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Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow. / Mironov, S. G.; Kirilovskiy, S. V.; Poplavskaya, T. V. et al.

In: Journal of Applied Mechanics and Technical Physics, Vol. 62, No. 2, 03.2021, p. 183-192.

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

Harvard

Mironov, SG, Kirilovskiy, SV, Poplavskaya, TV & Tsyryulnikov, IS 2021, 'Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow', Journal of Applied Mechanics and Technical Physics, vol. 62, no. 2, pp. 183-192. https://doi.org/10.1134/S0021894421020012

APA

Mironov, S. G., Kirilovskiy, S. V., Poplavskaya, T. V., & Tsyryulnikov, I. S. (2021). Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow. Journal of Applied Mechanics and Technical Physics, 62(2), 183-192. https://doi.org/10.1134/S0021894421020012

Vancouver

Mironov SG, Kirilovskiy SV, Poplavskaya TV, Tsyryulnikov IS. Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow. Journal of Applied Mechanics and Technical Physics. 2021 Mar;62(2):183-192. doi: 10.1134/S0021894421020012

Author

Mironov, S. G. ; Kirilovskiy, S. V. ; Poplavskaya, T. V. et al. / Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow. In: Journal of Applied Mechanics and Technical Physics. 2021 ; Vol. 62, No. 2. pp. 183-192.

BibTeX

@article{2ad29fed6f9c40928eb050c90eb72c8b,
title = "Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow",
abstract = "Results of experimental and numerical investigations of a supersonic flow of cylindrical models aligned at a zero angle of attack with frontal inserts made of cellular porous nickel are reported. The experiments are performed in a supersonic wind tunnel at Mach numbers (Formula presented.) and 7.00 and unit Reynolds numbers (Formula presented.) and (Formula presented.), respectively. Numerical simulations with the use of a ring-shaped skeletal model of the porous material are also performed. A possibility of drag control is studied for two thermal methods: external heating of the porous insert and internal heating of the insert by a glow discharge. The mechanisms of the thermal action and the efficiency of the thermal methods of drag control are analyzed.",
keywords = "drag, flow control, porous gas-dynamic inserts, supersonic flows",
author = "Mironov, {S. G.} and Kirilovskiy, {S. V.} and Poplavskaya, {T. V.} and Tsyryulnikov, {I. S.}",
note = "Funding Information: This work was performed within the framework of the Program of Scientific Research of the State Academies of Sciences in 2013–2020 (Project No. AAAA-A17-117030610126-4). Publisher Copyright: {\textcopyright} 2021, Pleiades Publishing, Ltd.",
year = "2021",
month = mar,
doi = "10.1134/S0021894421020012",
language = "English",
volume = "62",
pages = "183--192",
journal = "Journal of Applied Mechanics and Technical Physics",
issn = "0021-8944",
publisher = "Maik Nauka-Interperiodica Publishing",
number = "2",

}

RIS

TY - JOUR

T1 - Thermal methods of drag control for cylindrical bodies with porous inserts in a supersonic flow

AU - Mironov, S. G.

AU - Kirilovskiy, S. V.

AU - Poplavskaya, T. V.

AU - Tsyryulnikov, I. S.

N1 - Funding Information: This work was performed within the framework of the Program of Scientific Research of the State Academies of Sciences in 2013–2020 (Project No. AAAA-A17-117030610126-4). Publisher Copyright: © 2021, Pleiades Publishing, Ltd.

PY - 2021/3

Y1 - 2021/3

N2 - Results of experimental and numerical investigations of a supersonic flow of cylindrical models aligned at a zero angle of attack with frontal inserts made of cellular porous nickel are reported. The experiments are performed in a supersonic wind tunnel at Mach numbers (Formula presented.) and 7.00 and unit Reynolds numbers (Formula presented.) and (Formula presented.), respectively. Numerical simulations with the use of a ring-shaped skeletal model of the porous material are also performed. A possibility of drag control is studied for two thermal methods: external heating of the porous insert and internal heating of the insert by a glow discharge. The mechanisms of the thermal action and the efficiency of the thermal methods of drag control are analyzed.

AB - Results of experimental and numerical investigations of a supersonic flow of cylindrical models aligned at a zero angle of attack with frontal inserts made of cellular porous nickel are reported. The experiments are performed in a supersonic wind tunnel at Mach numbers (Formula presented.) and 7.00 and unit Reynolds numbers (Formula presented.) and (Formula presented.), respectively. Numerical simulations with the use of a ring-shaped skeletal model of the porous material are also performed. A possibility of drag control is studied for two thermal methods: external heating of the porous insert and internal heating of the insert by a glow discharge. The mechanisms of the thermal action and the efficiency of the thermal methods of drag control are analyzed.

KW - drag

KW - flow control

KW - porous gas-dynamic inserts

KW - supersonic flows

UR - http://www.scopus.com/inward/record.url?scp=85110993860&partnerID=8YFLogxK

U2 - 10.1134/S0021894421020012

DO - 10.1134/S0021894421020012

M3 - Article

AN - SCOPUS:85110993860

VL - 62

SP - 183

EP - 192

JO - Journal of Applied Mechanics and Technical Physics

JF - Journal of Applied Mechanics and Technical Physics

SN - 0021-8944

IS - 2

ER -

ID: 34092909