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Thermodynamics and Fluid Mechanics (Essay Sample)

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Question 1 Water at 50  C flows at a mass flow rate of 20 kg /s in a 2 00 mm diameter pipeline. a) Find the density and dynamic viscosity of the water at this temperature (you will need to use your tables). (2) b) Calculate the velocity of the water. (4 ) c) Hence calculate the Reynolds number Re. (2) d) Is the fl ow laminar or turbulent? Give a reason for your answer. (2) Question 2 Water flows in a circular pipe , as shown in Fig. Q2, overleaf . At one section the diameter of the pipe is 0 .3 m, the static pressure is 260 k Pa, the velocity is 3 m/s , and the elevation is 10 m above ground level. The elevation at a section downstream is at ground level and the pipe diameter is 0.15 m . Find the gauge pressure at the downstream section. Frictional effects may be neglected. Assume the density of water to be 99 9 kg/m 3 . (8)

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Content:

UNIVERSITY OF SUNDERLAND
DEPARTMENT OF COMPUTING, ENGINEERING AND TECHNOLGY
EAT106 – THERMODYNAMICS AND FLUID MECHANICS
REFERRED COURSEWORK 2013-2014
NAME:
DATE:
Question 1
Water at 50 degrees Celsius flows at a mass flow rate of 20 kg/s in a 200 mm diameter pipeline.
* Find the density and dynamic viscosity of the water at this temperature
letbe the dynamic viscosity
(kg/ms)= {[2.414 x 10-5)] x[10(247k/(temp-140k))]}
={[2.414 x 10^-5)] x [10(247k/(50 + 273 -140))]}
=0.00002414 x 101.4
=0.000605914kg/ms
 =6. 091 x 10^ -4 kg/ms
Density=988.1kg/m3
(Source Engineeringtoolbox.com, 2014)
* Calculate the velocity of the water.
Q=AV
V=Q/A
Volume flow rate= {(mass low rate)/ density}
Q=20/988.1
= 0.0202m3/s
A=r2
= x 0.1 x 0.1
=0.031m2
V=0.0202/0.031
=0.652m/s
* Hence, calculate the Reynolds number Re.
Re=density x velocity x diameter)
(Dynamic viscosity)
Re=xVx D

=988.1x 0.652 x 0.2
6. 091 x 10^ -4
Re=21255.94
* Is the flow laminar or turbulent?
The flow is turbulent
Because the Reynolds number is greater than 2000
Question 2
Water flows in a circular pipe. At one section the diameter of the pipe is 0.3 m, the static pressure is 260 kPa, the velocity is 3 m/s, and the elevation is 10 m above ground level. The elevation at a section downstream is at ground level and the pipe diameter is 0.15 m.
Find the gauge pressure at the downstream section.
Let upward section be section 1
Pressure at 1= 260Kpa =260 x 103 N/m2
Area 1 = (/4) x (D2)
= (/4) x (0.3 x 0.3)
=0.07071m2
Let downstream section be section 2
Pressure at 2= P
Area 2= (/4) x (0.15 x 0.15)
=0.0176
Equation of flow rate, Q= AV
Q is constant
AV1=AV2
3 x 0.07071= V2 x 0.0176
V2=12.052m/s
Bernoulli equation
(Source Princeton.edu, 2014)
{[260 x 103)/ 999 x 9.81]+ [(32)/ 2 x 9.81] + 10}={ [P/999 x 9.81]+ [12.052x12.052)/ 2x9.81] + 0.075}
26.5+0.459+10=7.478+ P/999 x 9.81
P=29.179 x 999 x 9.81
P=285, 959.74 N/m2
P= 285.959 Kpa
Question 3
A 40 m long horizontal pipe is connected to a water tank at one end and discharges freely into the atmosphere at the other. For the first 25 m of its length from the tank, the pipe is 150 mm diameter. Its diameter is then suddenly enlarged to 300 mm, as shown. The water level in the tank is 8 m above the centre of the pipe. If the Darcy-Weisbach friction factor in both pipes is 0.04, calculate the exit velocity V2 of the water and the volumetric flow rate in m3/s.
(Source Nptel.ac.in, 2014)
Using line XX as the datum
Using pipe1 and the tank
Bernoulli equation
P1=P2=0
Vt for tank=0
Pt/g + V2t/2g + Zt=P1/2g + {V12/2 x g} +Z1+hf
(The crossed values mean they are zero)
8+0.075=V21 /2x9.81 +0.15+ (0.04x25xV2)/ (0.15x2x9.81)
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