501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
16x12 (16x12.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 0.1155 0.0561 0.005 0.299 0.241 3.533 0.034 1.073 30.980 0.06 30416. 0.5581
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0.48 0.0317 0.0635 0.1145 0.0572 0.005 0.304 0.239 3.600 0.034 1.064 30.133 0.06 30443. 0.5404
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0.96 0.0635 0.1234 0.1134 0.0583 0.005 0.310 0.237 3.668 0.035 1.053 29.278 0.06 30473. 0.5225
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1.44 0.0952 0.1797 0.1121 0.0594 0.005 0.316 0.234 3.735 0.036 1.041 28.422 0.06 30507. 0.5043
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1.92 0.1269 0.2325 0.1106 0.0604 0.005 0.321 0.231 3.800 0.036 1.027 27.570 0.06 30544. 0.4859
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2.40 0.1587 0.2817 0.1089 0.0614 0.005 0.326 0.228 3.861 0.037 1.012 26.724 0.06 30585. 0.4675
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2.88 0.1904 0.3274 0.1071 0.0623 0.005 0.331 0.224 3.917 0.037 0.994 25.889 0.06 30630. 0.4489
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3.37 0.2221 0.3699 0.1049 0.0630 0.005 0.335 0.219 3.966 0.038 0.975 25.068 0.06 30679. 0.4304
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3.85 0.2539 0.4091 0.1026 0.0637 0.005 0.339 0.214 4.006 0.038 0.953 24.262 0.06 30733. 0.4119
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4.33 0.2856 0.4453 0.1000 0.0641 0.005 0.341 0.209 4.035 0.039 0.929 23.472 0.06 30790. 0.3933
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4.81 0.3173 0.4785 0.0971 0.0644 0.005 0.342 0.203 4.052 0.039 0.902 22.699 0.06 30852. 0.3748
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5.29 0.3491 0.5087 0.0939 0.0644 0.005 0.343 0.196 4.054 0.039 0.872 21.941 0.06 30919. 0.3563
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5.77 0.3808 0.5362 0.0904 0.0642 0.005 0.341 0.189 4.040 0.039 0.840 21.198 0.06 30989. 0.3378
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6.25 0.4126 0.5608 0.0866 0.0637 0.005 0.339 0.181 4.008 0.038 0.804 20.467 0.06 31064. 0.3192
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6.73 0.4443 0.5827 0.0825 0.0629 0.005 0.334 0.172 3.956 0.038 0.766 19.745 0.06 31144. 0.3005
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7.21 0.4760 0.6017 0.0780 0.0617 0.005 0.328 0.163 3.885 0.037 0.725 19.030 0.06 31228. 0.2818
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7.69 0.5078 0.6178 0.0733 0.0603 0.005 0.321 0.153 3.793 0.036 0.681 18.317 0.06 31316. 0.2629
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8.17 0.5395 0.6307 0.0684 0.0585 0.005 0.311 0.143 3.683 0.035 0.636 17.600 0.06 31409. 0.2440
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8.65 0.5712 0.6402 0.0633 0.0565 0.005 0.300 0.132 3.553 0.034 0.588 16.874 0.06 31506. 0.2250
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9.14 0.6030 0.6460 0.0580 0.0541 0.005 0.288 0.121 3.406 0.033 0.539 16.129 0.06 31607. 0.2059
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9.62 0.6347 0.6473 0.0526 0.0515 0.004 0.274 0.110 3.242 0.031 0.488 15.355 0.06 31713. 0.1866
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10.10 0.6664 0.6436 0.0470 0.0487 0.004 0.259 0.098 3.061 0.029 0.436 14.539 0.06 31823. 0.1670
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10.58 0.6982 0.6336 0.0413 0.0455 0.004 0.242 0.086 2.864 0.027 0.384 13.663 0.07 31937. 0.1472
