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Questions and Answers
What directly affects the amount of lift produced by an aircraft wing?
What happens to the angle of attack as aircraft weight increases?
Which of the following signals a stall condition in an aircraft?
What is the critical angle of attack?
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To recover from a stall, what must be done?
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What does not directly contribute to the stalling of an aircraft?
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What is Total Air Temperature (TAT) in aircraft operating at high Mach numbers?
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What material is commonly used for TAT probes to ensure good thermal conductivity and strength?
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Which of the following best describes the design purpose of the inner tube of the TAT probe?
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What precaution should be taken when handling TAT probes?
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During flight, how does the air pressure within the TAT probe compare to the air pressure outside?
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What is the function of the axial wire wound heating element in some TAT probes?
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What primarily causes the vane-type sensor to move?
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Which feature is included in angle of attack sensors to prevent in-flight issues?
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What is the function of index pins in the vane-type sensor?
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Why is care advised when moving the vane-type sensor?
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What is the significance of the stagnation point in aircraft aerodynamics?
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How does the heater element in angle of attack sensors adjust under specific conditions?
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What is primarily the function of the probe-type sensor in aircraft?
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What action should be taken when installing angle of attack probes?
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What happens to the current in winding B when the temperature of the sensor Rx increases?
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In a ratiometer, what effect does the constant torque of winding A have when the current ratio changes?
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What is generated when the junction of two dissimilar metals is heated in a thermocouple system?
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How does the operating mechanism of thermocouple systems differ from variable resistance systems?
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What is necessary for the operation of a thermocouple system?
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What role does the iron core play in the ratiometer construction?
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When the measuring element stabilizes in a ratiometer, what does the angular deflection represent?
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What factors influence the magnitude of the EMF produced in a thermocouple circuit?
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What is a suitable application for thermocouple systems?
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What occurs when the torques produced by both windings of a ratiometer become balanced?
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Study Notes
Aircraft Stall and Angle of Attack
- Aircraft can stall at any airspeed, flight attitude, or weight due to the angle of attack (AOA).
- Lift production depends on air density, aerofoil design, angle of attack, and the aircraft's weight and speed.
- Lower speeds and heavier weights necessitate a higher AOA to maintain lift, increasing the risk of reaching the critical angle of attack and stalling.
- Stall occurs when the AOA causes airflow to separate from the leading edge, leading to a complete loss of lift at the critical angle.
Stall Recovery
- To recover from a stall, reduce the angle of attack below the critical threshold to restore smooth airflow.
Angle of Attack Indicators
- Aircraft warn of impending stalls through buffeting, pitch attitude changes, or wing drops.
- Direct sensing of angle of attack is beneficial for preventing stalls, often achieved with potentiometer outputs to cockpit indicators.
Vane-Type Angle of Attack Sensor
- Composed of a counterbalanced aerodynamic vane, this sensor rotates in response to airflow changes, indicating the angle of attack.
- The vane is shielded against ice formation and correctly aligned using index pins.
Angle of Attack Sensor Precautions
- AoA sensors feature heating elements to prevent freezing and may adjust power when the aircraft is on the ground to avoid overheating.
- Care is essential to avoid damage to probe and vane-type sensors during handling and installation.
Stall Warning Systems
- The stagnation point is where airflow separates at a wing's leading edge, critical in stall detection.
Thermocouple Systems
- Thermocouples generate an Electromotive Force (EMF) when dissimilar metals are heated, allowing temperature measurement without external power.
- These systems are suitable for high-temperature applications like engine turbine and cylinder head temperatures.
Total Air Temperature Measurement
- Total Air Temperature (TAT) reflects maximum temperature rise in high Mach number flights and is measured when airflow is nearly at rest.
- TAT probes are made from nickel-plated beryllium copper, featuring an integrated heating element to prevent ice formation.
- Careful handling of TAT probes is crucial to avoid damage.
Modern Cockpit Technologies
- Glass cockpits replace traditional mechanical gauges with displays driven by flight management systems, enhancing navigation and operation.
- Electronic Attitude and Heading Reference Systems (AHRS) and Air Data Computers (ADCs) improve reliability and customization.
- Glass cockpits may include Synthetic Vision Systems (SVS) and Enhanced Vision Systems (EVS) for improved situational awareness.
- General aviation aircraft increasingly adopt glass cockpit technologies, exemplified by the Garmin G1000 in models like the Cessna 172.
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Description
This quiz focuses on the principles of lift and stalling in aircraft, emphasizing that stalling can occur at any airspeed, attitude, or weight. Understanding the angle of attack and its relation to lift is crucial for pilot training and aircraft performance.