Lecture Notes on How Airplanes Fly

Jul 27, 2024

Lecture Notes on How Airplanes Fly

Introduction

  • Understanding how airplanes fly is crucial for all students.
  • Aim: Go beyond FAA requirements to grasp the mechanics of flight.

Airplane Parts

  • Propeller: Located at the front; part of the engine.
  • Fuselage: Main body of the airplane where passengers sit.
  • Wings: Extend from the fuselage.
  • Tail Components:
    • Vertical part: Rudder (controls side-to-side motion).
    • Horizontal part: Elevator (controls up and down motion).
  • Landing gear: Wheels for landing.

Key Forces on an Airplane

  • Lift: Upward force.
  • Weight: Downward force.
  • Thrust: Forward force.
  • Drag: Opposes thrust.
    • Lift must exceed weight for ascent.
    • Thrust must exceed drag for forward motion.

Theories of Lift

  • Conservation of Momentum:
    • Air molecules are pushed downward, resulting in lift upwards.
  • Airfoil: Shape of the wing crucial to lift generation.
  • Common Misconceptions:
    • Equal Transit Theory: Incorrect notion that air molecules from both top and bottom reach the tail at the same time.
      • This theory falsely suggests that faster airflow over the wing’s top generates lift.

Correct Understanding of Lift

  • Bernoulli's Principle: An increase in airspeed results in a decrease in pressure.
  • The downward deflection of air by the airfoil creates lift.
  • Lift relationships:
    • Lift also generated by entire aircraft, not just wings.
    • All objects moving through fluid can generate lift.

Mathematical Representation of Lift

  • Lift equation involves:
    • L: Lift
    • ρ: Air density
    • V: Velocity
    • A: Wing area
    • Cl: Coefficient of lift

Factors Affecting Lift

  • Wing Shape and Size
  • Velocity of Air
  • Angle of Attack: Inclined orientation affecting lift.
  • Fluid medium influences lift, e.g., viscosity and compressibility.

Stability and Control

  • Three Axes of Flight:
    • Longitudinal (nose to tail): Controlled by elevator.
    • Lateral (wingtip to wingtip): Controlled by ailerons.
    • Vertical: Controlled by rudder.
  • Left Turning Tendencies:
    • A result of torque, P-factor, corkscrew effect, and gyroscopic precession.

Maneuvering Flight

  • Climbing: When lift exceeds weight.
  • Descending: When weight exceeds lift.
  • Stalling: Loss of lift due to excessive angle of attack.
  • Ground Effect: Reduced drag when close to ground.

Conclusion

  • Summarized concepts of lift, stability, and the forces affecting flight.
  • Acknowledged challenges in calculating lift accurately.
  • Discussion of integrated systems within aviation.