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11.06 0.7299 0.6158 0.0355 0.0421 0.004 0.224 0.074 2.651 0.025 0.330 12.701 0.07 32055. 0.1269
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11.54 0.7616 0.5877 0.0297 0.0385 0.003 0.205 0.062 2.423 0.023 0.276 11.616 0.07 32178. 0.1061
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12.02 0.7934 0.5455 0.0238 0.0346 0.003 0.184 0.050 2.179 0.021 0.221 10.352 0.07 32304. 0.0847
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12.50 0.8251 0.4832 0.0179 0.0305 0.003 0.162 0.037 1.921 0.018 0.166 8.817 0.07 32435. 0.0625
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12.98 0.8568 0.3900 0.0119 0.0262 0.002 0.139 0.025 1.650 0.016 0.111 6.852 0.07 32570. 0.0397
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13.46 0.8886 0.2453 0.0060 0.0217 0.002 0.115 0.013 1.366 0.013 0.056 4.156 0.07 32709. 0.0170
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13.94 0.9203 0.0046 0.0001 0.0170 0.001 0.090 0.000 1.070 0.010 0.001 0.075 0.07 32852. 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 0.1160 0.0508 0.034 1.082 0.969 25.592 0.122 4.311 17.178 0.13 60831. 0.6202
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0.97 0.0320 0.0707 0.1150 0.0520 0.035 1.106 0.961 26.160 0.125 4.274 16.660 0.13 60886. 0.5989
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1.94 0.0639 0.1370 0.1139 0.0531 0.036 1.130 0.951 26.735 0.128 4.232 16.142 0.13 60946. 0.5774
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2.90 0.0959 0.1990 0.1126 0.0542 0.037 1.154 0.941 27.306 0.130 4.184 15.626 0.13 61014. 0.5558
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3.87 0.1278 0.2566 0.1111 0.0553 0.037 1.177 0.928 27.861 0.133 4.130 15.116 0.13 61090. 0.5342
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4.84 0.1598 0.3101 0.1095 0.0564 0.038 1.200 0.915 28.389 0.136 4.068 14.614 0.13 61173. 0.5125
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5.81 0.1917 0.3597 0.1076 0.0574 0.039 1.220 0.899 28.875 0.138 3.999 14.122 0.13 61264. 0.4910
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6.78 0.2237 0.4053 0.1055 0.0582 0.039 1.238 0.881 29.305 0.140 3.921 13.642 0.13 61363. 0.4697
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7.75 0.2556 0.4474 0.1031 0.0589 0.040 1.254 0.862 29.665 0.142 3.833 13.175 0.13 61471. 0.4485
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8.71 0.2876 0.4860 0.1005 0.0595 0.040 1.265 0.840 29.938 0.143 3.735 12.722 0.13 61587. 0.4275
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9.68 0.3195 0.5214 0.0976 0.0598 0.040 1.272 0.815 30.109 0.144 3.627 12.283 0.13 61713. 0.4068
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10.65 0.3515 0.5536 0.0944 0.0599 0.040 1.275 0.789 30.162 0.144 3.507 11.857 0.13 61847. 0.3861
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11.62 0.3834 0.5829 0.0909 0.0598 0.040 1.271 0.759 30.082 0.144 3.376 11.444 0.13 61990. 0.3656
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12.59 0.4154 0.6094 0.0870 0.0593 0.040 1.262 0.727 29.854 0.143 3.233 11.043 0.13 62142. 0.3453
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13.55 0.4473 0.6330 0.0828 0.0585 0.040 1.245 0.692 29.465 0.141 3.078 10.652 0.13 62303. 0.3250
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14.52 0.4793 0.6539 0.0784 0.0574 0.039 1.222 0.655 28.909 0.138 2.912 10.271 0.13 62473. 0.3047
