MATLAB Program Problem D= 0.02 m d = 0.01 m P = 3.0 kPa (1) Air (2) (3) 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. Also determine the air velocity at points 1, 2 and 3.
MATLAB Program Problem D= 0.02 m d = 0.01 m P = 3.0 kPa (1) Air (2) (3) 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. Also determine the air velocity at points 1, 2 and 3.
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Transcribed Image Text:MATLAB Program Problem
D= 0.02 m
d= 0.01 m
P = 3.0 kPa
(1)
Air
(2)
(3)
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. Also determine the air velocity at points 1, 2 and 3.
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