| 摘要 |
<p>The invention relates to an aircraft the fuselage (2) of which extends along a longitudinal axis. The fuselage includes a more or less cylindrical central portion (3) and a rear portion (4) that may have a flattened or conventional shape. This rear portion (4) which comprises the rear end of the fuselage includes a support surface (6) which bears at least one horizontal stabilizer (8) and/or vertical stabilizer (10). This is able to pivot in relation in relation to the central portion (3) around an axis such as the pitch axis, at least one stabilizer (8, 10) or the support surface (6) being equipped with at least one control surface (12a-b, 14a-b, 7).</p> |
