Fundamentals Of Engineering Thermodynamics
9th Edition
ISBN: 9781119391388
Author: MORAN, Michael J., SHAPIRO, Howard N., Boettner, Daisie D., Bailey, Margaret B.
Publisher: Wiley,
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On the diagram below sketch a basic Rankine cycle with superheating. Assume that
there are irrevesibilities in the turbine and pump. Identify the device associate with each
process. Make sure to label: the states and include important features, e.g. lines of constant
temperature, volume, pressure, entropy, vapor dome, etc.
Explain how to improve the thermal efficiency of Rankine cycle without changing the main component in the cycle?Give some examples and state your assumption.
SIMPLE NON-IDEAL BRAYTON CYCLE GAS TURBINE: Use Cold-Air Standard Analysis
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- SIMPLE NON-IDEAL BRAYTON CYCLE GAS TURBINE: Use Cold-Air Standard Analysis Show complete solution and explain briefly.arrow_forwardFind the efficiency of Brayton cycle with, (a) Pressure ratio = 6 (b) Pressure ratio = 8 (c) Pressure ratio = 12 What can you observe?arrow_forwardProve that there is an increase in efficiency between a Simple Rankine Cycle and a Reheat Rankine Cycle. What is worth using for considering the efficiency?arrow_forward
- Consider an ideal gas-turbine cycle with the following details in Table 1. Table 1 No. of stages at compression No. of stages at expansion 2 2 Pressure ratio 3 T of air at compressor inlet T of air at turbine inlet 300 K 1200 K Analyse the back work ratio and compare the thermal efficiency of the cycle for these two cases: i. no regenerator is used ii. a regenerator is used with 75 percent effectivenessarrow_forward(b) Derive an expression for thermal efficiency of ideal Brayton cyclearrow_forwardExample-1 A Brayton cycle operates with air entering the compressor at 100 kPa, 25 °C, a pressure ratio of 6, and a turbine inlet temperature of 800 °C. Determine the compressor work input, the turbine work, the work ratio, the heat rejection and the cycle thermal efficiency for equal turbine and compressor efficiency of 100%; 80%; 70%; and 60%. Tarrow_forward
- Prove that there is an increase in efficiency between a Simple Rankine Cycle and a Reheat Rankine Cycle. What is worth using for?arrow_forwardWrite the expression for efficiency of a Rankine cycle in terms of Wturb, Wpump, Qin, Qout, and enthalpies. Thermodynamics question briefly explanation pleasearrow_forwardFor the given question determine optimum velocity of steam, asaparrow_forward
- Air enters the compressor of a gas turbine at 100 kPa and 25°C. pressure ratio 5 and For a maximum temperature of 850°C, the back work rate and thermal efficiency of the Brayton cycle Please specify.arrow_forwardA turbine receives steam at 10 MPa, 6000C and exhaust it at 0.2 MPa. (a) for the ideal Rankine engine, determine the work, steam rate, thermal efficiency, and means effective pressure. (b) for the actual engine,the brake engine efficiency is 84%; the driven generator efficiency is 93% and the rated output of the generator is 30 MW. Estimate the enthalpy ang quality (or temperature) of the exhaust..Compute the combined work, combined heat rate, and the total throttle flow for the rated power. Don't answer the given problem, just give me the schematic diagram andT-S diagram of the given problemarrow_forwardProvide the given, manual step by step solution, and diagram. A Carnot cycle has an efficiency of 60 %. The heat added is 1000 KJ.What is the heat rejected from the cycle?arrow_forward
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