An Experimental- and-Computational Complex for Predicting the Stability of Blade Assemblies Against Subsonic Flutter

Authors

  • A.P. Zinkovskii G.S. Pisarenko Institute for Problems of Strength NAS of Ukraine, Kyiv
  • V.A. Tsymbalyuk G.S. Pisarenko Institute for Problems of Strength NAS of Ukraine, Kyiv

DOI:

https://doi.org/10.15407/scin8.05.038

Keywords:

blade assembly, modeling, subsonic flutter, aerodynamic stability, prediction.

Abstract

The basic principles of the experimental-and-computational complex for predicting the subsonic flutter stability of aircraft gas turbine compressor blading are stated. Based on the approaches of physical modeling of phenomena observed under full-scale conditions, the similarity criteria are defined, which allow modeling the behavior of blade assemblies at their interaction with flow. The methodology for the experimental determination of non-stationary aerodynamic forces and moments acting on blades during their in-flow vibrations; the calculation of the dynamic stability of a blade assembly against flutter; the aerodynamic rig design and peculiar features of its components to perform testing of airfoil cascades are described. The results of testing of the developed experimental-and-computational complex are presented.

References

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Published

2024-06-06

Issue

Section

Research and Engineering Innovative Projects of the National Academy of Sciences of Ukraine