612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
13.5x13.5 (135x135.dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1199 0.0703 0.003 0.160 0.127 1.892 0.018 0.565 30.419 0.05 21802. 0.4710
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0.51 0.0400 0.0666 0.1194 0.0718 0.003 0.163 0.126 1.933 0.018 0.562 29.665 0.05 21827. 0.4584
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1.02 0.0801 0.1296 0.1189 0.0734 0.003 0.167 0.126 1.976 0.019 0.560 28.878 0.05 21856. 0.4452
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1.54 0.1201 0.1889 0.1182 0.0752 0.003 0.171 0.125 2.022 0.019 0.557 28.065 0.05 21889. 0.4315
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2.05 0.1601 0.2444 0.1175 0.0770 0.003 0.175 0.124 2.071 0.020 0.553 27.234 0.05 21926. 0.4174
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2.56 0.2002 0.2961 0.1166 0.0788 0.003 0.179 0.123 2.120 0.020 0.549 26.393 0.05 21968. 0.4029
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3.07 0.2402 0.3440 0.1155 0.0807 0.003 0.183 0.122 2.170 0.021 0.544 25.548 0.05 22014. 0.3882
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3.58 0.2803 0.3881 0.1142 0.0825 0.003 0.188 0.121 2.219 0.021 0.538 24.707 0.05 22066. 0.3734
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4.09 0.3203 0.4286 0.1126 0.0842 0.003 0.191 0.119 2.265 0.022 0.530 23.877 0.05 22123. 0.3583
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4.61 0.3603 0.4657 0.1108 0.0857 0.003 0.195 0.117 2.307 0.022 0.522 23.060 0.05 22185. 0.3432
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5.12 0.4004 0.4995 0.1086 0.0870 0.003 0.198 0.115 2.342 0.022 0.511 22.262 0.05 22253. 0.3281
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5.63 0.4404 0.5303 0.1060 0.0880 0.003 0.200 0.112 2.369 0.023 0.499 21.484 0.05 22326. 0.3128
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6.14 0.4804 0.5581 0.1030 0.0887 0.003 0.202 0.109 2.386 0.023 0.485 20.726 0.05 22405. 0.2975
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6.65 0.5205 0.5830 0.0995 0.0889 0.003 0.202 0.105 2.391 0.023 0.469 19.987 0.05 22489. 0.2820
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7.17 0.5605 0.6052 0.0956 0.0885 0.003 0.201 0.101 2.382 0.023 0.450 19.266 0.05 22579. 0.2663
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7.68 0.6006 0.6246 0.0911 0.0876 0.003 0.199 0.096 2.357 0.023 0.429 18.559 0.05 22674. 0.2505
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8.19 0.6406 0.6413 0.0861 0.0860 0.003 0.196 0.091 2.315 0.022 0.405 17.862 0.05 22775. 0.2344
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8.70 0.6806 0.6550 0.0807 0.0839 0.003 0.191 0.085 2.256 0.022 0.380 17.170 0.05 22881. 0.2181
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9.21 0.7207 0.6655 0.0749 0.0811 0.003 0.184 0.079 2.183 0.021 0.353 16.476 0.05 22992. 0.2016
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9.72 0.7607 0.6723 0.0688 0.0779 0.003 0.177 0.073 2.095 0.020 0.324 15.770 0.06 23108. 0.1850
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10.24 0.8007 0.6750 0.0625 0.0741 0.003 0.169 0.066 1.994 0.019 0.294 15.042 0.06 23229. 0.1681
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10.75 0.8408 0.6727 0.0559 0.0699 0.003 0.159 0.059 1.881 0.018 0.263 14.277 0.06 23355. 0.1510
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11.26 0.8808 0.6643 0.0492 0.0653 0.002 0.148 0.052 1.756 0.017 0.232 13.457 0.06 23485. 0.1335
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11.77 0.9208 0.6481 0.0424 0.0602 0.002 0.137 0.045 1.621 0.015 0.200 12.557 0.06 23621. 0.1156
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12.28 0.9609 0.6215 0.0355 0.0548 0.002 0.125 0.038 1.475 0.014 0.167 11.540 0.06 23761. 0.0972
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12.80 1.0009 0.5805 0.0284 0.0490 0.002 0.112 0.030 1.320 0.013 0.134 10.348 0.06 23905. 0.0780
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13.31 1.0410 0.5184 0.0214 0.0429 0.002 0.098 0.023 1.155 0.011 0.101 8.886 0.06 24055. 0.0581
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13.82 1.0810 0.4232 0.0143 0.0365 0.001 0.083 0.015 0.981 0.009 0.067 6.985 0.06 24208. 0.0373
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14.33 1.1210 0.2708 0.0072 0.0297 0.001 0.068 0.008 0.799 0.008 0.034 4.310 0.06 24366. 0.0163
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14.84 1.1611 0.0062 0.0001 0.0227 0.001 0.052 0.000 0.611 0.006 0.001 0.096 0.06 24529. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1204 0.0635 0.018 0.577 0.510 13.660 0.065 2.268 16.928 0.11 43604. 0.5253
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1.03 0.0404 0.0745 0.1200 0.0650 0.019 0.591 0.508 13.992 0.067 2.259 16.464 0.11 43655. 0.5100
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2.06 0.0807 0.1446 0.1194 0.0667 0.019 0.607 0.506 14.351 0.069 2.249 15.982 0.11 43713. 0.4940
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3.10 0.1211 0.2102 0.1188 0.0685 0.020 0.623 0.503 14.735 0.070 2.238 15.487 0.11 43779. 0.4775
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4.13 0.1614 0.2711 0.1181 0.0703 0.020 0.640 0.500 15.137 0.072 2.224 14.984 0.11 43854. 0.4605
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5.16 0.2018 0.3274 0.1172 0.0722 0.021 0.657 0.496 15.552 0.074 2.208 14.477 0.11 43938. 0.4433
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6.19 0.2421 0.3792 0.1162 0.0742 0.021 0.675 0.492 15.970 0.076 2.188 13.972 0.11 44033. 0.4259
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7.22 0.2825 0.4266 0.1149 0.0761 0.022 0.692 0.487 16.380 0.078 2.164 13.473 0.11 44138. 0.4085
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8.25 0.3229 0.4699 0.1134 0.0779 0.022 0.709 0.480 16.770 0.080 2.135 12.984 0.11 44253. 0.3910
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9.29 0.3632 0.5092 0.1115 0.0796 0.023 0.724 0.472 17.126 0.082 2.101 12.507 0.11 44379. 0.3736
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10.32 0.4036 0.5448 0.1093 0.0810 0.023 0.737 0.463 17.433 0.083 2.059 12.045 0.11 44517. 0.3562
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11.35 0.4439 0.5771 0.1067 0.0821 0.024 0.747 0.452 17.673 0.084 2.010 11.598 0.11 44665. 0.3389
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12.38 0.4843 0.6062 0.1037 0.0828 0.024 0.754 0.439 17.831 0.085 1.953 11.168 0.11 44825. 0.3216
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13.41 0.5246 0.6324 0.1002 0.0831 0.024 0.756 0.424 17.889 0.085 1.887 10.754 0.11 44996. 0.3044
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14.45 0.5650 0.6558 0.0961 0.0828 0.024 0.754 0.407 17.832 0.085 1.811 10.355 0.11 45179. 0.2872
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15.48 0.6054 0.6764 0.0916 0.0820 0.024 0.746 0.388 17.644 0.084 1.725 9.969 0.11 45372. 0.2698
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16.51 0.6457 0.6944 0.0865 0.0805 0.023 0.732 0.366 17.319 0.083 1.630 9.595 0.11 45576. 0.2524
