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Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section. / Yavorsky, N. I.; Meledin, V. G.; Kabardin, I. K. и др.

19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 030122 (AIP Conference Proceedings; Том 2027).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование

Harvard

Yavorsky, NI, Meledin, VG, Kabardin, IK, Gordienko, MR, Pravdina, MK, Kulikov, DV, Polyakova, VI & Pavlov, VA 2018, Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section. в Fomin (ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том. 2027, 030122, AIP Conference Proceedings, Том. 2027, American Institute of Physics Inc., 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018, Akademgorodok, Novosibirsk, Российская Федерация, 13.08.2018. https://doi.org/10.1063/1.5065216

APA

Yavorsky, N. I., Meledin, V. G., Kabardin, I. K., Gordienko, M. R., Pravdina, M. K., Kulikov, D. V., Polyakova, V. I., & Pavlov, V. A. (2018). Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section. в Fomin (Ред.), 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 (Том 2027). [030122] (AIP Conference Proceedings; Том 2027). American Institute of Physics Inc.. https://doi.org/10.1063/1.5065216

Vancouver

Yavorsky NI, Meledin VG, Kabardin IK, Gordienko MR, Pravdina MK, Kulikov DV и др. Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section. в Fomin, Редактор, 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Том 2027. American Institute of Physics Inc. 2018. 030122. (AIP Conference Proceedings). doi: 10.1063/1.5065216

Author

Yavorsky, N. I. ; Meledin, V. G. ; Kabardin, I. K. и др. / Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section. 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. Редактор / Fomin. Том 2027 American Institute of Physics Inc., 2018. (AIP Conference Proceedings).

BibTeX

@inproceedings{209e1a537135469d99b277071c288db0,
title = "Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section",
abstract = "The flow structure inside the Ranque vortex tube is investigated by LDA method. The mean velocity field is presented in the working channel of square cross-section at overpressures of 0.1 and 0.3 MPa. Two-dimensional mean velocity pattern is analyzed for the center longitudinal plane, and all the three velocity components all over the transverse coordinate are shown in three cross-sections of the working channel: near the guiding apparatus, in the center and near the hot exit.",
author = "Yavorsky, {N. I.} and Meledin, {V. G.} and Kabardin, {I. K.} and Gordienko, {M. R.} and Pravdina, {M. Kh} and Kulikov, {D. V.} and Polyakova, {V. I.} and Pavlov, {V. A.}",
note = "Publisher Copyright: {\textcopyright} 2018 Author(s).; 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018 ; Conference date: 13-08-2018 Through 19-08-2018",
year = "2018",
month = nov,
day = "2",
doi = "10.1063/1.5065216",
language = "English",
volume = "2027",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin",
booktitle = "19th International Conference on the Methods of Aerophysical Research, ICMAR 2018",

}

RIS

TY - GEN

T1 - Velocity field diagnostics inside the Ranque-Hilsh vortex tube with square cross-section

AU - Yavorsky, N. I.

AU - Meledin, V. G.

AU - Kabardin, I. K.

AU - Gordienko, M. R.

AU - Pravdina, M. Kh

AU - Kulikov, D. V.

AU - Polyakova, V. I.

AU - Pavlov, V. A.

N1 - Publisher Copyright: © 2018 Author(s).

PY - 2018/11/2

Y1 - 2018/11/2

N2 - The flow structure inside the Ranque vortex tube is investigated by LDA method. The mean velocity field is presented in the working channel of square cross-section at overpressures of 0.1 and 0.3 MPa. Two-dimensional mean velocity pattern is analyzed for the center longitudinal plane, and all the three velocity components all over the transverse coordinate are shown in three cross-sections of the working channel: near the guiding apparatus, in the center and near the hot exit.

AB - The flow structure inside the Ranque vortex tube is investigated by LDA method. The mean velocity field is presented in the working channel of square cross-section at overpressures of 0.1 and 0.3 MPa. Two-dimensional mean velocity pattern is analyzed for the center longitudinal plane, and all the three velocity components all over the transverse coordinate are shown in three cross-sections of the working channel: near the guiding apparatus, in the center and near the hot exit.

UR - http://www.scopus.com/inward/record.url?scp=85056354032&partnerID=8YFLogxK

U2 - 10.1063/1.5065216

DO - 10.1063/1.5065216

M3 - Conference contribution

AN - SCOPUS:85056354032

VL - 2027

T3 - AIP Conference Proceedings

BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

A2 - Fomin, null

PB - American Institute of Physics Inc.

T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018

Y2 - 13 August 2018 through 19 August 2018

ER -

ID: 17413382