Publication detail
Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
AUGUSTIN, P.
English title
Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
Type
summary research report - contract. research
Language
en
Original abstract
The report deals with the description of experimental set-up, procedure and results of fatigue crack growth test and residual strength test of the built-up panel representing L 410 NG bottom wing panel in section 22-23.
English abstract
The report deals with the description of experimental set-up, procedure and results of fatigue crack growth test and residual strength test of the built-up panel representing L 410 NG bottom wing panel in section 22-23.
Keywords in English
fatigue, damage tolerance, aircraft structure
Released
24.11.2016
Pages count
101