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 13 of 17

Discover more Topics under Mechanical Engineering

Q121.
The operation of the reciprocating air motor is similar to reciprocating air compressor.
Discuss
Answer: (b).False
Q122.
In axial flow compressors, the flow of air is parallel to the axis of compressor.
Discuss
Answer: (a).Correct
Q123.
The ratio of the isothermal power to the shaft power or brake power of the motor or engine required to drive the compressor is called overall isothermal efficiency.
Discuss
Answer: (a).True
Discuss
Answer: (c).in a single cylinder on both sides of the piston
Q125.
The basic principle of the rocket propulsion is the same as that of jet propulsion.
Discuss
Answer: (a).Yes
Q126.
In a centrifugal compressor, the flow of air is __________ to the axis of compressor.
Discuss
Answer: (b).perpendicular
Q127.
The volume of air delivered in a medium capacity air compressor per unit time is
Discuss
Answer: (b).0.15 to 5 m³/s
Q128.
In a closed cycle gas turbine, the air is compressed
Discuss
Answer: (c).isentropically
Q129.
In a single stage, single acting reciprocating air compressor, without clearance volume, the workdone is minimum during
Discuss
Answer: (a).isothermal compression
Q130.
A simple turbo-jet engine is basically a gas turbine engine equipped with a propulsive nozzle and diffuser.
Discuss
Answer: (a).Agree