学习目标: 一、掌握算术、逻辑和布尔运算符 二、自动类型转换和强制类型转换 三、条件判断语句 四、 switch结构

观察超音速下飞行器的升力、阻力的产生及绕飞行器流动的流场细节,包括激波、膨胀波的构型,可以采用以下两种方法: (1) Conduct flight tests using the actual vehicle 进行实际飞行器的飞行试验 (2) Run wind-tunnel tests on a small-scale modelof the vehicle 用飞行器的缩小模型进行风洞实验

\The compressibilty correction rule for thin wing The effect of compressibility in 3-D flows is somewhat less dramatic than with 2-D flows, but many of the same effects become important. Many of the same techniques for predicting linear compressibility effects work in 3-D too. For example

All real substances are compressible to some greater or lesser extend. When you squeeze or press on them, their density will change. This is particularly true of gases. (所有的真实物质都是可压缩的,当我们压挤 它们时,它们的密度会发生变化对于气体尤 其是这样)

一、能量方程的各种特殊表达形式 二、总温的计算公式 三、总压、总密度的计算公式 四、临界参数的定义与计算公式 五、特征马赫数(速度系数)M*的定义及计算公式

第八章我们讨论了正激波,本章我们讨论斜激波,及超音速流场中的另一个重要特征——膨胀波

如上图所示的斜激波在真实情况下有时会碰到固壁或与其它激 波、膨胀波相交,进而发生相互作用,这种现象称为激波的干 扰与反射。本节的目的就是要定性地讨论激波的干扰问题

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

5.1 Introduction The properties of airfoils are the same as the properties of a wing with infinite span. However, all real airplanes have wings of finite span. In the present chapter, we will apply our knowledge of airfoil properties to the analysis for finite wings. As we have mentioned in the previous chapter, the analysis for the aerodynamics of wings is separated in two steps.now, we are going on the second-step in Prandtl's philosophy of wing theory

17.1基本概念 17.2活性污泥法处理系统 17.3活性污泥法主要设计参数 17.4活性污泥反应动力学基础 17,5活性污泥处理系统的运行方式 17.6曝气的基本理论 7,7活性污泥处理系统的工艺设计 17.8活性污泥处理系统的运行管理