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17.54 0.6861 0.7098 0.0810 0.0783 0.023 0.712 0.343 16.857 0.080 1.526 9.230 0.11 45791. 0.2350
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18.57 0.7264 0.7223 0.0751 0.0756 0.022 0.687 0.318 16.267 0.078 1.415 8.870 0.11 46016. 0.2175
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19.61 0.7668 0.7316 0.0690 0.0723 0.021 0.657 0.292 15.558 0.074 1.299 8.512 0.11 46251. 0.1999
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20.64 0.8071 0.7373 0.0625 0.0685 0.020 0.623 0.265 14.738 0.070 1.178 8.150 0.11 46497. 0.1823
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21.67 0.8475 0.7387 0.0559 0.0642 0.019 0.584 0.237 13.814 0.066 1.053 7.776 0.11 46752. 0.1645
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22.70 0.8879 0.7348 0.0492 0.0594 0.017 0.541 0.208 12.792 0.061 0.926 7.383 0.11 47017. 0.1464
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23.73 0.9282 0.7239 0.0423 0.0542 0.016 0.493 0.179 11.675 0.056 0.797 6.958 0.11 47292. 0.1280
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24.76 0.9686 0.7036 0.0353 0.0486 0.014 0.442 0.150 10.469 0.050 0.665 6.481 0.11 47576. 0.1090
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25.80 1.0089 0.6696 0.0283 0.0426 0.012 0.388 0.120 9.176 0.044 0.533 5.921 0.11 47870. 0.0891
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26.83 1.0493 0.6140 0.0212 0.0362 0.010 0.330 0.090 7.802 0.037 0.399 5.221 0.11 48173. 0.0680
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27.86 1.0896 0.5213 0.0141 0.0295 0.009 0.268 0.060 6.352 0.030 0.266 4.268 0.11 48484. 0.0454
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28.89 1.1300 0.3546 0.0070 0.0224 0.006 0.204 0.030 4.832 0.023 0.133 2.799 0.11 48805. 0.0210
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29.92 1.1704 0.0024 0.0000 0.0151 0.004 0.137 0.000 3.253 0.016 0.001 0.018 0.11 49133. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1207 0.0607 0.059 1.242 1.150 44.067 0.140 5.113 11.832 0.16 65406. 0.5514
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1.55 0.0405 0.0782 0.1202 0.0622 0.061 1.274 1.145 45.202 0.144 5.095 11.493 0.16 65482. 0.5346
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3.11 0.0810 0.1517 0.1197 0.0639 0.062 1.308 1.141 46.432 0.148 5.074 11.142 0.16 65569. 0.5172
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4.66 0.1215 0.2202 0.1191 0.0657 0.064 1.345 1.135 47.747 0.152 5.049 10.782 0.16 65669. 0.4993
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6.21 0.1620 0.2837 0.1184 0.0676 0.066 1.384 1.128 49.129 0.156 5.019 10.418 0.16 65782. 0.4810
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7.76 0.2024 0.3421 0.1176 0.0696 0.068 1.424 1.120 50.557 0.161 4.983 10.051 0.16 65909. 0.4624
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9.32 0.2429 0.3957 0.1166 0.0716 0.070 1.465 1.111 51.999 0.166 4.940 9.687 0.16 66051. 0.4437
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10.87 0.2834 0.4445 0.1153 0.0735 0.072 1.505 1.099 53.419 0.170 4.887 9.328 0.16 66209. 0.4250
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12.42 0.3239 0.4889 0.1138 0.0754 0.073 1.543 1.084 54.774 0.174 4.822 8.978 0.16 66384. 0.4063
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13.98 0.3644 0.5292 0.1120 0.0771 0.075 1.578 1.067 56.014 0.178 4.745 8.638 0.16 66574. 0.3877
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15.53 0.4049 0.5656 0.1098 0.0786 0.077 1.608 1.046 57.088 0.182 4.652 8.309 0.16 66781. 0.3693
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17.08 0.4454 0.5986 0.1072 0.0797 0.078 1.632 1.021 57.938 0.184 4.542 7.994 0.16 67006. 0.3511
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18.63 0.4859 0.6283 0.1041 0.0805 0.078 1.648 0.992 58.508 0.186 4.413 7.691 0.16 67247. 0.3329
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20.19 0.5263 0.6549 0.1006 0.0809 0.079 1.655 0.958 58.738 0.187 4.263 7.401 0.16 67505. 0.3149
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21.74 0.5668 0.6788 0.0966 0.0806 0.079 1.650 0.920 58.571 0.186 4.091 7.123 0.16 67780. 0.2969
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23.29 0.6073 0.7001 0.0920 0.0798 0.078 1.633 0.876 57.959 0.184 3.897 6.856 0.16 68072. 0.2789
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24.84 0.6478 0.7188 0.0869 0.0783 0.076 1.602 0.828 56.875 0.181 3.681 6.599 0.16 68380. 0.2609
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26.40 0.6883 0.7350 0.0813 0.0761 0.074 1.559 0.775 55.323 0.176 3.446 6.351 0.16 68704. 0.2429
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27.95 0.7288 0.7485 0.0754 0.0734 0.072 1.502 0.718 53.328 0.170 3.195 6.109 0.16 69044. 0.2250
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29.50 0.7693 0.7592 0.0692 0.0701 0.068 1.435 0.659 50.920 0.162 2.931 5.870 0.17 69399. 0.2071
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31.06 0.8098 0.7666 0.0627 0.0662 0.065 1.356 0.597 48.129 0.153 2.657 5.630 0.17 69769. 0.1892
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32.61 0.8502 0.7701 0.0561 0.0619 0.060 1.267 0.534 44.975 0.143 2.376 5.387 0.17 70155. 0.1711
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34.16 0.8907 0.7689 0.0493 0.0571 0.056 1.169 0.469 41.477 0.132 2.088 5.134 0.17 70555. 0.1529
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35.71 0.9312 0.7614 0.0424 0.0518 0.050 1.061 0.404 37.651 0.120 1.796 4.863 0.17 70969. 0.1343
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37.27 0.9717 0.7453 0.0354 0.0461 0.045 0.944 0.337 33.509 0.107 1.499 4.562 0.17 71398. 0.1151
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38.82 1.0122 0.7163 0.0283 0.0400 0.039 0.819 0.270 29.065 0.093 1.200 4.209 0.17 71841. 0.0950
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40.37 1.0527 0.6667 0.0212 0.0335 0.033 0.686 0.202 24.336 0.077 0.899 3.767 0.17 72298. 0.0736
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41.93 1.0932 0.5794 0.0141 0.0266 0.026 0.545 0.134 19.341 0.062 0.598 3.152 0.17 72768. 0.0502
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43.48 1.1337 0.4106 0.0070 0.0194 0.019 0.397 0.067 14.106 0.045 0.298 2.154 0.17 73251. 0.0242
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45.03 1.1741 0.0021 0.0000 0.0119 0.012 0.244 0.000 8.661 0.028 0.001 0.011 0.17 73746. 0.0000
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1209 0.0591 0.137 2.152 2.047 101.822 0.243 9.105 9.118 0.21 87207. 0.5670
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2.07 0.0406 0.0805 0.1204 0.0607 0.140 2.209 2.040 104.533 0.250 9.074 8.851 0.21 87308. 0.5495
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4.15 0.0811 0.1559 0.1200 0.0624 0.144 2.271 2.032 107.477 0.257 9.038 8.575 0.21 87424. 0.5312
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6.22 0.1217 0.2262 0.1194 0.0642 0.148 2.338 2.022 110.626 0.264 8.995 8.291 0.21 87558. 0.5125
