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Category: Theory of Flight Theory of Flight
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Description

In aerodynamics, drag refers to forces that oppose the relative motion of an object through the air. Drag always opposes the motion of the object and, in an aircraft, is overcome by thrust.

Types of Drag

There are many different types of drag. The most commonly encountered are:

  • Parasitic Drag, composed of
    • Form Drag, which is the result of the aerodynamic resistance to motion due to the shape of the aircraft,
    • Skin Friction Drag, which is due to the smoothness or roughness of the surfaces of the aircraft, and
    • Interference Drag, which may occur where surfaces with different characteristics meet (e.g. wing and fuselage)
  • Induced Drag, which is a secondary effect of the production of lift, and
  • Wave Drag which comes into play when shock waves are developed close to the surface of the aircraft in transonic and supersonic flight.

Drag and Airspeed

Parasitic drag increases with the square of the airspeed, while induced drag, being a function of lift, is greatest when maximum lift is being developed, usually at low speeds. The diagram below shows the relationship of parasitic drag and induced drag to each other and to total drag.

Relationship of Drag with Airspeed
Relationship of Drag with Airspeed

There is an airspeed at which total drag is minimum, and in theory, this is the maximum range speed; however, flight at this speed is unstable because a small decrease in speed results in an increase in drag, and a further fall in speed. The further decrease in speed causes yet more drag and, without the addition of thrust or initiation of a descent, could result in a stall or Loss of Control. In practice, for stable flight, maximum range is achieved at a speed a little above the minimum drag speed where a small speed decrease results in a reduction in drag.

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