Detail publikace

SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY

KATRŇÁK, T. PLHAL, M.

Anglický název

SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

Originální abstrakt

The article presents a shape optimization of critical fuselage wall segments and undercarriage spars, a localization of stress concentrations and modifications for a reduction and removing of stress peaks. Structural analyses are made on main fuselage parts on the aircraft in CS-23 Commuter category. There are described main types of proper shape modifications with graphic comparisons and highlighted stress peaks.

Klíčová slova anglicky

Fatigue durability, Fuselage, Spar, Stress concentration

Vydáno

2012-10-19

Nakladatel

VUT v Brně

Místo

VUT v Brně

ISSN

1425-2104

Časopis

RESEARCH BULLETIN

Ročník

2012

Číslo

22

Strany od–do

1–8

Počet stran

8

BIBTEX


@article{BUT94806,
  author="Tomáš {Katrňák} and Martin {Plhal}",
  title="SHAPE MODIFICATIONS OF CRITICAL FUSELAGE PARTS ACCORDING TO FATIGUE DURABILITY",
  journal="RESEARCH BULLETIN",
  year="2012",
  volume="2012",
  number="22",
  pages="1--8",
  issn="1425-2104"
}