A way to secure operational safety for an aircraft structure according to a strength criterion-Reference-Cited by-同舟云学术

A way to secure operational safety for an aircraft structure according to a strength criterion

Published:2013-01 Issue:1 Volume:42 Page:62-75
ISSN:1052-6188
Container-title:Journal of Machinery Manufacture and Reliability
language:en
Short-container-title:J. Mach. Manuf. Reliab.

Author:

Nesterenko B. G.,Nesterenko G. I.

Publisher

Allerton Press

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Safety, Risk, Reliability and Quality

Link

http://link.springer.com/content/pdf/10.3103/S1052618813010093.pdf

Reference30 articles.

1. Swift, T., Fail-Safe Design Requirements and Features, Regulatory Requirements, Proc. AIAA/ICAS Int. Air and Space Symposium and Exposition. The Next 100 Years, Dayton, July 14–17, 2003.

2. Advisory Circular AC 25.571-1D: Damage Tolerance and Fatigue Evaluation of Structure, 2011.

3. FAR 26, Part 26: Continued Airworthiness and Safety Improvement for Transport Category Airplanes. Subpart E — Aging Airplane Safety — Damage Tolerance Data for Repairs and Alteration, 2008.

4. Military Specification no. Mil-A-83444: Damage Tolerance Design Requirement for Aircraft Structures, USAF, 1974.

5. Aviatsionnye Pravila (Aviation Requirements) no. AP 25.571: The Way to Estimate Fatigue Damages Acceptability for Structures, Mezhgosudarstvennyi aviatsionnyi komitet, Aviatsionnyi registr, 2009.

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