Influence of sound-absorbing coatings on the development of disturbances in a flowing mixture of vibrationally excited gases
- Authors: Poplavskaya T.V.1, Reshetova A.I.1, Tsyryulnikov I.S.1
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Affiliations:
- Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
- Issue: Vol 26, No 3 (2019)
- Pages: 417-428
- Section: Article
- URL: https://journals.rcsi.science/1531-8699/article/view/218447
- DOI: https://doi.org/10.1134/S0869864319030107
- ID: 218447
Cite item
Abstract
In the present paper, we study the development of disturbances on a solid (continuous) plate and on a plate covered with a sound-absorbing coating, both installed at an angle of attack in a hypersonic flow (M∞ = 8.44) of a vibrationally excited mixture of carbon dioxide with nitrogen. The rms fluctuations of pressure were measured on the surface of the plates in a short-duration IT-302M wind tunnel of ITAM SB RAS. The numerical simulation was performed on the basis of solving the two-dimensional unsteady Navier-Stokes equations and a two-temperature model of relaxation flows. In modeling a real porous coating, a skeletal model was used. The model is formed by square elements arranged in staggered order with a distance between elements equal to the diameter of the pores in the sound-absorbing material used in the experiment. Data on the dynamics of the disturbance development on the solid plate and on the plate with the sound-absorbing coating under different conditions of the incident flow are reported. The effect of various parameters of the sound-absorbing coating (depth, length, and location on the plate) was studied. It is shown that the sound-absorbing coating significantly (up to 50 %) suppresses the intensity of pressure fluctuations on the plate surface as compared with the solid surface. A good agreement between the calculated and experimental data on the pressure pulsations on the surface of the plates is demonstrated.
About the authors
T. V. Poplavskaya
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
Author for correspondence.
Email: popla@itam.nsc.ru
Russian Federation, Novosibirsk
A. I. Reshetova
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
Email: popla@itam.nsc.ru
Russian Federation, Novosibirsk
I. S. Tsyryulnikov
Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
Email: popla@itam.nsc.ru
Russian Federation, Novosibirsk