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8.30 0.1623 0.2911 0.1187 0.0662 0.153 2.408 2.011 113.943 0.272 8.944 8.004 0.21 87709. 0.4933
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10.37 0.2028 0.3509 0.1179 0.0682 0.157 2.480 1.997 117.374 0.280 8.882 7.716 0.21 87879. 0.4739
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12.45 0.2434 0.4054 0.1169 0.0702 0.162 2.554 1.980 120.847 0.289 8.806 7.431 0.21 88070. 0.4545
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14.52 0.2839 0.4551 0.1157 0.0722 0.167 2.626 1.959 124.274 0.297 8.714 7.150 0.22 88281. 0.4350
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16.59 0.3245 0.5002 0.1142 0.0741 0.171 2.695 1.934 127.551 0.305 8.601 6.876 0.22 88514. 0.4156
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18.67 0.3651 0.5411 0.1124 0.0758 0.175 2.759 1.903 130.561 0.312 8.465 6.611 0.22 88769. 0.3964
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20.74 0.4056 0.5780 0.1102 0.0773 0.179 2.814 1.866 133.176 0.318 8.300 6.356 0.22 89046. 0.3774
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22.82 0.4462 0.6113 0.1076 0.0785 0.181 2.858 1.822 135.260 0.323 8.106 6.111 0.22 89346. 0.3585
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24.89 0.4868 0.6413 0.1046 0.0794 0.183 2.888 1.771 136.674 0.326 7.876 5.877 0.22 89669. 0.3399
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26.97 0.5273 0.6683 0.1010 0.0797 0.184 2.901 1.711 137.277 0.328 7.610 5.653 0.22 90014. 0.3214
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29.04 0.5679 0.6925 0.0970 0.0795 0.184 2.893 1.642 136.929 0.327 7.304 5.439 0.22 90382. 0.3030
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31.11 0.6085 0.7141 0.0924 0.0787 0.182 2.863 1.564 135.513 0.324 6.957 5.235 0.22 90773. 0.2846
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33.19 0.6490 0.7333 0.0872 0.0772 0.178 2.810 1.477 132.962 0.317 6.571 5.040 0.22 91185. 0.2662
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35.26 0.6896 0.7500 0.0817 0.0751 0.173 2.732 1.383 129.286 0.309 6.151 4.851 0.22 91619. 0.2480
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37.34 0.7301 0.7642 0.0757 0.0723 0.167 2.632 1.282 124.543 0.297 5.702 4.669 0.22 92073. 0.2298
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39.41 0.7707 0.7758 0.0694 0.0690 0.159 2.510 1.176 118.805 0.284 5.231 4.490 0.22 92549. 0.2117
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41.49 0.8113 0.7844 0.0630 0.0651 0.150 2.370 1.066 112.137 0.268 4.743 4.313 0.22 93044. 0.1936
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43.56 0.8518 0.7893 0.0563 0.0607 0.140 2.210 0.953 104.593 0.250 4.240 4.133 0.22 93560. 0.1754
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45.63 0.8924 0.7899 0.0495 0.0559 0.129 2.033 0.838 96.214 0.230 3.726 3.949 0.22 94095. 0.1571
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47.71 0.9330 0.7848 0.0425 0.0505 0.117 1.839 0.720 87.037 0.208 3.203 3.752 0.22 94650. 0.1384
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49.78 0.9735 0.7717 0.0355 0.0448 0.103 1.629 0.601 77.094 0.184 2.673 3.536 0.22 95224. 0.1191
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51.86 1.0141 0.7466 0.0284 0.0386 0.089 1.403 0.481 66.418 0.159 2.139 3.284 0.23 95816. 0.0990
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53.93 1.0547 0.7017 0.0213 0.0320 0.074 1.163 0.360 55.048 0.131 1.602 2.968 0.23 96427. 0.0774
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56.01 1.0952 0.6197 0.0141 0.0250 0.058 0.909 0.239 43.035 0.103 1.065 2.524 0.23 97056. 0.0537
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58.08 1.1358 0.4524 0.0070 0.0177 0.041 0.643 0.119 30.440 0.073 0.530 1.777 0.23 97703. 0.0267
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60.15 1.1764 0.0014 0.0000 0.0101 0.023 0.366 0.000 17.335 0.041 0.001 0.005 0.23 98364. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1211 0.0582 0.263 3.309 3.203 195.750 0.374 14.248 7.422 0.27 109007. 0.5774
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2.60 0.0406 0.0820 0.1207 0.0598 0.270 3.399 3.193 201.076 0.384 14.202 7.202 0.27 109134. 0.5593
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5.19 0.0812 0.1588 0.1202 0.0615 0.277 3.497 3.181 206.865 0.395 14.148 6.974 0.27 109279. 0.5406
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7.79 0.1219 0.2302 0.1197 0.0633 0.286 3.602 3.166 213.069 0.407 14.084 6.740 0.27 109446. 0.5213
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10.39 0.1625 0.2961 0.1190 0.0653 0.295 3.712 3.149 219.614 0.419 14.007 6.504 0.27 109635. 0.5016
|
|
12.98 0.2031 0.3567 0.1182 0.0673 0.304 3.827 3.128 226.395 0.432 13.913 6.267 0.27 109848. 0.4817
|
|
15.58 0.2437 0.4119 0.1172 0.0694 0.313 3.943 3.102 233.272 0.446 13.798 6.032 0.27 110087. 0.4617
|
|
18.17 0.2843 0.4622 0.1160 0.0714 0.322 4.058 3.070 240.073 0.459 13.657 5.801 0.27 110351. 0.4418
|
|
20.77 0.3250 0.5077 0.1146 0.0733 0.331 4.168 3.031 246.591 0.471 13.484 5.576 0.27 110643. 0.4220
|
|
23.37 0.3656 0.5489 0.1128 0.0751 0.339 4.270 2.984 252.593 0.482 13.273 5.358 0.27 110962. 0.4023
|
|
25.96 0.4062 0.5861 0.1106 0.0767 0.346 4.358 2.927 257.826 0.492 13.020 5.149 0.27 111310. 0.3829
|
|
28.56 0.4468 0.6197 0.1080 0.0779 0.351 4.429 2.859 262.019 0.500 12.717 4.949 0.27 111686. 0.3637
|
|
31.16 0.4874 0.6499 0.1050 0.0788 0.355 4.478 2.779 264.894 0.506 12.360 4.758 0.27 112091. 0.3447
|
|
33.75 0.5280 0.6771 0.1015 0.0791 0.357 4.499 2.685 266.170 0.508 11.945 4.576 0.27 112524. 0.3259
|
|
36.35 0.5687 0.7016 0.0974 0.0790 0.356 4.489 2.578 265.570 0.507 11.466 4.403 0.27 112985. 0.3072
|
|
38.95 0.6093 0.7235 0.0928 0.0782 0.352 4.443 2.456 262.859 0.502 10.923 4.237 0.27 113474. 0.2886
|
|
41.54 0.6499 0.7430 0.0877 0.0767 0.346 4.360 2.320 257.902 0.493 10.318 4.080 0.27 113991. 0.2701
|
|
44.14 0.6905 0.7601 0.0821 0.0745 0.336 4.238 2.171 250.715 0.479 9.658 3.928 0.27 114535. 0.2516
|
|
46.74 0.7311 0.7749 0.0761 0.0718 0.324 4.081 2.013 241.412 0.461 8.954 3.782 0.27 115105. 0.2332
|
|
49.33 0.7718 0.7871 0.0698 0.0684 0.309 3.890 1.847 230.132 0.440 8.214 3.640 0.28 115701. 0.2150
|
|
51.93 0.8124 0.7965 0.0633 0.0645 0.291 3.668 1.674 217.004 0.414 7.446 3.499 0.28 116322. 0.1968
|
|
54.52 0.8530 0.8026 0.0565 0.0601 0.271 3.417 1.496 202.133 0.386 6.656 3.358 0.28 116968. 0.1785
|
|
57.12 0.8936 0.8046 0.0497 0.0552 0.249 3.137 1.315 185.601 0.354 5.848 3.213 0.28 117639. 0.1601
|
|
59.72 0.9342 0.8012 0.0427 0.0498 0.225 2.831 1.130 167.478 0.320 5.027 3.061 0.28 118334. 0.1414
|
|
62.31 0.9749 0.7904 0.0356 0.0440 0.198 2.499 0.943 147.830 0.282 4.195 2.893 0.28 119053. 0.1221
|
|
64.91 1.0155 0.7683 0.0285 0.0377 0.170 2.142 0.754 126.722 0.242 3.355 2.700 0.28 119796. 0.1019
|
|
67.51 1.0561 0.7273 0.0213 0.0310 0.140 1.762 0.565 104.233 0.199 2.512 2.458 0.28 120561. 0.0803
|
|
70.10 1.0967 0.6499 0.0142 0.0239 0.108 1.360 0.375 80.463 0.154 1.669 2.115 0.28 121349. 0.0563
|
|
72.70 1.1373 0.4851 0.0070 0.0165 0.074 0.939 0.186 55.535 0.106 0.829 1.522 0.28 122160. 0.0286
