Publication detail

Flight by Flight Fatigue Test of Aircraft Structure

AUGUSTIN, P.

English title

Flight by Flight Fatigue Test of Aircraft Structure

Type

Paper in proceedings (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.

Keywords in English

Fatigue Test

Released

2003-06-03

Publisher

Brno University of Technology, Institute of Mechanics of Solids

Location

Brno

ISBN

80-214-2314-5

Book

Experimental Stress Analysis 2003

Pages from–to

1–

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",
  pages="2",
  publisher="Brno University of Technology, Institute of Mechanics of Solids",
  address="Brno",
  isbn="80-214-2314-5"
}