Fatigue Crack Growth Investigation on a Maintenance Welding Repair Applied on a High Responsibility Airframe

Author:

Nascimento Marcelino P.,Batista Carolina C.,Sorrija Bruno A.,Voorwald Herman J.C.

Publisher

Elsevier BV

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference6 articles.

1. Godefroid, L.B. Fatigue crack growth under constant and variable amplitude loading in aluminium alloys of aeronautical applications, Ph.D. Thesis, COPPE, Federal University of Rio de Janeiro 1993, Brazil.

2. Goranson, U.G. Fatigue issues in aircraft maintenance and repairs International Journal of Fatigue 1993, 19, S3-S21.

3. Latorella, K.A. and Prabhu, P. A review of human error in aviation maintenance and inspection, International Journal of Industrial Ergonomics V. International Journal of Industrial Ergonomics 2000, 26, 133-161.

4. Nascimento, M.P. Effects of TIG welding repair on the structural integrity of AISI 4130 aeronautical steel. Ph.D Thesis in Mechanical Engineering. State University of São Paulo/UNESP-FEG, Brazil (in Portuguese), 2004, 240p.

5. Paris, P. and Erdogan, F. A Critical Analysis of Crack Propagation Laws Journal of Basic Engineering, Transactions of the ASME 1963, 85, 528-534.

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