1.
On Conformal Transformation Constituted by the Function of Wing’s Section, It’s Inverse Function and Their Application;
机翼剖面函数及其反函数构成的保形变换与应用
2.
Shape Parameter Optimization for Wing and Wingtip Based on RBF
基于径向基函数的机翼和翼梢小翼外形优化
3.
An improved empirical orthogonal functions(EOF) on the forecast of ocean sound speed profile
改进型经验正交函数海洋声速剖面预报方法
4.
APPLICATION OF THE MULTIPLIER PENALTY FUNCTION METHOD TO THE OPTIMUM DESIGN OF WING CONFIGURATIONS OF AEROSPACE VEHICLE
乘子罚函数法在航天飞机机翼外形优化设计中的应用
5.
Ac- cording to these methods, we have calculated two aerofoil drag coefficients under different Reynolds numbers and Mach numbers.
按照上述方法计算了在不同雷诺数和不同马赫数下两个翼型剖面的摩阻系数。
6.
Numerical Simulation of Using Blade Tip Winglet in Plane Compressor Cascade
压气机平面叶栅加装叶尖小翼的数值研究
7.
total wing area
机翼总面积(含机身部分)
8.
log log profile
对数的对数形纵剖面
9.
CAD of reappearance function flat connecting rod machine;
再现函数平面连杆机构的计算机辅助设计
10.
An Empirical Orthogonal Function (EOF) Analysis of Ionospheric Electron Density Profiles Based on the Observation of Incoherent Scatter Radars;
非相干散射雷达的电离层电子浓度剖面观测数据的经验正交函数分析
11.
The aerofoils are held in place by upright vanes, or endplates.
剖面小翼被垂直叶片或终板固定在有效位置。
12.
Discussion about the Methods of Using Constructor Function to Construct Data Members of Class;
C++构造函数构造类成员的方法剖析
13.
The author modifies spanwise shape and makes the analog function of the aerofoil curve by use of the computer.
利用计算机来辅助叶片叶展形状的修正和构造翼型曲线的模拟函数。
14.
Analysis of Output Function of 4 bar Linkages Using Wavelet Transform
平面四杆机构函数输出的小波变换分析
15.
The Research on the Simple Method for Function Synthesis of Planar Six-Bar Mechanism;
平面六杆机构简化函数综合方法的研究
16.
Research on the Theory and Approach of Function Synthesis for Planar Six-Bar Dwell Mechanism;
平面六杆机构间歇函数综合理论与方法研究
17.
Research of Functional Synthesis and Optimal Design of Planar Linkage Mechanisms;
平面连杆机构函数综合及其优化设计的研究
18.
A New Method to Select the Precision Points for Function Synthesis of Spherical Four-bar Mechanisms
球面四杆机构函数综合精确点选择新方法