Acoustic resonance phenomena in air bleed channels in aviation engines
- Authors: Aleksentsev A.A.1, Sazhenkov A.N.2, Sukhinin S.V.3
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Affiliations:
- Perm National Research Polytechnic University
- Open Joint Stock Company “Aviadvigatel” (“UEC Perm Engines”)
- Lavrentyev Institute of Hydrodynamics, Siberian Branch
- Issue: Vol 57, No 6 (2016)
- Pages: 971-978
- Section: Article
- URL: https://journals.rcsi.science/0021-8944/article/view/159862
- DOI: https://doi.org/10.1134/S002189441606002X
- ID: 159862
Cite item
Abstract
The existence of axial–radial acoustic resonance oscillations of the basic air flow in bleed channels of aviation engines is demonstrated theoretically and experimentally. Numerical and analytical methods are used to determine the frequency of acoustic resonance oscillations for the lowest modes of open and closed bleed channels of the PS-90A engine. Experimental investigations reveal new acoustic resonance phenomena arising in the air flow in bleed channel cavities in the core duct of this engine owing to instability of the basic air flow. The results of numerical, analytical, and experimental studies of the resonance frequencies reached in the flow in bleed channel cavities in the core duct of the PS-90A engine are found to be in reasonable agreement. As a result, various types of resonance oscillations in bleed channels can be accurately described.
About the authors
A. A. Aleksentsev
Perm National Research Polytechnic University
Author for correspondence.
Email: aleksentsev@avid.ru
Russian Federation, Perm, 614990
A. N. Sazhenkov
Open Joint Stock Company “Aviadvigatel” (“UEC Perm Engines”)
Email: aleksentsev@avid.ru
Russian Federation, Perm, 614990
S. V. Sukhinin
Lavrentyev Institute of Hydrodynamics, Siberian Branch
Email: aleksentsev@avid.ru
Russian Federation, Novosibirsk, 630090
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