Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow. / Mironov, S. G.; Poplavskaya, T. V.; Kirilovskiy, S. V.
в: Thermophysics and Aeromechanics, Том 24, № 4, 01.07.2017, стр. 629-632.Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование
}
TY - JOUR
T1 - Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow
AU - Mironov, S. G.
AU - Poplavskaya, T. V.
AU - Kirilovskiy, S. V.
PY - 2017/7/1
Y1 - 2017/7/1
N2 - In the present paper, we report on experimental and simulated data on the impact of cellular-porous-material heating on the wave drag of a cylinder with a frontal gas-permeable porous insert streamlined by a supersonic flow (М∞ = 4.85, Re1∞ = 3.3×106 m-1). Weighing data obtained in the supersonic wind tunnel are compared with data simulated using a discrete model of the cellular-porous material. An increase of the wave drag with a growth of porous-insert temperature and its decrease occurring upon decreasing the temperature are demonstrated.
AB - In the present paper, we report on experimental and simulated data on the impact of cellular-porous-material heating on the wave drag of a cylinder with a frontal gas-permeable porous insert streamlined by a supersonic flow (М∞ = 4.85, Re1∞ = 3.3×106 m-1). Weighing data obtained in the supersonic wind tunnel are compared with data simulated using a discrete model of the cellular-porous material. An increase of the wave drag with a growth of porous-insert temperature and its decrease occurring upon decreasing the temperature are demonstrated.
KW - gas-permeable cellular-porous materials
KW - impact of temperature
KW - numerical simulation
KW - supersonic flow around a body
UR - http://www.scopus.com/inward/record.url?scp=85030846387&partnerID=8YFLogxK
U2 - 10.1134/S0869864317040151
DO - 10.1134/S0869864317040151
M3 - Article
AN - SCOPUS:85030846387
VL - 24
SP - 629
EP - 632
JO - Thermophysics and Aeromechanics
JF - Thermophysics and Aeromechanics
SN - 0869-8643
IS - 4
ER -
ID: 10067777