Compressors,Gas Dynamics and Gas Turbines MCQs

Welcome to our comprehensive collection of Multiple Choice Questions (MCQs) on Compressors,Gas Dynamics and Gas Turbines, a fundamental topic in the field of Mechanical Engineering. Whether you're preparing for competitive exams, honing your problem-solving skills, or simply looking to enhance your abilities in this field, our Compressors,Gas Dynamics and Gas Turbines 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 Compressors,Gas Dynamics and Gas Turbines mcq questions that explore various aspects of Compressors,Gas Dynamics and Gas Turbines problems. Each MCQ is crafted to challenge your understanding of Compressors,Gas Dynamics and Gas Turbines principles, enabling you to refine your problem-solving techniques. Whether you're a student aiming to ace Mechanical Engineering tests, a job seeker preparing for interviews, or someone simply interested in sharpening their skills, our Compressors,Gas Dynamics and Gas Turbines MCQs are your pathway to success in mastering this essential Mechanical Engineering topic.

Note: Each of the following question comes with multiple answer choices. Select the most appropriate option and test your understanding of Compressors,Gas Dynamics and Gas Turbines. 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 Compressors,Gas Dynamics and Gas Turbines knowledge to the test? Let's get started with our carefully curated MCQs!

Compressors,Gas Dynamics and Gas Turbines MCQs | Page 2 of 17

Discuss
Answer: (b).The compression ratio for the compressor is always greater than unity.
Discuss
Answer: (a).the propulsive matter is ejected from within the propelled body
Q13.
The type of rotary compressor used in gas turbines, is of
Discuss
Answer: (b).axial flow type
Q14.
The volume of air delivered by the compressor is called
Discuss
Answer: (b).compressor capacity
Q15.
The efficiency of a jet engine is higher at
Discuss
Answer: (d).high altitudes
Q16.
The actual volume of air delivered by a compressor, When reduced to the normal temperature and pressure conditions is called compressor capacity.
Discuss
Answer: (b).No
Q17.
The compression ratio in a gas turbine is

a.

4

b.

1

c.

9

d.

12

Discuss
Answer: (b).1
Q18.
Intercooling in compressors results in saving of power in compressing given volume of air to a given pressure.
Discuss
Answer: (a).Correct
Discuss
Answer: (d).they are not air-breathing engines
Q20.
The maximum combustion pressure in gas turbine is __________ as compared to I.C. engine.
Discuss
Answer: (b).less
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