My Report

Steam and Gas Turbines Practice 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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1. When airfoil shape moves through fluid it produces __________

2. Convergent divergent nozzles used in rocket engines have _________ area ratio.

3. When divergent section is added _________

4. ______________ is commonly called as carry over velocity.

5. Unit of flow resistance is _________

6. If mach number is less than one then its flow is ______________

7. Pressure loss occurs in nozzle due to __________

8. Over expansion occurs when exit area of nozzle is _________ than primary nozzle.

9. Corrosion and Erosion takes place if dryness factor of steam is __________ in last stage.

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


 

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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