Lab 5: System Analysis 1

The lab calculated efficiency of AEV in different circumstances.  The 3 inch propellers were far more consistent than the 2.5 inch propellers.  Overall though, the 2.5 inch pusher proved to be the best choice to use in the overall project.  The different values were calculated by looking at the displaced grams and the figures were placed on graphs.  Throughout the lab, there were a few errors that were arisen.  For example, the wind speed was not always consistent.  Based on the results of the lab and graph analysis, new solutions were found that can be implemented in future projects and versions of our design.

Table 1: Wind Tunnel Testing Data for 3030 Pusher Propeller Configuration.

Current (Amps) Thrust Scale Reading (grams) Propeller RPM Arduino Power Setting (%)
0.00 153.1 0 0
0.02 153.7 2095 10
0.11 155.7 3053 15
0.21 158.1 3812 20
0.32 159.4 4670 25
0.41 163.5 5389 30
0.52 167.2 6167 35
0.62 170.1 6826 40
0.72 174 7425 45
0.82 178.3 8023 50
0.92 182.2 8682 55
1.03 186.5 9401 60

 

Table 2: Wind Tunnel Data Analysis for 3030 Pusher Propeller Configuration.

Thrust Calibration (grams) RPM Power Input (Watts) Power Output (Horsepower) Power Output (Watts) Propulsion Efficiency (%) Advance Ratio
0.00 0 0.00 0.00000000 0.000 0.00 0.00
0.25 2095 0.01 0.00000908 0.007 45.75 1.05
1.07 3053 0.12 0.00003935 0.029 24.03 0.72
2.06 3812 0.31 0.00007566 0.056 18.15 0.58
2.59 4670 0.59 0.00009534 0.071 12.01 0.47
4.27 5389 0.91 0.00015738 0.117 12.89 0.41
5.80 6167 1.35 0.00021337 0.159 11.81 0.36
6.99 6826 1.84 0.00025726 0.192 10.45 0.32
8.59 7425 2.40 0.00031628 0.236 9.84 0.30
10.36 8023 3.03 0.00038135 0.284 9.37 0.27
11.96 8682 3.74 0.00044036 0.328 8.77 0.25
13.73 9401 4.57 0.00050544 0.377 8.24 0.23

 

Figure 1

Figure1

  

Table 3: Wind Tunnel Testing Data for 3030 Puller Propeller Configuration.

Current (Amps) Thrust Scale Reading (grams) Propeller RPM Arduino Power Setting (%)
0.19 153.6 0 0
0.29 154.7 2095 10
0.37 157.4 3113 15
0.47 160.5 4071 20
0.55 164.4 4850 25
0.66 169.1 5748 30
0.76 174.2 6407 35
0.86 179.3 7065 40
0.95 184.3 7664 45
1.04 189.2 8383 50
1.14 195.7 8922 55
1.24 204.3 9760 60

 

Table 4: Wind Tunnel Data Analysis for 3030 Puller Propeller Configuration.

Thrust Calibration (grams) RPM Power Input (Watts) Power Output (Horsepower) Power Output (Watts) Propulsion Efficiency (%) Advance Ratio
0.00 0 0.00 0.00000000 0.000 0.00 0.00
0.45 2095 0.21 0.00001490 0.011 5.16 0.94
1.56 3113 0.41 0.00005130 0.038 9.32 0.63
2.84 4071 0.70 0.00009320 0.070 9.99 0.48
4.44 4850 1.02 0.00014600 0.109 10.69 0.41
6.37 5748 1.47 0.00020900 0.156 10.66 0.34
8.47 6407 1.97 0.00027800 0.208 10.54 0.31
10.56 7065 2.55 0.00034700 0.259 10.17 0.28
12.62 7664 3.16 0.00041500 0.309 9.78 0.26
14.63 8383 3.85 0.00048100 0.359 9.32 0.23
17.30 8922 4.64 0.00056900 0.424 9.14 0.22
20.84 9760 5.51 0.00068500 0.511 9.28 0.20

 

Figure 3

Figure 3

 

 

Table 5: Wind Tunnel Testing Data for 2510 Pusher Propeller Configuration.

Current (Amps) Thrust Scale Reading (grams) Propeller RPM Arduino Power Setting (%)
0.04 193.0 0 0
0.15 194.7 1017 10
0.23 194.3 1676 15
0.32 194.5 2275 20
0.4 195.3 2874 25
0.48 195.8 3473 30
0.55 196.6 4071 35
0.61 195.9 4670 40
0.66 197.2 5209 45
0.71 199.7 5808 50
0.74 203.3 6347 55
0.77 205.5 6886 60

 

Table 6: Wind Tunnel Data Analysis for 2510 Pusher Propeller Configuration.

Thrust Calibration (grams) RPM Power Input (Watts) Power Output (Horsepower) Power Output (Watts) Propulsion Efficiency (%) Advance Ratio
0.00 0 0.00 0.00000000 0.000 0.00 0.00
80.02 1017 0.11 0.00295000 2.197 1979.37 2.60
79.86 1676 0.26 0.00294000 2.193 858.83 1.58
79.94 2275 0.47 0.00294000 2.195 463.44 1.16
80.27 2874 0.74 0.00296000 2.204 297.82 0.92
80.47 3473 1.07 0.00296000 2.210 207.35 0.76
80.80 4071 1.42 0.00298000 2.219 155.74 0.65
80.51 4670 1.81 0.00296000 2.211 122.43 0.57
81.05 5209 2.20 0.00298000 2.225 101.25 0.51
82.08 5808 2.63 0.00302000 2.254 85.78 0.46
83.56 6347 3.01 0.00308000 2.294 76.17 0.42
84.46 6886 3.42 0.00311000 2.319 67.83 0.38

 

Figure5

Figure5

 Table 7: Wind Tunnel Testing Data for 2510 Puller Propeller Configuration.

Current (Amps) Thrust Scale Reading (grams) Propeller RPM Arduino Power Setting (%)
0.08 176 0 0
0.2 175.8 2035 10
0.29 176 3293 15
0.38 176.6 4610 20
0.46 177.3 5748 25
0.54 178.7 7065 30
0.5 183 9760 35
0.59 183.2 9760 40
0.74 185.6 10848 45
0.79 187.6 12155 50
0.84 190.5 13293 55
0.88 193.3 14431 60

 

Table 8: Wind Tunnel Data Analysis for 2510 Puller Propeller Configuration.

Thrust Calibration (grams) RPM Power Input (Watts) Power Output (Horsepower) Power Output (Watts) Propulsion Efficiency (%) Advance Ratio
0.00 0 0.00 0.00000000 0.000 0.00 0.00
-0.08 2035 0.15 -0.00000270 -0.002 -1.36 1.16
0.00 3293 0.32 0.00000000 0.000 0.00 0.72
0.25 4610 0.56 0.00000811 0.006 1.07 0.51
0.53 5748 0.85 0.00001760 0.013 1.54 0.41
1.11 7065 1.20 0.00003650 0.027 2.27 0.33
2.88 9760 1.30 0.00009460 0.071 5.45 0.24
2.96 9760 1.75 0.00009730 0.073 4.15 0.24
3.95 10848 2.46 0.00013000 0.097 3.93 0.22
4.77 12155 2.92 0.00015700 0.117 4.00 0.19
5.96 13293 3.42 0.00019600 0.146 4.27 0.18
7.11 14431 3.91 0.00023400 0.174 4.46 0.16

 

 

Figure 7

Figure 7