Prepare
Practice
Interview
Aptitude
Reasoning
English
GD
Placement papers
HR
Current affairs
Engineering
MCA
MBA
Online test
Login
Shapes of blade passages in compressors
Home
>>
Category
>>
Mechanical Engineering (MCQ) questions and answers
>>
Turbo Machines
Q. The blade passages in a compressor are ________
- Published on 16 Sep 15
a.
converging
b.
diverging
c.
constant
d.
unpredictable
ANSWER: diverging
Related Content
Fluid Mechanics (
75
)
Manufacturing Processes - 1 (
75
)
Manufacturing Processes - 2 (
65
)
Material Science (
70
)
Theory of Machines - 1 (
60
)
Metrology and Quality Control (
151
)
Theory of Machines - 2 (
75
)
Heat Transfer (
271
)
Hydraulics & Pneumatics (
228
)
Thermodynamics (
388
)
Basic Mechanical Engineering (
91
)
Dynamics of Machinery (
92
)
Engineering Metallurgy (
61
)
Design of Machine Elements - 1 (
81
)
Mechatronics (
60
)
Turbo Machines (
70
)
Mechanical System Design (
73
)
Engineering Mechanics (
103
)
Strength of Materials (
110
)
Design of Machine Elements - 2 (
69
)
Discussion
Pankaj
-Posted on 16 Oct 15
Generally, an axial flow compressor is similar in appearance to an axial flow reaction turbine. But there are some differences between both of them.
If we consider the rotor blades of axial flow compressor and axial flow reaction turbine, it is noticeable that the section of compressor blades are of airfoil section and the area of passages through the blades are different.
In axial flow reaction turbine, the flow of working fluid is accelerating. Therefore, the blade passages are converging.
Whereas in axial flow compressor, the flow of working fluid is diffusing or decelerating.
Therefore, the blade passages in compressor are diverging.
➨
Post your comment / Share knowledge
Required!
Required!
Invalid Email Id!
Required!
Enter the code shown above:
Please enter the code shown above
(Note: If you cannot read the numbers in the above image, reload the page to generate a new one.)
MCQs
English
Tutorials
Download
▲