FUND OF ENG THERMODYN(LLF)+WILEYPLUS
9th Edition
ISBN: 9781119391777
Author: MORAN
Publisher: WILEY
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Consider an ideal Brayton cycle of air where the pressure ratio ñ across the compressor is equal to
5 and the air temperature at the turbine inlet is 900 °C. If the pressure and temperature of the air
ambient are equal to 1 bar and 40 °C, respectively
a) Determine the pressure, temperature and specific volume in the different states of the cycle.
b) Calculate the work per unit mass developed by the turbine.
e) Determine the work per unit mass required by the compressor.
d) Calculate the net work per unit mass developed by the gas turbine.
e) Determine the thermal efficiency of the cycle.
The temperature at the beginning of a compression process of an air standard Otto cycle with acompression ratio of 8 is 300 K, the pressure is 1 bar and the cylinder volume is 560 cm3. Themaximum temperature during the cycle is 2000 K. Determine a) the temperature, pressure andvolume at the end of each process of the cycle, tabulating your answers, b) the thermal efficiencyof the cycle, and c) the mean effective pressure, in Bar. Take γ = 1.4, and cv = 718 J/kg/K
7.42. Jets of high-speed steam are used in spray cleaning. Steam at 15.0 bar with 150°C of superheat is fed to
a well-insulated valve at a rate of 1.00 kg/s. As the steam passes through the valve, its pressure drops to
1.0 bar. The outlet stream may be totally vapor or a mixture of vapor and liquid. Kinetic and potential
energy changes may be neglected.
(a) Draw and label a flowchart, assuming that both liquid and vapor emerge from the valve.
(b) Write an energy balance and use it to determine the total rate of flow of enthalpy in the outlet stream
(Hout = mH¡ + m,Ĥv). Then determine whether the outlet stream is in fact a mixture of liquid and
vapor or whether it is pure vapor. Explain your reasoning.
Problems 393
(c) What is the temperature of the outlet stream?
(d) Assuming that your answers to Parts (b) and (c) are correct and that the pipes at the inlet and outlet
of the valve have the same inner diameter, would AĖk across the valve be positive, negative, or
zero? Explain your…
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- = The owner of a propose steam power plant received bids from two fuel supplier. The first supplier offers coal whose ultimate analysis is: C = 71.5%, H = 5%, 0 = 7%, S = 3.6%, N = 1.3%, A = 8.2%, and M 3.4%. The other supplier offers natural gas whose HHV is 52.2MJ/kg and whose volumetric analysis is: 60% CH4, 30%C2H6, and 10%CO. Excess air for both cases is 20%. Other data for the power plant are: net output = 100MW, heat added at the boiler = 90% of energy chargeable, specific enthalpy in kJ/kg: turbine inlet = 3582.3, turbine outlet = 2251.881, pump inlet = 289.23, boiler inlet = 304.534. Atmospheric air temperature is 35C. Find possible steam consumption of this propose plant in kg/s.arrow_forward1. In less than 100 words, describe how the reciprocating air compressors (applicable to a particular purpose) can be improved in terms of sustainability in terms of energy use and pollution effect. 2. Cost implications or projections data/calculations from the idea(s)arrow_forward(a) Answer these questions: ii. iii. i. State three (3) variables or parameters which remain unchanged over time in a steady flow system. State the main purpose for a compressor and a turbine. Write down the mass balance equation for a single-stream (one-inlet and one-outlet) steady-flow device in terms of density, area and velocity.arrow_forward
- a (a) Air in (b) (c) Diffuser Compressor Combustors 2 State State 1 80 State 2 3300 State 3 3200 State 4 400 State 5 80 wwww Pressure (kPa) 3 Turbine 4 Figure 1: Figure for Problem 2. In a modern jet engine, air passes through the following states from the inlet to the outlet, as shown in Figure 1: Product gases out 260 780 1500 900 640 K 5 > Nozzle justify them) to find the compressor specific work. Temperature (K) For this problem, you may neglect any heat transfer, as well as neglect kinetic energy except at the outlet (state 5). Use the tables for obtaining properties (do not assume constant specific heat). Assume air is an ideal gas with ideal gas constant of R = 0.287 kJ/kg-K. Use the appropriate conservation equations and make approximations (and In a similar manner, find the turbine specific work. And finally, using similar arguments, find the nozzle exit velocity.arrow_forwardThere are two turbine stages with a reheater in between, as shown below and the following conditions are provided. Assume the mass flow rate of air = 1 Kg/s. Turbine stage 1 Stream 1 2 3 4 Reheat combustor P (kPa) T (K) 1200 350 350 100 1200 1200 3 Turbine stage 2 h (kJ/kg) W cycle • Determine the total work developed, which is the sum of the work developed by the first stage and the work developed in the second stage. • Determine the heat added in the reheater. • If the reheat is turned off, streams 2 and 3 no longer exist and we go directly from 1 to a new state at stream 4. What is h4 and what is the work generated in the turbine in this case?arrow_forward10) a turbine operating under steady flow conditions receives 4500 lg of steam per hour. The steam enters the turbine at a velocity of 2800m/min, an elevation of 5.5 m and a specific enthalpy of 2800 kj/kg. It leaves the turbine at a velocity of 5600 m/min, an elevation of 1.5 m and a specific enthalpy of 2300 KJ/kg. heat losses from the turbine to the surroundings amount to 16000 KJ/hr. Determine the output power of the turbine.arrow_forward
- * Your answer is incorrect. A pump is used to circulate hot water in a home heating system. Water enters the well-insulated pump operating at steady state at a rate of 0.42 gal/min. The inlet pressure and temperature are 14.7 lbf/in.², and 180°F, respectively; at the exit the pressure is 90 lbf/in.² The pump requires 1/15 hp of power input. Water can be modeled as an incompressible substance with constant density of 60.58 lb/ft3 and constant specific heat of 1 Btu/lb. °R. Neglecting kinetic and potential energy effects, determine the temperature change, in °R, as the water flows through the pump. ΔΤ : = i 0.36 °Rarrow_forwardNumber 6arrow_forwardSolve the question given in the image attached below Note question is taken from power plant coursearrow_forward
- QUESTION 3 (Analysis of steam cycles) A steam power plant operates on a theoretical reheat cycle. Steam at boiler at 140 bar, 500°C expands through the high-pressure turbine. It is reheated at a constant pressure of 40 bar to 500°C and expands through the low-pressure turbine to a condenser at 0.1 bar. 3.1 Draw T-s and h-s diagramsarrow_forwardPLEASE ANSWER WITH COMPLETE SOLUTION AND DIAGRAM.arrow_forwardAir enters the compressor of a gas turbine at a pressure of 100 kPa and a temperature of 300 K, where it is compressed to a temperature of 680 K. The pressure ratio of the cycle is 8. Before entering the turbine, there is a heat transfer of 950 kJ/kg to the air. Since the turbine's isentropic efficiency is 84 percent,a) Show the cycle in the T-s diagram.b) The ratio of the work required to operate the compressor to the work obtained from the turbine.c) Calculate the thermal efficiency.(Ignore the variation of specific heats for air with temperature)arrow_forward
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