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1)  Integrated Spacecraft
一体化飞行器
1.
Research on Orbit Injection Strategy of Integrated Spacecraft;
一体化飞行器入轨策略研究
2)  integrated hypersonic vehicle
一体化高超声速飞行器
1.
Evaluation of aero-propulsive performance for integrated hypersonic vehicle;
一体化高超声速飞行器气动-推进性能评估
2.
Numerical simulation of integrated hypersonic vehicle's aerodynamic performance
一体化高超声速飞行器气动特性数值仿真
3.
Two-dimension coupled implicit NS equations and standard k-epsilon viscous models were used to simulate the angle of attack characteristics of integrated hypersonic vehicle with hark head configuration under three kinds of working conditions,i.
采用二维耦合隐式NS方程和标准kε-湍流模型,对采用Hark形头部的一体化高超声速飞行器在进气道关闭、发动机通流和发动机点火工况下的攻角特性进行了数值仿真研究。
3)  buoyancy-lifting vehicle
浮升一体化飞行器
4)  airframe/propulsion integrative hypersonic flight vehicle
机体/推进一体化高超声速飞行器
5)  Propulsion-airframe integration
飞行器/发动机一体化设计
6)  integrated optical flying head
一体化光学飞行头
1.
A new structure of integrated optical flying head (OFH), with both perfect mechanical and optical performance, is designed, which can achieve stable flying height and high signal/noise ratio optical signal during the read/write motion in near field recording (NFR) system.
设计了一种新型一体化光学飞行头,通过对光学飞行头滑块气浮力分布和飞行姿态(飞行高度、仰俯角和滚动角)的数值仿真分析,对滑块气体轴承表面(ABS)形貌参数进行了优化设计,确定了滑块的主要结构参数。
补充资料:复杂气象飞行(见飞行技术)


复杂气象飞行(见飞行技术)
instrument meteorological conditions flight

fuza qixiangfe主xing复杂气象飞行(instrument meteorologiealconditions flight)见飞行技术。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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