Detail publikace

Flight by Flight Fatigue Test of Aircraft Structure

AUGUSTIN, P.

Anglický název

Flight by Flight Fatigue Test of Aircraft Structure

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

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

Klíčová slova anglicky

Fatigue Test

Vydáno

2003-06-03

Nakladatel

Brno University of Technology, Institute of Mechanics of Solids

Místo

Brno

ISBN

80-214-2314-5

Kniha

Experimental Stress Analysis 2003

Strany od–do

1–

Počet stran

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"
}