|
|
75.30 1.1780 -0.0027 0.0000 0.0088 0.040 0.500 -0.001 29.594 0.057 -0.002 -0.008 0.29 122986. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1212 0.0576 0.449 4.718 4.620 334.903 0.533 20.550 6.257 0.32 130806. 0.5846
|
|
3.12 0.0406 0.0830 0.1209 0.0592 0.462 4.848 4.606 344.141 0.548 20.486 6.070 0.32 130958. 0.5662
|
|
6.24 0.0813 0.1606 0.1204 0.0609 0.475 4.990 4.589 354.199 0.564 20.412 5.876 0.32 131132. 0.5471
|
|
9.35 0.1219 0.2328 0.1199 0.0628 0.489 5.142 4.569 364.995 0.581 20.324 5.678 0.32 131332. 0.5275
|
|
12.47 0.1626 0.2995 0.1193 0.0648 0.505 5.302 4.545 376.407 0.599 20.218 5.477 0.32 131560. 0.5076
|
|
15.59 0.2032 0.3606 0.1185 0.0668 0.521 5.469 4.516 388.254 0.618 20.089 5.276 0.32 131816. 0.4873
|
|
18.71 0.2439 0.4163 0.1176 0.0689 0.537 5.639 4.480 400.296 0.637 19.929 5.077 0.32 132102. 0.4670
|
|
21.82 0.2845 0.4670 0.1164 0.0709 0.553 5.807 4.436 412.229 0.656 19.731 4.881 0.32 132420. 0.4468
|
|
24.94 0.3252 0.5128 0.1150 0.0729 0.568 5.969 4.381 423.695 0.674 19.488 4.690 0.32 132770. 0.4267
|
|
28.06 0.3658 0.5543 0.1132 0.0747 0.582 6.118 4.314 434.285 0.691 19.190 4.506 0.32 133154. 0.4068
|
|
31.18 0.4065 0.5917 0.1111 0.0763 0.595 6.248 4.233 443.551 0.706 18.830 4.329 0.32 133571. 0.3871
|
|
34.30 0.4471 0.6254 0.1085 0.0776 0.605 6.354 4.136 451.017 0.718 18.399 4.160 0.32 134023. 0.3677
|
|
37.41 0.4878 0.6558 0.1055 0.0785 0.612 6.426 4.022 456.195 0.726 17.889 3.999 0.33 134510. 0.3485
|
|
40.53 0.5284 0.6832 0.1020 0.0789 0.615 6.460 3.888 458.585 0.730 17.293 3.845 0.33 135030. 0.3295
|
|
43.65 0.5690 0.7079 0.0980 0.0788 0.614 6.448 3.733 457.704 0.728 16.605 3.699 0.33 135585. 0.3107
|
|
46.77 0.6097 0.7300 0.0933 0.0780 0.608 6.383 3.557 453.131 0.721 15.822 3.561 0.33 136173. 0.2919
|
|
49.88 0.6503 0.7498 0.0882 0.0765 0.596 6.264 3.361 444.628 0.708 14.949 3.428 0.33 136794. 0.2732
|
|
53.00 0.6910 0.7673 0.0826 0.0744 0.580 6.089 3.147 432.213 0.688 13.996 3.302 0.33 137447. 0.2546
|
|
56.12 0.7316 0.7825 0.0766 0.0716 0.558 5.861 2.918 416.082 0.662 12.978 3.181 0.33 138132. 0.2361
|
|
59.24 0.7723 0.7953 0.0703 0.0682 0.532 5.585 2.677 396.479 0.631 11.907 3.062 0.33 138848. 0.2178
|
|
62.36 0.8129 0.8054 0.0637 0.0643 0.501 5.263 2.427 373.628 0.595 10.795 2.946 0.33 139595. 0.1995
|
|
65.47 0.8536 0.8124 0.0569 0.0598 0.466 4.898 2.170 347.712 0.553 9.651 2.830 0.33 140372. 0.1812
|
|
68.59 0.8942 0.8155 0.0500 0.0549 0.428 4.492 1.907 318.877 0.508 8.481 2.712 0.33 141178. 0.1628
|
|
71.71 0.9349 0.8136 0.0430 0.0494 0.385 4.046 1.639 287.245 0.457 7.291 2.588 0.34 142013. 0.1440
|
|
74.83 0.9755 0.8048 0.0359 0.0435 0.339 3.563 1.368 252.929 0.403 6.085 2.453 0.34 142877. 0.1247
|
|
77.94 1.0162 0.7853 0.0287 0.0372 0.290 3.043 1.095 216.046 0.344 4.869 2.298 0.34 143770. 0.1045
|
|
81.06 1.0568 0.7478 0.0215 0.0304 0.237 2.490 0.820 176.735 0.281 3.647 2.104 0.34 144689. 0.0828
|
|
84.18 1.0974 0.6750 0.0143 0.0233 0.181 1.904 0.545 135.168 0.215 2.424 1.829 0.34 145637. 0.0587
|
|
87.30 1.1381 0.5146 0.0071 0.0158 0.123 1.290 0.271 91.567 0.146 1.208 1.345 0.34 146610. 0.0305
|
|
90.41 1.1787 0.0024 0.0000 0.0079 0.062 0.651 0.001 46.184 0.074 0.003 0.006 0.34 147602. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1214 0.0573 0.709 6.383 6.299 528.651 0.721 28.017 5.404 0.37 152604. 0.5895
|
|
3.64 0.0407 0.0837 0.1211 0.0589 0.729 6.561 6.280 543.367 0.741 27.934 5.242 0.37 152781. 0.5710
|
|
7.28 0.0814 0.1620 0.1207 0.0606 0.750 6.755 6.259 559.418 0.763 27.839 5.075 0.37 152984. 0.5518
|
|
10.92 0.1220 0.2347 0.1202 0.0625 0.773 6.963 6.233 576.683 0.787 27.726 4.903 0.38 153218. 0.5320
|
|
14.56 0.1627 0.3018 0.1196 0.0645 0.798 7.184 6.203 594.970 0.812 27.590 4.729 0.38 153483. 0.5119
|
|
18.20 0.2034 0.3634 0.1189 0.0665 0.823 7.414 6.165 613.999 0.838 27.421 4.554 0.38 153782. 0.4915
|
|
21.84 0.2441 0.4195 0.1180 0.0686 0.849 7.648 6.118 633.385 0.864 27.213 4.381 0.38 154116. 0.4710
|
|
25.48 0.2847 0.4704 0.1168 0.0707 0.875 7.880 6.060 652.647 0.890 26.953 4.211 0.38 154487. 0.4506
|
|
29.12 0.3254 0.5165 0.1154 0.0727 0.900 8.105 5.987 671.205 0.916 26.632 4.046 0.38 154896. 0.4303
|
|
32.76 0.3661 0.5582 0.1137 0.0746 0.923 8.312 5.898 688.397 0.939 26.236 3.886 0.38 155344. 0.4102
|
|
36.40 0.4068 0.5957 0.1116 0.0762 0.943 8.494 5.790 703.494 0.960 25.754 3.733 0.38 155832. 0.3904
|
|
40.04 0.4474 0.6296 0.1091 0.0775 0.960 8.642 5.660 715.726 0.976 25.174 3.587 0.38 156360. 0.3709
|
|
43.68 0.4881 0.6602 0.1061 0.0785 0.971 8.746 5.505 724.295 0.988 24.486 3.447 0.38 156928. 0.3515
|
|
47.32 0.5288 0.6877 0.1026 0.0789 0.977 8.795 5.323 728.395 0.994 23.679 3.315 0.38 157537. 0.3324
|
|
50.96 0.5695 0.7125 0.0986 0.0788 0.975 8.781 5.113 727.238 0.992 22.744 3.189 0.38 158185. 0.3134
|
|
54.60 0.6102 0.7348 0.0940 0.0780 0.966 8.695 4.874 720.140 0.982 21.679 3.070 0.38 158872. 0.2946
|
|
58.24 0.6508 0.7548 0.0888 0.0766 0.948 8.533 4.606 706.705 0.964 20.488 2.956 0.38 159598. 0.2758
|
|
61.88 0.6915 0.7726 0.0832 0.0744 0.921 8.295 4.313 686.952 0.937 19.186 2.848 0.38 160362. 0.2571
|
|
65.52 0.7322 0.7882 0.0771 0.0716 0.887 7.984 4.000 661.191 0.902 17.793 2.744 0.38 161163. 0.2385
|
|
69.16 0.7729 0.8015 0.0708 0.0682 0.845 7.605 3.671 629.818 0.859 16.327 2.643 0.39 162000. 0.2201
|
|
72.80 0.8135 0.8122 0.0642 0.0643 0.795 7.163 3.328 593.196 0.809 14.804 2.545 0.39 162873. 0.2018
|
|
76.44 0.8542 0.8199 0.0574 0.0598 0.740 6.661 2.976 551.619 0.753 13.235 2.447 0.39 163780. 0.1834
|
|
80.08 0.8949 0.8240 0.0504 0.0548 0.678 6.102 2.615 505.324 0.689 11.631 2.347 0.39 164723. 0.1650
|
|
83.72 0.9356 0.8234 0.0433 0.0492 0.610 5.488 2.248 454.509 0.620 9.999 2.243 0.39 165699. 0.1462
|
|
87.36 0.9762 0.8161 0.0362 0.0433 0.536 4.822 1.876 399.354 0.545 8.345 2.131 0.39 166708. 0.1269
|
|
91.00 1.0169 0.7987 0.0289 0.0368 0.456 4.106 1.501 340.051 0.464 6.676 2.002 0.39 167751. 0.1066
|
|
94.64 1.0576 0.7641 0.0217 0.0300 0.371 3.343 1.124 276.821 0.378 4.999 1.842 0.40 168826. 0.0849
|
|
98.28 1.0983 0.6951 0.0144 0.0227 0.282 2.535 0.747 209.944 0.286 3.322 1.613 0.40 169932. 0.0606
|
|
101.92 1.1390 0.5382 0.0072 0.0151 0.187 1.688 0.371 139.784 0.191 1.651 1.205 0.40 171070. 0.0319
|
|
105.56 1.1796 -0.0019 0.0000 0.0072 0.089 0.806 -0.001 66.737 0.091 -0.003 -0.004 0.40 172227. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1217 0.0571 1.055 8.313 8.241 786.796 0.939 36.657 4.751 0.43 174401. 0.5928
|
|
4.16 0.0407 0.0841 0.1213 0.0587 1.085 8.545 8.219 808.810 0.965 36.557 4.609 0.43 174602. 0.5743
|
|
8.32 0.0814 0.1628 0.1209 0.0605 1.117 8.800 8.193 832.874 0.994 36.441 4.462 0.43 174835. 0.5550
|
|
12.49 0.1221 0.2360 0.1205 0.0623 1.152 9.074 8.162 858.814 1.025 36.303 4.310 0.43 175101. 0.5352
|
|
16.65 0.1628 0.3034 0.1199 0.0643 1.189 9.365 8.124 886.361 1.058 36.135 4.157 0.43 175404. 0.5150
|
|
20.81 0.2035 0.3653 0.1192 0.0664 1.227 9.668 8.077 915.100 1.092 35.928 4.004 0.43 175745. 0.4946
|
|
