This course covers the basic principles and definitions of aerodynamics, including wing parameters, aspect ratio, compressible and incompressible flow, viscosity, control volume, continuity principle, Mach number, Reynolds number, forces acting on the aircraft, lift calculation, lift coefficient, and angle of attack. The teaching method includes theory explanations, example problems, and vector calculations. The course is intended for individuals interested in aerospace engineering and aerodynamics.
Overview
Syllabus
Wing parameters. Introduction to Aerospace Engineering..
What is aspect ratio? Example problem and solution..
What is compressible and incompressible flow?.
What is viscosity? Viscous and inviscid flow..
What is Control Volume and Control Surface? Aerodynamics..
Principle of continuity. Part 1. Theory..
Dot product of 2 vectors. (refresher).
Surface normal vector explained.
Principle of continuity. Part 2. Mass flow rate..
Mach number explained..
Reynolds number explained..
Forces acting on the aircraft.
How to calculate lift? Lift coefficient and angle of attack..
What is the correct lift theory?.
Introduction to Aerodynamics: Lift.
Taught by
Aliya Burkit
