Detail publikace

Flight by Flight Fatigue Test with Random Application of Loads

AUGUSTIN, P.

Originální název

Flight by Flight Fatigue Test with Random Application of Loads

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

Originální abstrakt

The most realistic method of experimental determining the mean fatigue life of an aircraft structure is a random application of loads on a flight by flight basis. This paper deals with the development of such load sequence which simulates a load history as it can occur in service. A computer program was written for generation of load sequence. Calculations were also performed for the determination of the influence the small amplitude cycles omission on propagation of cracks in the spar web and wing skin. Practical example of the wing spar specimen fatigue test using created load sequence is presented.

Klíčová slova

Fatigue Test

Autoři

AUGUSTIN, P.

Rok RIV

2003

Vydáno

21. 11. 2003

Nakladatel

VZLÚ, a.s.

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Ročník

2003

Číslo

3

Stát

Česká republika

Strany od

3

Strany do

6

Strany počet

4

BibTex

@article{BUT41352,
  author="Petr {Augustin}",
  title="Flight by Flight Fatigue Test with Random Application of Loads",
  journal="Letecký zpravodaj",
  year="2003",
  volume="2003",
  number="3",
  pages="4",
  issn="1211-877X"
}