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Problem: 16 Air at 60 F flows from a large tank through a convergent nozzle, which...
30 points Air flows from a tank through a nozzle and it is discharged into a...
30 points Air flows from a tank through a nozzle and it is discharged into a standard atmosphere, as shown in the Figure. A normal shock stands in the exit of the nozzle, with an area of Ae-12cm2 and an Mach number of Me-2 just before the normal shock. Air velocity is neglected in the large tank with an air temperature of 100°C. Determine: 3. a) b) The area and the temperature at the throat The pressure before the normal...
Air in a large storage tank is 91 psia and 60°F is flowing isentropically through the...
Air in a large storage tank is 91 psia and 60°F is flowing isentropically through the duct shown below to the atmosphere. The pressure, psia, in the duct throat is most nearly Po = 91 psia مها : 7 Pater Hint: Assume the flow is choked, then the fluid speed in the throat is equal to the speed of sound and the pressure in the throat is equal to the critical pressure p
g through a nozzle. The inlet pressure is p 3.7 kPa (gage) air flowing and the air exhausts into the atmosphere. The...
g through a nozzle. The inlet pressure is p 3.7 kPa (gage) air flowing and the air exhausts into the atmosphere. The nozzle has an inlet diameter of 60 mm and an exit diameter of 10 mm, and the nozzle is connected to the supply pipe by flanges. Find the force required to hold the nozzle stationary. Assume the air has a constant density of 1.22 kg/m Neglect the weight of the nozzle. m Flanges Flow 2
g through a...
Water flows through the nozzle below and exits with a velocity of 60 ft/s. The flow...
Water flows through the nozzle below and exits with a velocity of 60 ft/s. The flow area is 0.3 ft2 at the flange and 0.1 ft2 at the exit. Find the total force in the bolts at the flange. (assume inviscid flow and Pa14.7 psia atmospheric pressure) 2. (assume inviscid flow and P atmospheric pressure) C.V. V. P2 Pa
Water is siphoned from a large tank and discharges into the atmosphere through a 2-in.-diameter tube...
Water is siphoned from a large tank and discharges into the
atmosphere through a 2-in.-diameter tube as shown in the figure
below. The end of the tube is 3 ft below the tank bottom, and
viscous effects are negligible. Determine the volume flowrate from
the tank. Determine the maximum height, H, over which the water can
be siphoned without cavitation occurring. Atmospheric pressure is
14.7 psia, and the water vapor pressure is 0.26 psia
MATLAB Program Problem D 0.02 m d 0.01 m 0 P1 3.0 kPa Air Review the tank diagram above. Air flow...
MATLAB Program Problem D 0.02 m d 0.01 m 0 P1 3.0 kPa Air Review the tank diagram above. Air flows steadily from a tank, through a hose of diameter D-0.02 m, and exits to the atmosphere from a nozzle of diameter d-0.01 m. The pressure in the tank remains constant at 3.0 KPa and the atmospheric conditions are standard temperature and pressure. Determine the flow rate at the exit and the pressure in the hose. File Submission Save your...
Water at 60 °F flows through the elbow as shown below and is then injected to...
Water at 60 °F flows through the elbow as shown below and is then injected to the atmosphere through a nozzle (on a horizontal plane). The pipe diameter is Di = 4 in. while the diameter of the exit of the nozzle is D2 = 1 in. At a flow rate of Q = 245 gpm, the gage pressure at the section (1) where the flange locates is Pi = 34 psig. Neglect the weight of the water and elbow,...
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m....
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m. Both the tank free surface and jet exit are exposed to the atmosphere. Take the density of water p = 1000 kg/m3, dynamic viscosity of water u = 0.001 kg/m.s, atmospheric pressure = 100 kPa, and gravity = 9.8 m/s2. Calculate the volumetric flow rate through the pipe. Neglect entrance losses to the pipe. Hint: Consider the inlet and outlet sections of the pipe...
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m....
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m. Both the tank free surface and jet exit are exposed to the atmosphere. Take the density of water p = 1000 kg/m3, dynamic viscosity of water j = 0.001 kg/m.s, atmospheric pressure = 100 kPa, and gravity = 9.8 m/s2. Calculate the volumetric flow rate through the pipe. Neglect entrance losses to the pipe. Hint: Consider the inlet and outlet sections of the pipe...
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a th...
