1) Waverider
乘波机
1.
Cone-derived Waverider Configuration Design and Performance Research;
锥导乘波机的构型设计与性能研究
2.
Waverider configurations were generated by Osculating-Cone in that the inlet curve were given.
以圆锥绕流流场为基础,给定进气道进口曲线运用吻切锥理论生成了不同的乘波机构型,并对乘波机进行了包括升力、粘性阻力、波阻、升阻比、乘波机长度、体积、容积效率等各主要性能指标在内的性能计算,初步确定出了吻切锥乘波机构型和性能的变化规律及其决定性定型参数。
3.
The computation of generating waverider configurations using the theories of conical flow field,OC(Osculating Cone) and OA (Osculating Axisymmetric) flows are presented.
计算了由锥型流理论、吻切锥理论及吻切轴对称理论生成的不同乘波机外形。
2) waverider
乘波
1.
Integrated design and performance research of waverider forebody/inlet
两种乘波前体/进气道一体化设计与性能研究
2.
Based on the calculation, two waverider configurations with inlet are designed.
以此为基础,分别生成了具有三道封闭激波的乘波前体模型和作为对比模型的一道封闭激波两道平面激波的乘波前体模型以及乘波前体/进气道模型。
3.
A new design method of the hypersonic forebody is present based on the waverider and liftbody concept.
综合升力体和乘波构型的气动性能优势,发展了一种高超声速飞行器前体气动构型的设计方法。
3) take occasion to
乘机
4) Waverider configuration
乘波构型
1.
Waverider configuration is an important approach in hypersonic high L/D vehicle s design.
乘波构型是高超声速飞行器高升阻比气动布局设计的参考外形之一,设计中需要综合考虑升阻比、容积率和容积等要求。
5) waveriders
乘波器
1.
Parametric waveriders design method study;
乘波器的参数化设计研究
6) waverider
乘波体
1.
Spline-based waverider configuration optimization method;
基于样条曲线的乘波体外形优化方法
2.
Altitude and Design Length Effects of Optimized Waverider Derived from Cone Flow;
飞行高度及设计长度对锥形流乘波体优化的影响
3.
Numerical Investigation of the Pre-Compression of Leadedge-Composited Waverider;
组合前缘乘波体预压缩性能计算研究
补充资料：一乘之机
【一乘之机】
（术语）可闻一乘法之根机者。
（术语）可闻一乘法之根机者。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条