W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel singularity distributions, based on the USSAERO program by Woodward. W12SC3 combines source and vortex panel singulari

基于主动形状模型的人脸识别特征点征点标定，-Face recognition based on active shape models feature point calibration feature points,

comsol仿真建立一个空间变化的电介质分布， 如可能与超材料被工程。这里，凸透镜形状被定义 通过矩形域的已知变形。电介质分布定义 在未变形的，原始的矩形域和被映射到变形 塑造镜头。虽然这里所限定的透镜的形状是凸的，该介电 分布使入射光束发散。-comsol demonstrates how to set up a spatially varying dielectric distribution, such as might be engineered with a m