Publication detail

Flight by Flight Fatigue Test with Random Application of Loads

AUGUSTIN, P.

English title

Flight by Flight Fatigue Test with Random Application of Loads

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

Original abstract

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.

Keywords in English

Fatigue Test

Released

2003-11-21

Publisher

VZLÚ, a.s.

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2003

Number

3

Pages from–to

3–

Pages count

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"
}