You are measuring the velocity of air at standard temperature and pressure in a
1” pipe. You initially estimate the velocity to be 50 ft/s, if the mass flow rate is
independent of the velocity in the section where you are making the
measurements
determine the extent a probe that can be considered a 1/4” tube
will disturb the velocity of the flow.

You are measuring the velocity of air at standard temperature and pressure in a 1” pipe....
4. Air enters a converging pipe where the temperature reaches 300 K at a 50 mm diameter section. Given the stagnation pressure and stagnation temperature as 200 kPa and 40°C, determine the mass flow rate (kg/s) within the pipe. (15 pts)
You will be measuring velocity with the Pitot tube. Assume that the air density is 1.18 ± 1 x 10-4 kg/m3 and that the pressure sensor measures a differential pressure of 29.4Pa ± 1.0% FS. (Sensor range 0-60 Pa) Determine the uncertainty in the velocity reading. (Hint: Calculate the expected velocity from the Pitot tube. Remember uncertainty theory when multiple variables are involved!)
problem # 5
that corresponds to a Reynolds number of 20007 onml sieutn e0 pipe, what is the tlow rate Air at standard conditions flows through a 2 standard type M copper tube. What is the maximum velocity allowable for laminar flow conditions to exist? (At standard conditions, air can be treated as incompressible.) 4. One hundred cubic feet per minute of air flows through an 2 standard type M copper tube. Is the flow laminar or turbulent? 5. Pressure...
The air in the driven section of a shock tube is initially at the temperature and pressure of 300 k and 0.1 atm. After the diaphragm is broken, an incident shock wave with a velocity of 1440 m/s is propagating into the driven section where a pitot tube is placed. The pitot tube is facing toward the oncoming incident shock wave With its axis parallel to the axis of the shock tube. calculate : a) the total pressure of the...
please solve this
Consider the flow of air in a long frictional pipe under isothermal conditions. At the pipe inlet 10 N/m2. respectively, and the velocity the static temperature and pressure are 318 K and 1 is 100 m/s. The pipe diameter is 0.25 m and the friction coefficient is 0.05. For air, take 7 1.4. Analyze the problem as the isothermal Fanno flow and calculate iThe length of pipe to choke the flow. The limiting velocity. The limiting pressure....
part a-d
2 A paint sprayer pumps air through a constriction in a 0.025- m diameter pipe, as shown in the figure. The flow causes the pressure in the constricted area to drop and paint rises up the feed tube and enters the air stream. The speed of the air stream in the 0.025-m diameter sections is 5.00 m/s. The density of the air is 1.29 kg/m3, and the density of the paint is 1200 kg/m3. We can treat the...
find mach 1 as a function of stagnation pressure for air,
sulfur hexafluoride (sf6) and helium
find mass flow rate as a function of stagnation pressure for
air, sulfur hexafluoride (sf6) and helium
1 Flow enters the above nozzle isentropically. At section 1, where d = 50 cm, a pitot-static tube measures the local flow properties as shown in the table below. The stagnation temperature is 450 K throughout P. (kPa) 75 100 Instance 1 2 3 4 5 P....
Air flow is induced in an insulated tube of 7.16 mm diameter by a vacuum pump. Air is drawn from a room where stagnation pressure is 101 kPa (abs) and stagnation temperature 23 °C, through a smoothly contoured converging nozzle. At station (1), where the converging nozzle joins the constant area tube, the static pressure is 98.5 kPa (abs). At section (2), located some distance downstream in the constant area tube, the air temperature is 14 °C. Determine a) the...
Velocity data analysis: Air flow speed is tested using a Pitot tube. Table 1 summarizes the Power supply of the wind tunnel and the dynamic pressure DP. The dynamic pressure P, is the difference between the total pressure P, and the static pressure P, measured by the Pitot tube. Please determine: 1) the air flow speed at each power supply (consider room 2) Plot the flow speed vs power supply using a computer 3) If the relation of the flow...
(c) Fuel oil, with a density of 870 kg m-, is pumped through a horizontal pipe, as shown in Figure Q2.2. The pipe is 100 mm in diameter and contains an orifice plate with a throat diameter of 40 mm. The pressure drop across the orifice is measured on a U-tube manometer, containing mercury with a specific gravity 13.6. The difference in levels of the columns is measured as 45 mm. The coefficient of discharge for the orifice plate Ca...