The present invention belongs to the field of aeronautical structures such as an aircraft airfoil, and in particular to the profiles that are coupled to a trailing edge of an airfoil. In addition, the present invention provides a method to repair the trailing edge profile of an aircraft airfoil.
PROFILE FOR A TRAILING EDGE OF AN AIRFOIL AND METHOD TO REPAIR THEREOF
PROFIL FÜR DIE HINTERKANTE EINES TRAGFLÜGELS UND VERFAHREN ZUR REPARATUR DAVON
PROFIL POUR UN BORD DE FUITE D'UN PROFIL AÉRODYNAMIQUE ET SON PROCÉDÉ DE RÉPARATION
2025-02-12
Patent
Electronic Resource
English
Divergent-Trailing-Edge Airfoil
NTRS | 1988
|Divergent-Trailing-Edge Airfoil Flow
Online Contents | 1996
|Leading edge - Trailing edge airfoil interactions
AIAA | 1995
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