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15.49 0.5112 0.6720 0.0736 0.0560 0.038 1.191 0.615 28.185 0.135 2.735 9.896 0.13 62652. 0.2846
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16.46 0.5432 0.6873 0.0686 0.0542 0.037 1.154 0.573 27.300 0.130 2.550 9.525 0.13 62840. 0.2645
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17.43 0.5751 0.6995 0.0634 0.0522 0.035 1.110 0.530 26.258 0.125 2.357 9.155 0.13 63036. 0.2444
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18.40 0.6071 0.7083 0.0581 0.0498 0.034 1.059 0.485 25.066 0.120 2.159 8.782 0.13 63241. 0.2244
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19.36 0.6390 0.7132 0.0526 0.0471 0.032 1.003 0.439 23.727 0.113 1.955 8.401 0.13 63455. 0.2042
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20.33 0.6710 0.7136 0.0470 0.0442 0.030 0.940 0.393 22.245 0.106 1.746 8.005 0.13 63677. 0.1839
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21.30 0.7029 0.7084 0.0413 0.0410 0.028 0.872 0.345 20.622 0.098 1.534 7.586 0.13 63909. 0.1634
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22.27 0.7349 0.6960 0.0355 0.0375 0.025 0.797 0.296 18.862 0.090 1.319 7.129 0.13 64148. 0.1424
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23.24 0.7668 0.6739 0.0296 0.0337 0.023 0.717 0.247 16.967 0.081 1.101 6.616 0.13 64396. 0.1207
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24.21 0.7988 0.6380 0.0237 0.0297 0.020 0.631 0.198 14.942 0.071 0.881 6.012 0.13 64653. 0.0981
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25.17 0.8307 0.5807 0.0178 0.0254 0.017 0.541 0.148 12.793 0.061 0.660 5.262 0.13 64918. 0.0743
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26.14 0.8627 0.4874 0.0118 0.0209 0.014 0.445 0.099 10.527 0.050 0.439 4.252 0.13 65191. 0.0490
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27.11 0.8946 0.3248 0.0059 0.0162 0.011 0.345 0.049 8.153 0.039 0.219 2.733 0.13 65473. 0.0222
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28.08 0.9266 -0.0008 0.0000 0.0113 0.008 0.240 0.000 5.680 0.027 0.000 -0.007 0.13 65759. 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 0.1164 0.0487 0.111 2.332 2.187 82.772 0.263 9.728 11.985 0.19 91245. 0.6500
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1.46 0.0320 0.0741 0.1154 0.0499 0.114 2.387 2.169 84.740 0.270 9.647 11.608 0.19 91327. 0.6269
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2.91 0.0641 0.1434 0.1143 0.0511 0.116 2.444 2.148 86.734 0.276 9.554 11.232 0.19 91419. 0.6037
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4.37 0.0961 0.2080 0.1130 0.0522 0.119 2.500 2.124 88.717 0.282 9.447 10.859 0.19 91521. 0.5804
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5.82 0.1281 0.2679 0.1115 0.0534 0.122 2.554 2.097 90.652 0.289 9.326 10.491 0.19 91634. 0.5571
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7.28 0.1602 0.3234 0.1099 0.0544 0.124 2.606 2.066 92.497 0.294 9.189 10.130 0.19 91759. 0.5340
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8.74 0.1922 0.3745 0.1080 0.0554 0.126 2.654 2.031 94.204 0.300 9.033 9.778 0.19 91896. 0.5110
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10.19 0.2243 0.4217 0.1059 0.0563 0.128 2.697 1.991 95.723 0.305 8.858 9.436 0.19 92046. 0.4883
