| Citation: | WANG Peng-fei, TIAN Hui, YU Nan-jia, CAI Guo-biao. Two-phase flow numerical calculation of H2O2/HTPB hybrid rocket engine with diaphragm in grain[J]. Journal of Aerospace Power, 2013, 28(11): 2621-2626. |
| [1] |
田辉.固液混合火箭发动机工作过程数值仿真.北京:北京航空航天大学,2005. TIAN Hui.Numerical simulation of the operation process of a hybrid rocket motor.Beijing:Beijing University of Aeronautics and Astronautics,2005.(in Chinese)
|
| [2] |
Chiaverini M J,Kuo K K.Fundamental of hybrid rocket combustion and propulsion[M].Reston,US:AIAA,2007.
|
| [3] |
田辉,蔡国飙,王慧玉,等.固液混合火箭发动机燃烧室和喷管流动数值模拟[J].宇航学报,2006,27(2):281-285. TIAN Hui,CAI Guobiao,WANG Huiyu,et al.Numerical simulation of combustion chamber and nozzle flow in classical hybrid rocket motors[J].Journal of Astronautics,2006,27(2):281-285.(in Chinese)
|
| [4] |
Marxman G A,Wooldridge C E,Muzzy R J.Fundamentals of hybrid boundary combustion[J].Heterogeneous Combustion,Progress in Astronautic and Aeronautics,1964,15:485-521.
|
| [5] |
田辉,蔡国飙,孙再庸.N2O/HTPB固液火箭发动机喷管两相流计算[J].航空动力学学报,2008,23(6):1146-1150. TIAN Hui,CAI Guobiao,SUN Zaiyong.Computation of nozzle two-phase flow in a N2O/HTPB hybrid rocket motor[J].Journal of Aerospace Power,2008,23(6):1146-1150.(in Chinese)
|
| [6] |
朱浩,蔡国飙.不同药型固液火箭发动机性能特点[J].航空动力学报,2011,26(10):2347-2351. ZHU Hao,CAI Guobiao.Performance characteristics of hybrid rocket motors with different grain types[J].Journal of Aerospace Power,2011,26(10):2347-2351.(in Chinese)
|
| [7] |
饶大林,李新田,田辉,等.基于混合优化算法的固液发动机装药优化设计[J].航空动力学报,2010,25(5):1151-1152. RAO Dalin,LI Xintian,TIAN Hui,et al.Optimization of grain design for hybrid rocket engine based on hybrid optimization algorithm[J].Journal of Aerospace Power,2010,25(5):1151-1152.(in Chinese)
|
| [8] |
Kim H,Kim S,Woo K,et al.Investigation on the effect of liquefying diaphragm in hybrid rocket motors using paraffin-based fuel.AIAA-2011-5824,2011.
|
| [9] |
Matthias G,Gerhard S.Development of a hybrid rocket motor using a diaphragm for a small test rocket.AIAA-2008-4831,2008.
|
| [10] |
Matthias G.Effect of a diaphragm on performance and fuel regression of a laboratory scale hybrid rocket motor using nitrous oxide and paraffin.AIAA-2009-5113,2009.
|
| [11] |
Lin J L.Two-phase flow effect on hybrid rocket combustion[J].Acta Astronautic,2009,65(7):1042-1057.
|
| [12] |
Alberto B,Marta L,Nicolas B.Testing and CFD simulation of diaphragm hybrid rocket motors.AIAA-2011-6023,2011.
|
| [13] |
Magnussen B F,Hjertager B H.On mathematical models of turbulent combustion with special emphasis on soot formation and combustion[J].Symposium (International) on Combustion,1977,16(1):719-729.
|
| [14] |
CAI Guobiao,ZENG Peng,LI Xintian,et al.Scale effect of fuel regression rate in hybrid rocket motor[J].Aerospace Science and Technology,2013,24(1):141-146.
|
| [15] |
Shih T H,Liou W W,Shabbir A,et al.A new k-ε eddy-viscosity model for high Reynolds number turbulent flows:model development and validation[J].Computers Fluids,1995,24(3):227-238.
|