Standard

Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack. / Lukashevich, S. V.; Morozov, S. O.; Shiplyuk, A. N.

In: Experiments in Fluids, Vol. 59, No. 8, 130, 01.08.2018.

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

Harvard

Lukashevich, SV, Morozov, SO & Shiplyuk, AN 2018, 'Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack', Experiments in Fluids, vol. 59, no. 8, 130. https://doi.org/10.1007/s00348-018-2585-1

APA

Lukashevich, S. V., Morozov, S. O., & Shiplyuk, A. N. (2018). Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack. Experiments in Fluids, 59(8), [130]. https://doi.org/10.1007/s00348-018-2585-1

Vancouver

Lukashevich SV, Morozov SO, Shiplyuk AN. Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack. Experiments in Fluids. 2018 Aug 1;59(8):130. doi: 10.1007/s00348-018-2585-1

Author

Lukashevich, S. V. ; Morozov, S. O. ; Shiplyuk, A. N. / Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack. In: Experiments in Fluids. 2018 ; Vol. 59, No. 8.

BibTeX

@article{c68a4c50f29b4545b6386330aad47a4b,
title = "Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack",
abstract = "Abstract: Experimental investigations are performed to understand the effect of the passive porous coating on the high-frequency disturbances and laminar–turbulent transition of a hypersonic boundary layer on the sharp cone with an apex half-angle Θc = 7° aligned at normalized angles of attack up to α = 1° at the Mach number M∞ = 5.8. It is demonstrated that the passive porous coating effectively suppresses the most unstable second-mode disturbances in the hypersonic boundary layer at the studied angles of attack. It is found that the passive porous coating delays the laminar–turbulent transition both on the windward and leeward sides. The reflection coefficient of the passive porous coating for ultrasonic acoustic waves is also measured.",
keywords = "HEAT-TRANSFER, STABILIZATION, DISTURBANCES, TRANSITION, SURFACE, FLOW",
author = "Lukashevich, {S. V.} and Morozov, {S. O.} and Shiplyuk, {A. N.}",
year = "2018",
month = aug,
day = "1",
doi = "10.1007/s00348-018-2585-1",
language = "English",
volume = "59",
journal = "Experiments in Fluids",
issn = "0723-4864",
publisher = "Springer-Verlag GmbH and Co. KG",
number = "8",

}

RIS

TY - JOUR

T1 - Passive porous coating effect on a hypersonic boundary layer on a sharp cone at small angle of attack

AU - Lukashevich, S. V.

AU - Morozov, S. O.

AU - Shiplyuk, A. N.

PY - 2018/8/1

Y1 - 2018/8/1

N2 - Abstract: Experimental investigations are performed to understand the effect of the passive porous coating on the high-frequency disturbances and laminar–turbulent transition of a hypersonic boundary layer on the sharp cone with an apex half-angle Θc = 7° aligned at normalized angles of attack up to α = 1° at the Mach number M∞ = 5.8. It is demonstrated that the passive porous coating effectively suppresses the most unstable second-mode disturbances in the hypersonic boundary layer at the studied angles of attack. It is found that the passive porous coating delays the laminar–turbulent transition both on the windward and leeward sides. The reflection coefficient of the passive porous coating for ultrasonic acoustic waves is also measured.

AB - Abstract: Experimental investigations are performed to understand the effect of the passive porous coating on the high-frequency disturbances and laminar–turbulent transition of a hypersonic boundary layer on the sharp cone with an apex half-angle Θc = 7° aligned at normalized angles of attack up to α = 1° at the Mach number M∞ = 5.8. It is demonstrated that the passive porous coating effectively suppresses the most unstable second-mode disturbances in the hypersonic boundary layer at the studied angles of attack. It is found that the passive porous coating delays the laminar–turbulent transition both on the windward and leeward sides. The reflection coefficient of the passive porous coating for ultrasonic acoustic waves is also measured.

KW - HEAT-TRANSFER

KW - STABILIZATION

KW - DISTURBANCES

KW - TRANSITION

KW - SURFACE

KW - FLOW

UR - http://www.scopus.com/inward/record.url?scp=85050762035&partnerID=8YFLogxK

U2 - 10.1007/s00348-018-2585-1

DO - 10.1007/s00348-018-2585-1

M3 - Article

AN - SCOPUS:85050762035

VL - 59

JO - Experiments in Fluids

JF - Experiments in Fluids

SN - 0723-4864

IS - 8

M1 - 130

ER -

ID: 15966698