Study Materials/Principles of Flight
✈️

Principles of Flight

Aerodynamics, flight mechanics, and aircraft performance fundamentals.

Overview

Principles of Flight covers the science of aerodynamics and how aircraft achieve and maintain flight. This includes understanding the four forces (lift, weight, thrust, drag), airfoil theory, stability and control, performance limitations, and flight envelope boundaries.

Key Topics

1. The Four Forces of Flight

Lift opposes weight, thrust opposes drag. In steady level flight, these forces are in equilibrium. Understanding how changing one force affects the others is fundamental to all flight maneuvers.

2. Airfoil Theory and Lift

How an airfoil generates lift through pressure differential (Bernoulli's principle) and Newton's Third Law. The angle of attack is the primary factor controlling lift, with the critical angle of attack causing a stall.

3. Drag

Parasite drag (form, skin friction, interference) increases with airspeed squared. Induced drag (a byproduct of lift) decreases with airspeed. Total drag is minimized at the speed where these two components are equal.

4. Stalls and Spins

A stall occurs when the critical angle of attack is exceeded, regardless of airspeed or attitude. Factors affecting stall speed include weight, load factor, configuration, and bank angle. Spin recovery follows the PARE procedure.

5. Stability and Control

Longitudinal (pitch), lateral (roll), and directional (yaw) stability. Static stability is the initial tendency to return to equilibrium; dynamic stability determines whether oscillations damp out over time.

6. Load Factor and Maneuvering

Load factor (G-force) increases in turns and pull-ups. In a 60° bank turn, load factor is 2G, which increases stall speed by √2 (×1.41). Understanding the V-n diagram defines the aircraft's maneuvering envelope.

Key Terms & Definitions

Angle of Attack (AoA)
The angle between the chord line of the wing and the relative airflow
Load Factor
The ratio of lift to weight, expressed in G units. 1G is normal straight-and-level flight
V-speeds
Reference speeds: Vs (stall), Va (maneuvering), Vne (never exceed), Vfe (max flap extended)
Centre of Pressure
The point on an airfoil where the total aerodynamic force acts
Induced Drag
Drag generated as a byproduct of lift, caused by wingtip vortices and spanwise flow

Exam Tips

  • Tip 1:Remember: stall occurs at a critical angle of attack, NOT at a specific airspeed
  • Tip 2:Know the relationship between bank angle and load factor (1/cosθ)
  • Tip 3:Understand why induced drag increases at lower speeds and parasite drag at higher speeds
  • Tip 4:Learn the effects of flaps on stall speed, lift, and drag
  • Tip 5:Know the axis of rotation for each control surface (ailerons, elevator, rudder)

Recommended References

Pilot's Handbook of Aeronautical Knowledge Ch. 5

FAA handbook covering aerodynamics of flight

Principles of Flight (EASA)

European study material for principles of flight examination

Aerodynamics for Naval Aviators

Classic reference text on aerodynamics and aircraft performance

Ready to Test Your Principles of Flight Knowledge?

Take a mock exam with practice questions covering everything in this study guide.