Consider the tube and inlet conditions of Problem 1.36. Heat transfer at a rate of
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- Pressurized water (pin = 10 bar, Tin =110◦C) enters the bottom of an L = 12m long vertical tube of diameter D = 110 mm at a mass flow rate of m =1.5kg/s . The tube is located inside a combustion chamber, resulting in heat transfer to the tube. Superheated steam exits the top of the tube at pout = 7 bar, Tout = 600◦C. Determine the change in the rate at which the following quantities enter and exit the tube: (a) the combined thermal and flow work, (b) the mechanical energy, and (c) the total energy of the water. Also, (d) determine the heat transfer rate, Q˙. Hint: Relevant properties may be obtained from a thermodynamics text.arrow_forwardApply the first law of thermodynamics to flow system with two inlets and one outlet. Assume that heat is supplied to the system. Draw the neat sketch and lable inlet and outlet propertiesarrow_forwardI solved most of this but need some guidence towards the end after you have m flow rate and both h_2 and h_1.arrow_forward
- During the experiment at time 1:40 min, manometer reading is 5 bar and power consumption at ammeter is 3.3 A. Calculate the work done at that particular time and outlet temperature. Ambient condition: 1 bar and 20 °C Equation for the work done, i.e. output work: n n-1 RT. (S W12 = n- 1 n-1 P. T, = T, Given: Polytropic coefficient: n = 1.3 Ideal gas constant: R = 287 kg K %3D kg Density of air at 20°C: p = 1.2041 Volume flow rate: V = 115 L min Motor Voltage: 230 V at 50 Hz What is the inlet temperature in K and the inlet pressure in bar? What is the outlet temperature at time 1:40 min? At time 1:40 min, how much work is done by the piston? What is the input power at time 1.40 min?arrow_forwardFor an inlet valve, the mass flow rate through the valve is 0.44 kg/s. The flow coefficient is 0.62 and the cylinder pressure is 105 kPa. Assume intake system pressure and temperature are 180 kPa and 527 K, the specific heat ratio is 1.3 and R =287 J / kg.K. The area of the valve is (SI unit): Select one: a. 2.30*10-3 O b. 3.45*10-2 O c. 1.43*10-3 O d. 1.75*10-3 O e. 0.85*10-2arrow_forward3. In a refinery, certain oil with sp.gr 0.9 flows with a velocity of 2 m/s in a pipe of diameter 30cm. Along the flow, the pipe diameter gets reduced to 25 cm. Determine the velocity and mass flow rate of oil at this section. 4. A circular pipe of uniform diameter 500mm carries water under pressure 30 N/cm2 . The mean velocity of water at the inlet (at the datum) is 2.0 m/s. Find the total head or total energy per unit weight of the water at a cross-section, which is 5 m above the datum line. 5. A tapered pipe, through which water is flowing, is having diameter, 30cm and 20 cm at the cross-sections 1 and 2 respectively. The velocity of water at section 1 is given as 3.5m/s. Find the velocity head at section 1 and 2 and also rate of discharge. 6. Water is flowing through a pipe having diameter 300mm and 200 mm at the bottom and upper end respectively. The pressure at the lower(bigger) end is 25 N/cm2 and the pressure at the upper end is 10 N/cm2. Determine the difference in datum…arrow_forward
- Nitrogen gas flows through a compressor and a heat exchanger as shown in the figure below. All the provided properties at the inlets and outlets of both devices are shown. Nitrogen is modeled as an ideal gas. A separate cooling stream of Helium, also modeled as ideal gas, flows through the heat exchanger to lower the temperature of nitrogen. Assume that both devices are perfectly insulated and both gasses have constant specific heat values: Cpo of nitrogen = 1.042 kJ/kg. K) and Cpo of helium = 5.193 kJ/kg.K) A. Identify the systems, the process that each system goes through, and the assumptions you need to make for each process. B. Find the temperature of nitrogen at the exit of the compressor (T2) C. Determine the mass flow rate of the helium. 50 kW Compressor N₂ P₁ = 100 kPa T₁ = 280 K m₁ = 0.25 kg/s T₁ = 175°C +5 Helium 4+T4= 4+T4=25°C www www. T3 = 350 K Heat exchangerarrow_forwardpls show complete solutionarrow_forwardConsider the same problem in which an axial compressor with a mean diameter of 0.8 m is being designed to run at 3000 rpm. The whirl velocities at the inlet and outlet are 5m/s and 30 m/s, respectively. The air mass flow rate through the compressor is 2 kg/s at a temperature of 27 °C. Assume C, of air equal to 1000 J/kg-K and Cy = 718 J/kg-K. %3D The temperature change is equal to O 3.14 K 5.28 K 7.42 K OOKarrow_forward
- A nozzle is a device for increasing the velocity of a steadily flowing stream of fluid. At the inlet to a certain nozzle the enthalpy of the fluid is 3025 kJ/kg and the velocity is 60 m/s. At the exit from the nozzle the enthalpy is 2790 kJ/kg. The nozzle is horizontal and there is negligible heat loss from it. (i) Find the velocity at the nozzle exit. (ii) If the inlet area is 0.1 m2 and specific volume at inlet is 0.19 m3/kg, find the rate of flow of fluid (iii) If the specific volume at the nozzle exit is 0.5 m3/kg, find the exit area of the nozzle.arrow_forwardAutomobile air-conditioner gives up 18 kW at 65 km/h if the outside temperature is 35°C. The refrigerant temperature is constant at 65°C under these conditions, and the air rises 6°C in temperature as it flows across the heat exchanger tubes. The heat exchanger is of the finned-tube type shown in Fig. 3.6b, with U? 200 W/m°K. If U? (Air velocity) 0.7 and the mass flow rate increases directly with the velocity, plot the percentage reduction of heat transfer in the condenser as a function of air velocity between 15 and 65 km/h. b. A section of an automotive air condition- tall wavy fins is allowed to mix with itself while unmixedarrow_forwardIn a reaction turbine, the drum diameter is 2.15 m, speed of turbine is 750 rev/min and the steam flow is 14.2 kg/sec. At a particular ring of blades, the blade height is 15.875 cm and the discharge angle (α & ϕ) is 25°. Here, the pressure of steam is 0.04 N/mm2 abs, and its dryness fraction is 0.97. Determine the following: 1.Heat drop, in kJ, through this turbine pair, assuming turbine efficiency of 80% a. 141.6 b. 77.14 c. 12.47 d. 22.89 e. 42.02arrow_forward
- Principles of Heat Transfer (Activate Learning wi...Mechanical EngineeringISBN:9781305387102Author:Kreith, Frank; Manglik, Raj M.Publisher:Cengage Learning