Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
Experimental study of the impact of N-wave on heat transfer in a boundary layer of a flat plate at the Mach number 2. / Kocharin, V. L.; Yatskikh, A. A.; Prishchepova, D. S. et al.
International Conference on the Methods of Aerophysical Research, ICMAR 2020. ed. / Vasily M. Fomin; Alexander Shiplyuk. American Institute of Physics Inc., 2021. 040036 (AIP Conference Proceedings; Vol. 2351).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
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TY - GEN
T1 - Experimental study of the impact of N-wave on heat transfer in a boundary layer of a flat plate at the Mach number 2
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: © 2021 Author(s). Copyright: Copyright 2021 Elsevier B.V., All rights reserved.
PY - 2021/5/24
Y1 - 2021/5/24
N2 - This work is devoted to the results of an experimental study of the impact of n-wave on heat transfer in a boundary layer of a flat plate at the Mach number 2. To generate N-wave into the flow, a roughness on the lower part of the nozzle of the test section of wind tunnel was used. As a result of the experiments, heat transfer data on the surface of a flat plate were obtained. A double longitudinal structure is shown in the form of a defect in temperature change caused by the interaction of two vortices with the surface of a flat plate model. The paper shows comparisons of the obtained distributions of the surface temperature difference in the cross section of the plate with measurements using a pitot tube and a constant temperature anemometer
AB - This work is devoted to the results of an experimental study of the impact of n-wave on heat transfer in a boundary layer of a flat plate at the Mach number 2. To generate N-wave into the flow, a roughness on the lower part of the nozzle of the test section of wind tunnel was used. As a result of the experiments, heat transfer data on the surface of a flat plate were obtained. A double longitudinal structure is shown in the form of a defect in temperature change caused by the interaction of two vortices with the surface of a flat plate model. The paper shows comparisons of the obtained distributions of the surface temperature difference in the cross section of the plate with measurements using a pitot tube and a constant temperature anemometer
UR - http://www.scopus.com/inward/record.url?scp=85107205898&partnerID=8YFLogxK
U2 - 10.1063/5.0051930
DO - 10.1063/5.0051930
M3 - Conference contribution
AN - SCOPUS:85107205898
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: 28729232