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Archive / FAA Pilot’s Handbook of Aeronautical Knowledge / Pilot’s Handbook: Chapter 4 — Principles of Flight

Chapter 4, Part 5

Principles of Flight — Part 5

FAA-H-8083-25C (2023)

vortex

Tip

Figure 4-8. Tip vortex.

are identical. In both examples, the only difference is the

relationship of the airfoil with the oncoming airstream

(angle). A paper airplane, which is simply a flat plate, has a

bottom and top exactly the same shape and length. Yet, these

airfoils do produce lift, and “flow turning” is partly (or fully)

responsible for creating lift.

As an airfoil moves through air, the airfoil is inclined

against the airflow, producing a different flow caused by the

airfoil’s relationship to the oncoming air. Think of a hand

being placed outside the car window at a high speed. If the

hand is inclined in one direction or another, the hand will

move upward or downward. This is caused by deflection,

which in turn causes the air to turn about the object within

the air stream. As a result of this change, the velocity about

the object changes in both magnitude and direction, in turn

resulting in a measurable velocity force and direction.

A Third Dimension

To this point, the discussion has centered on the flow across

the upper and lower surfaces of an airfoil. While most of the

lift is produced by these two dimensions, a third dimension,

the tip of the airfoil also has an aerodynamic effect. The high-

pressure area on the bottom of an airfoil pushes around the tip

to the low-pressure area on the top. [Figure 4-8] This action

creates a rotating flow called a tip vortex. The vortex flows

behind the airfoil creating a downwash that extends back to

the trailing edge of the airfoil. This downwash results in an

overall reduction in lift for the affected portion of the airfoil.

Manufacturers have developed different methods to

counteract this action. Winglets can be added to the tip of

an airfoil to reduce this flow. The winglets act as a dam

preventing the vortex from forming. Winglets can be on the

top or bottom of the airfoil. Another method of countering

the flow is to taper the airfoil tip, reducing the pressure

differential and smoothing the airflow around the tip.

Chapter Summary

Modern general aviation aircraft have what may be considered

high performance characteristics. Therefore, it is increasingly

necessary that pilots appreciate and understand the principles

upon which the art of flying is based. For additional

information on the principles discussed in this chapter, visit

the National Aeronautics and Space Administration (NASA)

Beginner’s Guide to Aerodynamics at www.grc.nasa.gov/

www/k-12/airplane/bga.html.

Original source PDFPublished from pages 9–10 of the recorded source chapter.
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