Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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.
в: Journal of Physics: Conference Series, Том 894, № 1, 012074, 22.10.2017.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
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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