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STATUS: Completed CATEGORY: Aerospace

Anderson’s Introduction to Flight — Study Notes

This project is my working notebook for John D. Anderson, Jr. and Mary L. Bowden’s Introduction to Flight (McGraw-Hill, 2021). Each chapter gets its own deep-dive note with full derivations, interactive calculators, and worked examples. I’m building this as I study — chapters appear here as I complete them.

Book Structure & Progress

ChapterTopicStatusNotes
1The First Aeronautical EngineersCayley, Lilienthal, Langley, Wright brothers — the incremental breakthroughs that solved lift, propulsion, and control
2Fundamental ThoughtsPhysical quantities, perfect gas law, aerodynamic forces/moments, center of pressure, dimensional analysis, flow similarity
3The Standard AtmosphereHydrostatic equation, pressure/density/temperature vs. altitude, geopotential vs. geometric altitude, interactive ISA calculator
4Basic Aerodynamics
5Airfoils, Wings, and Other Aerodynamic Shapes
6Incompressible Flow over Airfoils
7Incompressible Flow over Finite Wings
8Three-Dimensional Incompressible Flow
9Compressible Flow: Some Preliminary Aspects
10Compressible Flow Through Nozzles, Diffusers, and Wind Tunnels
11Subsonic Compressible Flow over Airfoils
12Linearized Supersonic Flow
13Introduction to Numerical Techniques
14Elements of Hypersonic Flow
15Introduction to the Fundamental Principles and Equations of Viscous Flow
16Some Special Cases; Couette and Poiseuille Flows
17Introduction to Boundary Layers
18Laminar Boundary Layers
19Turbulent Boundary Layers
20Navier-Stokes Solutions: Some Examples
21Elements of Flight Vehicle Design

Why This Project?

Anderson’s book is the canonical undergraduate aerospace textbook, and working through it thoroughly means understanding every equation, not just skimming. These notes force me to derive everything from scratch, implement the models in code, and explain the physics clearly. The interactive calculators make the theory tangible — you can see exactly how pressure drops with altitude or how viscosity changes with temperature.

If you spot an error or want to discuss a derivation, open an issue on the site repository.