Detail publikace

Fatigue Crack Growth Test of the Built-up Panel in Section 22-23

AUGUSTIN, P.

Originální název

Fatigue Crack Growth Test of the Built-up Panel in Section 22-23

Typ

souhrnná výzkumná zpráva - smluv. výzkum

Jazyk

angličtina

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.

Klíčová slova

fatigue, damage tolerance, aircraft structure

Autoři

AUGUSTIN, P.

Vydáno

24. 11. 2016

Strany počet

101

BibTex

@misc{BUT134362,
  author="Petr {Augustin}",
  title="Fatigue Crack Growth Test of the Built-up Panel in Section 22-23",
  year="2016",
  pages="101",
  note="summary research report - contract. research"
}