Publication detail

Flight by Flight Fatigue Test of Aircraft Structure

AUGUSTIN, P.

Czech title

Únavová zkouška letecké konstrukce typu let za letem

English title

Flight by Flight Fatigue Test of Aircraft Structure

Type

conference paper

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. Practical example of the wing spar specimen fatigue test using created load sequence is presented.

Czech abstract

Článek se zabývá metodikou sestavení zatěžovací sekvence pro únavovou zkoušku letecké konstrukce, která simuluje reálné provozní zatěžování. Současně je prezentována praktická aplikace při únavové zkoušce nosníku křídla.

English 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. Practical example of the wing spar specimen fatigue test using created load sequence is presented.

Keywords in Czech

únavové zkoušky

Keywords in English

Fatigue Test

Released

03.06.2003

Publisher

Brno University of Technology, Institute of Mechanics of Solids

Location

Brno

ISBN

80-214-2314-5

Book

Experimental Stress Analysis 2003

Pages count

2

BIBTEX


@inproceedings{BUT8054,
  author="Petr {Augustin},
  title="Flight by Flight Fatigue Test of Aircraft Structure",
  booktitle="Experimental Stress Analysis 2003",
  year="2003",
  month="June",
  publisher="Brno University of Technology, Institute of Mechanics of Solids",
  address="Brno",
  isbn="80-214-2314-5"
}