Based on the modern digital technology of fluid mechanics, the eight-parameter optimum axisymmetric bodies for minimum drag are obtained by using COMPLEX method.
本文利用现代流体力学计算技术，采用复合形法(COMPLEX)，对八维参量的回转体最小阻力外形进行优化设计。
Based on the modern digital technology of fluid mechanics, the optimization design method of the shape of axisymmetric body tail for minimum drag is presented by using COMPLEX method.
利用现代流体力学计算技术，采用复合形优化策略，提出了一种适用于回转体尾部外形的优化设计方法。
The boundary layer separation points, minimum pressure positions on the surface and the drag coefficients are in agreement with numerical solutions and experimental results.
边界层分离点、物面最小压力点及阻力系数的计算结果与一些数值解及实验结果是符合的。
Not only are they easy to use - just click and drag - but you can also see how your selection fits between the minimum and maximum of an available range.
你不但很容易的使用，只需点击和拖动，而且你可以了解到你的选择在最小值和最大值的有效范围内是否合适。
Not only are they easy to use — just click and drag — but you can also see how your selection fits between the minimum and maximum of an available range.
不仅仅因为它们很容易使用——只要点点拖拖就行了——而且你可以看到你的选择在最小值和最大值的范围里处在一个什么位置。
The spanwise distribution of lift for minimum induced drag of wings having a given lift and a given bending moment.
分布展升降机最低诱导阻力的机翼有鉴于一部升降机和弯曲某一特定时刻。
The spanwise distribution of lift for minimum induced drag of wings having a given lift and a given bending moment.
分布展升降机最低诱导阻力的机翼有鉴于一部升降机和弯曲某一特定时刻。
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