The numerical analyzis for unsteady loads and elastic behaviour of the blades in seven stage axial compressor
Abstract
The numerical analyzis for unsteady interaction of the blade rows of seven stage axial compressor in 3D ideal gas flow has been presented. There shown that the principal contribution in unsteady loads is brought by the harmonics with frequencies which are equal to the product of rotation frequency on the stator blades numbersDownloads
Published
2016-07-29
Issue
Section
Aero- and hydrodynamics in energy machines
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Copyright (c) 2016 Л. В. Колодяжная
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