Standard

Experimental and numerical study of heat transfer in a flame jet impingement system. / Malikov, G. K.; Lobanov, D. L.; Malikov, Y. K. et al.
In: Journal of the Institute of Energy, Vol. 72, No. 490, 1999, p. 2 - 9.

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

Harvard

Malikov, GK, Lobanov, DL, Malikov, YK, Lisienko, VG, Viskanta, R & Fedorov, AG 1999, 'Experimental and numerical study of heat transfer in a flame jet impingement system', Journal of the Institute of Energy, vol. 72, no. 490, pp. 2 - 9.

APA

Malikov, G. K., Lobanov, D. L., Malikov, Y. K., Lisienko, V. G., Viskanta, R., & Fedorov, A. G. (1999). Experimental and numerical study of heat transfer in a flame jet impingement system. Journal of the Institute of Energy, 72(490), 2 - 9.

Vancouver

Malikov GK, Lobanov DL, Malikov YK, Lisienko VG, Viskanta R, Fedorov AG. Experimental and numerical study of heat transfer in a flame jet impingement system. Journal of the Institute of Energy. 1999;72(490):2 - 9.

Author

Malikov, G. K. ; Lobanov, D. L. ; Malikov, Y. K. et al. / Experimental and numerical study of heat transfer in a flame jet impingement system. In: Journal of the Institute of Energy. 1999 ; Vol. 72, No. 490. pp. 2 - 9.

BibTeX

@article{4085da2161c24edab12b1067a6ca3d1a,
title = "Experimental and numerical study of heat transfer in a flame jet impingement system",
abstract = "Combustion and heat transfer processes were studied in a specially designed, rapid heating experimental furnace, equipped with a multijet combustion chamber for natural gas/air firing. The system has no special combustion tunnels or flame holders and results were obtained for high velocities (up to 400 m s-1) and firing rates. Maximum convective heat fluxes of up to 260 kW m-2 were obtain with relatively 'cold' refractory wall temperatures (< 1300 K). The combustion gas temperatures ranged from 1400 to 1700 K. The mean flame jet flow characteristics and temperature profiles together with rates of heat transfer were measured. A simple two-dimensional numerical model was developed to predict combustion and radiative as well as convective heat transfer to the load and refractories in order to obtain an improved understanding of the processes.",
author = "Malikov, {G. K.} and Lobanov, {D. L.} and Malikov, {Y. K.} and Lisienko, {V. G.} and R. Viskanta and Fedorov, {A. G.}",
year = "1999",
language = "English",
volume = "72",
pages = "2 -- 9",
journal = "Journal of the Institute of Energy",
issn = "0144-2600",
publisher = "Taylor and Francis Ltd.",
number = "490",

}

RIS

TY - JOUR

T1 - Experimental and numerical study of heat transfer in a flame jet impingement system

AU - Malikov, G. K.

AU - Lobanov, D. L.

AU - Malikov, Y. K.

AU - Lisienko, V. G.

AU - Viskanta, R.

AU - Fedorov, A. G.

PY - 1999

Y1 - 1999

N2 - Combustion and heat transfer processes were studied in a specially designed, rapid heating experimental furnace, equipped with a multijet combustion chamber for natural gas/air firing. The system has no special combustion tunnels or flame holders and results were obtained for high velocities (up to 400 m s-1) and firing rates. Maximum convective heat fluxes of up to 260 kW m-2 were obtain with relatively 'cold' refractory wall temperatures (< 1300 K). The combustion gas temperatures ranged from 1400 to 1700 K. The mean flame jet flow characteristics and temperature profiles together with rates of heat transfer were measured. A simple two-dimensional numerical model was developed to predict combustion and radiative as well as convective heat transfer to the load and refractories in order to obtain an improved understanding of the processes.

AB - Combustion and heat transfer processes were studied in a specially designed, rapid heating experimental furnace, equipped with a multijet combustion chamber for natural gas/air firing. The system has no special combustion tunnels or flame holders and results were obtained for high velocities (up to 400 m s-1) and firing rates. Maximum convective heat fluxes of up to 260 kW m-2 were obtain with relatively 'cold' refractory wall temperatures (< 1300 K). The combustion gas temperatures ranged from 1400 to 1700 K. The mean flame jet flow characteristics and temperature profiles together with rates of heat transfer were measured. A simple two-dimensional numerical model was developed to predict combustion and radiative as well as convective heat transfer to the load and refractories in order to obtain an improved understanding of the processes.

UR - http://www.scopus.com/inward/record.url?partnerID=8YFLogxK&scp=0033096987

UR - https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=tsmetrics&SrcApp=tsm_test&DestApp=WOS_CPL&DestLinkType=FullRecord&KeyUT=000087692700001

M3 - Article

VL - 72

SP - 2

EP - 9

JO - Journal of the Institute of Energy

JF - Journal of the Institute of Energy

SN - 0144-2600

IS - 490

ER -

ID: 56800420