例句與造句

1. It is clearly that only two geometrical parameters i . e . maximal misalignment angle ( ) and distortion width ( s ) need to be determined experimentally
   纖維彎曲模型（ fdm ）只有兩個幾何參數(shù)（最大纖維偏轉(zhuǎn)角和變形區(qū)寬度）需要由實(shí)驗(yàn)確定。
2. 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
   并且分四種情況對系統(tǒng)進(jìn)行了仿真，分析了加速計零偏和陀螺漂移對失準(zhǔn)角估計誤差和姿態(tài)誤差的影響。
3. 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
   研究結(jié)果表明：隨著縫紉密度、縫紉線直徑、最大纖維偏轉(zhuǎn)角和縫紉變形區(qū)寬度的增加，縫紉復(fù)合材料層合板面內(nèi)等效模量逐漸降低，最大降幅一般在5 %左右；縫紉復(fù)合材料層合板的拉伸強(qiáng)度隨縫紉針距的增加而增大，隨縫紉行距的增加而降低，因此縫紉密度對拉伸強(qiáng)度的影響程度要看具體的縫紉針距和行距。
4. 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
   從縫紉孔附近纖維變形的細(xì)觀結(jié)構(gòu)出發(fā)，建立的纖維彎曲模型，以面內(nèi)纖維的彎曲變形作為縫紉影響層合板面內(nèi)力學(xué)性能的主要原因，同時考慮了纖維變形區(qū)、厚度增強(qiáng)區(qū)以及樹脂富集區(qū)的影響，得到單向板內(nèi)任意一點(diǎn)處的纖維偏轉(zhuǎn)角和纖維體積百分含量。
5. It's difficult to find misalignment angle in a sentence. 用misalignment angle造句挺難的