Pressurized water
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- Q (16)A constant area combustion chamber is supplied by air at 223k and 70kpa the air stream velocity is 130 m/s. Determine (M₁, To2, T2, P2) if heat of 140 Kw/Kg is added in the combustion process and the chamber handles the maximum possible amount of air see figure: (2) Combustion chamber Q=140 KWarrow_forwardحالة إكمال الأسئلة The power output of an adiabatic steam turbine is 4.5 MW, and the inlet and outlet conditions of the steam are given below. Perform the following calculations a) Calculate Ah, Ake, Ape (in kJ/kg) and the mass flow rate of the steam in kg/s Outlet parameters Inlet parameters P2 = 10 kPa P1 = 2.5 MPa T1 = 450 °C V1 = 53 m/s X2 = 83% V2 = 183 m/s z2 = 4.5 m 21 = 8.5 m g = 9.81 m/s2 Steam * 44 F5 F1 PrtSc F10 4t3 3 4. 01 7 V. 8 9. %D Y U P : A S GYH 1. L. 13 C V BYNIM Alt 3e Alf Crl 11 V n JU DIarrow_forwardA steam turbine is operated under the following steam conditions:a. Steam in: P1 = 10 atm (abs) ; and T1 = 200oCb. Steam out: P2 = 0.8 atm (abs) ; and T2 = 105oCCalculate TSR, ASR and estimate this type of steam turbine!arrow_forward
- A heat exchanger, shown below, is used to cool an air flow from 550 K to 250 K, both states at 1 MPa. The coolant is a water flow at 30 °C, 0.1 MPa. If the water leaves as saturated vapor, 0.1 MPa. 1 air 3 water The initial state enthalpy for air (h;(kJ/kg)) is equal to: The final state enthalpy for air (h2(kJ/kg)) is equal to: The initial state enthalpy for water (h3(kJ/kg)) is equal to: The final state enthalpy for water (ha(kJ/kg)) is equal to: Mµ20/Mair| The ratio of the flow ratesarrow_forward(a) An Ocean Thermal Energy Converter (OTEC) pumps 200 m^3/s through a heat exchanger in which the temperature (expressed in Kelvins) drops by 1%. All the heat extracted is delivered to the ammonia boiler [11. The ammonia temperature. THT at turbine inlet is equal to the mean temperature of the water in the warm water heat exchanger minus 1 °K. The temperature, TCT, of the ammonia leaving the turbine is kept at 10 °C by the cooling effect of 250 m³/s of cold water. The efficiency of turbine/generator system is 90% of the Carnot efficiency of a heat engine working between THT and TCT . 12 MW of the produced electricity is used for pumping. Heat capacity of water is 4.2 MJ m³ K-1. Calculate the intake temperature of the warm water for the following cases: i) A total of 20 MW of electricity is available for sale? ii) The OTEC produces exactly equal to the amount of power needed for pumping?arrow_forwardREFERENCE: FROM BOOK - ENGINEERING THERMOFLUIDS, M. MASSOUDarrow_forward
- Please use Book: Introduction to Chemical Engineering Thermodynamics 8 edition, 2018 (Smith, J.M., Van Ness, H.C., Abbot, M.M., Swihart.)arrow_forwardQuestion 20 Separate streams of steam and air flow through the turbine and heat exchanger arrangement shown in the figure below, where mass flow rate m5 is 2000 kg/min and power output Wt1 is 12,000 kW. Steady-state operating data are provided on the figure. Heat transfer with the surroundings can be neglected, as can all kinetic and potential energy effects. m5 Steam in Turbine T₁ = 600°C P₁ = 20 bar Determine: (a) T3, in K. W₁l T₂ = 400°C P2= 10 bar > 6 VT6 = 1200 K P6 = 1 bar kW P3= 10 bar T3=? www tw Heat exchanger Turbine 2 Air in (b) the power output of the second turbine, in kW. W₁2=? T5 = 1500 K -5 P5= 1.35 bar m5 T₁ = 240°C P4 = 1 bararrow_forward2. Two gaseous streams enter a combined tube in a steady flow manner and leave as a single mixture Gas A at Tube A Gas B at Tube B A= 400 cm? V= 150 m/s V=0.6 m³/kg A= 250 cm? m= 455kg/min p= 2kg/m³. Data at exit: V= 100 m/s v=0.55 m/kg Find the following: a. Speed of gas at tube B b. Mass flow rate at exitparrow_forward
- I need help with some review problemsfor thermo! thank you Air at 100 kPa and 280K is compressed steadily to 600 kPa and 400K in an air compressor. The mass flow rate of air through the compressor is 0.02 kg/s and the compressor a heat loss of 16 kJ/kg from the compressor occurs. Assuming steady state steady flow conditions and ideal gas behavior (with constant specific heats, Cp=1.009 kJ/kgK, R=0.287 kJ/kgK, determine: a)The necessary power input to the compressor (kW).b)The volumetric flow rate of air at the exit of the compressor (m3/s).arrow_forward#2 Separate streams of steam and air flow through the turbine and heat exchanger arrangement shown in the figure below, where the air stream mass rate m'5 ranges from 1500 kg/min to 3500 kg/min in increments of 500 kg/min and Wt1= 10,000 kW,. Steady-state operating data are provided on the figure. Heat transfer with the surroundings can be neglected, as can all kinetic and potential energy effects. Steam in 1500 kg/min 2000 kg/min 2500 kg/min Mass Rate of Air M5 in kg/min 3000 kg/min 3500 kg/min Turbine T₁ = 600°C P₁ = 20 bar W₁ T3 T₂=400°C P2 10 bar Temperature T6 = 1200 K P6 = 1 bar tmt tm Heat exchanger TWO TURBINE PROBLEM Py = 10 bar T3 = ? Analyze the two-compressor system for different air mass flow rates into the heat exchanger. Provide clearly detailed professional written sample of the calculations needed to analyze each component of the system and the overall system. Complete the following table and plot the mass of air M5 against the Temperate T3, plot the mass rate M5…arrow_forwardmnot Tnot = 75°C Tout-? %3D mcold Tcod = 18°C %3D Hot and cold stream of water are mixing together as shown in Figure. The temperature of the hot and cold streams at the inlet are 75 deg-C and 18 deg-C, respectively. Mass flow rates of the hot and the cold streams are (1.50x10^-1) kg and (1.000x10^-1) kg, respectively. Find the temperature of the mixed stream. The specific heat of the hot water stream is 4000 J/kg-K and the cold stream is 3800 J/kg-K. Note: Your answer is assumed to be reduced to the highest power possible. Your Answer: х10 Answerarrow_forward
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