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1)  stall margin
失速余度
1.
Under such conditions, a considerable increase in stall margin improvement and stall flow m.
实验证明,当第2级与第1级转子的转速比为15,轴向间隙距离为030~025倍第1级转子叶片弦长时,第1级转子的失速特性得到改善,风机的失速余度得到改进,风机的失速流量及压力增加。
2.
Further, the air-separator improves the low flow rate range performance and increase stall margin of the axial flow fan.
例如:降低了风机的最高效率尚2%-4%),改进失速余度的范围小,大约只有20%的流量失速金度的改进。
2)  leaving loss
余速损失
1.
Analysis shows that controlled-vortex aerodynamics can make reaction more uniform,but it is limited to some extent because of larger leaving loss when it is used to last stage of large steam turbine.
分析结果表明:尽管可控涡流型与等轮周功分布方案相比能够使涡轮级的反动度沿叶展的分布趋于均匀,但在应用于末级长叶片的设计时由于积分余速损失的增加而受到了一定的限制。
3)  stall speed
失速速度
4)  terminal velocity
剩余速度
1.
The limit velocity formula adapted for battle damage simulation was chosen, and the method of calculating the terminal velocity was proposed.
选择了适用于战斗损伤仿真的极限速度公式,并提出了剩余速度的求解方法。
5)  residual velocity
残余速度
1.
The principles implied in the process of EFP(explosively formed projectile) impacting the plate covered explosive and the ceramic composite armor have provided the evidence for calculating the residual velocity of EFP(explosive formed projectile) impacting a new integrated armor,and a calculation model has been induced.
根据平板装药和陶瓷复合装甲与爆炸成型弹丸(EFP)相互作用的原理,提出了新型集成装甲与EFP作用的计算模型;据此模型进行了EFP残余速度计算,证明了在相同面密度的新型集成装甲和陶瓷复合装甲防护下,EFP的残余速度有明显差异;根据该计算模型可进行集成装甲的优化和EFP的反装甲目标设计。
6)  residual velocity
剩余速度
1.
Then we can formulate some empirical formulas about ballistics limit and residual velocity,which are based on a large number of computation data.
运用有限元模型仿真弹丸侵彻靶板的全过程,通过计算得到大量数据,然后在弹丸穿透平板时极限速度和剩余速度经验公式的基础上,来探讨弹丸穿透单筋板时的极限速度和剩余速度的经验公式。
2.
This paper analyzes the impact damage forecast for the airplane structure from the following four aspects: ballistic limit, residual velocity, residual mass, forecast of damage size in structure penetrated or not penetrated, simultaneously discusses the development tendency of damage forecast and finally points out the main direction and means in the future damage forecast research.
从弹道极限、剩余速度、剩余质量、未击穿及击穿条件下损伤尺寸预测等方面对飞机结构撞击损伤的预测进行了分析,并对损伤预测的发展趋势进行论述,提出今后损伤预测研究的主要方向和手段。
3.
According to the ballistic experimental results and the theoretical analysis,the linear relation between ballistic limit vBL and area density ρad was confirmed;the versatile experiment relation between vr and ρad was found based on that relative parameters in the experiential relation of residual velocity were expressed by the function of ρad.
根据弹道试验结果和理论分析进一步确定了弹道极限速度vBL与面密度ρad的线性关系;又将剩余速度vr的经验关系式中的相关参数表示为ρad的函数,得到了vr与aρd的经验关系式。
补充资料:余度
1.犹大度。
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