Matching Research of Terminal Maneuver And Guidance System for Subsonic Anti-ship Missile
亚音速反舰导弹末端机动与导引头匹配
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本文以非定常涡环速度势函数为基本解,应用时间历程方法,计算非共面机一尾翼组合体的非定常气动力性能。
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进口速度分布对二元亚音速扩压器的流动和性能的影响
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Study of subsonic flows has significant physical as well as practical importance.
所以研究亚音速流对生产、生活和国防等方面有着广泛而重要的现实意义。
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A Numerical Study of Steady Subsonic Lift Characteristics on a Wing-Body Combination
翼身组合体定常亚音速升力特性的数值研究
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Design of attitude determination and control system of high subsonic UAV flight
高亚音速无人机姿态确定与控制系统设计
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Analysis of Character and Calculating Method Concerning Subsonic Air Ejector
亚音速气体喷射器的性能分析及其计算方法
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Two-dimensional subsonic diffuser flow with uniform shear velocity profile at inlet
进口为均匀剪切流的二元亚音扩压器
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Numerical simulation on the flow field of COIL mixing nozzle with injection from subsonic region
COIL亚声速段横向喷流混合流场数值分析
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Therefore, it is necessary to improve the current navigation means of the subsonic vehicle.
因此,有必要对亚音速飞行器的导航方案进行改进。
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Numerical Simulation of Sound Wave Propagation in Subsonic and Supersonic Nozzle
亚、超音喷管中声传播的数值模拟
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Least squares finite element analysis of steady high subsonic plane potential flows
平面亚声速定常势流的最小二乘有限元法
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Optimization of geometrical parameters for a subsonic axial flow compressor stage
高效亚音轴流压气机级几何参数最佳选择
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首次利用一台亚音速小型连续波化学氧碘激光器做探测光源,用放大法直接测量超音速化学氧碘激光器的小信号增益系数,测得了小信号增益系数随时间和气流方向的变化。
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