1.
It is inadvisable, therefore, to rely on the stability of high value resistors for the performance of a system.
因此，让系统的性能依赖于高阻值电阻的稳定性的做法是不可取的。
2.
Investigation and Design of the Testing Device Based on LPC938 for the High Resistance Gas Sensor;
基于LPC938的高阻值气敏传感器测量电路的研究和设计
3.
Investigation and Design of the Testing Device Based on ARM for the High Resistance Gas Sensor;
基于ARM的高阻值气敏传感器测量装置的研究与设计
4.
Numerical Calculation of Aerodynamic Drag of Train in Tunnel
隧道中高速列车空气阻力的数值计算
5.
Numerical Calculation of Wavemaking Resistance for High-Speed Displacement Trimarans;
高速排水型三体船兴波阻力数值计算
6.
Numerical computation of aerodynamic drag coefficient for high temperature particles
高温固体颗粒气动阻力系数数值计算
7.
Design of high g piezoresistive micro-accelerometer
高g值压阻式微加速度计设计(英文)
8.
Preparation of Scale Inhibitors Adapting to High Hardness, High Alkalinity and High pH;
耐高硬度、高碱度、高pH值阻垢分散剂的研制
9.
G Damp- The friction for Goal. Higher values dampen the effect of the goal on the soft body.
G 阻尼-作为目标的磨擦力。较高的阻尼数值使目标对软体的效果。
10.
G Damp - The friction for Goal. Higher values dampen the effect of the goal on the soft body.
阻尼-作为目标的磨擦力。较高的阻尼数值使目标对软体的效果。
11.
Study of the lead impedance and the threshold in long-term performance and comparing the a high-impedance tined endocardial pacemaker lead
电极阻抗与起搏阈值的长期临床研究及高阻抗电极的相关比较
12.
The heavy damping makes it impractical to read gravity directly from the displacement of the beam.
高阻尼不能使其直接从横臂的位移读出重力值。
13.
Numerical Simulation on the Aerodynamic Drag of High-Speed Train of Evacuated Tube Transportation System;
真空管道运输高速列车空气阻力数值仿真
14.
Method in reducing the shared grounding resistance value in the tall building;
高层建筑中降低共用接地电阻值的方法
15.
The Meaning and Calibration Methods with High-value Standard Resistor Voltage Coefficient
高值标准电阻器电压系数的意义及其校准方法
16.
EXPERIMENTAL RESEARCH AND NUMERICAL SIMULATION OF SUPERCAVITY DRAG REDUCTION OF A HIGH SPEED PROJECTILE
高速射弹超空泡减阻试验研究与数值模拟分析
17.
Numerical calculation of wave-making resistance of a high-speed trimaran in deep or shallow water
深浅水中高速三体船兴波阻力数值计算
18.
Numerical Simulation Investigation on Plasma Injection for Drag Reduction of Hypersonic Vehicle
高速飞行器等离子体减阻的数值模拟研究