An optimization method is used to obtain deflection Angle of controlsurface and the aerodynamic efficiency of airfoil is calculated.
用数值优化方法取得自适应翼型最优的舵面偏角，并计算其气动特性。
2
The result indicates that the derivative of the Angle between the fault and the bedding surface is the major control factor on the development of fracture pore space associated with fault.
结果表明，断层面与层面的夹角变化率是控制断层相关裂隙空间的主控因素。
3
Finally, the control stability was discussed and it was found out that trim Anglecontrol is a simple and effective method to make the submersible stable near the free surface.