Which is correct?    The pressure ratio of a gas turbine engine compressor is: - equal to the number of compression stages - the ratio between compressor outlet and compressor inlet pressure - the ratio between exhaust inlet and exhaust outlet pressure - never greater than 5 to 1

Refrigeration and Air Conditioning Technology (MindTap Course List)
8th Edition
ISBN:9781305578296
Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Chapter45: Domestic Refrigerators And Freezers
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Which is correct? 
 
The pressure ratio of a gas turbine engine compressor is:

- equal to the number of compression stages
- the ratio between compressor outlet and compressor inlet pressure
- the ratio between exhaust inlet and exhaust outlet pressure
- never greater than 5 to 1
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