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Methodology for assessing and reducing the aerodynamic imbalance of the impellers of GTE fans
Kudashov E.V., Grachev I.A., Bolotov M.A.
Investigation of the influence of broadband mechanical disturbances on the quality of recording interference patterns of GTE-wheel oscillations using a digital speckle pattern interferometer
Ivchenko A.V., Safin A.I.
Development of a model for determination of preloads on blade shrouds
Pechenina E.Y., Kudashov E.V., Pechenin V.A.
The calculated study of fluid structure in a hub an axial aviation turbine
1 1., 1 1.
Formation of spread in resonance stresses in bladed disks with non-identical blades and loose vibration conectedness
Ermakov A.I., Urlapkin A.V., Fedorchenko D.G.
Modeling oil separation in the impeller of a radial-type centrifugal breather
Petrukhin A.G., Tryanov A.E.
The results of gas dynamic and strength improvement of turbocharger TK-32 axial turbine
Kolmakova D.A.
Analysis of the applicability of laser stereolithography technology for the production of turbodrives
Shabliy L.S.
Construction of a blade beam finite element as a component of the blade disk rotary-symmetrical system
Davydov D.P.
Fast algorithm for finding the resonance frequencies of gas turbine engine rotating blade disks
Davydov D.P.
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