[2] Repeat Example 8.1 (pages 303-305) but with the following exceptions: steam fed to the turbine is at 9,000 kPa & 600 °C, the turbine exhaust is at 10 kPa, and for parts b & c the efficiencies are both 0.8.
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- In a nozzle, steam enters at T = 673.15 K and P = 800,000 Pa while u = 15m/s. It exits at T = 400,000 Pa and u = 320m/s. What is the ration of the inlet and outlet diameters (D1/D2)?can you please solve this for me, thanks. 10 kg/s of steam (H2O) enters a turbine at 10 m/s and a specific enthalpy of 3500 kJ/kg and leaves at an outlet 10m below the inlet with a specific enthalpy of 2500 kJ/kg and a velocity of 20 m/s. Assume steady-state steady-flow. If the heat lost from the turbine is 20% that of the turbine work, determine a.) the turbine horsepower. If the turbine is coupled to a generator with a 90% electrical efficiency, and the turbine horsepower has an 80% mechanical efficiency, b.) how much income will a power plant generate in one year if the electrical energy is sold at PhP 3.51 per kW-hr? (Hint: Mechanical efficiency = actual turbine work / ideal turbine work. Electrical efficiency of a generator = electrical output / actual turbine work.)(Use Mollier Chart, note: tolerance of temperature & enthalpy is∓1,pressure is ∓0.1, entropy is ∓0.01) Steam at a pressure of 3.5546 Mpa and temperature of 400 degree celsius.Locate the specificenthalpy and specific entropy.
- A single row impulse turbine develops 132.4 kW at a blade speed of 175 m/s, using 2 kg of steam per sec. Steam leaves the nozzle at 400 m/s. Velocity coefficient of the blades is 0.9. Steam leaves the turbine blades axially. Determine nozzle angle, blade angles at entry and exit, assuming no shock.A combustion chamber consists of combustion pipes with a diameter of 15 cm. Compressed air enters the pipes at 550 K, 480 kPa and 80 m/S (Figure 3). A fuel with a thermal value (ID) of 42000 kJ/kg is injected into the air and burned in such a way that the mass air-fuel ratio (HY) is 40. Considering the combustion event as a heat transfer to the air, at the exit of the combustion chambera) temperature,b) pressure,c) find the speed and Mach Number values. Note : k=1.4, cp=1.005 kJ/kg.K, R=0.287 kJ/kg.KExample 3.6Water is flowing in a pipe. At point 1 the inside diameter is 0.25 m and the velocity is 2 m/s.What are the mass flow rate and the volumetric flow rate? What is the velocity at point 2 wherethe inside diameter is 0.125 m?
- Steam enters a turbine at 600 ᵒC at 7300kPa pressure and leaves the turbine as saturated steam at 75 kPa.. Turbine inlet diameter is 50 mm and outlet diameter is 300 mm. In case the velocity at the turbine inlet is 200 m / sFind the turbine output power a) find the heat transfer, ignoring kinetic and potential energy changes. B) kineticsExplain by calculating whether the energy change is negligible.In a turbine 4500 kg/min of air expands polytropically from 425 kPa & 1360K to 101 kPa. The exponent n is equal to 1.45 for the process. Calculate the heat and work steady flow.HANDWRITTEN AND FINAL ANSWER MUST BE IN ENGLISH UNITS. Show solution. An experimental gas turbine engine is under development to increase its mechanical efficiency. It has a turbine efficiency of 95% and compressor efficiency of 85%. The following parameters are provided: P1 = 550 kPa, T1 = 25 deg C, rp = 5.5, T3 = 1450 deg C, Wnet = 5500 kW. Compute for the (a) flow rate and (b) mean effective pressure. Consider Ethane as your working fluid.
- A blade pair in an axial flow compressor is being designed. The axial flow component of gas velocity is 174m/s. The engine diameter at the mean blade height is 0.73m and the blade height at the rotor inlet is 0.21m. The rotor's absolute inlet flow angle is 26 degrees. The stagnation conditions at the inlet to the blade pair are 298K and 130kN/m² Using Cp 1.005k/kg/K, R-0.287k/kg/K, and taking the ratio of specific heat capacities as 1.4, calculate the engine mass flow rate to the nearest kg/sSuppose that a nuclear power plant is located on the banks of a major river that is 95 m wide near the plant, an average of 5 m deep, and that flows at a rate of 1.5 m / s. Suppose that we re-route all of this water into the plant and distribute the plant’s waste heat (1940 MJ) evenly throughout the water before returning it to the river bed. How much warmer is the river downstream of the plant compared to upstream? The temperature difference ΔTΔT is ___ K.Provide complete solution and detailed diagram. Steam at 4 Mpa and 300oC enters a turbine and expands isentropically to 100 Kpa. Find theturbine work. At 4 Mpa and 300oC: h = 2960.7, s = 6.3615 At 0.10 Mpa: sf = 1.3026, sfg =6.0568, hf = 417.46, hfg = 2258 A. 234.56 KJ/kg B. 657.26 KJ/kg C. 345.66 KJ/kg D. 543.45 KJ/kg