3.1 数据压缩的基本原理 3.2 数据压缩方法分类 3.3 常用压缩编码方法 3.3.1 信息熵编码

3.3.3 变换编码 1. 变换编码的一般原理 2. DCT变换编码方法 ⑴ DCT变换的基本过程 ⑵ DCT变换的基本算法 3.3.4 矢量量化编码 1. VQ编码的基本原理 ⑴ 总体设计目标 ⑵ 量化器设计 ⑶ VQ编码器设计 2. 码本生成的优化算法

4.1 光盘技术的发展与应用 4.2 CD_ROM光盘系统 4.2.1 光盘制作原理与方法 1.光盘驱动方式与光道结构 2.信息存储原理与调制编码 3.光盘制作的基本过程 4.2.2 CD_ROM的物理存储格式 1.CD_ROM盘片的物理结构 2.数据的扇区结构和帧结构 3.一组典型数据计算

6.3.1 超文本技术的发展与应用 6.3.2 超文本与超媒体概念 6.3.3 超文本组成要素 6.4 超文本系统的结构模型 6.4.1 Combell & Goodman模型 6.4.2 Dexter模型 6.4.3 其它超文本模型

Table of contents PARTO- PRELUDE: REVIEW OF \UNIFIED ENGINEERING THERMODYNAMICS\ 0.1 What it's all about 0. 2 Definitions and fundamentals ideas of thermodynamics 0.3 Review of thermodynamics concepts

a B: The second Law of Thermodynamics [AW 42-50: VN Chapter 5; VwB&S-6.3, 6.4, Chapter 7 1. B. Concept and statements of the Second law why do we need a second law?) The unrestrained expansion, or the temperature equilibration of the two bricks, are familiar

PARTO- PRELUDE: REVIEW OF UNIFIED ENGINEERING THERMODYNAMICS [AW pp 2-22, 32-41(see IAW for detailed SB&vw references): VN Chapter 1] 0.1 What it's all about The focus of thermodynamics in 16.050 is on the production of work, often in the form of kinetic energy(for example in the exhaust of a jet engine)or shaft power

PART 2- POWER AND PROPULSION CYCLE 2A -Gas Power and propulsion cycles SB&vW-118,119,11.10,11.11,11.12,1113,11.14] In this section we analyze several gas cycles used in practical applications for propulsion and power generation, using the air standard cycle. The air standard cycle is an the actual cycle behavior, and the term specifically refers to analysis using the folpproximation to assumptions

Part 2.: introduction to thermochemistry SB&VW-14.1-14.6 Until now, we have specified the heat given to the devices analyzed, and not concerned ourselves with how this heat might be produced. In this section, we examine the issue of how obtain the heat needed for work

Introduction to Engineering Heat Transfer These notes provide an introduction to engineering heat transfer. Heat transfer processes set limits to the performance of aerospace components and systems and the subject is one of an enormous range of application. The notes are intended to describe the three types of heat transfer and provide basic tools to enable the readers to estimate the magnitude of heat transfer rates in realistic aerospace