AJD 21103 TOPIC 4 - AUXILIARY

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30 Terms

1
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What is the primary function of airflow control devices on swept wings?

To control the spanwise flow of the boundary layer air over the top of the wing.

2
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Where are wing fences typically located?

About mid-span, on the leading edge of the wing.

3
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What is the purpose of a saw tooth leading edge on military aircraft?

To form an invisible 'wall' of high-velocity air, straightening the spanwise flow over the wing.

4
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How do winglets improve aircraft performance?

By reducing drag and improving airflow control at higher speeds.

5
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What type of vortex is created by vortex generators?

A tip vortex that helps delay flow separation and aerodynamic stalling.

6
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What is the function of stall wedges on aircraft wings?

To disrupt boundary layer airflow at large angles of attack, ensuring wing root stalls before wing tips.

7
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What does active load control sense in aircraft?

Disturbances in the air that may cause discomfort to passengers and crew.

8
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What is 'flutter' in the context of control surfaces?

A phenomenon where air load distorts the control surface, causing it to lag behind and produce aerodynamic forces.

9
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What are the three principal methods of achieving aerodynamic balancing?

Horn balance, inset hinge, and pressure balancing.

10
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How does a horn balance operate on a control surface?

It assists movement away from the neutral position by utilizing airflow on the control surface.

11
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What is the function of an adjustable plate in pneumatic stall warning systems?

To coincide with the stagnation point of the wing during normal flight attitude.

12
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How does the electrical stall warning system provide alerts?

It uses a micro-switch and vane that detect changes in angle of attack to illuminate a warning light and sound an alarm.

13
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What is the purpose of a stick shaker device in aircraft?

To alert pilots of an impending stall by shaking the control column.

14
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What is the role of the stick pusher in stall prevention systems?

To pitch down the aircraft by pushing the control column in response to high angles of attack.

15
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What is boundary layer control and how does it enhance aircraft performance?

Methods to delay flow separation and improve airflow over control surfaces, enhancing lift.

16
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What is a vortex generator and where is it typically installed?

A device that creates a tip vortex to improve airflow, usually installed on the front third of a wing.

17
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Define stall in the context of aircraft performance.

A condition where the angle of attack increases to a point that lift begins to decrease.

18
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What materials are commonly used for mass balance weights?

Lead or depleted uranium.

19
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What systems are used to warn pilots of impending stalls?

Pneumatic and electrical stall warning systems.

20
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How does the stall warning horn operate in light aircraft?

It emits a noise when the angle of attack exceeds a certain threshold, indicating an impending stall.

21
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What is the advantage of using a blended winglet compared to a conventional wingtip?

It creates a smaller vortex, leading to less drag.

22
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How does a leading-edge stall warning system function in larger aircraft?

Using a vane and micro-switch to detect changes in airflow at the stall angle.

23
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What design principle underlies the function of horn balances?

To reduce pilot control loads by balancing aerodynamic forces around the hinge line.

24
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What happens to a stick shaker when an aircraft approaches a stall angle?

It activates to shake the control column, alerting the pilot.

25
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What is the purpose of using a plenum chamber in pneumatic stall warning systems?

To detect low-pressure areas caused by increasing angles of attack.

26
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What is the benefit of a saw tooth leading edge compared to a wing fence?

It reduces drag and weight while maintaining airflow control.

27
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In the context of stall prevention, what is the desired outcome of using stall wedges?

To ensure that the wing root stalls before the tips, providing safer handling characteristics.

28
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How does a pilot override a stick pusher system?

By using a switch located at the control column.

29
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What is one common external feature of all stall warning systems?

They aim to alert pilots to prevent loss of control before a stall.

30
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Why is aerodynamic balancing important for larger aircraft controls?

To reduce high stick forces experienced by pilots at higher speeds.