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AUGUSTIN, P.
Originální název
Flight by Flight Fatigue Test of Aircraft Structure
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
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
Fatigue Test
Autoři
Vydáno
3. 6. 2003
Nakladatel
Brno University of Technology, Institute of Mechanics of Solids
Místo
Brno
ISBN
80-214-2314-5
Kniha
Experimental Stress Analysis 2003
Strany od
1
Strany do
2
Strany počet
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" }