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Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. / Kocharin, V. L.; Yatskikh, A. A.; Prishchepova, D. S. et al.

High-Energy Processes in Condensed Matter, HEPCM 2020: Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, Dedicated to the 90th Anniversary of the Birth of RI Soloukhin. ed. / Vasily M. Fomin. American Institute of Physics Inc., 2020. 030014 (AIP Conference Proceedings; Vol. 2288).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review

Harvard

Kocharin, VL, Yatskikh, AA, Prishchepova, DS, Panina, AV, Yermolaev, YG, Kosinov, AD, Semionov, NV & Afanasev, LV 2020, Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. in VM Fomin (ed.), High-Energy Processes in Condensed Matter, HEPCM 2020: Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, Dedicated to the 90th Anniversary of the Birth of RI Soloukhin., 030014, AIP Conference Proceedings, vol. 2288, American Institute of Physics Inc., 27th Conference on High-Energy Processes in Condensed Matter, HEPCM 2020, Novosibirsk, Russian Federation, 29.06.2020. https://doi.org/10.1063/5.0028302

APA

Kocharin, V. L., Yatskikh, A. A., Prishchepova, D. S., Panina, A. V., Yermolaev, Y. G., Kosinov, A. D., Semionov, N. V., & Afanasev, L. V. (2020). Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. In V. M. Fomin (Ed.), High-Energy Processes in Condensed Matter, HEPCM 2020: Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, Dedicated to the 90th Anniversary of the Birth of RI Soloukhin [030014] (AIP Conference Proceedings; Vol. 2288). American Institute of Physics Inc.. https://doi.org/10.1063/5.0028302

Vancouver

Kocharin VL, Yatskikh AA, Prishchepova DS, Panina AV, Yermolaev YG, Kosinov AD et al. Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. In Fomin VM, editor, High-Energy Processes in Condensed Matter, HEPCM 2020: Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, Dedicated to the 90th Anniversary of the Birth of RI Soloukhin. American Institute of Physics Inc. 2020. 030014. (AIP Conference Proceedings). doi: 10.1063/5.0028302

Author

Kocharin, V. L. ; Yatskikh, A. A. ; Prishchepova, D. S. et al. / Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. High-Energy Processes in Condensed Matter, HEPCM 2020: Proceedings of the XXVII Conference on High-Energy Processes in Condensed Matter, Dedicated to the 90th Anniversary of the Birth of RI Soloukhin. editor / Vasily M. Fomin. American Institute of Physics Inc., 2020. (AIP Conference Proceedings).

BibTeX

@inproceedings{df3bb22a70984b64961eab9e77481bb4,
title = "Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge",
abstract = "This paper is devoted to the results of an experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. The experimental study was conducted on the model of blunt flat plate at Mach 2. To generate weak shock waves into the flow, a roughness on the lower part of the nozzle of the test section of wind tunnel was used. Visualization experiments of heat flows were carried out using an infrared camera. As a result of experiments, data on the features of heat transfer on the surface of a flat plate were obtained. A double longitudinal structure in the form of a temperature change defect caused by the interaction of two vortices with the model surface is shown. Temperature changes in the vortex region downstream in a direction parallel to the leading edge have a similar structure, but different amplitudes.",
keywords = "MACH WAVE, FLOW",
author = "Kocharin, {V. L.} and Yatskikh, {A. A.} and Prishchepova, {D. S.} and Panina, {A. V.} and Yermolaev, {Yu G.} and Kosinov, {A. D.} and Semionov, {N. V.} and Afanasev, {L. V.}",
note = "Publisher Copyright: {\textcopyright} 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.; 27th Conference on High-Energy Processes in Condensed Matter, HEPCM 2020 ; Conference date: 29-06-2020 Through 03-07-2020",
year = "2020",
month = oct,
day = "26",
doi = "10.1063/5.0028302",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin, {Vasily M.}",
booktitle = "High-Energy Processes in Condensed Matter, HEPCM 2020",

}

RIS

TY - GEN

T1 - Experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge

AU - Kocharin, V. L.

AU - Yatskikh, A. A.

AU - Prishchepova, D. S.

AU - Panina, A. V.

AU - Yermolaev, Yu G.

AU - Kosinov, A. D.

AU - Semionov, N. V.

AU - Afanasev, L. V.

N1 - Publisher Copyright: © 2020 Author(s). Copyright: Copyright 2020 Elsevier B.V., All rights reserved.

PY - 2020/10/26

Y1 - 2020/10/26

N2 - This paper is devoted to the results of an experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. The experimental study was conducted on the model of blunt flat plate at Mach 2. To generate weak shock waves into the flow, a roughness on the lower part of the nozzle of the test section of wind tunnel was used. Visualization experiments of heat flows were carried out using an infrared camera. As a result of experiments, data on the features of heat transfer on the surface of a flat plate were obtained. A double longitudinal structure in the form of a temperature change defect caused by the interaction of two vortices with the model surface is shown. Temperature changes in the vortex region downstream in a direction parallel to the leading edge have a similar structure, but different amplitudes.

AB - This paper is devoted to the results of an experimental study of heat transfer in the boundary layer of a flat plate with the impact of weak shock waves on the leading edge. The experimental study was conducted on the model of blunt flat plate at Mach 2. To generate weak shock waves into the flow, a roughness on the lower part of the nozzle of the test section of wind tunnel was used. Visualization experiments of heat flows were carried out using an infrared camera. As a result of experiments, data on the features of heat transfer on the surface of a flat plate were obtained. A double longitudinal structure in the form of a temperature change defect caused by the interaction of two vortices with the model surface is shown. Temperature changes in the vortex region downstream in a direction parallel to the leading edge have a similar structure, but different amplitudes.

KW - MACH WAVE

KW - FLOW

UR - http://www.scopus.com/inward/record.url?scp=85096658645&partnerID=8YFLogxK

U2 - 10.1063/5.0028302

DO - 10.1063/5.0028302

M3 - Conference contribution

AN - SCOPUS:85096658645

T3 - AIP Conference Proceedings

BT - High-Energy Processes in Condensed Matter, HEPCM 2020

A2 - Fomin, Vasily M.

PB - American Institute of Physics Inc.

T2 - 27th Conference on High-Energy Processes in Condensed Matter, HEPCM 2020

Y2 - 29 June 2020 through 3 July 2020

ER -

ID: 26098340