Abstract
This paper demonstrates application of reliability and maintainability (R&M) factors to determine supportability of aircraft turbine engines. R&M factors are expressed as operating and support parameters consistent with those required for LCC analysis as well as operating support level determinations.
Cite
CITATION STYLE
APA
Callis, C. L., & Curry, C. E. (1987). Applied Reliability/Maintainability Methodology as a Function Within Life Cycle Cost. In Proceedings of the ASME Turbo Expo (Vol. 2). American Society of Mechanical Engineers (ASME). https://doi.org/10.1115/87-GT-172
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