Verification of an individual aircraft fatigue monitoring system-Reference-Cited by-同舟云学术

Verification of an individual aircraft fatigue monitoring system

Published:2012-10 Issue: Volume:43 Page:128-133
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Molent L.,Barter S.,Foster W.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference19 articles.

1. Schütz W. Fatigue life prediction for aircraft structures and materials. AGARD-LS-62, ICAF-Doc-693. France: Advisory Group for Aerospace Research and Development; 1973.

2. Jones DJ, Duffield MJ, Holford DM. Future fatigue monitoring systems for fixed wing aircraft. Proposals for a new policy and a strategy for the way ahead. DERA/AS/ASD/CR/97600/1.0. UK: Defence Evaluation and Research Agency; 1998.

3. Defence Standard 00–970, Issue 5 Part 1 Section 3 Structure. UK: Ministry of Defence; 2007.

4. Joint Service Specification Guide (JSSG-2006), Aircraft structures. USA: Department of Defense; 1998.

5. MIL-STD-1530A, Military standard: military structural integrity program, airplane requirements USA; 1972.

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