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11.65 0.2563 0.4650 0.1036 0.0571 0.130 2.733 1.947 97.002 0.309 8.660 9.104 0.19 92208. 0.4659
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13.11 0.2883 0.5047 0.1010 0.0577 0.131 2.761 1.898 97.987 0.312 8.441 8.784 0.19 92384. 0.4437
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14.56 0.3204 0.5410 0.0980 0.0581 0.132 2.779 1.843 98.624 0.314 8.196 8.474 0.19 92573. 0.4219
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16.02 0.3524 0.5742 0.0948 0.0582 0.133 2.785 1.782 98.859 0.315 7.927 8.176 0.19 92775. 0.4003
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17.47 0.3844 0.6043 0.0913 0.0581 0.132 2.779 1.715 98.637 0.314 7.630 7.888 0.19 92991. 0.3789
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18.93 0.4165 0.6316 0.0874 0.0576 0.131 2.758 1.643 97.906 0.312 7.307 7.610 0.19 93220. 0.3577
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20.39 0.4485 0.6561 0.0832 0.0569 0.130 2.722 1.564 96.624 0.308 6.956 7.341 0.19 93463. 0.3367
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21.84 0.4806 0.6780 0.0787 0.0558 0.127 2.670 1.479 94.765 0.302 6.579 7.080 0.19 93719. 0.3158
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23.30 0.5126 0.6971 0.0739 0.0543 0.124 2.601 1.389 92.329 0.294 6.180 6.825 0.19 93989. 0.2950
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24.76 0.5446 0.7136 0.0689 0.0526 0.120 2.517 1.295 89.334 0.284 5.760 6.575 0.19 94272. 0.2744
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26.21 0.5767 0.7272 0.0637 0.0505 0.115 2.417 1.197 85.798 0.273 5.325 6.328 0.19 94568. 0.2539
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27.67 0.6087 0.7377 0.0583 0.0481 0.110 2.303 1.096 81.738 0.260 4.875 6.082 0.19 94877. 0.2335
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29.12 0.6407 0.7447 0.0528 0.0454 0.103 2.174 0.992 77.167 0.246 4.414 5.832 0.19 95200. 0.2131
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30.58 0.6728 0.7475 0.0471 0.0424 0.097 2.031 0.886 72.096 0.229 3.942 5.576 0.19 95535. 0.1925
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32.04 0.7048 0.7452 0.0414 0.0392 0.089 1.875 0.778 66.536 0.212 3.462 5.306 0.20 95883. 0.1717
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33.49 0.7368 0.7364 0.0356 0.0356 0.081 1.704 0.669 60.495 0.193 2.975 5.015 0.20 96245. 0.1504
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34.95 0.7689 0.7186 0.0297 0.0318 0.072 1.521 0.558 53.984 0.172 2.483 4.690 0.20 96619. 0.1285
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36.41 0.8009 0.6876 0.0238 0.0277 0.063 1.325 0.447 47.020 0.150 1.987 4.308 0.20 97006. 0.1056
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37.86 0.8330 0.6357 0.0178 0.0233 0.053 1.116 0.335 39.620 0.126 1.488 3.830 0.20 97405. 0.0812
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39.32 0.8650 0.5465 0.0118 0.0187 0.043 0.896 0.222 31.812 0.101 0.989 3.170 0.20 97817. 0.0548
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40.77 0.8970 0.3795 0.0059 0.0139 0.032 0.666 0.111 23.629 0.075 0.492 2.123 0.20 98241. 0.0259
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42.23 0.9291 -0.0019 0.0000 0.0089 0.020 0.425 0.000 15.100 0.048 -0.002 -0.010 0.20 98672. 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 0.1167 0.0476 0.257 4.052 3.900 191.744 0.458 17.347 9.226 0.25 121657. 0.6681
