Publication detail

Flight by Flight Fatigue Test with Random Application of Loads

AUGUSTIN, P.

Original Title

Flight by Flight Fatigue Test with Random Application of Loads

Type

journal article - other

Language

English

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

Fatigue Test

Authors

AUGUSTIN, P.

RIV year

2003

Released

21. 11. 2003

Publisher

VZLÚ, a.s.

ISBN

1211-877X

Periodical

Letecký zpravodaj

Year of study

2003

Number

3

State

Czech Republic

Pages from

3

Pages to

6

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"
}