Numerical investigation of two-phase detonation with the osbstacles
National Key Lab. of Transient Physics, Nanjing Univ. of Science and Technology, Nanjing 210094,China;National Key Lab. of Transient Physics, Nanjing Univ. of Science and Technology, Nanjing 210094,China
[2] Louis A Povinelli,Shaye Yungter.Real gas effects on the performance of hydrocarbon-fueled pulse detonation engines[R].AIAA 2003-0712 . [3] Kailasanath K.Recent developments in the research on pulse detonation engines[R].AIAA 2002-0470. [4] Morris C I.Numerical modeling of pulse detonation rocket engine gas-dynamics and performance[R].AIAA 2004-463. [5] 张群,严传俊,范玮,等.点火能量对两相爆震波形成影响的数值研究[J].火工品,2007,(3):6-10. [6] 张群,闫朝,严传俊.两相爆震波爆燃向爆震转变过程的数值模拟[J].计算机仿真,2008,25(2). [7] 翁春生,王浩.计算内弹道[M].北京:国防工业出版社,2006. [8] Chang S C.The method of space-time conservation element and solution element- a new approach for solving the Navier-Stokes and euler equations[J].Journal of Computational Physics, 5,9:295-324. [9] 马丹花,翁春生.二维守恒元和求解元方法在两相爆震流场计算中的应用[J].燃烧科学与技术, 0,6(1):85-91. [10] 翁春生,王杰,白桥栋,等.脉冲爆震发动机进气压力对爆震影响的实验研究[J].弹道学报,8,0(3).
