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Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow. / Mironov, S. G.; Poplavskaya, T. V.; Kirilovskiy, S. V.

In: Thermophysics and Aeromechanics, Vol. 24, No. 4, 01.07.2017, p. 629-632.

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

Harvard

Mironov, SG, Poplavskaya, TV & Kirilovskiy, SV 2017, 'Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow', Thermophysics and Aeromechanics, vol. 24, no. 4, pp. 629-632. https://doi.org/10.1134/S0869864317040151

APA

Mironov, S. G., Poplavskaya, T. V., & Kirilovskiy, S. V. (2017). Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow. Thermophysics and Aeromechanics, 24(4), 629-632. https://doi.org/10.1134/S0869864317040151

Vancouver

Mironov SG, Poplavskaya TV, Kirilovskiy SV. Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow. Thermophysics and Aeromechanics. 2017 Jul 1;24(4):629-632. doi: 10.1134/S0869864317040151

Author

Mironov, S. G. ; Poplavskaya, T. V. ; Kirilovskiy, S. V. / Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow. In: Thermophysics and Aeromechanics. 2017 ; Vol. 24, No. 4. pp. 629-632.

BibTeX

@article{50cbf6a718614fbea701928fdd283997,
title = "Impact of frontal-porous-insert temperature on the cylinder drag in supersonic flow",
abstract = "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.",
keywords = "gas-permeable cellular-porous materials, impact of temperature, numerical simulation, supersonic flow around a body",
author = "Mironov, {S. G.} and Poplavskaya, {T. V.} and Kirilovskiy, {S. V.}",
year = "2017",
month = jul,
day = "1",
doi = "10.1134/S0869864317040151",
language = "English",
volume = "24",
pages = "629--632",
journal = "Thermophysics and Aeromechanics",
issn = "0869-8643",
publisher = "PLEIADES PUBLISHING INC",
number = "4",

}

RIS

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