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Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating. / Morozov, S. O.; Shiplyuk, A. N.

International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics Inc., 2021. 040022 (AIP Conference Proceedings; Vol. 2351).

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

Harvard

Morozov, SO & Shiplyuk, AN 2021, Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating. in VM Fomin & A Shiplyuk (eds), International Conference on the Methods of Aerophysical Research, ICMAR 2020., 040022, AIP Conference Proceedings, vol. 2351, American Institute of Physics Inc., 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020, Akademgorodok, Novosibirsk, Russian Federation, 01.11.2020. https://doi.org/10.1063/5.0052162

APA

Morozov, S. O., & Shiplyuk, A. N. (2021). Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating. In V. M. Fomin, & A. Shiplyuk (Eds.), International Conference on the Methods of Aerophysical Research, ICMAR 2020 [040022] (AIP Conference Proceedings; Vol. 2351). American Institute of Physics Inc.. https://doi.org/10.1063/5.0052162

Vancouver

Morozov SO, Shiplyuk AN. Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating. In Fomin VM, Shiplyuk A, editors, International Conference on the Methods of Aerophysical Research, ICMAR 2020. American Institute of Physics Inc. 2021. 040022. (AIP Conference Proceedings). doi: 10.1063/5.0052162

Author

Morozov, S. O. ; Shiplyuk, A. N. / Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating. International Conference on the Methods of Aerophysical Research, ICMAR 2020. editor / Vasily M. Fomin ; Alexander Shiplyuk. American Institute of Physics Inc., 2021. (AIP Conference Proceedings).

BibTeX

@inproceedings{789560fd4f8e4f8fb0f213cad3b32197,
title = "Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating",
abstract = "The effect of the local surface heating on the stability of the boundary layer of the contoured nozzle M6 has been studied numerically for the hypersonic wind tunnel Transit-M ITAM SB RAS. Boundary layer profiles on the nozzle surface are found by the numerical simulation. Disturbance stability in the boundary layer is calculated in the context of the linear stability theory. It is shown that the local heating results in the slow-down of Goertler vortices amplification and Mack first mode in respect to the basic case; the stronger the heating, the stronger the effect. The second mode stabilizes at the local surface heating up to the temperature approaching to the stagnation temperature and de-stabilizes at further temperature rise. The optimal temperature of the local surface heating has been determined for the contoured nozzle M6 to stabilize disturbances in the boundary layer.",
author = "Morozov, {S. O.} and Shiplyuk, {A. N.}",
note = "Funding Information: The reported study was funded by RFBR according to the research project №19-08-00794. Publisher Copyright: {\textcopyright} 2021 Author(s).; 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020 ; Conference date: 01-11-2020 Through 07-11-2020",
year = "2021",
month = may,
day = "24",
doi = "10.1063/5.0052162",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Fomin, {Vasily M.} and Alexander Shiplyuk",
booktitle = "International Conference on the Methods of Aerophysical Research, ICMAR 2020",

}

RIS

TY - GEN

T1 - Stability of the boundary layer in the Mach-6 contoured nozzle with local surface heating

AU - Morozov, S. O.

AU - Shiplyuk, A. N.

N1 - Funding Information: The reported study was funded by RFBR according to the research project №19-08-00794. Publisher Copyright: © 2021 Author(s).

PY - 2021/5/24

Y1 - 2021/5/24

N2 - The effect of the local surface heating on the stability of the boundary layer of the contoured nozzle M6 has been studied numerically for the hypersonic wind tunnel Transit-M ITAM SB RAS. Boundary layer profiles on the nozzle surface are found by the numerical simulation. Disturbance stability in the boundary layer is calculated in the context of the linear stability theory. It is shown that the local heating results in the slow-down of Goertler vortices amplification and Mack first mode in respect to the basic case; the stronger the heating, the stronger the effect. The second mode stabilizes at the local surface heating up to the temperature approaching to the stagnation temperature and de-stabilizes at further temperature rise. The optimal temperature of the local surface heating has been determined for the contoured nozzle M6 to stabilize disturbances in the boundary layer.

AB - The effect of the local surface heating on the stability of the boundary layer of the contoured nozzle M6 has been studied numerically for the hypersonic wind tunnel Transit-M ITAM SB RAS. Boundary layer profiles on the nozzle surface are found by the numerical simulation. Disturbance stability in the boundary layer is calculated in the context of the linear stability theory. It is shown that the local heating results in the slow-down of Goertler vortices amplification and Mack first mode in respect to the basic case; the stronger the heating, the stronger the effect. The second mode stabilizes at the local surface heating up to the temperature approaching to the stagnation temperature and de-stabilizes at further temperature rise. The optimal temperature of the local surface heating has been determined for the contoured nozzle M6 to stabilize disturbances in the boundary layer.

UR - http://www.scopus.com/inward/record.url?scp=85107228054&partnerID=8YFLogxK

U2 - 10.1063/5.0052162

DO - 10.1063/5.0052162

M3 - Conference contribution

AN - SCOPUS:85107228054

T3 - AIP Conference Proceedings

BT - International Conference on the Methods of Aerophysical Research, ICMAR 2020

A2 - Fomin, Vasily M.

A2 - Shiplyuk, Alexander

PB - American Institute of Physics Inc.

T2 - 20th International Conference on the Methods of Aerophysical Research, ICMAR 2020

Y2 - 1 November 2020 through 7 November 2020

ER -

ID: 34054399