Methodics of aviation engines diagnostics based on parameters measured at transitional regimes of engine operation
<span lang="EN-US">Presented are operational experimental results of effect of different types of engine core defect on the dynamic characteristics of turbojet engine</span>
Main Authors: | С. А. Дмитриев, Е. В. Путятин, Д. Агарвал, Х. Низар |
---|---|
Format: | Article |
Language: | English |
Published: |
National Aviation University
2000-09-01
|
Series: | Vìsnik Nacìonalʹnogo Avìacìjnogo Unìversitetu |
Online Access: | http://jrnl.nau.edu.ua/index.php/visnik/article/view/9697 |
Similar Items
-
Modeling of cross sections and volumes of transitional surfaces of air intakes of aviation engines
by: В. І. Мамчук, et al.
Published: (2002-04-01) -
AVIATION ENGINES DIAGNOSTICS BY ESTIMATING THE METAL CONTAMINATION IN OILS
by: K. I. Gryadunov, et al.
Published: (2019-06-01) -
Automatization of estimation of aviation personnel psychophysiological condition in operation regime
by: С. Н. Занько
Published: (2000-12-01) -
AVIATION ENGINE air-gas channel contamination DIAGNOSTIC CHARACTER
by: E. A. Konyaev, et al.
Published: (2016-11-01) -
AVIATION ENGINE air-gas channel contamination DIAGNOSTIC CHARACTER
by: E. A. Konyaev, et al.
Published: (2014-01-01)