misalignment angle meaning in Chinese
失调角
Examples
- It is clearly that only two geometrical parameters i . e . maximal misalignment angle ( ) and distortion width ( s ) need to be determined experimentally
纤维弯曲模型（ fdm ）只有两个几何参数（最大纤维偏转角和变形区宽度）需要由实验确定。 - The system was simulated in four kinds of conditions . the effect of gyro drift and accelerometer bias on the evaluation error of misalignment angles and attitude error was analyzed
并且分四种情况对系统进行了仿真，分析了加速计零偏和陀螺漂移对失准角估计误差和姿态误差的影响。 - The in - plane equivalent elastic modulus and tensile strength of stitched composite laminates are studied , and it ' s found that the in - plane equivalent elastic modulus decreases with the increase of stitch density , stitch thread diameter , maximal misalignment angle and the distortion width , and the range is about 5 % . the tensile strength of stitched composite laminate increases with the increase of stitch step and decreases with the stitch space . the
研究结果表明：随着缝纫密度、缝纫线直径、最大纤维偏转角和缝纫变形区宽度的增加，缝纫复合材料层合板面内等效模量逐渐降低，最大降幅一般在5 %左右；缝纫复合材料层合板的拉伸强度随缝纫针距的增加而增大，随缝纫行距的增加而降低，因此缝纫密度对拉伸强度的影响程度要看具体的缝纫针距和行距。 - The distortion of in - plane fibers is considered to be the main reason for the effect of stitching on the in - plane mechanical properties , and the fiber distortion region , the resin - rich pocket and the through - thickness reinforcement section are taken into account . the fiber misalignment angle and the inhomogeneous fiber volume fraction caused by stitching have been determined within the lamina . the elastic constants of a lamina are calculated using a micromechanical model , then the constitutive equations of the stitched composite laminates can be composed
从缝纫孔附近纤维变形的细观结构出发，建立的纤维弯曲模型，以面内纤维的弯曲变形作为缝纫影响层合板面内力学性能的主要原因，同时考虑了纤维变形区、厚度增强区以及树脂富集区的影响，得到单向板内任意一点处的纤维偏转角和纤维体积百分含量。