Methodology for fatigue life assessment of the structural integrity of fighter aircraft

Author:

REIS L.,FONSECA A.,DE FREITAS M.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference14 articles.

1. 1 M. Freitas, H. Goncalo, A. Fonseca, and J. C Pires (1995 ) Damage tolerance assessment on A7-P aircraft considering PoAF usage. AGARD Specialists' Meeting Widespread Fatigue Damage in Military Aircraft. Rotterdam , The NetherlandsAGARD-CP-568, pp. 16-1 -16-8 .

2. 4 A. R Fonseca . (2002 ) Instrumentacao de uma Aeronave Dassault/Dornier Alpha-Jet da Forca Aerea Portuguesa, para Monitorizacao de Cargas em Voo. GTEV Project EV-FAP/AJET-FLDR-003 , Instituto Superior Tecnico, Portugal.

3. 5 D. J Spiekhout . (1993 ) Reduction of Fatigue Load Experience as Part of the Fatigue Management Program for F-16 Aircraft of the RNLAF . In: Reduction of Fatigue Load Experience as Part of the Fatigue Management Program for F-16 Aircraft of the RNLAF , Bordeaux, France, AGARD-AG-797, pp19-1 -19-11 .

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