24.97 0.2442 0.4216 0.1184 0.0686 1.267 9.979 8.019 944.463 1.127 35.670 3.851 0.43 176127. 0.4740
|
|
29.14 0.2849 0.4728 0.1173 0.0707 1.306 10.288 7.946 973.722 1.162 35.345 3.701 0.43 176552. 0.4535
|
|
33.30 0.3256 0.5191 0.1160 0.0727 1.344 10.586 7.855 1002.002 1.196 34.940 3.556 0.43 177019. 0.4332
|
|
37.46 0.3663 0.5609 0.1143 0.0746 1.379 10.864 7.742 1028.289 1.227 34.438 3.415 0.43 177532. 0.4130
|
|
41.62 0.4070 0.5985 0.1122 0.0763 1.410 11.109 7.604 1051.472 1.255 33.822 3.280 0.43 178090. 0.3931
|
|
45.79 0.4477 0.6325 0.1098 0.0777 1.435 11.309 7.436 1070.367 1.278 33.078 3.151 0.43 178694. 0.3735
|
|
49.95 0.4884 0.6632 0.1068 0.0787 1.453 11.450 7.237 1083.750 1.294 32.189 3.029 0.43 179345. 0.3541
|
|
54.11 0.5291 0.6909 0.1033 0.0791 1.462 11.520 7.001 1090.390 1.302 31.142 2.912 0.43 180041. 0.3349
|
|
58.27 0.5698 0.7158 0.0993 0.0791 1.460 11.506 6.728 1089.082 1.300 29.926 2.802 0.44 180783. 0.3159
|
|
62.44 0.6105 0.7383 0.0947 0.0783 1.447 11.398 6.415 1078.775 1.288 28.536 2.697 0.44 181570. 0.2970
|
|
66.60 0.6512 0.7585 0.0895 0.0769 1.420 11.187 6.065 1058.847 1.264 26.978 2.598 0.44 182401. 0.2781
|
|
70.76 0.6919 0.7766 0.0839 0.0747 1.380 10.875 5.681 1029.308 1.229 25.271 2.504 0.44 183275. 0.2594
|
|
74.92 0.7326 0.7926 0.0778 0.0719 1.328 10.466 5.270 990.624 1.182 23.442 2.413 0.44 184192. 0.2408
|
|
79.08 0.7733 0.8063 0.0714 0.0685 1.265 9.967 4.837 943.396 1.126 21.515 2.326 0.44 185150. 0.2223
|
|
83.25 0.8140 0.8175 0.0648 0.0645 1.191 9.384 4.386 888.181 1.060 19.511 2.240 0.44 186149. 0.2039
|
|
87.41 0.8547 0.8259 0.0579 0.0599 1.107 8.721 3.922 825.431 0.985 17.446 2.155 0.44 187187. 0.1855
|
|
91.57 0.8954 0.8308 0.0509 0.0548 1.013 7.982 3.447 755.508 0.902 15.333 2.070 0.45 188266. 0.1670
|
|
95.73 0.9361 0.8313 0.0437 0.0493 0.910 7.171 2.964 678.711 0.810 13.183 1.981 0.45 189383. 0.1482
|
|
99.90 0.9768 0.8254 0.0365 0.0432 0.798 6.290 2.474 595.317 0.711 11.003 1.885 0.45 190538. 0.1288
|
|
104.06 1.0175 0.8100 0.0292 0.0367 0.678 5.342 1.979 505.613 0.604 8.803 1.775 0.45 191731. 0.1086
|
|
108.22 1.0582 0.7780 0.0219 0.0298 0.550 4.331 1.482 409.937 0.489 6.592 1.640 0.45 192960. 0.0868
|
|
112.38 1.0989 0.7126 0.0145 0.0224 0.414 3.262 0.984 308.716 0.369 4.379 1.446 0.45 194226. 0.0624
|
|
116.55 1.1396 0.5596 0.0072 0.0147 0.272 2.139 0.489 202.501 0.242 2.175 1.095 0.46 195528. 0.0333
|
|
120.71 1.1803 -0.0046 0.0000 0.0067 0.123 0.971 -0.002 91.888 0.110 -0.008 -0.009 0.46 196850. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1219 0.0571 1.502 10.515 10.450 1119.684 1.188 46.481 4.233 0.48 196196. 0.5948
|
|
4.68 0.0407 0.0843 0.1216 0.0587 1.544 10.810 10.423 1151.065 1.221 46.363 4.107 0.48 196422. 0.5763
|
|
9.37 0.0814 0.1633 0.1212 0.0604 1.590 11.133 10.393 1185.450 1.258 46.227 3.976 0.48 196683. 0.5572
|
|
14.05 0.1221 0.2367 0.1208 0.0623 1.640 11.482 10.357 1222.617 1.297 46.066 3.842 0.48 196983. 0.5374
|
|
18.74 0.1629 0.3044 0.1203 0.0643 1.693 11.854 10.313 1262.198 1.339 45.871 3.706 0.48 197323. 0.5173
|
|
23.42 0.2036 0.3665 0.1196 0.0665 1.748 12.243 10.258 1303.621 1.383 45.627 3.569 0.48 197707. 0.4968
|
|
28.11 0.2443 0.4230 0.1188 0.0686 1.805 12.642 10.189 1346.083 1.428 45.320 3.433 0.48 198136. 0.4763
|
|
32.79 0.2850 0.4743 0.1178 0.0708 1.862 13.040 10.101 1388.545 1.473 44.931 3.300 0.48 198613. 0.4558
|
|
37.48 0.3257 0.5207 0.1165 0.0729 1.917 13.427 9.991 1429.735 1.517 44.441 3.170 0.48 199140. 0.4355
|
|
42.16 0.3664 0.5626 0.1149 0.0748 1.969 13.788 9.853 1468.180 1.558 43.828 3.044 0.49 199717. 0.4153
|
|
46.84 0.4071 0.6004 0.1129 0.0766 2.015 14.108 9.683 1502.247 1.594 43.071 2.924 0.49 200345. 0.3954
|
|
51.53 0.4479 0.6345 0.1105 0.0780 2.052 14.371 9.476 1530.196 1.624 42.148 2.809 0.49 201025. 0.3758
|
|
56.21 0.4886 0.6652 0.1076 0.0790 2.079 14.559 9.226 1550.234 1.645 41.039 2.699 0.49 201758. 0.3564
|
|
60.90 0.5293 0.6930 0.1042 0.0796 2.093 14.656 8.931 1560.554 1.656 39.727 2.596 0.49 202542. 0.3372
|
|
65.58 0.5700 0.7181 0.1002 0.0795 2.091 14.645 8.587 1559.395 1.655 38.197 2.498 0.49 203378. 0.3181
|
|
70.27 0.6107 0.7408 0.0956 0.0788 2.072 14.512 8.193 1545.215 1.640 36.441 2.405 0.49 204264. 0.2992
|
|
74.95 0.6514 0.7612 0.0904 0.0773 2.034 14.247 7.749 1517.072 1.610 34.467 2.317 0.49 205200. 0.2803
|
|
79.63 0.6921 0.7796 0.0847 0.0752 1.978 13.852 7.261 1474.951 1.565 32.299 2.233 0.49 206185. 0.2615
|
|
84.32 0.7328 0.7958 0.0786 0.0724 1.904 13.331 6.738 1419.516 1.506 29.971 2.153 0.49 207218. 0.2429
|
|
89.00 0.7736 0.8099 0.0721 0.0689 1.813 12.694 6.186 1351.648 1.434 27.515 2.076 0.50 208297. 0.2244
|
|
93.69 0.8143 0.8217 0.0654 0.0649 1.706 11.947 5.611 1272.165 1.350 24.958 2.001 0.50 209422. 0.2060
|
|
98.37 0.8550 0.8307 0.0585 0.0602 1.585 11.098 5.019 1181.734 1.254 22.322 1.926 0.50 210593. 0.1876
|
|
103.06 0.8957 0.8364 0.0515 0.0551 1.449 10.151 4.412 1080.884 1.147 19.623 1.851 0.50 211807. 0.1690
|
|
107.74 0.9364 0.8378 0.0442 0.0495 1.301 9.110 3.794 970.053 1.029 16.874 1.774 0.50 213065. 0.1502
|
|
112.43 0.9771 0.8333 0.0369 0.0433 1.139 7.979 3.167 849.642 0.901 14.087 1.691 0.50 214366. 0.1308
|
|
117.11 1.0178 0.8195 0.0296 0.0367 0.966 6.762 2.534 720.065 0.764 11.272 1.596 0.51 215709. 0.1104
|
|
121.79 1.0586 0.7900 0.0221 0.0297 0.780 5.464 1.898 581.813 0.617 8.441 1.479 0.51 217094. 0.0886
|
|
126.48 1.0993 0.7280 0.0147 0.0222 0.584 4.090 1.261 435.500 0.462 5.607 1.313 0.51 218519. 0.0641
|
|
131.16 1.1400 0.5791 0.0073 0.0144 0.378 2.648 0.626 281.933 0.299 2.785 1.007 0.51 219984. 0.0346
|
|
135.85 1.1807 -0.0060 0.0000 0.0062 0.164 1.145 -0.003 121.964 0.129 -0.012 -0.010 0.51 221470. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1221 0.0572 2.063 13.003 12.926 1538.361 1.469 57.496 3.811 0.54 217988. 0.5956
|
|
5.21 0.0407 0.0844 0.1218 0.0588 2.121 13.366 12.896 1581.409 1.510 57.363 3.699 0.54 218240. 0.5773
|
|
10.41 0.0814 0.1635 0.1215 0.0605 2.184 13.766 12.862 1628.705 1.555 57.211 3.582 0.54 218530. 0.5583
|
|
15.62 0.1222 0.2370 0.1211 0.0624 2.253 14.200 12.822 1679.987 1.604 57.031 3.462 0.54 218862. 0.5388
|
|
20.83 0.1629 0.3049 0.1207 0.0645 2.326 14.663 12.772 1734.781 1.657 56.812 3.339 0.54 219239. 0.5187
|
|
26.03 0.2036 0.3671 0.1201 0.0666 2.404 15.149 12.711 1792.335 1.712 56.536 3.217 0.54 219665. 0.4984
|
|
31.24 0.2443 0.4238 0.1193 0.0688 2.483 15.650 12.632 1851.563 1.768 56.186 3.094 0.54 220142. 0.4780
|
|
36.44 0.2851 0.4752 0.1184 0.0710 2.563 16.153 12.531 1911.038 1.825 55.738 2.974 0.54 220672. 0.4576
|
|
41.65 0.3258 0.5217 0.1172 0.0732 2.640 16.642 12.402 1968.986 1.880 55.166 2.857 0.54 221257. 0.4373
|
|
46.86 0.3665 0.5636 0.1156 0.0752 2.713 17.102 12.240 2023.328 1.932 54.443 2.744 0.54 221898. 0.4172
|
|
52.06 0.4072 0.6015 0.1137 0.0770 2.778 17.511 12.037 2071.747 1.978 53.541 2.635 0.54 222596. 0.3974
|
|
57.27 0.4480 0.6356 0.1114 0.0785 2.832 17.849 11.788 2111.772 2.017 52.431 2.532 0.54 223352. 0.3778
|
|
62.48 0.4887 0.6665 0.1085 0.0796 2.871 18.095 11.486 2140.845 2.044 51.088 2.433 0.54 224167. 0.3584
