| 摘要 |
<p>Described herein is an aircraft (1; 1', 100) including : - a fuselage (2; 2'; 102); - a pair of wings (3, 4; 103, 104); - a propulsion apparatus (13; 13'; 113) configured for generating a propulsive thrust by processing a flow of fluid, in particular, air, and configured for varying the direction of said propulsive thrust by the Coanda effect; and - an equipment for generating lift (6, 7; 106, 107; 113, 113') arranged at a nose section (5; 5'; 105) in a substantially end position on said fuselage (2; 2'; 102).</p> |
