Air Data Systems MCQs

Welcome to our comprehensive collection of Multiple Choice Questions (MCQs) on Air Data Systems, a fundamental topic in the field of Avionics Engineering. Whether you're preparing for competitive exams, honing your problem-solving skills, or simply looking to enhance your abilities in this field, our Air Data Systems MCQs are designed to help you grasp the core concepts and excel in solving problems.

In this section, you'll find a wide range of Air Data Systems mcq questions that explore various aspects of Air Data Systems problems. Each MCQ is crafted to challenge your understanding of Air Data Systems principles, enabling you to refine your problem-solving techniques. Whether you're a student aiming to ace Avionics Engineering tests, a job seeker preparing for interviews, or someone simply interested in sharpening their skills, our Air Data Systems MCQs are your pathway to success in mastering this essential Avionics Engineering topic.

Note: Each of the following question comes with multiple answer choices. Select the most appropriate option and test your understanding of Air Data Systems. You can click on an option to test your knowledge before viewing the solution for a MCQ. Happy learning!

So, are you ready to put your Air Data Systems knowledge to the test? Let's get started with our carefully curated MCQs!

Air Data Systems MCQs | Page 1 of 7

Discover more Topics under Avionics Engineering

Q1.
The different probes that disturb the airflow is called ______
Discuss
Answer: (c).Intrusive probe
Q2.
The absolute pressure of the still air surrounding the aircraft is called as______
Discuss
Answer: (a).Static pressure
Discuss
Answer: (c).High angle of attack fighter aircraft
Q4.
What is the difference between the actual free stream pressure and the measured static pressure called?
Discuss
Answer: (b).Static defect
Discuss
Answer: (c).Wind tunnel tests to find spots of body-flow interference
Q6.
What are the tubes in the aircraft that carry the air pressure to the instruments is called as?
Discuss
Answer: (a).Pneumatic plumbing
Q7.
What is the difference between the static pressure and the stagnation pressure when the aircraft is stationary?
Discuss
Answer: (d).Static pressure
Q8.
The impact pressure and the dynamic pressure are the same.
Discuss
Answer: (b).False
Q9.
At supersonic speeds, a normal pitot tube cannot be used for speed measurements.
Discuss
Answer: (a).True
Q10.
Which of the following instruments use the pitot-static probe for its input?
Discuss
Answer: (d).Attitude indicator
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