CuriousTab
Search
CuriousTab
Home
Aptitude
Computer
C Programming
C# Programming
C++ Programming
Database
Java Programming
Networking
Engineering
Biochemical Engineering
Biochemistry
Biotechnology
Chemical Engineering
Civil Engineering
Computer Science
Digital Electronics
Electrical Engineering
Electronics
Electronics and Communication Engineering
Mechanical Engineering
Microbiology
Technical Drawing
GK
Current Affairs
General Knowledge
Reasoning
Data Interpretation
Logical Reasoning
Non Verbal Reasoning
Verbal Ability
Verbal Reasoning
Exams
AIEEE
Bank Exams
CAT
GATE
IIT JEE
TOEFL
Jobs
Analyst
Bank PO
Database Administrator
IT Trainer
Network Engineer
Project Manager
Software Architect
Discussion
Home
‣
Mechanical Engineering
‣
Compressors, Gas Dynamics and Gas Turbines
Comments
Question
The compression ratio for the compressor is always __________ unity.
Options
A. equal to
B. less than
C. more than
Correct Answer
more than
Compressors, Gas Dynamics and Gas Turbines problems
Search Results
1. Slip factor in a centrifugal compressor indicates the amount of air leaked from the storage vessel.
Options
A. Yes
B. No
Show Answer
Scratch Pad
Discuss
Correct Answer: No
2. A 3 m
3
/min compressor means that it
Options
A. compresses 3 m
3
/min of standard air
B. compresses 3 m
3
/ min of free air
C. delivers 3 m
3
/ min of compressed air
D. delivers 3 m
3
/ min of compressed air at delivery pressure
Show Answer
Scratch Pad
Discuss
Correct Answer: compresses 3 m
3
/ min of free air
3. The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is
Options
A. pressure drop across the valves
B. superheating in compressor
C. clearance volume and leakages
D. all of these
Show Answer
Scratch Pad
Discuss
Correct Answer: all of these
4. In a closed cycle gas turbine, the air is compressed
Options
A. isothermally
B. polytropically
C. isentropically
D. none of these
Show Answer
Scratch Pad
Discuss
Correct Answer: isentropically
5. For minimum work in multi-stage compression, the workdone on all stages should be equal.
Options
A. Yes
B. No
Show Answer
Scratch Pad
Discuss
Correct Answer: Yes
6. The thrust of a jet propulsion power unit can be increased by
Options
A. injecting water into the compressor
B. burning fuel after gas turbine
C. injecting ammonia into the combustion chamber
D. all of the above
Show Answer
Scratch Pad
Discuss
Correct Answer: all of the above
7. With the decrease in compression ratio, the volumetric efficiency
Options
A. does not change
B. increases
C. decreases
Show Answer
Scratch Pad
Discuss
Correct Answer: increases
8. The overall isothermal efficiency of the compressor is defined as the ratio of
Options
A. work required to compress the air isothermally to the actual work required to compress the air for the same pressure ratio
B. isothermal power to the shaft power or B.P. of the motor or engine required to drive the compressor
C. volume of free air delivery per stroke to the swept volume of the piston
D. isentropic power to the power required to drive the compressor
Show Answer
Scratch Pad
Discuss
Correct Answer: isothermal power to the shaft power or B.P. of the motor or engine required to drive the compressor
9. In a single stage, single acting reciprocating air compressor, without clearance volume, the workdone is minimum during
Options
A. isothermal compression
B. isentropic compression
C. polytropic compression
D. none of these
Show Answer
Scratch Pad
Discuss
Correct Answer: isothermal compression
10. The volumetric efficiency of the compressor is defined as the ratio of volume of free air delivery per stroke to the swept volume of the piston.
Options
A. Yes
B. No
Show Answer
Scratch Pad
Discuss
Correct Answer: Yes
Comments
There are no comments.
Enter a new Comment
Save
More in Mechanical Engineering:
Automobile Engineering
Compressors, Gas Dynamics and Gas Turbines
Engineering Materials
Engineering Mechanics
Heat Transfer, Refrigeration and Air Conditioning
Hydraulic Machines
Hydraulics and Fluid Mechanics
IC Engines and Nuclear Power Plants
Industrial Engineering and Production Management
Machine Design
Production Engineering
Steam Boilers and Engines
Steam Nozzles and Turbines
Strength of Materials
Theory of machines
Thermodynamics
Workshop Technology