel speed Ueand body angle αb,e

Measured parameters
Pseudo-equilibrium solutions
\({\partial}L_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}T_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}M_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}L_{\mathrm{r}}{/}{\partial}U\)
\({\partial}T_{\mathrm{r}}{/}{\partial}U\)
\({\partial}M_{\mathrm{r}}{/}{\partial}U\)
αb,eUe (m s−1)
LocustLr,refTr,refMr,ref(deg s−1)(deg s−1)(deg s−1)(m−1 s)(m−1 s)(m−1 s)(degrees)Tr=0Mr=0
`R' 0.95 1.01 0.84 0.048 −0.025 −0.019 −0.43 −0.50 5.78 5.13 
`G' 0.83 −0.18 −0.26 0.029 −0.038 −0.045 −0.59 −0.81 13 2.81 2.84 
`B' 0.87 0.94 0.78 0.049 −0.016 −0.015 −0.49 −0.59 10 5.33 4.75 
Measured parameters
Pseudo-equilibrium solutions
\({\partial}L_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}T_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}M_{\mathrm{r}}{/}{\partial}{\alpha}_{\mathrm{b}}\)
\({\partial}L_{\mathrm{r}}{/}{\partial}U\)
\({\partial}T_{\mathrm{r}}{/}{\partial}U\)
\({\partial}M_{\mathrm{r}}{/}{\partial}U\)
αb,eUe (m s−1)
LocustLr,refTr,refMr,ref(deg s−1)(deg s−1)(deg s−1)(m−1 s)(m−1 s)(m−1 s)(degrees)Tr=0Mr=0
`R' 0.95 1.01 0.84 0.048 −0.025 −0.019 −0.43 −0.50 5.78 5.13 
`G' 0.83 −0.18 −0.26 0.029 −0.038 −0.045 −0.59 −0.81 13 2.81 2.84 
`B' 0.87 0.94 0.78 0.049 −0.016 −0.015 −0.49 −0.59 10 5.33 4.75 
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