给出了采用牛顿法解超越方程，求解椭圆轨道及双曲线轨道开普勒方程中的偏近点角的源程序及例子；给出了解普适方程的函数及例子，是研究轨道理论中的重要函数，均基于matlab编程-Gives the solution of transcendental equation using Newton' s method, for solving elliptic orbit and the hyperbolic orbits Kepler equation Eccentric anomaly of t

利用牛顿面元法计算飞行器的升力、阻力、俯仰力矩等。-Calculation of the aircraft lift, drag, pitching moment, etc. Newton panel method.

运用面元法结合牛顿理论进行高超声速飞行器气动力工程估算(The aerodynamic engineering estimation of hypersonic vehicle is carried out by using the panel method and Newton theory)