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Lebiga, V. A.; Zinov'ev, V. N.; Pak, A. Yu.

doi:10.1023/a:1015391025644

Cited by 9 publications

(2 citation statements)

References 4 publications

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“…The decomposition of the output signal of the hot-wire anemometer on the pulsation of the mass flux and the total temperature is provided according to the well-known algorithm [7][8][9][10][11][12][13][14][15]. The hot-wire probe is sensitive to pulsations of mass flux m and temperature T0 .…”

Section: Experimental Setup and Data Processmentioning

confidence: 99%

“…The experience of many studies shows that unique experimental data on the composition of pulsations of highspeed flows can be obtained with a hot-wire anemometer [7][8][9][10][11][12][13][14]. It is possible to obtain data on the amplitude of total temperature and mass flux pulsations by measurements at different values of the probe overheating.…”

Section: Introductionmentioning

confidence: 99%

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The evolution of mass flow and total temperature pulsations in flat plate boundary layer at M=2.5

Yatskikh

Kolosov

Kosinov

et al. 2017

AIP Conference Proceedings

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Abstract. The work is devoted to the study of the regularities of laminar-turbulent transition in supersonic boundary layers. New experimental data are presented on the evolution downstream of natural disturbances in the boundary layer of a flat plate. The experiments were carried out in a low-noise supersonic wind tunnel T-325 of ITAM SB RAS at Mach number M=2.5. The measurements were made by a constant-temperature hot-wire anemometer in the scanning mode. The procedure of decomposition of the fluctuations of the boundary layer into temperature and mass flux disturbances is carried out.

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