第一章 金融工程概述 第二章 远期与期货概述 第三章 远期与期货定价 第四章 运期与期货的运用 第五章 股指期货、外汇期货、利率远期与利率期货 第六章 互换的概述 第七章 互换的定价与风险分析 第八章 互换的运用 第九章 期权与期权市场 第十章 期权的回报与价格分析 第十一章 期权的交易策略及其运用 第十二章 布莱克-舒尔斯-默顿期权定价模型

一、生态效益的系统分析 (一)植物措施的生态效益 1、小气候效益 治沙植被过程中会对其控制区的局部气象因子如气温、空气湿度、地温等产生影响,能够产生对环境的某些改善和某些有利于植物生长的因素和降低风速的效应,是固沙生态效益中最首要的,最重要的指标

2.1性质与使用性能 1.基础概念 2.性质与性能的区别与关系 3.材料的失效分析 4.材料(产品)使用性能的设计 5.材料性能数据库 6.其它问题

Lecture D32: Damped Free Vibration Spring-Dashpot-Mass System k Spring Force Fs =-kx, k>0 Dashpot Fd =-cx, c>0 Newton's Second Law (mx =EF) mx +cx+kx (Define)Natural Frequency wn=k/m,and

– 1、掌握设备有形、无形损耗的类型及其对设备价值的影响； – 2、掌握设备折旧的含义、折旧方法与计算； – 3、掌握设备经济寿命概念及其计算； – 4、掌握存在新设备的设备更新原则及方法； – 5、掌握存在税收影响的设备租赁与购买比较决策

Lecture D33: Forced Vibration Fosinwt m Spring Force Fs =-kx, k>0 Dashpot Fd =-ci, c>0 Forcing Fext Fo sin wt Newton's Second Law (mix =CF) mx+cx+kx= Fo sin wt =k/m,=c/(2mwn)

现金流量和瓷金等值计算 一、现金流量构成 现金流量( Cash flow,CF) 现金流入( Cash In flow,CI) 销售(经营)收入、资产回收、借款等 现金流出( Cash Out flow,CO) 投资、经营成本、税、贷款本息偿还等 净现金流量(NCF) NCF=CI-CO

When the only force acting on a particle is always directed to- wards a fixed point, the motion is called central force motion. This type of motion is particularly relevant when studying the orbital movement of planets and satellites. The laws which gov- ern this motion were first postulated by Kepler and deduced from observation. In this lecture, we will see that these laws are a con- sequence of Newton's second law. An understanding of central

In this lecture, we consider the problem of a body in which the mass of the body changes during the motion, that is, m is a function of t, i.e. m(t). Although there are many cases for which this particular model is applicable, one of obvious importance to us are rockets. We shall see that a significant fraction of the mass of a rocket is the fuel, which is expelled during flight at a high velocity and thus, provides the propulsive force for the rocket

In this lecture, we will consider how to transfer from one orbit, or trajectory, to another. One of the assumptions that we shall make is that the velocity changes of the spacecraft, due to the propulsive effects, occur instantaneously. Although it obviously takes some time for the spacecraft to accelerate to the velocity of the new orbit, this assumption is reasonable when the burn time of the rocket is much smaller than the period of the orbit. In such cases, the Av required to do the maneuver is simply the difference between the