Lab 5 – System Analysis 1

The following lab, team member Max worked alone to collect wind tunnel data. The point of this data was to determine what amount of thrust would allow the propellers to be as energy efficient as possible. Max did not personally collect the data. Instead, it was provided to him and members from other groups by a UTA who had control of the propeller and wind tunnel. After returning to the team table with the data, Max employed Davin to perform calculations. The original data and Davin’s analysis can be seen below.

 

Wind Tunnel Data

-0.1 154.8 0 0
-0.07 155.1 778 5
0 156.1 1856 10
0.09 157.6 2814 15
0.19 159.7 3712 20
0.28 161.8 4431 25
0.39 164.8 5269 30
0.49 167.4 5928 35
0.59 170.9 6646 40
0.67 173.9 7305 45
0.78 178 8023 50
0.89 182.2 8682 55
0.99 186.5 9000 60

 

Davin’s Wind Tunnel Data Analysis

Thrust Calibration (grams) RPM Power Input (Watts) Power Output (Horsepower) Power Output (Watts) Propulsion Efficiency (%) Advance Ratio
0 0 0 0 0 0 0
0.1233 778 -0.0259 2.91847E-06 0.002176304 -8.402716454 0.046272
0.5343 1856 0 1.26467E-05 0.009430649 0 0.019397
1.1508 2814 0.0999 2.72391E-05 0.020312167 20.33249907 0.012793
2.0139 3712 0.2812 4.76684E-05 0.035546292 12.6409287 0.009698
2.877 4431 0.518 6.80976E-05 0.050780416 9.803169197 0.008125
4.11 5269 0.8658 9.72824E-05 0.072543452 8.378777091 0.006832
5.1786 5928 1.2691 0.000122576 0.09140475 7.202328389 0.006073
6.6171 6646 1.7464 0.000156625 0.116794958 6.687755257 0.005417
7.8501 7305 2.2311 0.000185809 0.138557993 6.210299557 0.004928
9.5352 8023 2.886 0.000225695 0.168300809 5.831628855 0.004487
11.2614 8682 3.6223 0.000266554 0.198769059 5.487371522 0.004147
13.0287 9000 4.3956 0.000308385 0.229962743 5.231657635 0.004

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