Total Drag

081-01-05Pablo Asensio Martínez2026-04-011 min

Parasite Drag ($D_p$)

Drag not associated with the production of lift. Increases with speed squared ($V^2$).

  1. Skin Friction Drag: Due to viscosity of air moving over the surface.
    • Affected by roughness (ice, rivets) and surface area.
    • Laminar flow (smooth) creates less friction than Turbulent flow.
  2. Form Drag (Pressure Drag): Due to separation of airflow creating a turbulent wake behind the object.
    • Reduced by streamlining (fairings).
  3. Interference Drag: Due to mixing of airflows at junctions (e.g., wing/fuselage root).

Total Drag Curve

  • Induced Drag: Decreases as speed increases ($1/V^2$).
  • Parasite Drag: Increases as speed increases ($V^2$).
  • Total Drag: The sum of both. U-shaped curve.

Minimum Drag Speed ($V_{md}$)

The bottom of the drag curve.

  • At $V_{md}$, Induced Drag = Parasite Drag.
  • This is the speed for Maximum Range (for jets) and Maximum Glide Range.
  • Flying below $V_{md}$ is the "Back side of the power curve" (speed instability: slower speed = more drag).
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.