数值算例表明本文方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Numerical results show that present method is an effective one for solving the flow around wing body configuration with control surface deflection.
数值算例表明该方法是求解带操纵面偏转的翼身组合体绕流的有效方法。
Numerical results show that the present method is effective one for solving the flow around a wing body combination with control surface deflection.
为了验证方法和程序的正确性，论文中对M6机翼和F4翼身组合体的流场进行了数值模拟，并与试验结果进行了对比。
The viscous flow around M6 wing and F4 wing-body configuration are simulated and compared with the results of wind tunnel experiment.
本文研究涡流发生器控制超临界翼型和翼身组合体机翼的附面层分离问题。
The paper investigates the problem on vortex generator control boundary layer's separation of supercritical airfoil and wing for body configuration wing.
本文指出，只需少量修改，就可将单独翼分析程序扩展为可同时适用于翼-身组合体。
It is shown that only a few changes needed to expand the computer program for wing alone to cover wing-body combinations.
从全速位方程出发研究了机翼和翼身融合体跨音速绕流的有限元算法。
The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
讨论了一种区别于机翼与圆柱机身的传统民机外形——翼身融合体(BWB)外形。
A new type of transport, which is different from the conventional cylinder fuselage plus wing but a blended wing body (BWB), is discussed.
进行机翼，翼身组合体的气动优化设计。
本文开展了弧形翼及翼-身组合体在超高速下的空气动力学特性研究。
The research on aerodynamic characteristics of wrap-around fin and wing-body combination was carried out at super high speeds in this dissertation.
本文介绍了翼身融合体无人机的胶接技术。
In this paper, the bonding technique for the blended wing body mini UAV is presented.
对翼身组合体等弦长大展弦比超临界机翼，除翼梢处流动三维效应强外，机翼其余部分包括接近翼根附近，均具有近似二维流动的特征。
Most part of the supercritical wing with equal chord and high aspect ratio is provided with 2-D flow characteristics approximately except wing tip.
对翼身组合体等弦长大展弦比超临界机翼，除翼梢处流动三维效应强外，机翼其余部分包括接近翼根附近，均具有近似二维流动的特征。
Most part of the supercritical wing with equal chord and high aspect ratio is provided with 2-D flow characteristics approximately except wing tip.
应用推荐