Trim horizontal stabilizer for improving aircraft performances

oleh: Vasile ŢURCAN, Cristian PURDEL

Format: Article
Diterbitkan: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2010-06-01

Deskripsi

In order to have a smooth movement between the trim horizontal stabilizer and the posteriorfuselage, with a small influence on the aircraft performance, we had to envision such a mechanismwhich made the entire trim horizontal stabilizer remain in contact with aft fuselage surface, whilemaintaining the sealing of the cut-out and the spar cover, so that it made the aircraft moreaerodynamic.