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a throat diameter of 1 in. and an exit diameter of 1.75 in. (Figure 1) Determine the absolute pressure within the connected pipe, when the nozzle chokes and maintains isentropic supersonic flow within the divergent section of the nozzle. Express your answer to three significant figures and include the appropriate units P- psi Submit Incorrect; Try Again...
30 points Air flows from a tank through a nozzle and it is discharged into a standard atmosphere, as shown in the Figure. A normal shock stands in the exit of the nozzle, with an area of Ae-12cm2 and an Mach number of Me-2 just before the normal shock. Air velocity is neglected in the large tank with an air temperature of 100°C. Determine: 3. a) b) The area and the temperature at the throat The pressure before the normal...
Air in a large storage tank is 91 psia and 60°F is flowing isentropically through the duct shown below to the atmosphere. The pressure, psia, in the duct throat is most nearly Po = 91 psia مها : 7 Pater Hint: Assume the flow is choked, then the fluid speed in the throat is equal to the speed of sound and the pressure in the throat is equal to the critical pressure p
g through a nozzle. The inlet pressure is p 3.7 kPa (gage) air flowing and the air exhausts into the atmosphere. The nozzle has an inlet diameter of 60 mm and an exit diameter of 10 mm, and the nozzle is connected to the supply pipe by flanges. Find the force required to hold the nozzle stationary. Assume the air has a constant density of 1.22 kg/m Neglect the weight of the nozzle. m Flanges Flow 2
g through a...
Water flows through the nozzle below and exits with a velocity of 60 ft/s. The flow area is 0.3 ft2 at the flange and 0.1 ft2 at the exit. Find the total force in the bolts at the flange. (assume inviscid flow and Pa14.7 psia atmospheric pressure) 2. (assume inviscid flow and P atmospheric pressure) C.V. V. P2 Pa
Water is siphoned from a large tank and discharges into the
atmosphere through a 2-in.-diameter tube as shown in the figure
below. The end of the tube is 3 ft below the tank bottom, and
viscous effects are negligible. Determine the volume flowrate from
the tank. Determine the maximum height, H, over which the water can
be siphoned without cavitation occurring. Atmospheric pressure is
14.7 psia, and the water vapor pressure is 0.26 psia
MATLAB Program Problem D 0.02 m d 0.01 m 0 P1 3.0 kPa Air Review the tank diagram above. Air flows steadily from a tank, through a hose of diameter D-0.02 m, and exits to the atmosphere from a nozzle of diameter d-0.01 m. The pressure in the tank remains constant at 3.0 KPa and the atmospheric conditions are standard temperature and pressure. Determine the flow rate at the exit and the pressure in the hose. File Submission Save your...
Water at 60 °F flows through the elbow as shown below and is then injected to the atmosphere through a nozzle (on a horizontal plane). The pipe diameter is Di = 4 in. while the diameter of the exit of the nozzle is D2 = 1 in. At a flow rate of Q = 245 gpm, the gage pressure at the section (1) where the flange locates is Pi = 34 psig. Neglect the weight of the water and elbow,...
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m. Both the tank free surface and jet exit are exposed to the atmosphere. Take the density of water p = 1000 kg/m3, dynamic viscosity of water u = 0.001 kg/m.s, atmospheric pressure = 100 kPa, and gravity = 9.8 m/s2. Calculate the volumetric flow rate through the pipe. Neglect entrance losses to the pipe. Hint: Consider the inlet and outlet sections of the pipe...
Problem 1. Water flows from a large tank through a smooth pipe of length 80 m. Both the tank free surface and jet exit are exposed to the atmosphere. Take the density of water p = 1000 kg/m3, dynamic viscosity of water j = 0.001 kg/m.s, atmospheric pressure = 100 kPa, and gravity = 9.8 m/s2. Calculate the volumetric flow rate through the pipe. Neglect entrance losses to the pipe. Hint: Consider the inlet and outlet sections of the pipe...
Part B Review The large tank contains air at an absolute pressure of 64 psi and temperature of 70 F The nozzle has a throat diameter of 1 in. and an exit diameter of 1.75 in. (Figure 1) Determine the absolute pressure within the connected pipe, when the nozzle chokes and maintains isentropic supersonic flow within the divergent section of the nozzle. Express your answer to three significant figures and include the appropriate units P- psi Submit Incorrect; Try Again...
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