He spun the steering-wheel so that we yawed from side to side. 他急速打着舵轮,把我们搞得摇来晃去的。
Analysis of the nonlinear aerostatic stability of a long-span suspension bridge under yawed wind 斜风作用下大跨度悬索桥非线性静风稳定分析
The results show that the thermal effect is able to produce a transition phenomenon in panel flutter under yawed flow, and that the corresponding flow yaw angle also changes. 结果显示:温升使偏航壁板颤振发生“跳跃”现象,对应的气流偏角发生变化;
The thermal flutter speeds of the panel under yawed flow are obtained by means of a simulated annealing optimization algorithm. 利用模拟退火算法,对不同温度场下的偏航壁板颤振速度进行计算。
On condition that the thermal flutter modes are kept unchanged, the thermal flutter speed of the panel under yawed flow decreases approximately linearly as the temperature rises; 当壁板热颤振模态不变时,偏航壁板颤振速度随温升呈下降趋势,两者呈线性关系;
Numerical Analysis of Yawed Perforation for Semi-armor Piercing Missile 半穿甲导弹性能的攻角效应数值分析
Buffeting Performance of Free-Standing Tower of Long-Span Cable-Stayed Bridge under Yawed Wind 斜风作用下大跨度斜拉桥裸塔抖振性能
Calculation for Three-Dimentional turbulent boundary layer on a yawed wing in compressible flow 绕侧滑翼三维可压缩湍流边界层计算
A simplified theoretical model has been established to describe the big yawed rod penetration into semi-infinite Rolled Homogeneous Armor ( RHA) targets at normal incidence, the effect of ballistic yaw is quantitatively described in the rate of penetration. 本文建立了大攻角的长杆体垂直侵彻半无限靶的简化物理模型,定量地分析了大攻角对垂直侵彻的影响。
This paper starts from the equations of motion in generalized curvilinear coordinates and the model of Head's two-dimensional entrainment theory, and derives a set of equations along surface curve on normal profile of a yawed wing for a compressible three-dimensional turbulent boundary layer. 本文从广义曲线坐标运动方程出发,以及根据Head的二维牵引理论(entrainmenttheory)模型导出沿侧滑翼法向翼剖面表面曲线的三维可压缩湍流边界层运动方程组。
Port and shipping enterprises focusing on logistic Wave-making Problem of Yawed Slender Body 港航企业聚集物流斜航细长体的兴波问题
Experimental Research of Tangential Drage Force Coefficient on a Yawed Cylinder in Fluid Field 斜置细长圆柱体在平面流场中切向拖曳力系数的试验研究
Characteristics of Helicopter Inlet with Front Output Shaft at Yawed Flight 带前输出轴直升机进气道侧滑特性