The influence of the environment and corrosion on the structural integrity of aircraft materials

Author:

RUSSO S.,SHARP P. K.,DHAMARI R.,MILLS T. B.,HINTON B. R. W.,CLARK G.,SHANKAR K.

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference19 articles.

1. 1  Wanhill, R. J. H. , De Luccia, J. J. and Russo, M. T. (1989) The Fatigue in Aircraft Corrosion Testing (FACT) Programme. Report No. 713, North Atlantic Treaty Organisation, Advisory Group for Aerospace Research and Development (AGARD), London.

2. 2  Wanhill, R. J. H. and De Luccia, J. J. (1982) An AGARD-Corrosion Fatigue Cooperative Testing Program. Report No. 695, North Atlantic Treaty Organisation, Advisory Group for Aerospace Research and Development (AGARD), London.

3. 3 Military Specification MIL-C-5541. (1990) Chemical conversion coatings on aluminium and aluminium alloys, USA.

4. 4 Boeing Specification BMS 10/11 type II: Chemical and Solvent Resistant Finish, Revision Y, 9 May 2003.

5. 5 Military Specification MIL-C-16173D. (1968) Corrosion preventive compound, solvent cutback, cold-application, USA.

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