16.61 Aerospace Dynamics Spring 2003 Lagrange's equations Joseph-Louis lagrange 1736-1813 http://www-groups.dcs.st-and.ac.uk/-history/mathematicians/lagranGe.html Born in Italy. later lived in berlin and paris Originally studied to be a lawyer

化学热力学的研究对象和局限性 研究化学变化的方向、能达到的最大限度以及 外界条件对平衡的影响。化学热力学只能预测反应 的可能性,但无法预料反应能否发生?反应的速率 如何?反应的机理如何?

（1)解释术语构造地质学中的几何学、运动学和动力学。可以举例或绘图说明。 原生构造:Non- -Tectonic Structures 1)如何区分原生构造和次生构造?为什么区分之? 应力:

一.配位取代(substitution)反应 反应机理: 计量关系速率方程 反应机理硏究,影响反应速率的因素

16.61 Aerospace Dynamics Spring 2003 Generalized forces revisited Derived Lagrange s equation from d'Alembert's equation ∑m(8x+16y+22)=∑(Fx+F+F。=) Define virtual displacements sx Substitute in and noting the independence of the 8q,, for each

P CDN STANT Wow TAKE THE MOMENT OF MOMENTUM (ANGULAR MOMENTUM) MUST EXPLICITLY DEFINE A POWT ABOUT WHICH WE TAKE THE MOMENT

Chapter 4 Incompressible Flow Over Airfoils Of the many problems now engaging attention, the following are considered of immediate importance and will be considered by the committee as rapidly as funds can be secured for the purpose... The evolution of the more efficient

11. 4 PRANDTL-GLAUERT COMPRESSIBILITY CORRECTION The methods that approximately take into account of the effects of compressibility by correct the Incompressible flow results Is called compressible corrections

This chapter mainly deal with the properties of two-dimensional airfoils at mach number above 0.3 but below 1, where the compressibil ity must be considered

本节要点只有 一、计算通过正激波的流动特性变化