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1.94 0.0321 0.0761 0.1158 0.0488 0.264 4.152 3.868 196.498 0.469 17.205 8.929 0.25 121766. 0.6440
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3.89 0.0642 0.1472 0.1147 0.0500 0.270 4.254 3.832 201.319 0.481 17.043 8.632 0.25 121889. 0.6197
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5.83 0.0963 0.2133 0.1134 0.0512 0.276 4.356 3.790 206.125 0.492 16.856 8.339 0.25 122025. 0.5953
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7.78 0.1283 0.2745 0.1120 0.0524 0.283 4.455 3.742 210.822 0.503 16.644 8.050 0.25 122177. 0.5711
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9.72 0.1604 0.3311 0.1103 0.0535 0.289 4.550 3.687 215.309 0.514 16.402 7.768 0.25 122344. 0.5470
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11.67 0.1925 0.3833 0.1085 0.0545 0.294 4.638 3.626 219.470 0.524 16.127 7.493 0.25 122527. 0.5232
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13.61 0.2246 0.4313 0.1064 0.0554 0.299 4.716 3.556 223.187 0.533 15.817 7.226 0.25 122727. 0.4997
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15.56 0.2567 0.4753 0.1041 0.0562 0.304 4.782 3.477 226.330 0.540 15.467 6.969 0.25 122944. 0.4766
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17.50 0.2888 0.5156 0.1014 0.0568 0.307 4.834 3.390 228.772 0.546 15.077 6.720 0.25 123179. 0.4537
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19.45 0.3209 0.5525 0.0985 0.0572 0.309 4.868 3.292 230.380 0.550 14.643 6.481 0.26 123432. 0.4312
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21.39 0.3530 0.5862 0.0953 0.0574 0.310 4.882 3.184 231.022 0.552 14.162 6.251 0.26 123703. 0.4091
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23.34 0.3850 0.6169 0.0917 0.0573 0.309 4.872 3.065 230.567 0.550 13.634 6.030 0.26 123991. 0.3872
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25.28 0.4171 0.6447 0.0878 0.0568 0.307 4.837 2.935 228.890 0.546 13.057 5.817 0.26 124298. 0.3655
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27.23 0.4492 0.6698 0.0836 0.0561 0.303 4.773 2.795 225.885 0.539 12.431 5.612 0.26 124623. 0.3440
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29.17 0.4813 0.6922 0.0791 0.0550 0.297 4.680 2.643 221.491 0.529 11.758 5.413 0.26 124966. 0.3228
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31.11 0.5134 0.7121 0.0743 0.0536 0.289 4.558 2.483 215.708 0.515 11.044 5.221 0.26 125326. 0.3017
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33.06 0.5455 0.7294 0.0693 0.0518 0.280 4.407 2.314 208.573 0.498 10.294 5.033 0.26 125705. 0.2808
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35.00 0.5776 0.7440 0.0640 0.0497 0.268 4.229 2.139 200.131 0.478 9.515 4.848 0.26 126101. 0.2600
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36.95 0.6097 0.7556 0.0586 0.0473 0.255 4.024 1.958 190.421 0.455 8.711 4.665 0.26 126515. 0.2394
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38.89 0.6417 0.7640 0.0531 0.0446 0.241 3.792 1.773 179.474 0.428 7.886 4.480 0.26 126946. 0.2188
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40.84 0.6738 0.7685 0.0474 0.0415 0.224 3.535 1.583 167.316 0.399 7.043 4.292 0.26 127395. 0.1981
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42.78 0.7059 0.7683 0.0416 0.0382 0.206 3.253 1.390 153.969 0.368 6.185 4.096 0.26 127860. 0.1771
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44.73 0.7380 0.7620 0.0358 0.0346 0.187 2.947 1.195 139.457 0.333 5.314 3.886 0.26 128344. 0.1558