|
|
67.68 0.5294 0.6944 0.1051 0.0801 2.892 18.226 11.126 2156.407 2.059 49.489 2.340 0.54 225039. 0.3393
|
|
72.89 0.5701 0.7196 0.1011 0.0801 2.891 18.223 10.705 2155.966 2.059 47.614 2.252 0.54 225969. 0.3202
|
|
78.09 0.6109 0.7424 0.0965 0.0794 2.866 18.065 10.219 2137.332 2.041 45.453 2.169 0.55 226955. 0.3013
|
|
83.30 0.6516 0.7631 0.0914 0.0780 2.815 17.742 9.670 2099.131 2.005 43.014 2.090 0.55 227997. 0.2824
|
|
88.51 0.6923 0.7817 0.0857 0.0759 2.737 17.253 9.067 2041.286 1.949 40.328 2.015 0.55 229092. 0.2637
|
|
93.71 0.7330 0.7983 0.0795 0.0730 2.635 16.606 8.416 1964.711 1.876 37.437 1.943 0.55 230241. 0.2450
|
|
98.92 0.7738 0.8128 0.0730 0.0695 2.509 15.811 7.730 1870.654 1.786 34.381 1.874 0.55 231442. 0.2265
|
|
104.13 0.8145 0.8250 0.0663 0.0654 2.361 14.878 7.014 1760.286 1.681 31.197 1.807 0.55 232694. 0.2080
|
|
109.33 0.8552 0.8346 0.0593 0.0607 2.192 13.816 6.275 1634.556 1.561 27.910 1.741 0.55 233996. 0.1896
|
|
114.54 0.8959 0.8410 0.0521 0.0555 2.004 12.629 5.518 1494.218 1.427 24.542 1.675 0.56 235346. 0.1710
|
|
119.74 0.9367 0.8433 0.0448 0.0498 1.797 11.325 4.746 1339.890 1.280 21.109 1.607 0.56 236746. 0.1521
|
|
124.95 0.9774 0.8400 0.0374 0.0436 1.572 9.907 3.963 1172.134 1.119 17.627 1.533 0.56 238192. 0.1327
|
|
130.16 1.0181 0.8279 0.0300 0.0368 1.330 8.381 3.172 991.528 0.947 14.108 1.451 0.56 239686. 0.1123
|
|
135.36 1.0588 0.8006 0.0224 0.0297 1.071 6.751 2.376 798.752 0.763 10.567 1.349 0.57 241226. 0.0904
|
|
140.57 1.0996 0.7419 0.0149 0.0221 0.797 5.026 1.578 594.667 0.568 7.020 1.204 0.57 242810. 0.0657
|
|
145.78 1.1403 0.5973 0.0074 0.0141 0.510 3.215 0.784 380.404 0.363 3.486 0.935 0.57 244439. 0.0360
|
|
150.98 1.1810 -0.0072 0.0000 0.0058 0.211 1.328 -0.004 157.137 0.150 -0.017 -0.011 0.57 246089. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1224 0.0574 2.756 15.790 15.673 2054.899 1.784 69.714 3.459 0.59 239780. 0.5953
|
|
5.73 0.0407 0.0843 0.1221 0.0590 2.832 16.229 15.640 2112.093 1.834 69.569 3.359 0.59 240055. 0.5773
|
|
11.46 0.0815 0.1634 0.1218 0.0607 2.917 16.713 15.604 2175.132 1.888 69.405 3.254 0.59 240374. 0.5586
|
|
17.19 0.1222 0.2370 0.1215 0.0626 3.009 17.241 15.560 2243.732 1.948 69.212 3.145 0.59 240739. 0.5393
|
|
22.91 0.1629 0.3049 0.1211 0.0647 3.108 17.806 15.507 2317.314 2.012 68.975 3.035 0.59 241153. 0.5195
|
|
28.64 0.2037 0.3672 0.1206 0.0669 3.212 18.402 15.440 2394.937 2.079 68.677 2.924 0.59 241621. 0.4994
|
|
34.37 0.2444 0.4239 0.1199 0.0691 3.319 19.019 15.354 2475.191 2.149 68.293 2.814 0.59 242145. 0.4792
|
|
40.10 0.2851 0.4754 0.1190 0.0714 3.428 19.641 15.242 2556.179 2.219 67.795 2.705 0.59 242727. 0.4589
|
|
45.83 0.3259 0.5220 0.1179 0.0736 3.534 20.251 15.097 2635.505 2.288 67.151 2.598 0.59 243370. 0.4388
|
|
51.56 0.3666 0.5640 0.1164 0.0757 3.635 20.826 14.911 2710.312 2.353 66.325 2.495 0.59 244075. 0.4188
|
|
57.28 0.4073 0.6019 0.1146 0.0776 3.725 21.341 14.676 2777.398 2.411 65.281 2.397 0.59 244843. 0.3991
|
|
63.01 0.4481 0.6361 0.1123 0.0791 3.800 21.771 14.384 2833.320 2.460 63.982 2.303 0.60 245675. 0.3796
|
|
68.74 0.4888 0.6670 0.1095 0.0803 3.855 22.087 14.028 2874.531 2.495 62.396 2.213 0.60 246572. 0.3603
|
|
74.47 0.5296 0.6950 0.1062 0.0809 3.886 22.264 13.600 2897.474 2.515 60.491 2.129 0.60 247533. 0.3412
|
|
80.20 0.5703 0.7204 0.1022 0.0809 3.887 22.273 13.095 2898.715 2.516 58.245 2.049 0.60 248557. 0.3223
|
|
85.93 0.6110 0.7434 0.0977 0.0803 3.856 22.093 12.510 2875.223 2.496 55.643 1.973 0.60 249643. 0.3034
|
|
91.65 0.6518 0.7642 0.0925 0.0789 3.788 21.707 11.846 2825.042 2.452 52.692 1.902 0.60 250790. 0.2845
|
|
97.38 0.6925 0.7831 0.0868 0.0767 3.685 21.115 11.113 2747.984 2.386 49.430 1.834 0.60 251998. 0.2658
|
|
103.11 0.7332 0.8000 0.0806 0.0739 3.547 20.326 10.321 2645.266 2.296 45.908 1.770 0.60 253263. 0.2471
|
|
108.84 0.7740 0.8148 0.0740 0.0703 3.378 19.353 9.483 2518.615 2.186 42.180 1.708 0.61 254586. 0.2286
|
|
114.57 0.8147 0.8275 0.0672 0.0662 3.178 18.208 8.608 2369.663 2.057 38.287 1.648 0.61 255965. 0.2101
|
|
120.30 0.8554 0.8377 0.0601 0.0614 2.950 16.902 7.703 2199.741 1.910 34.265 1.588 0.61 257398. 0.1916
|
|
126.02 0.8962 0.8448 0.0529 0.0561 2.695 15.444 6.776 2009.897 1.745 30.139 1.529 0.61 258886. 0.1730
|
|
131.75 0.9369 0.8480 0.0455 0.0503 2.415 13.838 5.830 1800.976 1.563 25.931 1.468 0.61 260427. 0.1541
|
|
137.48 0.9776 0.8458 0.0380 0.0439 2.110 12.092 4.869 1573.745 1.366 21.658 1.403 0.62 262019. 0.1346
|
|
143.21 1.0184 0.8352 0.0304 0.0371 1.782 10.212 3.898 1328.990 1.154 17.339 1.330 0.62 263664. 0.1142
|
|
148.94 1.0591 0.8100 0.0228 0.0298 1.432 8.203 2.920 1067.626 0.927 12.989 1.241 0.62 265358. 0.0921
|
|
154.67 1.0998 0.7544 0.0151 0.0221 1.061 6.077 1.940 790.825 0.687 8.629 1.113 0.62 267103. 0.0674
|
|
160.39 1.1406 0.6139 0.0075 0.0140 0.671 3.843 0.963 500.127 0.434 4.282 0.873 0.63 268895. 0.0372
|
|
166.12 1.1813 -0.0111 -0.0001 0.0055 0.264 1.515 -0.007 197.114 0.171 -0.029 -0.015 0.63 270708. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1226 0.0578 3.604 18.930 18.692 2687.580 2.139 83.142 3.155 0.64 261569. 0.5928
|
|
6.28 0.0409 0.0843 0.1224 0.0594 3.703 19.451 18.657 2761.477 2.198 82.987 3.064 0.64 261870. 0.5753
|
|
12.55 0.0818 0.1634 0.1221 0.0611 3.813 20.026 18.619 2843.237 2.263 82.816 2.970 0.64 262219. 0.5570
|
|
18.83 0.1227 0.2371 0.1219 0.0631 3.933 20.656 18.574 2932.571 2.334 82.616 2.873 0.64 262618. 0.5381
|
|
25.10 0.1636 0.3052 0.1215 0.0651 4.062 21.334 18.519 3028.831 2.410 82.371 2.773 0.64 263072. 0.5187
|
|
31.38 0.2045 0.3677 0.1210 0.0673 4.199 22.052 18.449 3130.864 2.491 82.060 2.673 0.64 263584. 0.4990
|
|
37.65 0.2454 0.4246 0.1204 0.0696 4.341 22.799 18.357 3236.917 2.576 81.653 2.572 0.64 264158. 0.4790
|
|
43.93 0.2864 0.4763 0.1196 0.0719 4.485 23.557 18.237 3344.554 2.662 81.116 2.473 0.65 264796. 0.4590
|
|
50.20 0.3273 0.5230 0.1186 0.0742 4.627 24.305 18.077 3450.615 2.746 80.408 2.376 0.65 265502. 0.4391
|
|
56.48 0.3682 0.5651 0.1172 0.0764 4.762 25.013 17.869 3551.252 2.826 79.483 2.282 0.65 266276. 0.4193
|
|
62.76 0.4091 0.6031 0.1155 0.0783 4.884 25.653 17.602 3642.061 2.898 78.293 2.192 0.65 267120. 0.3997
|
|
69.03 0.4500 0.6373 0.1133 0.0800 4.986 26.190 17.265 3718.253 2.959 76.793 2.106 0.65 268035. 0.3803
|
|
75.31 0.4909 0.6683 0.1105 0.0812 5.062 26.588 16.847 3774.858 3.004 74.937 2.024 0.65 269021. 0.3611
|
|
81.58 0.5318 0.6964 0.1072 0.0819 5.105 26.814 16.342 3806.929 3.029 72.689 1.947 0.65 270078. 0.3421
|
|
87.86 0.5727 0.7218 0.1033 0.0819 5.109 26.834 15.741 3809.747 3.032 70.016 1.874 0.65 271205. 0.3232
|
|
94.13 0.6136 0.7449 0.0987 0.0813 5.068 26.619 15.041 3779.196 3.007 66.900 1.805 0.65 272400. 0.3043
|
|
100.41 0.6545 0.7660 0.0934 0.0798 4.979 26.150 14.243 3712.637 2.954 63.353 1.740 0.66 273663. 0.2854
|
|
106.69 0.6954 0.7850 0.0876 0.0776 4.841 25.426 13.358 3609.829 2.873 59.418 1.678 0.66 274991. 0.2666
|
|
