高超声速推进系统,hypersonic propulsion system
1)hypersonic propulsion system高超声速推进系统
2)hypersonic propulsion高超声速推进
英文短句/例句
1.REASONING ON DEVELOPMENT OF AIR-BREATHING HYPERSONIC PROPULSION TECHNOLOGY关于吸气式高超声速推进技术研究的思考
2.Hypersonic propulsion test facility is important for the scramjet ground tests.高超声速推进风洞是进行超燃冲压发动机模型地面模拟的重要试验设备。
3.Numerically Simulate Aero-Force&Heat of Hypersonic Vehicles and Region Marching Method for Supersonic Flow Simulation;高超声速飞行器气动力气动热数值模拟和超声速流动的区域推进求解
4.Study on the reliability of a single-sweep space marching algorithm for hypersonic flows单次扫描空间推进算法在高超声速流动中的适用性研究
5.Influence of head configuration on aerodynamic-propulsive performance of hypersonic vehicles机身头部构型对高超声速飞行器气动-推进性能的影响
6.Research on Overall Plan for Hypersonic Boostflight Experiment高超声速助推飞行试验技术方案研究
7.Iron oxide may be utilized in achieving propellants of ultrahigh burn rate.氧化铁可用以制出超高燃速的推进剂。
8.Effect of aspect ratio on 2-D hypersonic inlet performance宽高比对二元高超声速进气道性能的影响
9.Numerical Simulation and Experimental Research of Hypersonic Inlet;高超声速进气道流场数值模拟与试验研究
10.Design Method, Numerical Simulation and Experimental Research of Hypersonic Inlet;高超声速进气道的设计、计算与实验研究
11.Investigation of a Two-dimensional Mixed-compression Hypersonic Inlet一种高超声速二元混压式进气道的研究
12.Study of Optimization Method for Two-Dimensional Hypersonic Inlet二维高超声速进气道优化设计方法研究
13.Design and Experimental Verification of Hypersonic Inlet with Rectangular Section矩形截面高超声速进气道气动设计及实验验证
14.Analysis of drags trait in three-dimensional sidewall hypersonic inlet三维侧压式高超声速进气道阻力特性分析
15.Survey on Application of MDO in Design of Hypersonic Waverider-derived Vehicles高超声速乘波飞行器多学科设计优化研究进展
16.Impact of suction position on starting of hypersonic inlet抽吸位置对高超声速进气道起动性能的影响
17.On the New Research between Ultrasonic Bone-age and Sound of Speed in Ultrasound Device;超声骨龄与超声速值(SOS)研究的新进展
18.Aerodynamic Flutter and Limited Cycle of a 2-D Wing in the Hypersonic/Supersonic Flow Field超声速/高超声速流中二元机翼的颤振与极限环
相关短句/例句
hypersonic propulsion高超声速推进
3)super high burning rate propellant超高燃速推进剂
4)airframe/propulsion integrative hypersonic flight vehicle机体/推进一体化高超声速飞行器
5)hypersonic inlet高超声速进气道
1.Experimental investigation on the starting characteristics of ahypersonic inlet with moving entrance door;开启式高超声速进气道启动性能试验
2.Effect of suctions on maximum backpressure ratios ofhypersonic inlets;抽吸对高超声速进气道抗反压能力的影响
3.Numerical simulations ofhypersonic inlet flowfields in the binary mixed compression;二元混压式高超声速进气道流场数值模拟
6)hypersonic inlets高超声速进气道
1.Characteristic analysis of unstart/restart ofhypersonic inlets caused by variations of attack angle of freestream;攻角引起的高超声速进气道不起动/再起动特性分析
2.Effects of the forebody boundary layer state on flow structure and performance ofhypersonic inlets;前体边界层状态对高超声速进气道流动结构及性能的影响
3.Effects of wall temperature on unstart/restart characteristics ofhypersonic inlets壁面温度对高超声速进气道不起动/再起动特性的影响
延伸阅读
高超好得超过一般水平：见解～丨技术～。
