Mechanical Engineering - Heat Transfer, Refrigeration and Air Conditioning - Discussion

Discussion Forum : Heat Transfer, Refrigeration and Air Conditioning - Section 5 (Q.No. 21)

Heat Transfer, Refrigeration and Air Conditioning

21.

The cooling system used for supersonic aircrafts and rockets is

simple air cooling system

boot-strap air cooling system

reduced ambient air cooling system

regenerative air cooling system

Answer: Option

Explanation:

No answer description is available. Let's discuss.

Discussion:

2 comments Page 1 of 1.

Mahakal said: 2 years ago

I think option C is correct.

Nikhil said: 4 years ago

But according to nptel reduced ambient air system is used for supersonic aircraft and rockets so option C should be right.

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