Three-dimensional numerical simulation of the combined process of stretch spinning and drawing for the overlength circular cone pipe without mandrel;
超长圆锥管无芯模旋拉过程的三维数值模拟
The cone super subdifferential stability of multiobjective programming with a perturbed order;
扰动多目标规划的锥超次微分稳定性
The main machine uses frequency conversions for speed requlation, and super-taper twin-screwextruder with temperature-regulating in the screw core.
主机采用变频调速，螺杆芯部调温得超锥形双螺杆挤出机。
Optical Field Evolution and Transmission Characteristics of Ultra-short Pulse in the Tapered Region of a Single-mode Tapered Fiber
单模锥形光纤锥区光场及超短脉冲的传输特性
Superplastic Forming of Allotype Cone Made of TA15 Titanium Alloy
TA15钛合金异型锥筒形件超塑成形
Research and Design of Ultra-Wideband Discone Antenna
超宽带盘锥天线的HFSS仿真研究与设计
Attack of angle effect for supersonic blunt cone transition flow
超声速小攻角下的圆锥转捩攻角效应
An example for hypersonic blunted cone flow in ballistic range is illustrated.
示例给出了弹道靶中高超声速钝锥流动的应用
NUMERICAL CALCULATION WITH FINITE DIFFERENCE METHOD FOR SUPERSONIC FLOW OVER BENT CONES
绕弯曲头锥超音速流动差分法数值计算
NUMERICAL SIMULATION OF SUPERSONIC SEPARATED FLOW OVER BLUNT CONES AT HIGH ANGLES OF ATTACK
钝锥大攻角超声速分离流场的数值模拟
Ultrastructure Study of Keratoconus and the Evidence of Apoptotic Cell Death;
圆锥角膜的超微结构观察及细胞凋亡的表达
Integrative Hypersonic Waverider Design Based on Osculating Cones Method;
基于密切锥方法的高超声速乘波机一体化设计
The Numerical Study of Evolution of Perturbations in the Supersonic Blunted Cone Boundary Layer Flow;
高超音速钝锥边界层中扰动演化的数值研究
Numerical Simulation on Hypersonic Flowfield of Cone-derived Waverider
高超声速锥导乘波体流场的数值模拟研究
A Coning-Error Compensation Algorithm for Supersonic SINS
超音速捷联惯导系统圆锥误差补偿算法研究
Application research of the inertial cone crusher's crushing superhard materials
惯性圆锥破碎机破碎超硬物料的应用研究
CNC Machining Technology and Clamp Design for a Long Spreader
超长分流锥的数控加工工艺与夹具设计
Numerical Simulation on Off-Design Performance of Hypersonic Cone-Derived Waverider
高超声速锥导乘波体非设计点性能研究
The accuracy of ultrasound on locating conus medullaris in fetuses
超声定位胎儿脊髓圆锥末端位置方法的准确性
Stability Characteristics of the Boundary Layer of an Axisymmetric Blunt Nosed Cone in the Supersonic and Hypersonic Flow
超声速高超声速球锥绕流的边界层稳定性特点初探