For the given information: Flow equation: Qa= Cd A2 V2gAh , Where Ca is the discharge coefficient. 1) Plot a graph of Qa vs. VAh 2) Calibrate the coefficient with virtual data by fitting with least square. 3) Please compare your coefficient value with values in the literature that you find in books or online. *Reference your lab workout for conversions needed. Upstream Pipe Diameter = 0.03175 m Cross sectional area of upstream pipe A1= 7.92x 10-4m² Throat diameter = 0.015 m Cross sectional area of throat A2= 1.77 X 10-4m² Trial Qa (L/min) h1 (mm) h2 (mm) 1 2 70 65 2 4 85 74 104 80 4 8. 128 90 5 10 150 100 12 181 111 7 15 235 125

Structural Analysis
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Author:KASSIMALI, Aslam.
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Chapter2: Loads On Structures
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For the given information:
Flow equation: Qa= Cd A2 V2gAh , Where Ca is the discharge coefficient.
1) Plot a graph of Qa vs. VAh
2) Calibrate the coefficient with virtual data by fitting with least square.
3) Please compare your coefficient value with values in the literature that you find in books or
online.
*Reference your lab workout for conversions needed.
Upstream Pipe Diameter = 0.03175 m
Cross sectional area of upstream pipe A1= 7.92x 10-4m²
Throat diameter = 0.015 m
Cross sectional area of throat A2= 1.77 X 10-4m²
Trial
Qa (L/min)
h1 (mm)
h2 (mm)
1
2
70
65
2
4
85
74
3
6
104
80
4
8.
128
90
5
10
150
100
6
12
181
111
7
15
235
125
Transcribed Image Text:For the given information: Flow equation: Qa= Cd A2 V2gAh , Where Ca is the discharge coefficient. 1) Plot a graph of Qa vs. VAh 2) Calibrate the coefficient with virtual data by fitting with least square. 3) Please compare your coefficient value with values in the literature that you find in books or online. *Reference your lab workout for conversions needed. Upstream Pipe Diameter = 0.03175 m Cross sectional area of upstream pipe A1= 7.92x 10-4m² Throat diameter = 0.015 m Cross sectional area of throat A2= 1.77 X 10-4m² Trial Qa (L/min) h1 (mm) h2 (mm) 1 2 70 65 2 4 85 74 3 6 104 80 4 8. 128 90 5 10 150 100 6 12 181 111 7 15 235 125
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