Optimization of structures subjected to streams of hot gases.

摘要

Optimization of structures subjected to streams of hot gases. The invention relates to a fairing (10) to the horizontal stabilizer (3) of an aircraft, comprising a front (11) and a rear (12), covering the front (11) a limited surface extension fairing (10), which is part of the cowling (10) receiving the hot air stream (6) from the engine (4) of the aircraft, the front (11) of an anti-erosion material being made, covering the back (12) the rest of the surface of the cowling (10), the rear (12) resistant to existing aerodynamic loads on the cowling (10) material made. The invention also relates to an aircraft comprising a horizontal stabilizer (3) with a cover (10) such as that described.