Abstract
The incorporation of some specific and useful corrosion prevention concepts into aircraft design is dealt with. The environmental dimensions in which aircraft materials should perform and which must be considered in the design are discussed first. The principal character traits which affect reliable performance for high-strength steels, aluminum, titanium, and magnesium alloys are then examined.
| Original language | English (US) |
|---|---|
| Journal | AGARD Lect SerTheory, Significance and Prevent of Corros in Aircr |
| Issue number | 84 |
| State | Published - Dec 1 1976 |