PDF下载 分享
[1]吴家彤.6.5马赫超燃冲压发动机的近期飞行试验结果[J].火箭推进,2004,(02):48-53.
点击复制

6.5马赫超燃冲压发动机的近期飞行试验结果

相似文献/References:

[1]朱舒扬.全尺寸超燃冲压发动机推力测量台架研制[J].火箭推进,2015,41(05):106.
 ZHU Shuyang.Development of thrust measurement platform for full-scale scramjet[J].Journal of Rocket Propulsion,2015,41(02):106.
[2]王小永,张天平,江豪成,等.40 mN/3 000 s氙离子电推进系统工作性能在轨测试与分析[J].火箭推进,2015,41(01):76.
 WANG Xiao-yong,ZHANG Tian-ping,JIANG Hao-cheng,et al.In-orbit test and analysis of working performance for 40 mN/3 000 s xenon ion electric propulsion system[J].Journal of Rocket Propulsion,2015,41(02):76.
[3]姚照辉,李光熙,张蒙正,等.燃油分配对超燃冲压发动机的性能影响仿真分析[J].火箭推进,2013,39(04):30.
 YAO Zhao-hui,LI Guang-xi,ZHANG Meng-zheng,et al.Simulation and analysis for influence of fuel distribution on scramjet performance[J].Journal of Rocket Propulsion,2013,39(02):30.
[4]刘 昊,李光熙,杜 泉,等.超燃冲压发动机全流道反应流场仿真分析[J].火箭推进,2013,39(06):1.
 LIU Hao,LI Guang-xi,DU Quan,et al.Numerical simulation of reaction flow field in full flowpath of scramjet[J].Journal of Rocket Propulsion,2013,39(02):1.
[5]张 倩,王 兵,张耘隆,等.RBCC的可实现性方案—DRBCC分析[J].火箭推进,2014,40(05):1.
 ZHANG Qian,WANG Bing,ZHANG Yun-long,et al.An analysis of RBCC realizability scheme: DRBCC[J].Journal of Rocket Propulsion,2014,40(02):1.
[6]赵宏亮,张蒙正.超燃冲压发动机推阻力特性研究综述[J].火箭推进,2014,40(06):41.
 ZHAO Hong-liang,ZHANG Meng-zheng.Investigation of thrust/drag property of scramjet[J].Journal of Rocket Propulsion,2014,40(02):41.
[7]张蒙正,邹 宇.美国典型高超飞行器项目研发及启示[J].火箭推进,2012,38(02):1.
 ZHANG Meng-zheng,ZOU Yu.Development of American typical hypersonic flight vehicles and its enlightenment[J].Journal of Rocket Propulsion,2012,38(02):1.
[8]李龙飞,王延涛,杨伟东,等.超声速燃烧地面试验的蓄热式加热器及其关键技术[J].火箭推进,2012,38(02):16.
 LI Long-fei,WANG Yan-tao,YANG Wei-dong,et al.Thermal energy storage heater and its key technologies for supersonic combustion ground test facilities[J].Journal of Rocket Propulsion,2012,38(02):16.
[9]文 科,李旭昌,马岑睿,等.不同入口马赫数对超燃冲压发动机尾喷管的性能影响研究[J].火箭推进,2011,37(03):18.
 WEN Ke,LI Xu-chang,MA Cen-rui,et al.Influence of nozzle inlet Mach number on performance of scramjet nozzle[J].Journal of Rocket Propulsion,2011,37(02):18.
[10]冯锦虎,高峰,何至林.超燃冲压发动机隔离段内附面层/激波串相互干扰研究[J].火箭推进,2010,36(02):5.
 Feng Jinhu,Gao Feng,He Zhilin.Investigation of boundary layer/shock wave train interference in a scramjet isolator[J].Journal of Rocket Propulsion,2010,36(02):5.

更新日期/Last Update: 1900-01-01