Detail publikace
Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
AUGUSTIN, P.
Anglický název
Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
Typ
souhrnná výzkumná zpráva - smluv. výzkum
Jazyk
en
Originální abstrakt
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.
Anglický abstrakt
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.
Klíčová slova anglicky
fatigue, damage tolerance, aircraft structure
Vydáno
24.11.2016
Počet stran
101