112.96 0.7363 0.8022 0.0814 0.0747 4.657 24.458 12.401 3472.456 2.763 55.160 1.620 0.66 276384. 0.2479
|
|
119.24 0.7772 0.8173 0.0747 0.0710 4.429 23.264 11.386 3302.906 2.628 50.646 1.564 0.66 277840. 0.2293
|
|
125.51 0.8182 0.8303 0.0677 0.0667 4.162 21.859 10.325 3103.419 2.470 45.927 1.509 0.66 279357. 0.2108
|
|
131.79 0.8591 0.8409 0.0605 0.0619 3.857 20.256 9.228 2875.825 2.289 41.047 1.455 0.67 280934. 0.1922
|
|
138.06 0.9000 0.8485 0.0532 0.0564 3.516 18.465 8.102 2621.530 2.086 36.039 1.402 0.67 282571. 0.1734
|
|
144.34 0.9409 0.8522 0.0456 0.0504 3.140 16.494 6.953 2341.672 1.863 30.926 1.347 0.67 284265. 0.1543
|
|
150.61 0.9818 0.8504 0.0380 0.0438 2.732 14.350 5.785 2037.288 1.621 25.733 1.288 0.67 286017. 0.1347
|
|
156.89 1.0227 0.8402 0.0302 0.0368 2.292 12.040 4.604 1709.435 1.360 20.479 1.222 0.68 287825. 0.1139
|
|
163.17 1.0636 0.8149 0.0224 0.0292 1.823 9.575 3.414 1359.378 1.082 15.187 1.139 0.68 289688. 0.0915
|
|
169.44 1.1045 0.7569 0.0146 0.0213 1.326 6.965 2.221 988.829 0.787 9.881 1.019 0.68 291606. 0.0660
|
|
175.72 1.1454 0.6007 0.0068 0.0129 0.805 4.227 1.032 600.169 0.478 4.590 0.780 0.68 293575. 0.0344
|
|
181.99 1.1863
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1229 0.0589 4.667 22.625 21.982 3479.816 2.556 97.775 2.865 0.70 283355. 0.5839
|
|
6.80 0.0409 0.0831 0.1227 0.0604 4.790 23.225 21.946 3572.167 2.624 97.614 2.787 0.70 283682. 0.5674
|
|
13.61 0.0819 0.1613 0.1225 0.0622 4.928 23.892 21.907 3674.671 2.699 97.440 2.704 0.70 284059. 0.5501
|
|
20.41 0.1228 0.2343 0.1222 0.0641 5.078 24.622 21.862 3787.036 2.782 97.243 2.618 0.70 284490. 0.5321
|
|
27.22 0.1638 0.3020 0.1219 0.0661 5.241 25.412 21.808 3908.533 2.871 97.003 2.531 0.70 284981. 0.5137
|
|
34.02 0.2047 0.3642 0.1215 0.0683 5.415 26.253 21.739 4037.779 2.966 96.696 2.442 0.70 285536. 0.4949
|
|
40.82 0.2456 0.4211 0.1210 0.0706 5.596 27.129 21.648 4172.613 3.065 96.291 2.353 0.70 286157. 0.4759
|
|
47.63 0.2866 0.4730 0.1203 0.0729 5.780 28.022 21.525 4309.999 3.166 95.744 2.265 0.70 286848. 0.4568
|
|
54.43 0.3275 0.5200 0.1194 0.0752 5.962 28.906 21.359 4445.960 3.266 95.006 2.179 0.70 287611. 0.4377
|
|
61.24 0.3685 0.5625 0.1182 0.0774 6.136 29.749 21.137 4575.603 3.361 94.020 2.095 0.70 288450. 0.4187
|
|
68.04 0.4094 0.6009 0.1165 0.0794 6.294 30.514 20.846 4693.271 3.447 92.724 2.015 0.70 289365. 0.3998
|
|
74.84 0.4503 0.6357 0.1144 0.0811 6.427 31.161 20.471 4792.790 3.521 91.057 1.937 0.70 290357. 0.3810
|
|
81.65 0.4913 0.6671 0.1118 0.0823 6.528 31.649 20.001 4867.725 3.576 88.963 1.864 0.70 291427. 0.3623
|
|
88.45 0.5322 0.6955 0.1086 0.0831 6.587 31.934 19.422 4911.585 3.608 86.391 1.794 0.71 292574. 0.3436
|
|
95.26 0.5732 0.7213 0.1047 0.0832 6.595 31.976 18.728 4918.039 3.613 83.301 1.727 0.71 293797. 0.3249
|
|
102.06 0.6141 0.7447 0.1001 0.0826 6.546 31.738 17.912 4881.407 3.586 79.671 1.664 0.71 295096. 0.3061
|
|
108.86 0.6550 0.7659 0.0949 0.0812 6.434 31.194 16.976 4797.842 3.524 75.509 1.605 0.71 296468. 0.2874
|
|
115.67 0.6960 0.7853 0.0891 0.0789 6.258 30.341 15.933 4666.601 3.428 70.869 1.549 0.71 297911. 0.2687
|
|
122.47 0.7369 0.8027 0.0827 0.0759 6.021 29.191 14.799 4489.692 3.298 65.828 1.495 0.72 299425. 0.2500
|
|
129.27 0.7779 0.8183 0.0760 0.0722 5.727 27.764 13.594 4270.299 3.137 60.466 1.444 0.72 301006. 0.2314
|
|
136.08 0.8188 0.8318 0.0689 0.0679 5.379 26.082 12.332 4011.478 2.947 54.851 1.394 0.72 302654. 0.2128
|
|
142.88 0.8597 0.8429 0.0616 0.0629 4.983 24.159 11.024 3715.716 2.729 49.034 1.346 0.72 304367. 0.1942
|
|
149.69 0.9007 0.8512 0.0541 0.0573 4.539 22.008 9.680 3384.918 2.486 43.055 1.297 0.72 306144. 0.1754
|
|
156.49 0.9416 0.8557 0.0464 0.0511 4.051 19.639 8.306 3020.593 2.219 36.946 1.247 0.73 307983. 0.1562
|
|
163.29 0.9826 0.8549 0.0386 0.0444 3.519 17.062 6.910 2624.196 1.928 30.734 1.194 0.73 309885. 0.1364
|
|
170.10 1.0235 0.8458 0.0307 0.0372 2.947 14.287 5.495 2197.389 1.614 24.442 1.134 0.73 311848. 0.1156
|
|
176.90 1.0644 0.8214 0.0227 0.0295 2.336 11.328 4.068 1742.315 1.280 18.096 1.059 0.74 313870. 0.0928
|
|
183.71 1.1054 0.7631 0.0147 0.0213 1.692 8.205 2.636 1261.933 0.927 11.725 0.947 0.74 315951. 0.0669
|
|
190.51 1.1463 0.6007 0.0067 0.0129 1.020 4.943 1.206 760.299 0.558 5.363 0.719 0.74 318088. 0.0343
|
|
197.31 1.1873
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1231 0.0612 6.060 27.283 25.537 4519.030 3.082 113.588 2.563 0.75 305139. 0.5630
|
|
7.28 0.0407 0.0797 0.1229 0.0627 6.210 27.958 25.499 4630.938 3.159 113.421 2.497 0.75 305488. 0.5481
|
|
14.56 0.0814 0.1550 0.1227 0.0644 6.377 28.711 25.460 4755.518 3.244 113.248 2.428 0.75 305890. 0.5326
|
|
21.85 0.1221 0.2257 0.1225 0.0663 6.561 29.537 25.418 4892.483 3.337 113.059 2.356 0.75 306350. 0.5164
|
|
29.13 0.1627 0.2915 0.1223 0.0683 6.760 30.434 25.368 5041.012 3.438 112.836 2.282 0.75 306872. 0.4997
|
|
36.41 0.2034 0.3523 0.1220 0.0704 6.973 31.391 25.304 5199.462 3.547 112.554 2.207 0.75 307462. 0.4826
|
|
43.69 0.2441 0.4084 0.1216 0.0727 7.195 32.391 25.220 5365.167 3.660 112.179 2.132 0.75 308122. 0.4654
|
|
50.97 0.2848 0.4598 0.1210 0.0750 7.422 33.412 25.104 5534.313 3.775 111.664 2.057 0.75 308856. 0.4481
|
|
58.26 0.3255 0.5068 0.1202 0.0772 7.646 34.424 24.944 5701.871 3.889 110.951 1.984 0.75 309668. 0.4307
|
|
65.54 0.3662 0.5497 0.1192 0.0794 7.861 35.389 24.724 5861.669 3.998 109.972 1.913 0.75 310559. 0.4135
|
|
72.82 0.4069 0.5888 0.1177 0.0814 8.055 36.264 24.427 6006.570 4.097 108.650 1.845 0.76 311532. 0.3962
|
|
80.10 0.4476 0.6246 0.1159 0.0830 8.219 37.002 24.035 6128.844 4.180 106.909 1.779 0.76 312587. 0.3790
|
|
87.38 0.4882 0.6573 0.1134 0.0843 8.342 37.556 23.532 6220.623 4.243 104.672 1.716 0.76 313726. 0.3618
|
|
94.67 0.5289 0.6872 0.1104 0.0850 8.414 37.879 22.903 6274.149 4.280 101.874 1.656 0.76 314948. 0.3444
|
|
101.95 0.5696 0.7143 0.1067 0.0851 8.424 37.926 22.136 6281.981 4.285 98.462 1.598 0.76 316252. 0.3268
|
|
109.23 0.6103 0.7390 0.1023 0.0845 8.364 37.657 21.223 6237.305 4.254 94.402 1.543 0.76 317637. 0.3090
|
|
116.51 0.6510 0.7615 0.0972 0.0831 8.227 37.040 20.165 6135.173 4.185 89.695 1.491 0.77 319100. 0.2910
|
|
123.79 0.6917 0.7818 0.0915 0.0809 8.011 36.067 18.974 5974.094 4.075 84.397 1.441 0.77 320639. 0.2727
|
|
131.08 0.7324 0.8001 0.0852 0.0780 7.719 34.750 17.670 5755.842 3.926 78.597 1.392 0.77 322254. 0.2544
|
|
138.36 0.7730 0.8165 0.0784 0.0743 7.354 33.108 16.275 5483.836 3.740 72.390 1.346 0.77 323941. 0.2360
|
|
145.64 0.8137 0.8307 0.0714 0.0699 6.922 31.162 14.807 5161.585 3.521 65.860 1.301 0.77 325698. 0.2176
|
|
152.92 0.8544 0.8427 0.0640 0.0649 6.426 28.931 13.281 4792.090 3.269 59.074 1.257 0.78 327525. 0.1991
|
|
160.20 0.8951 0.8520 0.0564 0.0593 5.871 26.431 11.709 4377.911 2.986 52.082 1.213 0.78 329420. 0.1804
|
|
167.49 0.9358 0.8577 0.0487 0.0531 5.259 23.675 10.099 3921.404 2.675 44.922 1.168 0.78 331382. 0.1613
|
|
174.77 0.9765 0.8582 0.0408 0.0464 4.593 20.678 8.459 3425.051 2.336 37.624 1.120 0.79 333410. 0.1416
|
|
