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Structure of subsonic plane microjets. / Aniskin, V. M.; Maslov, A. A.; Mukhin, K. A.

в: Microfluidics and Nanofluidics, Том 23, № 4, 57, 01.04.2019.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Aniskin, VM, Maslov, AA & Mukhin, KA 2019, 'Structure of subsonic plane microjets', Microfluidics and Nanofluidics, Том. 23, № 4, 57. https://doi.org/10.1007/s10404-019-2223-0

APA

Aniskin, V. M., Maslov, A. A., & Mukhin, K. A. (2019). Structure of subsonic plane microjets. Microfluidics and Nanofluidics, 23(4), [57]. https://doi.org/10.1007/s10404-019-2223-0

Vancouver

Aniskin VM, Maslov AA, Mukhin KA. Structure of subsonic plane microjets. Microfluidics and Nanofluidics. 2019 апр. 1;23(4):57. doi: 10.1007/s10404-019-2223-0

Author

Aniskin, V. M. ; Maslov, A. A. ; Mukhin, K. A. / Structure of subsonic plane microjets. в: Microfluidics and Nanofluidics. 2019 ; Том 23, № 4.

BibTeX

@article{55cdf15465484498a9a49462e4a3cfd4,
title = "Structure of subsonic plane microjets",
abstract = "Results of experiments aimed at studying subsonic microjets escaping from a plane nozzle are reported. The Reynolds numbers based on the nozzle height and mean flow velocity at the nozzle exit are varied from 27 to 139, whereas the nozzle size is fixed at 83.3 × 3823 µm. The test gas is air at room temperature. The distributions of velocity and velocity fluctuations along the jet axis and in the lateral and transverse directions are determined. The fact of the laminar–turbulent transition in the jet is detected. The data obtained are compared with theoretical predictions for laminar plane jets. The experimental and theoretical data are found to be in good agreement at the laminar segment of the microjet.",
keywords = "TURBULENT, JET, VELOCITY, FLOW",
author = "Aniskin, {V. M.} and Maslov, {A. A.} and Mukhin, {K. A.}",
year = "2019",
month = apr,
day = "1",
doi = "10.1007/s10404-019-2223-0",
language = "English",
volume = "23",
journal = "Microfluidics and Nanofluidics",
issn = "1613-4982",
publisher = "Springer-Verlag GmbH and Co. KG",
number = "4",

}

RIS

TY - JOUR

T1 - Structure of subsonic plane microjets

AU - Aniskin, V. M.

AU - Maslov, A. A.

AU - Mukhin, K. A.

PY - 2019/4/1

Y1 - 2019/4/1

N2 - Results of experiments aimed at studying subsonic microjets escaping from a plane nozzle are reported. The Reynolds numbers based on the nozzle height and mean flow velocity at the nozzle exit are varied from 27 to 139, whereas the nozzle size is fixed at 83.3 × 3823 µm. The test gas is air at room temperature. The distributions of velocity and velocity fluctuations along the jet axis and in the lateral and transverse directions are determined. The fact of the laminar–turbulent transition in the jet is detected. The data obtained are compared with theoretical predictions for laminar plane jets. The experimental and theoretical data are found to be in good agreement at the laminar segment of the microjet.

AB - Results of experiments aimed at studying subsonic microjets escaping from a plane nozzle are reported. The Reynolds numbers based on the nozzle height and mean flow velocity at the nozzle exit are varied from 27 to 139, whereas the nozzle size is fixed at 83.3 × 3823 µm. The test gas is air at room temperature. The distributions of velocity and velocity fluctuations along the jet axis and in the lateral and transverse directions are determined. The fact of the laminar–turbulent transition in the jet is detected. The data obtained are compared with theoretical predictions for laminar plane jets. The experimental and theoretical data are found to be in good agreement at the laminar segment of the microjet.

KW - TURBULENT

KW - JET

KW - VELOCITY

KW - FLOW

UR - http://www.scopus.com/inward/record.url?scp=85063478917&partnerID=8YFLogxK

U2 - 10.1007/s10404-019-2223-0

DO - 10.1007/s10404-019-2223-0

M3 - Article

AN - SCOPUS:85063478917

VL - 23

JO - Microfluidics and Nanofluidics

JF - Microfluidics and Nanofluidics

SN - 1613-4982

IS - 4

M1 - 57

ER -

ID: 19038979