Fundamentals of Aerodynamics – Part 2
Course Description
In this module, the aerodynamic concepts introduced in Part 1 are extended to include real-world wing behavior, lift mechanisms, drag formation, and aircraft performance factors. Learners will explore how lift is generated on finite wings, how vortices influence drag, and how aircraft stability and control are achieved.
What you'll learn in this course?
Explain Reynolds number and its significance
Understand circulation theory of lift
Describe finite wing effects
Explain wingtip vortices and induced drag in depth
Understand lift distribution across span
Describe stall types and stall behavior
Explain high-lift devices and their functions
Understand aircraft performance parameters
Explain drag polar and aerodynamic efficiency
Understand stability vs control concepts
Explain longitudinal stability basics
Recognize control surfaces and their roles
Course Curriculum
- Introduction
- Reynolds Number (Re)
- Importance of Reynolds Number
- Circulation Theory of Lift
- Kutta Condition
- Finite Wing Effects
- Wingtip Vortices
- Induced Drag (Advanced)
- Lift Distribution
- Stall Fundamentals
- Types of Stall
- Stall Warning Signs
- High-Lift Devices
- Flaps
- Slats & Slots
- Lift-to-Drag Ratio (L/D)
- Drag Polar
- Aircraft Performance Factors
- Stability vs Control
- Longitudinal Stability
- Control Surfaces
- Summary of Lift Mechanics
- Summary of Performance & Control
- References
- Assessment Instructions
- Part 2