Lecture 1 :

Objective: Fundamental concepts of aerodynamics

Description: An introduction to computational fluid dynamics as anintegral part of the study of aerodynamics. Computational fluiddynamics (CFD) has recently become a third dimension in aerodynamics, complementing the previously existing dimensional ofpure experiment and pure theory. It is absolutely necessary that themodern student of aerodynamics be introduced to some of the basicideas of CFD—he or she will most certainly come face to face witheither its “machinery” or its results after entering theprofessional ranks of practicing aerodynamicists

学习目标：空气动力学的基本概念

学习描述：介绍计算流体动力学作为空气动力学研究的一个组成部分。计算流体动力学 (CFD) 最近已成为空气动力学的第三个维度，补充了先前存在的纯实验和纯理论维度。向现代空气动力学学生介绍 CFD 的一些基本概念是绝对必要的。

Lecture 2:

Objective: Governing equations of fluid dynamics, concepts of streamfunction, potential function, circulation and vorticity, andHelmholtz theorems

Description: In this section, we examine this motion more closely,paying particular attention to the orientation of the element andits change in shape as it moves along a streamline. In the process,we introduce the concept of vorticity, one of the most powerfulquantities in theoretical aerodynamics.

学习目标：流体动力学的控制方程，其中包括：流函数、势函数、环流和涡量的概念，以及亥姆霍兹定理。

学习描述：在本节中，我们将更仔细地研究这些，特别注意元素的方向及其沿流线移动时的形状变化。在这个过程中，我们引入了涡量的概念，涡量是理论空气动力学中最强大的量之一。

Lecture 3:

Objective: Irrotational flows and potential flow theory for flowpast bodies

Description: Why is it so important to make a distinction betweenrotational and irrotational flows? The answer becomes blatantlyobvious as we progress in our study of aerodynamics; we find thatirrotational flows are much easier to analyze than rotational flows.

学习目标：无旋流和势流理论

学习描述：为什么区分旋转流和非旋转流如此重要？随着我们对空气动力学的研究取得进展，答案变得非常明显-无旋流比旋转流更容易分析。

Lecture 4:

Objective: Kutta-Joukowski theorem and Thin airfoil theory

Descprition: The Kutta-Joukowski theorem states that lift per unitspan on atwo-dimensional body is directly proportional to the circulationaround the body. Indeed, the concept of circulation is so importantat this stage of our discussion.

学习目标：库塔-儒可夫斯基定理（Kutta-Joukowski theorem）

学习描述：库塔-儒可夫斯基定理（Kutta-Joukowski theorem）指出，每单位跨度的升力在二维身体与身体周围的循环成正比。事实上，在我们讨论的这个阶段，流通的概念非常重要

Lecture 5:

Objective: Finite wing (Lifting line) theory, Slender body theory

Description: As studied before, the flow over an airfoil istwo-dimensional. In contrast, a finite wing is a three-dimensionalbody, and consequently the flow over the finite wing isthree-dimensional; that is, there is a component of flow in thespanwise direction.

学习目标：有限翼展机翼及升力线理论

学习描述：如前所述，翼型上的流动是二维的。相反，有限翼是一个三维物体，因此有限翼上的流动是三维的；也就是说，在展向方向存在流动分量。

Lecture 6:

Summary, and Q&A

最终成果展示、课题答疑