High Temperature Surface Interactions
Abstract
In today's climate of life extension for military aircraft, the topic of corrosion control assumes a role of greater importance. At its sixty-eighth meeting, the Structures and Materials Panel conference of specialists focussed on controlling the degradative effects of flight environments on aircraft engine materials. The meeting reviewed the chemical and mechanical mechanisms involved in degradative process and considered some state-of-the-art solutions. Emphasis in discussions centred on hot salt corrosion topics but wear and erosion problems were also considered. Keywords: Corrosion prevention; Environments; Military aircraft; Erosion corrosion; Superalloys; Gas turbines; Ceramic surfaces; Sliding/Fretting; Titanium alloys; Protective coatings; Thermal shock; Corrosion mechanisms; Degradation; Surface chemistry; Surface temperature; Turbine components; Oxidation/Sulfidation; Hot corrosion; Molten salts; Thermal barrier coatings; Aluminum lithium alloys; Hot gases; NATO-furnished.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1989
- Accession Number
- ADA217461
Entities
Organizations
- AGARD