Wing Basics
Airflow
Airfoil Design
Wing Geometry
Wingtip Features
100

This imaginary straight line joins the leading and trailing edges of a wing.

The chord

100

The smooth airflow near the front of the wing is called this layer.

Laminar Layer

100

Conventional airfoils are thickest at this percentage of the chord.

25% of the chord

100

 This aircraft commonly has a high aspect ratio wing.

A glider

100

 Wing twist is designed to improve these characteristics.

Stall characteristics

200

The average chord of a wing is called this.

Mean Aerodynamic chord

200

This layer forms farther back on the wing after airflow slows because of skin friction.

Turbulent layer

200

Laminar flow airfoils are thickest at this percentage of the chord.

50% of the chord

200

This is the angle at which the wing is permanently attached relative to the aircraft's longitudinal axis.

The angle of incidence

200

If the wing root stalls before the tip, these controls remain effective longer.

Ailerons

300

 Aircraft designed for high speeds usually have this type of airfoil.

Thin Airfoil

300

As airspeed and angle of attack increase, this point moves forward.

Transition point

300

These are the three general wing planforms.

Rectangular, eliptical, and delta

300

Name one thing affected by the angle of incidence.

Flight visbility,Takeoff, landing,

300

These devices reduce induced drag by limiting wing-tip vortices.

Winglets

400

Aircraft designed to fly slowly usually have this type of airfoil.

Thick Airfoil

400

This force causes the boundary layer to slow down and become turbulent.

Skin Friction

400

This is the relationship between wing span and average chord.

Aspect Ratio

400

Decreasing the angle of incidence at the wing tip is called this

Washout

400

Another method of reducing wing-tip vortices is installing these.

Wing tip fuel tanks

500

This thin layer of air lies directly over the surface of the wing.

Boundary Layer

500

Laminar flow airfoils reduce this aerodynamic force.

Drag

500

High aspect ratio wings produce more lift with less of this type of drag.

Induced drag

500

 Increasing the angle of incidence at the wing tip is called this.

Wash In

500

This wing-tip modification also helps reduce induced drag.

Drooping the wing tip

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