您要查找的是不是：
- At first, the thermodynamic calculation of Solid Ducted Rocket is researche. 在此基础上，首先对固体冲压发动机热力计算展开了研究分析。
- Stowe R A, Champlain A De, Mayer A E H J. Modeling combustor performance of a ducted rocket[R]. AIAA paper 2000-3728. 张炜;方丁酉;夏智勋;等.;非壅塞固体火箭冲压发动机工作特性研究[J]
- Stowe R A,Champlain A D,Mayer A E H J.Modelling combustor performance of a ducted rocket[R].AIAA 2000-3728. 陈林泉;毛根旺;霍东兴;等.;燃气喷射方式对冲压发动机补燃室掺混效果的影响[J]
- In this paper, the theory of minitype Solid Ducted Rocket with shot is researche nd analyzed. 本文研究和分析了炮射小型固体火箭冲压发动机的工作原理。
- It would be of great reference value for development of air-to-air missile propelled by integral solid ducted rocket. 对我国发展采用整体式固冲发动机的空空导弹具有重要的参考价值。
- Mayer A E H J,Stowe R A.Experimental study into mixing in a solid fuel ducted rocket combustion chamber[R].AIAA 2000-3346. 余勇;陈小前;等.;三维实验固体火箭冲压发动机燃烧室湍流反应流数值模拟[J]
- The characterization of the combustion properties of the aluminum? magnesium fuel? rich propellant for unchoked ducted rocket was studied. 系统研究了铝镁贫氧推进剂低压燃烧特性的表征方法。
- Mayer A E H J,Stowe R A. Experimental Study Into Mixing in a Solid Fuel Ducted Rocket Combustion Chamber[R]. AIAA Paper 2000-3346. 张炜;夏智勋;姜春林;等.;新型非壅塞式固体火箭冲压发动机试验研究[J]
- The effects of TMOs and their mixtures on the burning rate and the pressure exponent of the aluminum magnesium fuel rich propellant for unchoked ducted rocket are investigated. 研究了过渡金属氧化物(TMO)及其复配物对非壅塞固体火箭冲压发动机铝镁贫氧推进剂燃烧特性的影响。
- Flight tests for an integrated ducted rocket were carried out successfully following ground tests in order to investigate the performance of the ducted rocket. 在地面试验基础上进行了整体式固体火箭冲压发动机飞行试验,以验证发动机的工作可靠性和飞行性能。
- In addition, the USAF continues to fund development work of the Aerojet (formerly Atlantic Research) Variable Flow Ducted Rocket ramjet system as a future propulsion option for an extended range AAM. 此外，美国空军继续投资于航空喷气研究所（原来的大西洋研究所）的可变喷流管火箭发动机系统，将其作为增程空空导弹的未来推进选项。
- The method developed in this paper can be used in the research field of the Ducted Rocket and fuel-rich propellant, to reduce the experimental cost effetely and shorten the research period greatly. 对于固体冲压发动机和贫氧推进剂的研制来说,本文研究的方法既可有效地降低试验成本,又可大大缩短研制周期,具有一定的工程应用价值。
- The burning rate of the fuel-rich propellants is the parameter which is important for Ducted Rocket design and performance analysis and is main inspection criterions of propellant prescriptions. 贫氧推进剂燃速是固体火箭冲压发动机设计和性能分析的重要参数,也是对推进剂配方进行检验验收的主要指标。
- unchoked solid ducted rocket engine 非壅塞固体火箭冲压发动机
- Our pilotless rocket enters the track of the earth. 我们把一个无人驾驶的火箭送入了地球的轨道里。
- NUMERICAL STUDY OF MIXING FLOWS IN A DUCTED ROCKET COMBUSTOR 火箭冲压发动机掺混流场数值方法研究
- Study of the Unchoked Ducted Rocket Engine and Fuel-Rich Propellant 非壅塞固体火箭冲压发动机及其贫氧推进剂
- They planned to send a rocket to the moon. 他们计划向月球发射火箭。
- Carrying down or away. Used of a duct or vessel. 传送的指通过导管或管道传送下来的或输送的
- Imagine a rocket that can travel at the rate of light! 想象一下能以光的速度飞行的火箭。
- 今日热词
-
- 深远海浮式风电平台 - deep-sea floating wind power platform
-
- 京雄高速公路 - Beijing-Xiongan expressway
-
- 农业及相关产业增加值 - the added value of agriculture and related industries
