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- subsonic effuser 亚音速喷管
- I have no idea what subsonic speed is. 我实在不明白什么是亚声速。
- Supersonic aircraft will not make all subsonic aircraft obsolete. 超音速飞机不会使所有亚音速飞机都淘汰。
- Nonlinear Aeroelastic Analysis of Complete Aircraft in Subsonic Flow. 亚音速流中全飞机的非线性气动弹性力学分析。
- This airplane can go out to high subsonic speeds very easily without using afterburner. 这架飞机能够很轻松地在不打开加力的状态下飞到高亚音速。
- This paper presents a ALGOL program for Calculating The lift distribution on wings with control surface in steady and unsteady subsonic flow. 本文提供了计算亚音速偏转操纵面机翼的定常和非定常升力分布的算法语言程序。
- When the Switchblade returns to subsonic speeds, the wing will rotate back to perpendicular. 当这种“转向翼飞机”恢复亚音速飞行时，机翼就转回垂于直机身的角度。
- Under subsonic blowing condition,low lance position, high top and bottom blowing rate can decrease the mixing time. 在亚音速喷吹条件下降低枪位、增加顶底吹气体流量可降低均混时间;
- The empty weight to total weight ratio of subsonic maneuverable missile was given experimentally. 利用经验的预测方法对亚声速飞航导弹的空重比进行预测。
- What he envisions is an ellipsoid with tiny wings that he says can take off vertically and move like an alien spaceship, albeit at subsonic speed. 他所设想是极有椭翅膀起飞;他说像一个垂直和举措外国人飞船;不过亚音速速度.
- A prediction method of lift to drag ratio of subsonic maneuverable missile was given. 利用客机/货机升阻特性的预测方法对亚声速飞航导弹的升阻特性进行预测，并给出了合理的修正。
- The drag of aftbody keeps constant in low subsonic flow, but increases in transonic flow due to the shock wave. 在低亚音速范围，后 体阻力基本不变化，随着马赫数增加至跨音速，出现激波阻力。
- A grid generation platform is provided in subsonic,transonic and supersonic CFD software platform. 在亚跨超CFD软件平台中,提供了一个网格生成平台。
- Subsonic intake pipe is the key test device for a pre-research project simulation test. 亚音速进气管是用于某课题仿真模拟试验设备的关键部件,设计技术要求高,制造难度大。
- Neutrino is the most unstable elementary state particle in numerous subsonic atom particles. 摘要在众多的亚原子粒子家族中，中微子是最令人捉摸不定的基本态粒子。
- Under subsonic blowing condition, low lance position, high top and bottom blowing rate can decrease the mixing time. 在亚音速喷吹条件下降低枪位、增加顶底吹气体流量可降低均混时间；
- For subsonic free stream, performance losses almost linearly increase with increasing Mach number. 低马赫数亚声速外流时，性能损失随外流马赫数的增加成近似线性增加；
- Jeffrey M. Stricker. Comparison Methodology for Long Range Subsonic Cruise Missile Propulsion System. 刘桐林等编.;世界导弹大全
- XFOIL is an interactive program for the design and analysis of subsonic isolated airfoils. (译)：XFOIL是一个互动计划的设计与分析亚音速孤立翼型。
- Unlike in subsonic and transonic speed regimes, the interference resulting from the finite size of the test region is seldom present. 不像在亚、跨音速区域，这里因试验段尺寸有限造成的干扰是难得存在的。
