TY - JOUR
T1 - Compare of plug nozzle's heat transfer characteristics in different operation condition and with different coolant flow rate
AU - Han, Fei
AU - Liu, Yu
AU - Li, Jun Wei
PY - 2006/8
Y1 - 2006/8
N2 - To understand the different heat transfer characteristics of regenerative cooling in plug nozzle at different operating conditions, computational model of two dimensional plug nozzle and internal nozzle were established and numerical simulation was employed. Heat transfer results of the internal nozzle and the parameter distribution at the outlet were obtained. Flowfield and heat transfer characteristics of the plug at different operating conditions with different coolant flow rates were investigated. For calculation, governing equations were discretized with second order upstream scheme. The results show that at sea level, coolant flow rate affects the plug pressure, heat flux and temperature; at design operating condition, coolant flow rate has no effect on pressure and heat flux on the plug wall. With the same coolant flow rate, plug temperature at sea level is higher than that at design operating condition; under the same operating condition, ramp temperature is higher than the plug base temperature.
AB - To understand the different heat transfer characteristics of regenerative cooling in plug nozzle at different operating conditions, computational model of two dimensional plug nozzle and internal nozzle were established and numerical simulation was employed. Heat transfer results of the internal nozzle and the parameter distribution at the outlet were obtained. Flowfield and heat transfer characteristics of the plug at different operating conditions with different coolant flow rates were investigated. For calculation, governing equations were discretized with second order upstream scheme. The results show that at sea level, coolant flow rate affects the plug pressure, heat flux and temperature; at design operating condition, coolant flow rate has no effect on pressure and heat flux on the plug wall. With the same coolant flow rate, plug temperature at sea level is higher than that at design operating condition; under the same operating condition, ramp temperature is higher than the plug base temperature.
KW - Aerospace propulsion system
KW - Heat flux
KW - Liquid propellant rocket engines
KW - Numerical simulation
KW - Plug nozzle
KW - Regenerative cooling
UR - http://www.scopus.com/inward/record.url?scp=33750391517&partnerID=8YFLogxK
M3 - Article
AN - SCOPUS:33750391517
SN - 1000-8055
VL - 21
SP - 778
EP - 783
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 4
ER -