Propellers and Thrust
Jet Engines
Turning Tendencies
Types of Drag
Drag Math & Ground Effect
100

 A propeller creates thrust based on which law of physics?

Newton’s Third Law.

100

What section of a jet engine increases pressure using spinning blades?

The compressor.

100

Spiral slipstream striking the tail causes which tendency?

Corkscrew effect (left yaw).

100

 Drag caused by the shape of an object is called what?

Form drag.

100

What is the drag equation?

D = (CD × ρ × V² × S) / 2.

200

Why do propeller blade tips move faster than the root?

They travel a longer distance in the same amount of time.

200

What turns the compressor in a jet engine?

The turbine via a connecting shaft.

200

What tendency occurs because the descending propeller blade on the right creates more thrust?

P-factor.

200

What type of drag is created by airflow mixing where components meet, such as at the wing root?

Interference drag.

200

In the drag equation, which variable has the largest effect on drag?

Velocity, because it is squared.

300

What major design feature helps equalize thrust along a propeller blade?

 Blade twist (changing angle of attack from root to tip).

300

 A turbofan differs from a turbojet because it uses what to produce extra thrust?

A large bypass fan.

300

According to Newton’s 3rd Law, engine/prop rotation causes the airplane to roll left. What is this called?

Torque reaction.

300

Parasite drag depends mainly on what variable?

Velocity squared.

300

 If velocity doubles, drag changes by what factor?

Drag × 4.

400

What is the main tradeoff of a fixed-pitch “climb” propeller?

Great takeoff thrust, but less efficient cruise.

400

What are the five stages of jet engine operation?

Intake, Compression, Combustion, Turbine, Exhaust.

400

Gyroscopic precession appears strongest during which type of airplane motion?

 Pitch changes (nose up or down).

400

What type of drag results from creating lift and forms wingtip vortices?

 Induced drag.

400

What does ground effect do to induced drag?

It reduces it by weakening wingtip vortices.

500

Name three factors engineers can change along a blade to balance thrust.

Angle of attack (twist), camber, and surface area.

500

 Why can’t propellers be used efficiently at very high speeds?

Propeller tips approach the speed of sound, becoming inefficient and creating shockwaves.

500

Name all four turning tendencies.

Corkscrew effect, Torque reaction, P-factor, Gyroscopic precession.

500

Describe how induced drag changes with airspeed, and why.

It decreases as speed increases, because producing the same lift requires a lower AOA at higher speeds.

500

What airspeed corresponds to minimum total drag and maximum glide range?

Best glide speed (the speed at which induced and parasite drag sum to the lowest point).

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