Jeppesen Private Pilot Ground Review Chapter 3, Section a

Key Terms:

 

Lift

Weight

Thrust

Drag

Vectors

Newton's Three Laws of Motion

Bernoulli's Principle

Venturi

Airfoil

Leading Edge

Trailing Edge

 

 

Upwash

Downwash

Relative Wind

Camber

Chord Line

Angle of Attack

Coefficient of Lift

Stall

Critical Angle of Attack

Aspect Ratio

Wing Area

 

 

Planform

Angle of Incidence

Stall Strips

Flaps

Configuration

Plain Flap

Split Flap

Slotted Flap

Fowler Flap

Parasite Drag

Form Drag

 

 

Interference Drag

Skin Friction Drag

Induced Drag

Wingtip Vortices

Ground Effect

1: Select the true statement(s) regarding the four forces of flight.

if an error occurs, please copy and paste into desired email program or write down answers on separate sheet of paper to go over during the next lesson.

Student Center

2: Refer to the following illustration and identify the aerodynamic terms associated with airfoil.

Wing Span       = 196 ft

Average Chord = 28 ft

Wing Span       = 35 ft

Average Chord = 5 ft

Wing Span       = 37 ft

Average Chord = 11 ft

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