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1.5 kg of gas flows through gas turbine unit from its initial pressure and temperature 600 kN/m2 and 1300 K respectively and exhausts at a pressure of 102 kN/m2
thermodynamics updated 3.2 years ago by teamques10 ★ 69k
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advance thermodynamics mechanical engineering technology
thermodynamics updated 3.0 years ago by RakeshBhuse • 3.2k
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Determine the cycle efficiency and work ratio for vapour power cycle
thermodynamics updated 2.9 years ago by teamques10 ★ 69k
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