A First Course on Aerodynamics[RareAbyss]

A First Course on Aerodynamics is designed to introduce the basics of aerodynamics to the unfamiliar reader. This text avoids lengthy and complicated derivations, focusing on primary equations and fundamental concepts. Detailed figures and explanations of important mathematical equations are interspersed throughout the text.
The field of aerodynamics studies the motion of air around an object, such as an aircraft. After introducing fundamental concepts such as fluid flow, Thin Airfoil Theory, and Finite Wing Theory, A First Course on Aerodynamics presents the fundamentals of three key topics: Inviscid Compressible Flow, Viscous Flow, and wind tunnels. Important subtopics include one dimensional flow, quasi one dimensional flow, oblique shocks and expansion waves, boundary layer, and low speed and supersonic speed wind tunnels.

Content

1 Fundamental Concepts in Aerodynamics and Inviscid Incompressible Flow
1.1 Introduction
1.2 Definition and approach
1.3 Fundamental concepts
1.4 Governing equations of fluid flow
1.5 Thin Airfoil Theory
1.6 Finite Wing Theory
1.7 Multiple choice questions
1.8 Figures

2 Fundamentals of Inviscid Compressible Flow
2.1 Introduction
2.2 One Dimensional Flow Equations: Isentropic flow, stagnation condition, Normal Shock
2.3 Quasi One Dimensional Flow: Nozzle and diffuser flow
2.4 Oblique shocks and Expansion waves
2.5 Linearised Theory: Compressible flow past thin airfoil
2.6 Hypersonic flow
2.7 Multiple choice questions
2.8 Figures

3 Fundamentals of Viscous Flow
3.1 Introduction
3.2 Exact Viscous Flow Solutions
3.3 Introduction to Boundary Layer
3.4 Multiple Choice Questions
3.5 Figures

4 Wind Tunnels and a Few Basic Experiments
4.1 Introduction
4.2 Low Speed Wind Tunnels
4.3 Supersonic Wind Tunnels
4.4 Some Basic Experiments in Low Speed Wind Tunnels
4.5 Some Basic Experiments in Supersonic Wind Tunnel
4.6 Multiple Choice Questions
4.7 Figures