Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
To the analysis of the natural pulsation development during laminar-turbulent transition in supersonic boundary layer. / Kosinov, A. D.; Yermolaev, Yu G.; Semionov, N. V. et al.
Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017: Dedicated to the 60th Anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. ed. / Fomin. Vol. 1893 American Institute of Physics Inc., 2017. 030073 (AIP Conference Proceedings; Vol. 1893).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
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TY - GEN
T1 - To the analysis of the natural pulsation development during laminar-turbulent transition in supersonic boundary layer
AU - Kosinov, A. D.
AU - Yermolaev, Yu G.
AU - Semionov, N. V.
AU - Kolosov, G. L.
AU - Panina, A. V.
PY - 2017/10/26
Y1 - 2017/10/26
N2 - Natural pulsation development is considered in order to verify the linear and nonlinear region of transition process in supersonic boundary layers. To define the regions statistical approach is used. The typical way to see the linear disturbance development is to consist in verification of the normality distribution for pulsation amplitude measured by hot-wire. More complicated task is to determine the initial disturbance amplitudes in supersonic boundary layer in quantities of velocity, density and temperature and its relations during transition process. Solving such a problem scanning constant temperature anemometer is necessary to apply. Pulsation decomposition procedure is analyzed and used for measured data.
AB - Natural pulsation development is considered in order to verify the linear and nonlinear region of transition process in supersonic boundary layers. To define the regions statistical approach is used. The typical way to see the linear disturbance development is to consist in verification of the normality distribution for pulsation amplitude measured by hot-wire. More complicated task is to determine the initial disturbance amplitudes in supersonic boundary layer in quantities of velocity, density and temperature and its relations during transition process. Solving such a problem scanning constant temperature anemometer is necessary to apply. Pulsation decomposition procedure is analyzed and used for measured data.
KW - FLAT-PLATE
KW - STABILITY
KW - WIRE
KW - WAVE
UR - http://www.scopus.com/inward/record.url?scp=85034217157&partnerID=8YFLogxK
U2 - 10.1063/1.5007531
DO - 10.1063/1.5007531
M3 - Conference contribution
AN - SCOPUS:85034217157
VL - 1893
T3 - AIP Conference Proceedings
BT - Proceedings of the XXV Conference on High-Energy Processes in Condensed Matter, HEPCM 2017
A2 - Fomin, null
PB - American Institute of Physics Inc.
T2 - 25th Conference on High-Energy Processes in Condensed Matter, HEPCM 2017
Y2 - 5 June 2017 through 9 June 2017
ER -
ID: 9696516