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Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material. / Poplavskaya, T. V.; Kirilovskiy, S. V.; Mironov, S. G.

In: Journal of Physics: Conference Series, Vol. 894, No. 1, 012074, 22.10.2017.

Research output: Contribution to journal › Article › peer-review

Harvard

Poplavskaya, TV, Kirilovskiy, SV & Mironov, SG 2017, 'Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material', Journal of Physics: Conference Series, vol. 894, no. 1, 012074. https://doi.org/10.1088/1742-6596/894/1/012074

APA

Poplavskaya, T. V., Kirilovskiy, S. V., & Mironov, S. G. (2017). Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material. Journal of Physics: Conference Series, 894(1), [012074]. https://doi.org/10.1088/1742-6596/894/1/012074

Vancouver

Poplavskaya TV, Kirilovskiy SV, Mironov SG. Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material. Journal of Physics: Conference Series. 2017 Oct 22;894(1):012074. doi: 10.1088/1742-6596/894/1/012074

Author

Poplavskaya, T. V. ; Kirilovskiy, S. V. ; Mironov, S. G. / Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material. In: Journal of Physics: Conference Series. 2017 ; Vol. 894, No. 1.

BibTeX

@article{1442ba575092455c806a2e38bb167ee7,
title = "Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material",
abstract = "Numerical simulation of supersonic flow past a cylinder with a frontal gas-permeable insert is performed using the skeleton model of a highly porous cellular material. Numerical simulation was carried out within the framework of two-dimensional RANS equations written in an axisymmetric form. The skeleton model is a system of coaxial rings of different diameters, arranged in staggered order. The calculations were carried out in a wide range of determining parameters: Mach numbers M∞ = 3, 4.85 and 7, unit Reynolds numbers Re1∞ = 13.8 105 13.8106 m-1, the cylinder diameter 640mm, the length of the porous insert 345mm, the cell diameter of 1 and 3 mm. The results of the calculations are consistent with the available experimental data. The applicability of the skeleton model for the description of supersonic flow around axisymmetric bodies with front inserts from cellular-porous materials is shown.",
keywords = "SHOCK LAYER, CYLINDER, PLATE",
author = "Poplavskaya, {T. V.} and Kirilovskiy, {S. V.} and Mironov, {S. G.}",
year = "2017",
month = oct,
day = "22",
doi = "10.1088/1742-6596/894/1/012074",
language = "English",
volume = "894",
journal = "Journal of Physics: Conference Series",
issn = "1742-6588",
publisher = "IOP Publishing Ltd.",
number = "1",

}

RIS

TY - JOUR

T1 - Simulation of a supersonic flow around a body with a frontal gas-permeable insert by using a skeleton model of a highly porous cellular material

AU - Poplavskaya, T. V.

AU - Kirilovskiy, S. V.

AU - Mironov, S. G.

PY - 2017/10/22

Y1 - 2017/10/22

N2 - Numerical simulation of supersonic flow past a cylinder with a frontal gas-permeable insert is performed using the skeleton model of a highly porous cellular material. Numerical simulation was carried out within the framework of two-dimensional RANS equations written in an axisymmetric form. The skeleton model is a system of coaxial rings of different diameters, arranged in staggered order. The calculations were carried out in a wide range of determining parameters: Mach numbers M∞ = 3, 4.85 and 7, unit Reynolds numbers Re1∞ = 13.8 105 13.8106 m-1, the cylinder diameter 640mm, the length of the porous insert 345mm, the cell diameter of 1 and 3 mm. The results of the calculations are consistent with the available experimental data. The applicability of the skeleton model for the description of supersonic flow around axisymmetric bodies with front inserts from cellular-porous materials is shown.

AB - Numerical simulation of supersonic flow past a cylinder with a frontal gas-permeable insert is performed using the skeleton model of a highly porous cellular material. Numerical simulation was carried out within the framework of two-dimensional RANS equations written in an axisymmetric form. The skeleton model is a system of coaxial rings of different diameters, arranged in staggered order. The calculations were carried out in a wide range of determining parameters: Mach numbers M∞ = 3, 4.85 and 7, unit Reynolds numbers Re1∞ = 13.8 105 13.8106 m-1, the cylinder diameter 640mm, the length of the porous insert 345mm, the cell diameter of 1 and 3 mm. The results of the calculations are consistent with the available experimental data. The applicability of the skeleton model for the description of supersonic flow around axisymmetric bodies with front inserts from cellular-porous materials is shown.

KW - SHOCK LAYER

KW - CYLINDER

KW - PLATE

UR - http://www.scopus.com/inward/record.url?scp=85033218188&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/894/1/012074

DO - 10.1088/1742-6596/894/1/012074

M3 - Article

AN - SCOPUS:85033218188

VL - 894

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012074

ER -

ID: 9720724