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46.67 0.7701 0.7473 0.0298 0.0307 0.166 2.616 0.997 123.807 0.296 4.434 3.652 0.26 128844. 0.1337
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48.62 0.8022 0.7202 0.0239 0.0266 0.144 2.262 0.798 107.055 0.256 3.547 3.379 0.26 129361. 0.1107
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50.56 0.8343 0.6728 0.0179 0.0222 0.120 1.886 0.597 89.249 0.213 2.656 3.035 0.26 129896. 0.0860
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52.51 0.8664 0.5881 0.0119 0.0175 0.094 1.489 0.397 70.452 0.168 1.765 2.555 0.26 130446. 0.0590
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54.45 0.8984 0.4208 0.0059 0.0126 0.068 1.072 0.197 50.749 0.121 0.877 1.763 0.26 131013. 0.0287
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56.40 0.9305 -0.0033 0.0000 0.0075 0.040 0.638 -0.001 30.200 0.072 -0.004 -0.013 0.26 131587. 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 0.1171 0.0470 0.496 6.249 6.115 369.656 0.706 27.198 7.503 0.32 152067. 0.6804
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2.43 0.0321 0.0774 0.1162 0.0482 0.508 6.408 6.066 379.099 0.724 26.982 7.258 0.32 152203. 0.6555
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4.87 0.0642 0.1496 0.1151 0.0494 0.521 6.571 6.010 388.691 0.742 26.733 7.013 0.32 152356. 0.6305
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7.30 0.0963 0.2167 0.1139 0.0506 0.534 6.732 5.946 398.265 0.761 26.448 6.772 0.32 152527. 0.6056
|
|
9.73 0.1285 0.2788 0.1125 0.0518 0.547 6.891 5.873 407.639 0.779 26.122 6.534 0.32 152717. 0.5807
|
|
12.16 0.1606 0.3361 0.1109 0.0530 0.559 7.043 5.789 416.607 0.796 25.748 6.302 0.32 152926. 0.5561
|
|
14.60 0.1927 0.3889 0.1090 0.0540 0.570 7.183 5.693 424.943 0.812 25.323 6.077 0.32 153155. 0.5317
|
|
17.03 0.2248 0.4374 0.1070 0.0550 0.580 7.310 5.585 432.406 0.826 24.842 5.858 0.32 153406. 0.5077
|
|
19.46 0.2569 0.4819 0.1046 0.0558 0.588 7.417 5.463 438.743 0.838 24.300 5.648 0.32 153678. 0.4841
|
|
21.90 0.2890 0.5227 0.1020 0.0564 0.595 7.500 5.326 443.695 0.847 23.691 5.445 0.32 153972. 0.4608
|
|
24.33 0.3211 0.5599 0.0991 0.0568 0.599 7.556 5.174 447.001 0.854 23.014 5.250 0.32 154288. 0.4379
|
|
26.76 0.3532 0.5940 0.0959 0.0570 0.601 7.580 5.005 448.397 0.856 22.264 5.063 0.32 154627. 0.4154
|
|
29.19 0.3854 0.6250 0.0923 0.0569 0.600 7.567 4.820 447.622 0.855 21.437 4.884 0.32 154989. 0.3932
|
|
31.63 0.4175 0.6532 0.0884 0.0565 0.596 7.513 4.616 444.429 0.849 20.533 4.711 0.32 155373. 0.3712
|
|
34.06 0.4496 0.6787 0.0842 0.0558 0.588 7.414 4.395 438.605 0.838 19.551 4.545 0.32 155780. 0.3495
|
|
36.49 0.4817 0.7016 0.0796 0.0547 0.577 7.269 4.158 430.026 0.821 18.495 4.386 0.32 156210. 0.3280
|
|
38.93 0.5138 0.7221 0.0748 0.0532 0.561 7.078 3.906 418.692 0.800 17.373 4.231 0.32 156662. 0.3067
|
|
41.36 0.5459 0.7400 0.0697 0.0515 0.543 6.841 3.641 404.673 0.773 16.196 4.081 0.32 157136. 0.2856
|
|
43.79 0.5780 0.7553 0.0645 0.0493 0.520 6.560 3.366 388.057 0.741 14.971 3.934 0.32 157632. 0.2647
|
|
46.22 0.6102 0.7678 0.0590 0.0469 0.495 6.236 3.082 368.920 0.705 13.707 3.789 0.32 158150. 0.2439
|
|
48.66 0.6423 0.7772 0.0534 0.0442 0.466 5.871 2.790 347.324 0.663 12.410 3.643 0.32 158690. 0.2232
|
|
51.09 0.6744 0.7830 0.0477 0.0411 0.434 5.466 2.492 323.317 0.617 11.084 3.496 0.32 159252. 0.2024
|
|
