Standard

The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing. / Semionov, N. V.; Yermolaev, Yu G.; Kosinov, A. D. et al.

International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. ed. / Vasily Fomin. American Institute of Physics Inc., 2016. 030050 (AIP Conference Proceedings; Vol. 1770).

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

Harvard

Semionov, NV, Yermolaev, YG, Kosinov, AD, Dryasov, AD, Semenov, AN & Yatskikh, AA 2016, The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing. in V Fomin (ed.), International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research., 030050, AIP Conference Proceedings, vol. 1770, American Institute of Physics Inc., 18th International Conference on the Methods of Aerophysical Research, ICMAR 2016, Perm, Russian Federation, 27.06.2016. https://doi.org/10.1063/1.4963992

APA

Semionov, N. V., Yermolaev, Y. G., Kosinov, A. D., Dryasov, A. D., Semenov, A. N., & Yatskikh, A. A. (2016). The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing. In V. Fomin (Ed.), International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research [030050] (AIP Conference Proceedings; Vol. 1770). American Institute of Physics Inc.. https://doi.org/10.1063/1.4963992

Vancouver

Semionov NV, Yermolaev YG, Kosinov AD, Dryasov AD, Semenov AN, Yatskikh AA. The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing. In Fomin V, editor, International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. American Institute of Physics Inc. 2016. 030050. (AIP Conference Proceedings). doi: 10.1063/1.4963992

Author

Semionov, N. V. ; Yermolaev, Yu G. ; Kosinov, A. D. et al. / The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing. International Conference on the Methods of Aerophysical Research, ICMAR 2016: Proceedings of the 18th International Conference on the Methods of Aerophysical Research. editor / Vasily Fomin. American Institute of Physics Inc., 2016. (AIP Conference Proceedings).

BibTeX

@inproceedings{7dfb030ce18044c6ab09da54155fea19,
title = "The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing",
abstract = "The paper is devoted to an experimental study of laminar-turbulent transition in a three-dimensional supersonic boundary layer. The experiments were conducted at the low nose supersonic wind tunnel T-325 of ITAM at Mach numbers M=2 - 4. Model is a symmetrical wing with a 45° sweep angle, a 3 percent-thick circular-arc airfoil. The influence of flow parameters, such as the Mach number, unit Reynolds number, angle of attack, level of perturbations on the transitions to turbulence are on the consideration. Transition Reynolds numbers are obtained. Analysis of all obtained data allow to determine reliable value of Retr of swept wing supersonic boundary layer, that especially important at consideration of experiments fulfilled at different flow conditions in different wind tunnels.",
author = "Semionov, {N. V.} and Yermolaev, {Yu G.} and Kosinov, {A. D.} and Dryasov, {A. D.} and Semenov, {A. N.} and Yatskikh, {A. A.}",
year = "2016",
month = oct,
day = "13",
doi = "10.1063/1.4963992",
language = "English",
series = "AIP Conference Proceedings",
publisher = "American Institute of Physics Inc.",
editor = "Vasily Fomin",
booktitle = "International Conference on the Methods of Aerophysical Research, ICMAR 2016",
note = "18th International Conference on the Methods of Aerophysical Research, ICMAR 2016 ; Conference date: 27-06-2016 Through 03-07-2016",

}

RIS

TY - GEN

T1 - The influence of flow parameters on the transition to turbulence in supersonic boundary layer on swept wing

AU - Semionov, N. V.

AU - Yermolaev, Yu G.

AU - Kosinov, A. D.

AU - Dryasov, A. D.

AU - Semenov, A. N.

AU - Yatskikh, A. A.

PY - 2016/10/13

Y1 - 2016/10/13

N2 - The paper is devoted to an experimental study of laminar-turbulent transition in a three-dimensional supersonic boundary layer. The experiments were conducted at the low nose supersonic wind tunnel T-325 of ITAM at Mach numbers M=2 - 4. Model is a symmetrical wing with a 45° sweep angle, a 3 percent-thick circular-arc airfoil. The influence of flow parameters, such as the Mach number, unit Reynolds number, angle of attack, level of perturbations on the transitions to turbulence are on the consideration. Transition Reynolds numbers are obtained. Analysis of all obtained data allow to determine reliable value of Retr of swept wing supersonic boundary layer, that especially important at consideration of experiments fulfilled at different flow conditions in different wind tunnels.

AB - The paper is devoted to an experimental study of laminar-turbulent transition in a three-dimensional supersonic boundary layer. The experiments were conducted at the low nose supersonic wind tunnel T-325 of ITAM at Mach numbers M=2 - 4. Model is a symmetrical wing with a 45° sweep angle, a 3 percent-thick circular-arc airfoil. The influence of flow parameters, such as the Mach number, unit Reynolds number, angle of attack, level of perturbations on the transitions to turbulence are on the consideration. Transition Reynolds numbers are obtained. Analysis of all obtained data allow to determine reliable value of Retr of swept wing supersonic boundary layer, that especially important at consideration of experiments fulfilled at different flow conditions in different wind tunnels.

UR - http://www.scopus.com/inward/record.url?scp=84994083549&partnerID=8YFLogxK

U2 - 10.1063/1.4963992

DO - 10.1063/1.4963992

M3 - Conference contribution

AN - SCOPUS:84994083549

T3 - AIP Conference Proceedings

BT - International Conference on the Methods of Aerophysical Research, ICMAR 2016

A2 - Fomin, Vasily

PB - American Institute of Physics Inc.

T2 - 18th International Conference on the Methods of Aerophysical Research, ICMAR 2016

Y2 - 27 June 2016 through 3 July 2016

ER -

ID: 25838581