Standard

Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets. / Aniskin, V. M.; Timofeev, I.; Maslov, N. A. и др.

в: Flow measurement and instrumentation, Том 70, 101655, 12.2019.

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

Harvard

Aniskin, VM, Timofeev, I, Maslov, NA & Tsibulskaya, EO 2019, 'Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets', Flow measurement and instrumentation, Том. 70, 101655. https://doi.org/10.1016/j.flowmeasinst.2019.101655

APA

Aniskin, V. M., Timofeev, I., Maslov, N. A., & Tsibulskaya, E. O. (2019). Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets. Flow measurement and instrumentation, 70, [101655]. https://doi.org/10.1016/j.flowmeasinst.2019.101655

Vancouver

Aniskin VM, Timofeev I, Maslov NA, Tsibulskaya EO. Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets. Flow measurement and instrumentation. 2019 дек.;70:101655. doi: 10.1016/j.flowmeasinst.2019.101655

Author

Aniskin, V. M. ; Timofeev, I. ; Maslov, N. A. и др. / Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets. в: Flow measurement and instrumentation. 2019 ; Том 70.

BibTeX

@article{4dd148e12f614406b0f4875acc438057,
title = "Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets",
abstract = "The article reports on results of estimating the Pitot tube diameter effect on the streamwise and lateral pressure distributions in plane supersonic air microjets. The study is aimed at obtaining reliable information on the microjet structure. The nozzles with the size of 22.3 × 2593 μm and 83.3 × 3823 μm are used in experiments. The supersonic flow from that nozzles is investigated by glass Pitot tubes in inner/outer diameters of 24/70 and 16/42 μm. Additional measurements are performed by a Pitot microtube 8 μm in outer diameter and ≈0.1 μm wall thickness. The value ranges for accuracy determination of supersonic jets main characteristics (shock cell sizes and supersonic core length) have been found.",
author = "Aniskin, {V. M.} and I. Timofeev and Maslov, {N. A.} and Tsibulskaya, {E. O.}",
note = "Funding Information: This work was supported by the Russian Science Foundation (Grant No. 17-19-01157 ). Publisher Copyright: {\textcopyright} 2019 Elsevier Ltd",
year = "2019",
month = dec,
doi = "10.1016/j.flowmeasinst.2019.101655",
language = "English",
volume = "70",
journal = "Flow measurement and instrumentation",
issn = "0955-5986",
publisher = "ELSEVIER SCI LTD",

}

RIS

TY - JOUR

T1 - Effect of the Pitot microtube diameter on pressure measurement in plane supersonic microjets

AU - Aniskin, V. M.

AU - Timofeev, I.

AU - Maslov, N. A.

AU - Tsibulskaya, E. O.

N1 - Funding Information: This work was supported by the Russian Science Foundation (Grant No. 17-19-01157 ). Publisher Copyright: © 2019 Elsevier Ltd

PY - 2019/12

Y1 - 2019/12

N2 - The article reports on results of estimating the Pitot tube diameter effect on the streamwise and lateral pressure distributions in plane supersonic air microjets. The study is aimed at obtaining reliable information on the microjet structure. The nozzles with the size of 22.3 × 2593 μm and 83.3 × 3823 μm are used in experiments. The supersonic flow from that nozzles is investigated by glass Pitot tubes in inner/outer diameters of 24/70 and 16/42 μm. Additional measurements are performed by a Pitot microtube 8 μm in outer diameter and ≈0.1 μm wall thickness. The value ranges for accuracy determination of supersonic jets main characteristics (shock cell sizes and supersonic core length) have been found.

AB - The article reports on results of estimating the Pitot tube diameter effect on the streamwise and lateral pressure distributions in plane supersonic air microjets. The study is aimed at obtaining reliable information on the microjet structure. The nozzles with the size of 22.3 × 2593 μm and 83.3 × 3823 μm are used in experiments. The supersonic flow from that nozzles is investigated by glass Pitot tubes in inner/outer diameters of 24/70 and 16/42 μm. Additional measurements are performed by a Pitot microtube 8 μm in outer diameter and ≈0.1 μm wall thickness. The value ranges for accuracy determination of supersonic jets main characteristics (shock cell sizes and supersonic core length) have been found.

UR - http://www.scopus.com/inward/record.url?scp=85074789610&partnerID=8YFLogxK

UR - https://elibrary.ru/item.asp?id=41700699

U2 - 10.1016/j.flowmeasinst.2019.101655

DO - 10.1016/j.flowmeasinst.2019.101655

M3 - Article

VL - 70

JO - Flow measurement and instrumentation

JF - Flow measurement and instrumentation

SN - 0955-5986

M1 - 101655

ER -

ID: 35705529