Spring 2003 1661AC22 Longitudinal Dynamics For notational simplicity, let X=Fn, Y= Fu, and Z= F aF Longitudinal equations(1-15 )can be rewritten as mi=X+X2- mg cos(0+△X

Aircraft Lateral Dynamics Using a procedure similar to the longitudinal case, we can develop the equa tions of motion for the lateral dynamics

美国麻省理工大学：《Aerospace Dynamics（航空动力学）》英文版 Lecture 15

美国麻省理工大学：《Aerospace Dynamics（航空动力学）》英文版 lecture 11

一、自由基聚合反应微观动力学方程 推导微观动力学方程的基本假设

Spring 2003 Derivation of lagrangian equations Basic Concept: Virtual Work Consider system of N particles located at(, x2, x,,.x3N )with 3 forces per particle(f. f, f..fn). each in the positive direction

2.7 双共振（Double resonance） 2.8 核磁共振中的动力学现象 2.9 核磁共振氢谱的解析

Spring 2003 Example Given: Catapult rotating at a constant rate(frictionless, in the horizontal plane) Find the eom of the particle as it leaves the tube

CoRIoLIS ACcELERAT0 EMYSTIF∈p CONSIOER CASE oF CONSTANT ROTA ToN.No AT0 N OF MME⊙AGUA,ANDc°srAT RADIAL VELOCITY ( As sEEN IN THE RomTIwG

第一节固相反应类型 第二节固相反应机理 第三节固相反应动力学 第四节影响固相反应的因素