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Steam and Gas Turbines Mock Test 3


Correct Answer: 2 points | Wrong: -1 point
Grades: A* (100% score) | A (80%-99%) | B (60%-80%) | C (40%-60%) | D (0%-40%)
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 10%

Question 1 of 10

1. In pressure compounded turbines flow passage is from ______________

Question 1 of 10

Question 2 of 10

2. Heavy frame engines are physically ___________

Question 2 of 10

Question 3 of 10

3. Jet engines can be accelerated to supersonic velocities with _______ section.

Question 3 of 10

Question 4 of 10

4. Coefficient of discharge is _____________

Question 4 of 10

Question 5 of 10

5. Convergent nozzles are used in jet engines upto nozzle pressure ratio of _______

Question 5 of 10

Question 6 of 10

6. For radial equilibrium constant velocity is assumed.

Question 6 of 10

Question 7 of 10

7. Coefficient of discharge of Nozzle is _______

Question 7 of 10

Question 8 of 10

8. If heat is added to the wet steam temperature _________

Question 8 of 10

Question 9 of 10

9. Pressure ratios below 20 are used in _____________ engines.

Question 9 of 10

Question 10 of 10

10. Aeroderivative engines have pressure ratios ___________

Question 10 of 10


 

Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

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