they are tinned t2 copper which assure the credible conductivity. there is thread in the inner hole of the afterbody of terminals, the insulation covering is hard, there is no break no rebound.
材质为t2紫铜料表面镀锡,保证了可靠的导电率,端头尾部内孔有螺纹线,绝缘套为硬质,不断裂,不回弹。
at the end of the analysis, it is suggested that exerting the elastic and damping restriction on the afterbody of the headstock was the best reasonable measurement.
通过各参数的比较分析,从而得出在系统动响应最小情况下,在主轴箱尾部施加弹性阻尼约束是最佳的改进措施。
the ejecting flying toy also comprises an afterbody form finalizing sheet which is fixed at the center of the rear part of the airfoil.
弹射飞行玩具还包括机尾定型片,机尾定型片固定在机翼后部中央。
in the study of civil aircraft afterbody test, it's adopted many kinds of afterbody shape models and the model with or without tail.
在民机后体试验技术研究中,采用多种不同后体形状和有无尾翼模型进行试验。
the drag increasing of the larger-upswept afterbody is due to the afterbody separation.
这种分离流动是导致大上翘角后体阻力增加的主要原因。
there are two shedding modes along the slender axes when the angle of attack is very high. the karman vortex shedding region is located in afterbody while the nose vortices region is near the apex.
在迎角很大时细长旋成体背部流场沿轴向通常有两个截然不同的区域,其中卡门涡脱落区域位于后体,而头涡区域靠近旋成体头部。
the key problem in the hull form design for a high speed round bilge displacement craft is to select an appropriate afterbody form.
高速圆舭排水艇的船型设计,关键是合理选择尾部线型。
experiment investigation shows: the main body zero drag can be reduced by faovurable interference of jet flow. then an optimuns afterbody configuration can be obtained.
实验研究表明,利用喷流的有益干扰,可使主弹体零阻显着下降,从而得到一种优化的后体外形。
a radio frequency electric wire is connected with the afterbody of the radio frequency cutter body and the anterior part of the radio frequency cutter body is provided with a bit.
其后端与刀柄连接、尾部连有射频电线、其前端带有刀头的射频刀体;
the method takes into account the effects of a variety of parameters concerning jet, nozzle and afterbody of a missile.
该方法及程序计及了喷流、喷管和火箭后体多种参数的影响,以及羽流诱导分离情况。
the friction drag coefficient increases with increasing afterbody fineness ratio and decreasing reynolds number.
后体摩擦阻力系数分别随后体的长细比的增加和雷诺数的减小而增加;
secondly, with the aid of flow visualization and seven-hole probe experiment on the fuselage, the afterbody wake flow was investigated clearly.
通过流动显示实验和七孔探针对尾流的移测实验,得到了单独机身后体尾迹流场随迎角变化的规律;