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Tolerable corrosion damage on aircraft aluminum structures: Local cladding patterns

  • Published:2012-04 Issue:1 Volume:58 Page:55-64
  • ISSN:0167-8442
  • Container-title:Theoretical and Applied Fracture Mechanics
  • language:en
  • Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Pantelakis Sp.G.,Chamos A.N.,Setsika D.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference36 articles.

1. Structural Integrity of Aging Airplanes;Atluri,1991

2. Milestone case histories in aircraft structural integrity;Wanhill;Compr. Struct. Integrity,2003

3. Corrosion and the threat to aircraft structural integrity;Mills,2009

4. Management of corrosion of aircraft;Smith;Shreir’s Corros.,2010

5. BRITE/EURAM No 1053, Structural maintenance of aging aircraft (SMAAC), CEC Brussels, Final Report, Brussels, 1999.
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