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Aerodynamics - Four Forces
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Understanding how these forces work and knowing how to control them with the use of power and flight controls are essential to flight.

In steady flight, the sum of these opposing forces is always zero.
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Drag
   
A rearward, retarding force caused by disruption of airflow by the wing, fuselage, and other protruding objects. As a general rule, drag opposes thrust and acts rearward parallel to the relative wind.

There are two basic types: parasite drag and induced drag.
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Parasite Drag
 
Called "parasite" because it in no way functions to aid flight.
   

Parasite drag is comprised of all the forces that work to slow an aircraft’s movement. This includes the displacement of the air by the aircraft, turbulence generated in the airstream, or a hindrance of air moving over the surface of the aircraft and airfoil.

Parasite drag varies with the speed of the airplane (higher at higher speeds).
Proportionate to square of the airspeed (2x as fast, 4x lift), aplane at constant altitude has four times as much parasitic drag at 160kts than it does at 80 kts.


There are three types of parasite drag:

   
Form Drag results from the turbulent wake caused by the separation of airflow from the surface of a structure. Examples include the engine cowlings, antennas, etc. (Stuff sticking out into the air). Related to both the size and shape of the structure that protrudes into the relative wind
   
Interference Drag comes from the intersection of airstreams that creates eddy currents, turbulence, or restricts smooth airflow. For example, the intersection of the wing and the fuselage at the wing root has significant interference drag.
   
Skin friction Drag is the aerodynamic resistance due to the contact of moving air with the surface of an aircraft. Every surface, no matter how apparently smooth, has a rough, ragged surface when viewed under a microscope.
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Induced Drag
 
Is a result of an any airfoil developing lift.

Inversely proportional to the square of the airspeed (if speed is decreased by half, induced drag increases fourfold).

When you practice slow flight, you must pull back on the yoke to bring the nose higher, increasing your AOA, and also increasing induced drag.
 

Induced Drag - Vorticies
 
Generated by the airflow circulation around the wing as it creates lift
 
The high-pressure air beneath the wing joins the low-pressure air above the wing at the trailing edge and wingtips, which causes a spiral vortex, which trails behind each wingtip when lift is being produced
 
These wingtip vortices have the effect of deflecting the air stream downward in the vicinity of the wing, creating an increase in downwash, and this deflects the average relative wind downward (not straight back). Since the lift produced by the wing is perpendicular to the relative wind, the lift is inclined aft by the same amount and not straight upward
 
This component of lift acting in a rearward direction (lost lift) is induced drag
 
As the air pressure differential increases with an increase in AOA, stronger vortices form and induced drag is increased
 
Low speed = High AOA = High Induced drag
 
High speed = Low AOA = Low Induced drag
       
     
You will learn more about these vortices when you are introduce to Wake Turbulence and Ground Effect
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You can read more about the concepts above in the Pilot’s Handbook of Aeronautical Knowledge.
Chapter 4: Principles of Flight
Chapter 5: Aerodynamics of Flight




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