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Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds. / Kozlov, V. V.; Grek, G. R.; Litvinenko, Yu A. et al.

In: Doklady Physics, Vol. 64, No. 3, 01.03.2019, p. 134-138.

Research output: Contribution to journal › Article › peer-review

Harvard

Kozlov, VV, Grek, GR, Litvinenko, YA, Shmakov, AG & Vikhorev, VV 2019, 'Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds', Doklady Physics, vol. 64, no. 3, pp. 134-138. https://doi.org/10.1134/S1028335819030169

APA

Kozlov, V. V., Grek, G. R., Litvinenko, Y. A., Shmakov, A. G., & Vikhorev, V. V. (2019). Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds. Doklady Physics, 64(3), 134-138. https://doi.org/10.1134/S1028335819030169

Vancouver

Kozlov VV, Grek GR, Litvinenko YA, Shmakov AG, Vikhorev VV. Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds. Doklady Physics. 2019 Mar 1;64(3):134-138. doi: 10.1134/S1028335819030169

Author

Kozlov, V. V. ; Grek, G. R. ; Litvinenko, Yu A. et al. / Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds. In: Doklady Physics. 2019 ; Vol. 64, No. 3. pp. 134-138.

BibTeX

@article{631e32ce310b4dcd8cbeb2a3a3432b7c,
title = "Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds",
abstract = "In this paper, we presented the results of experimental studies of the diffusion combustion of a plain hydrogen microjet flowing from a slit micronozzle at subsonic and supersonic speeds. For the first time, four scenarios of diffusion combustion of a plain hydrogen microjet including supersonic combustion in the presence of supersonic cells in both air and hydrogen are presented. The stabilization of the subsonic combustion of a hydrogen microjet was established to be due to the presence of a “flame constriction region,” while the stabilization of the supersonic combustion of a microjet was found to be associated with the presence of supersonic cells. The observed hysteresis of diffusion combustion of a plain hydrogen microjet depends on both the method of igniting the microjet (near or far from the nozzle exit) and the direction of change in the rate of its outflow (growth or reduction).",
author = "Kozlov, {V. V.} and Grek, {G. R.} and Litvinenko, {Yu A.} and Shmakov, {A. G.} and Vikhorev, {V. V.}",
year = "2019",
month = mar,
day = "1",
doi = "10.1134/S1028335819030169",
language = "English",
volume = "64",
pages = "134--138",
journal = "Doklady Physics",
issn = "1028-3358",
publisher = "Maik Nauka-Interperiodica Publishing",
number = "3",

}

RIS

TY - JOUR

T1 - Combustion of a Plane Hydrogen Microjet at Subsonic and Supersonic Speeds

AU - Kozlov, V. V.

AU - Grek, G. R.

AU - Litvinenko, Yu A.

AU - Shmakov, A. G.

AU - Vikhorev, V. V.

PY - 2019/3/1

Y1 - 2019/3/1

N2 - In this paper, we presented the results of experimental studies of the diffusion combustion of a plain hydrogen microjet flowing from a slit micronozzle at subsonic and supersonic speeds. For the first time, four scenarios of diffusion combustion of a plain hydrogen microjet including supersonic combustion in the presence of supersonic cells in both air and hydrogen are presented. The stabilization of the subsonic combustion of a hydrogen microjet was established to be due to the presence of a “flame constriction region,” while the stabilization of the supersonic combustion of a microjet was found to be associated with the presence of supersonic cells. The observed hysteresis of diffusion combustion of a plain hydrogen microjet depends on both the method of igniting the microjet (near or far from the nozzle exit) and the direction of change in the rate of its outflow (growth or reduction).

AB - In this paper, we presented the results of experimental studies of the diffusion combustion of a plain hydrogen microjet flowing from a slit micronozzle at subsonic and supersonic speeds. For the first time, four scenarios of diffusion combustion of a plain hydrogen microjet including supersonic combustion in the presence of supersonic cells in both air and hydrogen are presented. The stabilization of the subsonic combustion of a hydrogen microjet was established to be due to the presence of a “flame constriction region,” while the stabilization of the supersonic combustion of a microjet was found to be associated with the presence of supersonic cells. The observed hysteresis of diffusion combustion of a plain hydrogen microjet depends on both the method of igniting the microjet (near or far from the nozzle exit) and the direction of change in the rate of its outflow (growth or reduction).

UR - http://www.scopus.com/inward/record.url?scp=85066500111&partnerID=8YFLogxK

U2 - 10.1134/S1028335819030169

DO - 10.1134/S1028335819030169

M3 - Article

AN - SCOPUS:85066500111

VL - 64

SP - 134

EP - 138

JO - Doklady Physics

JF - Doklady Physics

SN - 1028-3358

IS - 3

ER -

ID: 20347289