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Category > Applied Sciences Posted 21 May 2017 My Price 4.00

Consider an ideal gas-turbine cycle with a pressure ratio

Consider an ideal gas-turbine cycle with a pressure ratio across the compressor of 12:1. The compressor inlet is at 300 K, 100 kPa, and the cycle has a maximum temperature of 1600 K. An ideal regenerator is also incorporated into the cycle. Find the thermal efficiency of the cycle using cold air (298 K) properties.

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Alpha Geek
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Status NEW Posted 21 May 2017 01:05 PM My Price 4.00

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