Applied Fluid Mechanics (7th Edition)
7th Edition
ISBN: 9780132558921
Author: Robert L. Mott, Joseph A. Untener
Publisher: PEARSON
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Textbook Question
Chapter 18, Problem 18.40PP
A tank of Refrigerant is at
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Water is ejected vertically from a pressurized tank as shown in Figure 2. The "3 atm" pressure value is an absolute pressure value.
Figure 2
Calculate the gauge pressure at the bottom of the tank in kPa if the height in the tank is H = 4.1 m.
calculate the velocity at the nozzle exit, in m/s, for H = 4.2 m.
calculate the maximum height of the water jet from the nozzle, h, in m, for a velocity at the nozzle of 21.0 m/s
Assume the density of water is 1000 kg/m3 and 1 atm = 1.01 x 105 Pa. Use g = 9.81 m/s2.
A pitot tube is used to measure the flow rate of air at a temperature of 500 K inside a
duct. If the measured static pressure was 200 kPa, the measured stagnation pressure
was 223 kPa and the air can be treated as an ideal gas what is the air velocity?
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Chapter 18 Solutions
Applied Fluid Mechanics (7th Edition)
Ch. 18 - A pipe in a compressed air system is carrying 2650...Ch. 18 - Prob. 18.2PPCh. 18 - Prob. 18.3PPCh. 18 - A duct in a heating system carries 8320 cfm....Ch. 18 - The velocity of flow in a ventilation duct is 1140...Ch. 18 - Prob. 18.6PPCh. 18 - Prob. 18.7PPCh. 18 - Prob. 18.8PPCh. 18 - Prob. 18.9PPCh. 18 - Prob. 18.10PP
Ch. 18 - Prob. 18.11PPCh. 18 - Describe a centrifugal fan with forward-curved...Ch. 18 - Prob. 18.13PPCh. 18 - Prob. 18.14PPCh. 18 - Name four types of positive-displacement...Ch. 18 - Name a type of compressor often used for pneumatic...Ch. 18 - Prob. 18.17PPCh. 18 - Prob. 18.18PPCh. 18 - Prob. 18.19PPCh. 18 - Compute the specific weight of nitrogen at 32...Ch. 18 - Compute the specific weight of air at 1260...Ch. 18 - Prob. 18.22PPCh. 18 - An air compressor delivers 820 cfm of free air....Ch. 18 - Prob. 18.24PPCh. 18 - Prob. 18.25PPCh. 18 - Prob. 18.26PPCh. 18 - Specify a size of Schedule 40 steel pipe suitable...Ch. 18 - For an aeration process, a sewage treatment plant...Ch. 18 - Prob. 18.29PPCh. 18 - Prob. 18.30PPCh. 18 - Prob. 18.31PPCh. 18 - Prob. 18.32PPCh. 18 - Prob. 18.33PPCh. 18 - Prob. 18.34PPCh. 18 - Prob. 18.35PPCh. 18 - Figure 18.14 iD shows a two-compartment vessel....Ch. 18 - Prob. 18.37PPCh. 18 - Prob. 18.38PPCh. 18 - Prob. 18.39PPCh. 18 - A tank of Refrigerant is at 150 kPa gage and 20C....Ch. 18 - Prob. 18.41PP
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- Answer this as fast as you can but answer should be correct (correct answer is priority) Air leaks slowly to atmosphere from a pressurized tank at 19 bar (gage) and 27°C through a hole of diameter 2 mm. The tank volume is 1 m3. Atmospheric conditions are 100 kPa and 27°C. Determine the time for the tank pressure to decrease to 100 kPa (gauge).arrow_forwardPlease answer all subparts. I will really really upvote. Thanksarrow_forwardRefrigerationarrow_forward
- Title of the book: Fluid Power, Theory and Applications, 3rd Edition, James A. Sullivanarrow_forwardAnswer the problem correctly and provide complete and readable solutions. If you can explain the process (briefly), please do so. Thank you!arrow_forwardI2 4.2, there is friction in the piping, which means that an additional pressure equivalent to a height of 100 m is needed to pump the water from the bottom tank to the top tank. What is the minimum power required when accounting for friction? By what percentage has friction increased the minimum power required? Remember to show your calculations.arrow_forward
- an air compressor of three stage compresses air from 100 kpa to 1000 kpa. calculate the intercooler pressure between the first and second stagearrow_forwardShow where the stagnation point, high-pressure area and low-pressure area are in the picture below.arrow_forward10 m3/min of free air is to be compressed to 8 bar gauge in two stages. Assuming a 2 bar gauge intercooler pressure and a polytropic index of 1.3, what is the flowrate out of the compressor plant ?arrow_forward
- 2) flow is exhausted from the nozzle exit at standard sea level conditions with a velocity of 50 m/s, calculate the height difference in a U-tube mercury manometer with one side connected Consider the nozzle of a subsonic turbojet with contraction ratio of 2:1. If the jet to the nozzle inlet and the nozzle exit.arrow_forwardWater flows through a horizontal coil heated by steam condenaing on the outside. If the inlet pressure and temperatire are 2 atm and 160°F (state 1) and at the exit 1 atm and 220 °F (state 2), calculate the heat added to the coil per pound mass of water. The entering velocity is 5 ft/s, and the leaving, 500 ft/s. Data: H1=127.9 Btu/lb, H2=1154.4 Btu/lbA. 1031 Btu/lbB. 1042 Btu/lbC. 1048 Btu/lbD. 1052 Btu/lbarrow_forwardWhat is the pressure difference across the valve prior to being opened? The pressure at the inlet pipe into tank 2 can be taken to be atmosphere. Take the height of the valve to be 8m. (HINT: if the valve is shut, what is the velocity everywhere?)arrow_forward
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