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Numerical study of possibility of reliable diagnostics of gas turbine engine by gasdynamic parameters using a linear mathematical model
- Authors: Gerasimov A.B.1, Sundukov M.Y.2
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Affiliations:
- JSC «Klimov»
- JSC «Klimov»,
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 29-36
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6851
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-29-36
- ID: 6851
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Abstract
Article offers a method for evaluating possible quantity of cases the identification of gas turbine engine to adequately describe test data with limited number of measured parameters. The dependence of the possible quantity of identifications on the number of identifiable and measured parameters is researched
About the authors
A. B. Gerasimov
JSC «Klimov»
Author for correspondence.
Email: klimov@klimov.ru
candidate of technical science
chief designer
M. Y. Sundukov
JSC «Klimov»,
Email: msunduk@mail.ru
engineer
Russian FederationReferences
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