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longitudinal相关的网络例句

查询词典 longitudinal

与 longitudinal 相关的网络例句 [注:此内容来源于网络,仅供参考]

Marginal regression model and its associated generalized estimating equation are becoming increasingly being used in longitudinal studies.

边际回归模型和与此有关的广义估计方程在纵向数据分析中得到了广泛的应用。

Drift Angle, Speed, Peak Drift Angle, Speed at Peak Drift, Current Sector, Sector Score, Total Score, Peak Longitudinal Acceleration, Average Speed

漂移角,速度,最大漂移角,最大漂移角时的速度,当前路段,路段分数,总分,最大纵向加速度,平均速度。

2 X User Defined Acceleration Range, 0-XXX-0, Maximum Velocity, Average Velocity, Peak Longitudinal Acceleration, 2 x User Defined Deceleration Range, Time to and Speed at (100m, 200m, 400mm, 1km, 1/8mile, 1/4 mile, 1/2mile, 1mile), BHP, Power Losses. Minimum apex speed.

0-60, 0-100, 2 x用户自定义的加速范围,0-XXX-0,最大速度,平均速度,最大纵向加速度,2 x用户自定义减速度范围,以时间为基准及到100m, 200m, 400mm, 1km, 1/8mile, 1/4 mile, 1/2mile, 1mile时的速度,BHP,功率损失,最小峰值速度。

The invention concerns a burner comprising a premix designed to produce a flammable air-fuel mixture, said burner including a vortex generator, wherein are provided two complementary burner shells forming a passage body, having each a first half-cone burner shell section (1) and delimiting together a turbulence chamber, widening in the axis in the form of a cone, as well as tangential air intake slots in the axial longitudinal direction of the cone.

描述了一种用于产生可点燃的燃料-空气混合物的预混燃烧器,该预混燃烧器具有涡流发生器,该涡流发生器设置了至少两个对穿流本体进行补充的燃烧器壳,所述燃烧器壳分别具有构造为分锥形状的第一燃烧器壳区段(1)并且共同限定着在轴向上按锥形方式扩展的涡流室并且限制着所述沿轴向的锥体纵向伸展方向相互相切的进气缝隙。

The transverse dynamic stiffness curve of a ship front shaft bracket ,and the transverse and longitudinal dynamic stiffness cruves of a back shaft bracket are obtained by means of experiment measurements.

采用实验方法对某舰尾轴架进行动刚度测量,得到了前尾轴架的横向动刚度曲线,后尾轴架的横向和纵向动刚度曲线;分析尾轴架的动刚度曲线,可得到尾轴架结构的固有频率。

The transverse dynamic stiffness curve of a ship front shaft bracket,and the transverse and longitudinal dynamic stiffness cruves of a back shaft bracket are obtained by means of experiment measurements.Analyses of these curves make the natural frequencies of the shaft brackets available.

采用实验方法对某舰尾轴架进行动刚度测量,得到了前尾轴架的横向动刚度曲线,后尾轴架的横向和纵向动刚度曲线;分析尾轴架的动刚度曲线,可得到尾轴架结构的固有频率。

Separate air chambers adjust the longitudinal and transverse contours of the backrest independently in the lumbar and side regions.

互相独立的气室可分别调节座椅靠背与腰部和侧部接触部分的横向及纵向凸凹轮廓。

Separate air chambers adjust the longitudinal and transverse contours of the backrest independently in the lumbar and side region s.

互相独立的气室可分别调节座椅靠背与腰部和侧部接触部分的横向及纵向凸凹轮廓。

The instructive conclusion was: 1 under the vertical loading, the shear-lag effect was produced badly, more severer under concentrated loading than under uniform loading .2 the longitudinal bending deformation of the beam flange was true of the imitating plane assumption of deformation . 3 the width length ratio was confirmed as the first factor working on the shear-lag effect among all the geometric parameters;4 the shear-lag coefficient of simple-supported box-girder was severer than the continuous box-girder, the shear-lag effect in the inner supported section of continuous beam was much more severer, we need paying more attention for it in designing. 5 the non-liner characteristics of material deformation have littlie influence on shear-lag effect in BGCW. 6 the experiential calculating formulation and calculating diagram for the effective flange width was raised with the only factor of the width-span ratio., but the primary location of axis of bending moments should not be changed while calculating the inertial moment .

研究认为:1室内模型试验和空间有限元分析结果均表明波形钢腹板组合箱梁在竖向荷载作用下,翼板出现了典型的纵向应力剪滞效应。2在竖向荷载作用下,截面高度上各点纵向正应变分布认为可符合"拟平截面假定",以此作为波形钢腹板组合箱梁抗弯计算的基本假定。3箱梁宽跨比是影响波形钢腹板组合箱梁翼板剪滞效应的主要因素。4连续波形钢腹板组合箱梁的翼板剪滞系数大于简支梁,且连续箱梁内支点截面翼板剪滞效应相当严重,对此需十分重视。5当混凝土翼板受力由弹性阶段进入弹塑性阶段时,材料的非线性特性对翼板的剪滞效应影响甚微。6提出了根据组合箱梁的宽跨比参数来计算翼板有效宽度比的经验公式和计算图表,但箱梁截面抗弯惯性矩的计算不应改变原先的截面中和轴位置。

The study shows that the longitudinal component of the pressure force is mainly balanced by the vertical eddy frictional term and the lateral component of the pressure force is mainly balanced by the Coriolis force.

研究表明:在磨刀门河口动力平衡中,纵向的主要平衡项为压力项和垂向涡动摩擦项,侧向的主要平衡项为侧向正压力项和科氏力项。

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