Concept explainers
Suppose you are looking into purchasing a water pump with the performance data shown in Table P14-32. Your supervisor asks for some more information about the pump. (a) Estimate the shutoff head
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FLUID MECHANICS FUNDAMENTALS+APPS
- For a venturi meter given below, the volumetric flow rate is defined in terms of the geometrical parameters, the density of working fluid (p), and density of the manometer liquid (pm) as 4. Q = f(D, D2, A2, g, h, Pmv Pr) %3D Write down the balance equations and show your work to end up with an expression for the volumetric flow rate in terms of the variables defined above.arrow_forward3. Problem Estimate the frictional resistance Rp for a container ship using the ITTC 1957 model-ship correlation line Equation (2): 0.075 CF [ log,,(Re) – 21 The ship has the following particulars: Full scale ship data length between perpendiculars Lep length in waterline length over wetted surface 195.40 m Lwz Los For the wetted surface S you can use the following formula by Kristensen and Lützen (2012) derived for container ships. 200.35 m 205.65 m breadth B 29.80 m draft T 10.10 m 37085.01 m3 S = 5 + Lw. T 0.995 displacement design speed Again, use the most up-to-date ITTC water properties sheet for density and kinematic viscosity. V 21.00 knarrow_forwardKindly answer correctly. PPlease show the necessary stepsarrow_forward
- (b) A pitot-static probe is use to determine the flow velocity by measuring the differential pressure. The pitot formula to obtain the flow velocity is, 2(P- P,) V = where, V is the velocity, P is pressure and pis fluid density. i) The pressure difference sensor use in the system is electronic types and the output of the device is measured in voltage. The output of the pressure device is 3.5 V and the linear relationship between the device and the pressure difference is 10 kPa/V. If the measured fluid is water at 20°C, determine the pressure difference inside the system the water velocity. ii) The Pitot-static tube is also commonly use in aircraft. An aircraft flying at 3000 m above sea level when the differential pressure reading clocked 3 kPa. Determine the speed of the aircraft.arrow_forwardUse Excel to plot the following data for a pump. Use two different y axes. Use a scale of zero to 140 cm for the head and zero to 100 for efficiency.arrow_forwardPlease I want answer for this question - 7 . Many Thanksarrow_forward
- Shown below is a performance data for a water pump. For each row of data, calculate the pump efficiency (percent). Estimate the best efficiency point (%) and the volume flow rate (gpm) and net head (ft) at the best efficiency point. gpm ft KW 200 75 4.9 300 73 6.7 400 71 7.2 500 66 8.1 600 60 9.0arrow_forwardThe SCAL results for a core sample taken from an exploration well is as follows: Capillary pressure, P (psia) Water saturation, (%) 100 Water density 64 lb/ft3 4.4 100 Oil density = 45 lb/ft3 %3D 5.3 90.1 5.6 82.4 10.5 43.7 15.7 32.2 35.0 29.8 76.5 Dementa of Reservoir Rock and Fluid Properties Ch4-Saturation and Capilary Pressure Slde 51 Exercise A P U ASIA PACInc UNIVERSITY or TECHNOLOGYA ovanoN L Convert the capillary pressure table to water saturation and height, H in ft. Plot H vs Sw. 19.5 Indicate the FWL, OWC and transition zone on the plot. LA sample was taken from a depth 80 ft above the OWC. What is the expected Sw of the sample at that elevation.arrow_forward9. Using simple reservoir simulation, estimate storage over time; maximum reservoir capacity is 10 volume units, and it starts full. Please a) estimate the largest spill over the simulated period, b) and the simulated storage at the beginning of 7 time step. Time Inflow Demand step (L^3) (L^3) 4 1. 10 4 2 8. 4 8. 6 7 3.arrow_forward
- 1. The observed and model simulated average daily flow in month flow at the outlet of a river catchment during a given period is presented as follows. Predicted flow Observed flow 0.25 0.30 0.70 0.73 0.80 0.87 0.71 0.90 0.71 0.65 1.60 1.45 0.90 0.70 0.71 0.61 0.24 0.22 1.00 0.64 0.81 1.00 1.05 0.90 0.46 0.48 0.27 0.23 0.80 0.24 0.32 0.42 0.80 0.89 (i) Evaluate the model performance based on any two computed statistical measures of performance of your choice. (ii) Explain possible reasons for model performance observed in (i) above. (Hint: Refer to reading material provided on model evaluation by Moriasi et al., 2007)arrow_forwardQ=What is the importance of regression analysis in transportation engineering? ANSWER in word fomatarrow_forwardLR = 5m, LG = 2.5m and LC = 1.1m Q2. The Skylark family of sounding rockets consisted of a number of variants (denoted Skylark 5, Skylark 7, and Skylark 12 respectively). These are illustrated on Page 3. The data given below is based on that for the rocket motors they used (all manufactured and named by what was Royal Ordinance – now part of Roxel): Raven XI Motor Total mass: 1280 kg Length = LR See Case Table (units are m) Diameter = 0.44 m Goldfinch IIA Motor Total mass: 420 kg Length = LG See Case Table (units are m) Diameter = 0.44 m Cuckoo IV Motor Total mass: 242 kg Length = LC See Case Table (units are m) Diameter = 0.44 m The payload mass which is additional to the motor masses is to be taken as 100 kg. (a) For the configurations of the three rockets shown on Page 3 in Fig. Q2: (i) Determine the Pitching/Yawing moment of inertia of each rocket about the base of each rocket. (ii) Explain how you could then find the the Pitching/Yawing moment of inertia of each rocket about its…arrow_forward
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