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A cryogenic probe is used to treat cancerous skin tissue. The probe consists of a single round jet of diameter
Assuming the cancerous skin tissue to be a semi-infinite medium with
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- Parvinbhaiarrow_forwardAir is flowing in a duct as shown in the figure below. A Pitot-static tube and a thermocouple are inserted into the flow stream as shown. Calculate the air velocity and the air-mass flowrate. The area of the duct is 1 ft², and the temperature of the control volume x is 40°F. V = m = i x ft/s lbm/s A Ps = 3 psig Po = 15 psigarrow_forwardGiven the 0.063 m length of the syringe. F=1N a. provide an equation to calculate its water flow rate if water is going to travel from a 0.063 m length of syringe with dextrose tube length of 0.5 meter to another 0.063 m syringe (see attached photo). The Inner diameter of the syringe is 0.02. While the inner diameter of dextrose tube is 0.003. b. provide an equation in order to calculate the maximum force or pressure that exerts in plunger in order to travel the water at its maximum speed.arrow_forward
- A blower supplies standard air to a plenum that feeds twohorizontal square sheet-metal ducts with sharp-edged entrances.One duct is 100 ft long, with a cross-section 6 in by6 in. The second duct is 200 ft long. Each duct exhausts tothe atmosphere. When the plenum pressure is 5.0 lbf/ft2(gage) the volume flow in the longer duct is three times theflow in the shorter duct. Estimate both volume flows andthe cross-section size of the longer duct.arrow_forwardWater is being pumped the through one inch diameter piping arrangement to a higher elevation (5 meters up). Assume incompressible fluid conditions and some heat losses to the surroundings. At the inlet water pressure is 1 bar, temperature 15C, and volumetric flow rate is 0.02 m3/s. At the exit pressure is 2.2 bar, temperature is 10C and velocity of the stream is 40 m/s. Determine: a.Density of the inlet stream using NIST tables. b.Mass flow rate [kg/s] c.Determine h2 from known p2 and T2 using NIST tables d.Find heat rate removed from Q=m(h1-h2) Use Energy Balance Equation with enthalpy difference and in the units of kW to find pumping power in kW. NOTE: The heat is removed from the system, so it should be negative in your equation! show all steps pleasearrow_forwardWater is being pumped the through one inch diameter piping arrangement to a higher elevation (5 meters up). Assume incompressible fluid conditions and some heat losses to the surroundings. At the inlet water pressure is 1 bar, temperature 15C, and volumetric flow rate is 0.02 m3/s. At the exit pressure is 2.2 bar, temperature is 10C and velocity of the stream is 40 m/s. Determine: a.Density of the inlet stream using NIST tables. b.Mass flow rate [kg/s] c.Determine h2 from known p2 and T2 using NIST tables d.Find heat rate removed from Q=m(h1-h2) Use Energy Balance Equation with enthalpy difference and in the units of kW to find pumping power in kW. NOTE: The heat is removed from the system, so it should be negative in your equation!arrow_forward
- Water is being pumped the through one inch diameter piping arrangement to a higher elevation (5 meters up). Assume incompressible fluid conditions and some heat losses to the surroundings. At the inlet water pressure is 1 bar, temperature 15C, and volumetric flow rate is 0.02 m3/s. At the exit pressure is 2.2 bar, temperature is 10C and velocity of the stream is 40 m/s. Determine: a.Density of the inlet stream using NIST tables. b.Mass flow rate [kg/s] c.Determine h2 from known p2 and T2 using NIST tables d.Find heat rate removed from Q=m(h1-h2) Use Energy Balance Equation with enthalpy difference and in the units of kW to find pumping power in kW. NOTE: The heat is removed from the system, so it should be negative in your equation! show all steps please thanksarrow_forwardQuestion : Water at 20°C flows through the piping junction, entering section (1) at 0.1 m3/min. The average velocity at section (2) is 2.75 m/s. A portion of the flow is diverted through the showerhead, which contains 150 holes of 1.5-mm diameter. Assuming uniform shower flow, estimate the exit velocity from the showerhead jets.arrow_forwardSketch the shear stress and velocity distribution for laminar flow across a pipe section?arrow_forward
- A 0.3 m diam. pipe through which water flows at the rate of 0.283 m°/s suddenly enlarges to 0.6 m in diam. the pipe ils horizontal and the water in connected to the larger pipe stands 0. 36 higher than the level in coefficient K if the shock loss is expressed as KV´/2g, where v is the velocity in the smaller pipe. 8. If the axis of a vertical tube tube connected to the smaller pipe, determine the a (0.496)arrow_forwardConsider a pipe on a horizontal plane: based on Bernoulli's equation A. none of the above B. the inlet velocity will be less than the outlet velocity C. the inlet velocity will be greater than the outlet velocity D. the elevation of the inlet will be greater than that of the outletarrow_forwardThe dimensions of a duct system, supplying air at 20°C to two zones 5 and 6 are shown in Fig. The flow rates to the two zones are 1.4 m³/s and 1.0 m³/s respectively. The fan generates a total pressure of 285 kPa at the entrance section 1. Calculate (a) (i) the velocity pressures in the duct sections, (ii) (ii) the total pressures at all sections from 1 to 6. (b) If a damper is installed just upstream of section 5 to make the total pressures at 5 and 6 equal, calculate the required pressure loss through the damper. From L12 = 45m 2 3 L35 = 40m fan 1.4 m/s 2.4 m/s 4 D12 = 0.6 m L46 = 70m 6. D35 = 0.5 m D46 = 0.4 m 1.0 m/s Fig. El1.2.1 Supply air duct systemarrow_forward
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