Table 1.

Non-dimensional stability derivatives

$$X_{\mathrm{u}}^{+}$$
$$Z_{\mathrm{u}}^{+}$$
$$M_{\mathrm{u}}^{+}$$
$$X_{\mathrm{w}}^{+}$$
$$Z_{\mathrm{w}}^{+}$$
$$M_{\mathrm{w}}^{+}$$
$$X_{\mathrm{q}}^{+}$$
$$Z_{\mathrm{q}}^{+}$$
$$M_{\mathrm{q}}^{+}$$
–1.28 –0.04 2.32 0.01 –1.26 0.05 –0.28 –0.03
$$X_{\mathrm{u}}^{+}$$
$$Z_{\mathrm{u}}^{+}$$
$$M_{\mathrm{u}}^{+}$$
$$X_{\mathrm{w}}^{+}$$
$$Z_{\mathrm{w}}^{+}$$
$$M_{\mathrm{w}}^{+}$$
$$X_{\mathrm{q}}^{+}$$
$$Z_{\mathrm{q}}^{+}$$
$$M_{\mathrm{q}}^{+}$$
–1.28 –0.04 2.32 0.01 –1.26 0.05 –0.28 –0.03

$$X_{\mathrm{u}}^{+}$$
⁠,
$$Z_{\mathrm{u}}^{+}$$
and
$$M_{\mathrm{u}}^{+}$$
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to the x-component(u+) of the non-dimensional velocity;
$$X_{\mathrm{w}}^{+}$$
,
$$Z_{\mathrm{w}}^{+}$$
and
$$M_{\mathrm{w}}^{+}$$
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to the z-component(w+) of the non-dimensional velocity;
$$X_{\mathrm{q}}^{+}$$
,
$$Z_{\mathrm{q}}^{+}$$
and
$$M_{\mathrm{q}}^{+}$$
, non-dimensional derivatives of the x- and z-component of the aerodynamic force and aerodynamic moment, respectively, with respect to the non-dimensional pitching rate(q+)

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