1)Solid Rocket Ramjet固冲发动机
1.During the study of Solid Rocket Ramjet (SRR), ablation of afterburner thermal insulation is a serious problem, which cannot be ignored.固冲发动机补燃室绝热层的烧蚀问题是目前固冲发动机研制过程中所面临的一个重要问题。
英文短句/例句
1.Design of Transition-control Module for Integral Solid Rocket-ramjet整体式固冲发动机转级控制模块设计
2.Numerical simulation and experimental study of deposition for ducted rockets固冲发动机沉积数值模拟与试验研究
3.Analysis of flux-adjustable and ramjet-nozzle-adjustable solid ducted rocket可调冲压喷管变流量固冲发动机工作特性分析
4.Numerical Simulation of Flow and Structural Field in Air Inlet of the Solid Ducted Rocket;某型固冲发动机进气道流场和结构模拟仿真
5.Heat Transfer and Ablation of Insulation in Second Combustion Chamber with Different Configuration in SRR不同构型固冲发动机补燃室绝热层传热烧蚀
6.Flow Regulation Technique of Solid Ramjet:Hardware Design of Control System固冲发动机的流量调节技术——调控系统硬件设计
7.Flow Regulation Technique of Solid Ramjet:Design of Flow Regulation System固冲发动机的流量调节技术——流量调节系统设计
8.Numerical simulation of deposition for aluminum/magnesium-loaded fuel-rich propellant ducted rockets铝镁贫氧推进剂固冲发动机沉积数值模拟
9.Flow Regulation Technique of Solid RamjetSoftware Design of Control System固冲发动机的流量调节技术(3)调控系统软件设计
10.Numerical Simulation of Interior Flow Field in SFRJ固体燃料冲压发动机内流场数值模拟
11.Aerodynamic Design of Turbo for Solid Rocket Turbo Ramjet Engine;固体火箭涡轮冲压发动机涡轮气动设计
12.An Application Research of Integral Sol id Propellant Rocket Ramjets整体式固体火箭冲压发动机的应用性能探讨
13.The wavelet transformation analysis for vibration signal of ignation shock section of SRM固体发动机点火冲击段信号小波变换分析
14.The Solid Rocket-Ramjet Engine Thrust Calculation and Experimental Research of Connected-Pipe Testing;固体火箭冲压发动机推力计算与实验研究
15.The Research on Characteristic Performance of Combustion Flow Field in Secondary Combustion Chamber for Extended Range Solid Rocket Ramjet增程固体火箭冲压发动机补燃室燃烧特性研究
16.Numerical analysis on two types of afterburning chamber for solid fuel ramjet固体燃料冲压发动机两种补燃室构型数值分析
17.Numerical simulation of cold swirl flow field for solid fuel ramjet固体燃料冲压发动机旋流冷流流场数值模拟
18.Numerical Simulation of Combustion Characteristic in Combustion Chamber of SFRJ固体燃料冲压发动机燃烧室燃烧特性数值模拟
相关短句/例句
solid ramjet固冲发动机
1.The necessity of flow regulation system in solid ramjet is presented,and the scheme of gas-fired flux adjustment about generator is analyzed.阐述了固冲发动机燃气流量调节的必要性,对发生器燃气流量调节方案进行了评述。
3)solid rocket engine specific impulse固体发动机比冲
4)solid propellant ramjet固体冲压发动机
1.Study on the C/SiC composites for hot gas valve of solid propellant ramjet;固体冲压发动机燃气阀用C/SiC复合材料研究
5)solid rocket ramjet固体火箭冲压发动机
1.Quick-forecasting algorithm for performance of solid rocket ramjet;固体火箭冲压发动机性能快速预估算法
2.Some technological problems of solid rocket ramjet;固体火箭冲压发动机的若干技术问题
3.Experimental study on solid rocket ramjet with central air-inlet mode;中心进气式固体火箭冲压发动机试验研究
6)solid fuel ramjet固体燃料冲压发动机
1.Analysis on thrust stationarity and flight stability of solid fuel ramjet;固体燃料冲压发动机推力平稳性及飞行稳定性分析
2.Influence of vortex on performance of solid fuel ramjet;涡流对固体燃料冲压发动机性能影响分析
3.Structure design on torch igniter of solid fuel ramjet;固体燃料冲压发动机火炬式点火器设计
延伸阅读
航空发动机推重比(见航空发动机推力)航空发动机推重比(见航空发动机推力)thrust to weight ratio of aeroengine hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。