TY - JOUR
T1 - Experimental investigation on heat flux measurement of nozzle throat
AU - Xiao, Hu Liang
AU - Hu, Chun Bo
AU - Zhang, Sheng Min
AU - Deng, Zhe
AU - Qin, Fei
PY - 2013/2
Y1 - 2013/2
N2 - In order to isolate the effect of thermochemistry ablation on measuring the heat flux of nozzle throat, the experiments were carried out by using a HT50-20 heat flux transducer to obtain the heat flux density in nozzle throat under various incoming flow conditions as well as the parameters of the burning gases. Meanwhile, on the basis of experiments, numerical simulation was conducted to investigate the heat flux of nozzle throat. The experimental results show that the heat flux density is 0.496 MW/m2, 0.471 MW/m2, 0.317 MW/m2 when the temperature of burning gases at the nozzle throat is 611 K, 551 K, 457 K respectively. Furthermore, the data of experiments can be used to validate the numerical simulation.
AB - In order to isolate the effect of thermochemistry ablation on measuring the heat flux of nozzle throat, the experiments were carried out by using a HT50-20 heat flux transducer to obtain the heat flux density in nozzle throat under various incoming flow conditions as well as the parameters of the burning gases. Meanwhile, on the basis of experiments, numerical simulation was conducted to investigate the heat flux of nozzle throat. The experimental results show that the heat flux density is 0.496 MW/m2, 0.471 MW/m2, 0.317 MW/m2 when the temperature of burning gases at the nozzle throat is 611 K, 551 K, 457 K respectively. Furthermore, the data of experiments can be used to validate the numerical simulation.
KW - Experimental measurement
KW - Heat flux density
KW - Heat flux transducer
KW - Nozzle throat
UR - http://www.scopus.com/inward/record.url?scp=84876071375&partnerID=8YFLogxK
U2 - 10.7673/j.issn.1006-2793.2013.01.027
DO - 10.7673/j.issn.1006-2793.2013.01.027
M3 - 文章
AN - SCOPUS:84876071375
SN - 1006-2793
VL - 36
SP - 138
EP - 142
JO - Guti Huojian Jishu/Journal of Solid Rocket Technology
JF - Guti Huojian Jishu/Journal of Solid Rocket Technology
IS - 1
ER -