Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion.The pressure ratio across
Posted: Sat Feb 19, 2022 3:31 pm
Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion.The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stageof the compressor at 300 K and each stage of the turbine at 1600 K. Determine the back work ratioand the thermal efficiency of the cycle, assuming a regenerator with 82 percent effectiveness isused.USE CONSTANT SPECIFC HEAT!!!!!and sketch T-S Diagram
Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion.
The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stage
of the compressor at 300 K and each stage of the turbine at 1600 K. Determine the back work ratio
and the thermal efficiency of the cycle, assuming a regenerator with 82 percent effectiveness is
used.
USE CONSTANT SPECIFC HEAT!!!!!
and sketch T-S Diagram
Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion. The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stage of the compressor at 300 K and each stage of the turbine at 1600 K. Determine the back work ratio and the thermal efficiency of the cycle, assuming a regenerator with 82 percent effectiveness is used.
Consider an ideal gas-turbine cycle with two stages of compression and two stages of expansion.
The pressure ratio across each stage of the compressor and turbine is 3. The air enters each stage
of the compressor at 300 K and each stage of the turbine at 1600 K. Determine the back work ratio
and the thermal efficiency of the cycle, assuming a regenerator with 82 percent effectiveness is
used.
USE CONSTANT SPECIFC HEAT!!!!!
and sketch T-S Diagram
- Consider An Ideal Gas Turbine Cycle With Two Stages Of Compression And Two Stages Of Expansion The Pressure Ratio Across 1 (18.11 KiB) Viewed 51 times