182.05 1.0172 0.8503 0.0327 0.0392 3.878 17.459 6.793 2891.899 1.973 30.216 1.065 0.79 335502. 0.1207
|
|
189.33 1.0579 0.8270 0.0246 0.0315 3.119 14.042 5.109 2325.826 1.586 22.725 0.996 0.79 337657. 0.0979
|
|
196.61 1.0985 0.7705 0.0165 0.0235 2.323 10.456 3.413 1731.942 1.181 15.182 0.894 0.79 339875. 0.0718
|
|
203.90 1.1392 0.6221 0.0083 0.0151 1.498 6.743 1.714 1116.843 0.762 7.622 0.696 0.80 342153. 0.0396
|
|
211.18 1.1799 0.0158 0.0001 0.0066 0.655 2.948 0.018 488.301 0.333 0.082 0.017 0.80 344458. 0.0001
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1232 0.0656 7.990 33.572 29.346 5957.902 3.793 130.530 2.234 0.80 326919. 0.5260
|
|
7.80 0.0407 0.0746 0.1230 0.0671 8.169 34.327 29.305 6091.958 3.878 130.347 2.182 0.80 327292. 0.5134
|
|
15.61 0.0814 0.1455 0.1229 0.0687 8.371 35.172 29.264 6241.945 3.974 130.168 2.126 0.80 327723. 0.5000
|
|
23.41 0.1221 0.2123 0.1227 0.0706 8.593 36.106 29.223 6407.667 4.079 129.982 2.069 0.80 328215. 0.4860
|
|
31.22 0.1628 0.2749 0.1225 0.0725 8.835 37.123 29.176 6588.221 4.194 129.775 2.009 0.80 328773. 0.4716
|
|
39.02 0.2035 0.3332 0.1223 0.0747 9.094 38.213 29.119 6781.628 4.317 129.522 1.948 0.80 329403. 0.4568
|
|
46.82 0.2442 0.3872 0.1219 0.0769 9.366 39.356 29.044 6984.496 4.446 129.187 1.886 0.81 330108. 0.4418
|
|
54.63 0.2849 0.4371 0.1215 0.0792 9.644 40.524 28.939 7191.713 4.578 128.722 1.825 0.81 330892. 0.4268
|
|
62.43 0.3256 0.4832 0.1209 0.0814 9.919 41.677 28.790 7396.354 4.709 128.060 1.766 0.81 331759. 0.4117
|
|
70.24 0.3663 0.5259 0.1200 0.0836 10.178 42.767 28.579 7589.847 4.832 127.120 1.708 0.81 332711. 0.3968
|
|
78.04 0.4070 0.5654 0.1188 0.0855 10.409 43.740 28.284 7762.359 4.942 125.808 1.653 0.81 333751. 0.3820
|
|
85.85 0.4477 0.6022 0.1171 0.0870 10.599 44.534 27.883 7903.431 5.031 124.023 1.600 0.81 334881. 0.3673
|
|
93.65 0.4884 0.6365 0.1148 0.0881 10.732 45.094 27.353 8002.795 5.095 121.665 1.550 0.81 336101. 0.3524
|
|
101.45 0.5291 0.6684 0.1120 0.0887 10.797 45.366 26.674 8051.045 5.125 118.645 1.503 0.81 337411. 0.3373
|
|
109.26 0.5698 0.6980 0.1085 0.0885 10.782 45.303 25.829 8039.841 5.118 114.889 1.457 0.82 338810. 0.3219
|
|
117.06 0.6105 0.7253 0.1042 0.0877 10.677 44.864 24.809 7961.988 5.069 110.350 1.413 0.82 340297. 0.3060
|
|
124.87 0.6512 0.7504 0.0991 0.0860 10.477 44.022 23.611 7812.477 4.974 105.023 1.371 0.82 341868. 0.2895
|
|
132.67 0.6919 0.7733 0.0934 0.0836 10.179 42.771 22.250 7590.499 4.832 98.967 1.330 0.82 343521. 0.2726
|
|
140.47 0.7325 0.7940 0.0871 0.0804 9.788 41.129 20.748 7299.100 4.647 92.286 1.289 0.82 345255. 0.2552
|
|
148.28 0.7732 0.8125 0.0803 0.0765 9.310 39.122 19.131 6942.814 4.420 85.096 1.250 0.83 347067. 0.2376
|
|
156.08 0.8139 0.8286 0.0732 0.0719 8.752 36.773 17.423 6526.085 4.155 77.498 1.211 0.83 348954. 0.2197
|
|
163.89 0.8546 0.8420 0.0657 0.0667 8.118 34.111 15.641 6053.521 3.854 69.573 1.172 0.83 350916. 0.2015
|
|
171.69 0.8953 0.8520 0.0579 0.0609 7.416 31.160 13.800 5529.884 3.520 61.384 1.132 0.84 352951. 0.1828
|
|
179.50 0.9360 0.8573 0.0500 0.0546 6.650 27.942 11.910 4958.809 3.157 52.977 1.089 0.84 355056. 0.1634
|
|
187.30 0.9767 0.8559 0.0419 0.0478 5.824 24.471 9.980 4342.758 2.765 44.391 1.042 0.84 357232. 0.1431
|
|
195.10 1.0174 0.8435 0.0337 0.0406 4.944 20.775 8.016 3686.903 2.347 35.657 0.986 0.84 359477. 0.1214
|
|
202.91 1.0581 0.8109 0.0253 0.0330 4.021 16.898 6.027 2998.771 1.909 26.808 0.912 0.85 361789. 0.0973
|
|
210.71 1.0988 0.7363 0.0169 0.0252 3.068 12.889 4.020 2287.438 1.456 17.880 0.797 0.85 364167. 0.0695
|
|
218.52 1.1395 0.5572 0.0084 0.0172 2.097 8.812 2.005 1563.915 0.996 8.920 0.582 0.85 366610. 0.0358
|
|
226.32 1.1802 -0.0014 0.0000 0.0093 1.127 4.737 -0.003 840.620 0.535 -0.012 -0.001 0.86 369092. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1230 0.0724 10.699 42.144 33.342 7977.882 4.761 148.306 1.896 0.86 348708. 0.4757
|
|
8.34 0.0408 0.0678 0.1229 0.0738 10.912 42.987 33.294 8137.423 4.857 148.092 1.856 0.86 349105. 0.4654
|
|
16.68 0.0815 0.1326 0.1227 0.0755 11.153 43.936 33.249 8317.032 4.964 147.891 1.813 0.86 349564. 0.4544
|
|
25.02 0.1223 0.1939 0.1225 0.0773 11.421 44.992 33.205 8516.899 5.083 147.695 1.768 0.86 350088. 0.4429
|
|
33.35 0.1631 0.2517 0.1224 0.0793 11.716 46.151 33.159 8736.426 5.214 147.492 1.722 0.86 350684. 0.4309
|
|
41.69 0.2038 0.3059 0.1222 0.0814 12.034 47.405 33.108 8973.700 5.356 147.263 1.673 0.86 351354. 0.4185
|
|
50.03 0.2446 0.3563 0.1219 0.0837 12.371 48.731 33.043 9224.787 5.506 146.974 1.625 0.86 352105. 0.4059
|
|
58.37 0.2854 0.4034 0.1216 0.0860 12.715 50.090 32.952 9481.930 5.659 146.573 1.576 0.86 352940. 0.3933
|
|
66.71 0.3261 0.4472 0.1211 0.0883 13.056 51.432 32.822 9736.056 5.811 145.990 1.529 0.86 353862. 0.3807
|
|
75.05 0.3669 0.4881 0.1204 0.0905 13.377 52.696 32.630 9975.333 5.954 145.138 1.484 0.86 354876. 0.3684
|
|
83.39 0.4077 0.5267 0.1194 0.0924 13.658 53.803 32.352 10184.899 6.079 143.904 1.441 0.86 355985. 0.3562
|
|
91.72 0.4484 0.5633 0.1179 0.0939 13.878 54.671 31.960 10349.075 6.177 142.160 1.401 0.87 357190. 0.3442
|
|
100.06 0.4892 0.5981 0.1160 0.0948 14.018 55.220 31.424 10453.065 6.239 139.775 1.364 0.87 358492. 0.3322
|
|
108.40 0.5300 0.6315 0.1134 0.0951 14.059 55.384 30.717 10484.048 6.257 136.627 1.329 0.87 359893. 0.3201
|
|
116.74 0.5707 0.6634 0.1100 0.0947 13.989 55.108 29.813 10431.918 6.226 132.610 1.296 0.87 361390. 0.3076
|
|
125.08 0.6115 0.6937 0.1059 0.0934 13.799 54.358 28.699 10289.894 6.141 127.654 1.265 0.87 362981. 0.2946
|
|
133.42 0.6523 0.7222 0.1010 0.0912 13.482 53.110 27.369 10053.699 6.000 121.739 1.235 0.88 364665. 0.2808
|
|
141.76 0.6930 0.7489 0.0953 0.0882 13.041 51.374 25.837 9725.021 5.804 114.923 1.205 0.88 366438. 0.2662
|
|
150.09 0.7338 0.7735 0.0890 0.0845 12.486 49.184 24.130 9310.524 5.557 107.329 1.175 0.88 368297. 0.2510
|
|
158.43 0.7746 0.7959 0.0822 0.0800 11.827 46.588 22.279 8819.085 5.264 99.098 1.146 0.88 370240. 0.2351
|
|
166.77 0.8153 0.8157 0.0750 0.0749 11.074 43.624 20.314 8258.045 4.929 90.357 1.116 0.89 372264. 0.2186
|
|
175.11 0.8561 0.8328 0.0674 0.0693 10.236 40.321 18.256 7632.714 4.555 81.202 1.085 0.89 374367. 0.2015
|
|
183.45 0.8969 0.8452 0.0595 0.0631 9.329 36.749 16.119 6956.571 4.152 71.697 1.051 0.89 376547. 0.1834
|
|
191.79 0.9376 0.8502 0.0514 0.0566 8.370 32.973 13.916 6241.743 3.725 61.897 1.011 0.89 378804. 0.1640
|
|
200.12 0.9784 0.8429 0.0430 0.0499 7.379 29.067 11.655 5502.323 3.284 51.839 0.961 0.90 381135. 0.1426
|
|
208.46 1.0192 0.8197 0.0345 0.0429 6.341 24.981 9.351 4728.805 2.822 41.592 0.897 0.90 383538. 0.1192
|
|
216.80 1.0599 0.7687 0.0259 0.0357 5.275 20.780 7.014 3933.598 2.348 31.199 0.809 0.90 386014. 0.0931
|
|
225.14 1.1007 0.6662 0.0172 0.0284 4.199 16.542 4.660 3131.346 1.869 20.728 0.675 0.91 388561. 0.0633
|
|
233.48 1.1415 0.4587 0.0085 0.0212 3.135 12.350 2.310 2337.817 1.395 10.275 0.448 0.91 391176. 0.0296
|
|
241.82 1.1822 -0.0025 0.0000 0.0142 2.102 8.282 -0.008 1567.778 0.936 -0.036 -0.002 0.92 393847. 0.0000
|
|
|
|
|
|
|