53.52 0.7065 0.7844 0.0419 0.0378 0.398 5.020 2.189 296.946 0.567 9.735 3.343 0.33 159836. 0.1814
|
|
55.96 0.7386 0.7801 0.0360 0.0341 0.360 4.535 1.881 268.256 0.512 8.366 3.180 0.33 160441. 0.1599
|
|
58.39 0.7707 0.7680 0.0301 0.0302 0.318 4.011 1.570 237.302 0.453 6.982 3.000 0.33 161067. 0.1379
|
|
60.82 0.8028 0.7441 0.0241 0.0260 0.274 3.451 1.256 204.154 0.390 5.587 2.791 0.33 161715. 0.1147
|
|
63.25 0.8350 0.7007 0.0180 0.0215 0.227 2.855 0.941 168.909 0.323 4.186 2.527 0.33 162384. 0.0899
|
|
65.69 0.8671 0.6207 0.0120 0.0167 0.177 2.226 0.626 131.694 0.252 2.784 2.155 0.33 163073. 0.0625
|
|
68.12 0.8992 0.4560 0.0060 0.0118 0.124 1.567 0.312 92.677 0.177 1.388 1.527 0.33 163783. 0.0313
|
|
70.55 0.9313 0.0008 0.0000 0.0066 0.070 0.878 0.000 51.963 0.099 0.001 0.003 0.33 164499. 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 0.1176 0.0467 0.851 8.937 8.840 634.430 1.010 39.319 6.320 0.38 182473. 0.6891
|
|
2.92 0.0321 0.0783 0.1167 0.0479 0.873 9.171 8.772 651.039 1.036 39.017 6.111 0.38 182637. 0.6638
|
|
5.84 0.0643 0.1513 0.1156 0.0491 0.896 9.409 8.694 667.935 1.063 38.670 5.904 0.38 182821. 0.6384
|
|
8.77 0.0964 0.2190 0.1144 0.0504 0.918 9.647 8.604 684.828 1.090 38.269 5.698 0.38 183026. 0.6130
|
|
11.69 0.1286 0.2817 0.1131 0.0516 0.941 9.881 8.500 701.393 1.116 37.808 5.497 0.38 183253. 0.5877
|
|
14.61 0.1607 0.3395 0.1115 0.0528 0.962 10.104 8.381 717.266 1.142 37.280 5.300 0.38 183504. 0.5627
|
|
17.53 0.1929 0.3927 0.1097 0.0539 0.982 10.312 8.246 732.047 1.165 36.676 5.109 0.38 183780. 0.5380
|
|
20.46 0.2250 0.4416 0.1076 0.0548 0.999 10.499 8.091 745.308 1.186 35.990 4.924 0.38 184081. 0.5137
|
|
23.38 0.2572 0.4864 0.1053 0.0557 1.015 10.658 7.917 756.603 1.204 35.214 4.746 0.38 184409. 0.4897
|
|
26.30 0.2893 0.5275 0.1027 0.0563 1.027 10.783 7.721 765.473 1.218 34.342 4.575 0.38 184763. 0.4662
|
|
29.22 0.3215 0.5651 0.0998 0.0568 1.035 10.868 7.502 771.454 1.228 33.368 4.411 0.38 185143. 0.4430
|
|
32.15 0.3536 0.5994 0.0965 0.0570 1.038 10.905 7.259 774.083 1.232 32.287 4.253 0.38 185551. 0.4202
|
|
35.07 0.3857 0.6307 0.0930 0.0569 1.036 10.888 6.991 772.899 1.230 31.095 4.103 0.38 185987. 0.3978
|
|
37.99 0.4179 0.6592 0.0891 0.0565 1.029 10.811 6.697 767.468 1.221 29.789 3.958 0.38 186449. 0.3756
|
|
40.91 0.4500 0.6850 0.0848 0.0557 1.016 10.670 6.378 757.415 1.205 28.368 3.819 0.38 186939. 0.3537
|
|
43.84 0.4822 0.7083 0.0803 0.0546 0.996 10.460 6.034 742.521 1.182 26.839 3.686 0.39 187456. 0.3320
|
|
46.76 0.5143 0.7292 0.0754 0.0532 0.969 10.182 5.668 722.780 1.150 25.213 3.557 0.39 187999. 0.3106
|
|
49.68 0.5465 0.7476 0.0703 0.0514 0.936 9.837 5.285 698.317 1.111 23.506 3.432 0.39 188570. 0.2894
|
|
52.60 0.5786 0.7635 0.0650 0.0492 0.898 9.428 4.885 669.284 1.065 21.730 3.311 0.39 189167. 0.2684
|
|
55.52 0.6108 0.7767 0.0595 0.0468 0.853 8.957 4.473 635.816 1.012 19.895 3.191 0.39 189790. 0.2475
|
|
58.45 0.6429 0.7869 0.0539 0.0440 0.802 8.424 4.049 598.019 0.952 18.012 3.071 0.39 190440. 0.2267
|
|
61.37 0.6751 0.7938 0.0481 0.0409 0.746 7.832 3.617 555.984 0.885 16.087 2.950 0.39 191115. 0.2058
|
|
64.29 0.7072 0.7965 0.0422 0.0375 0.684 7.181 3.176 509.786 0.811 14.127 2.826 0.39 191817. 0.1847
|
|
67.21 0.7394 0.7938 0.0363 0.0338 0.616 6.473 2.729 459.508 0.731 12.139 2.694 0.39 192545. 0.1632
|
|
70.14 0.7715 0.7837 0.0303 0.0298 0.543 5.709 2.277 405.246 0.645 10.129 2.549 0.39 193298. 0.1410
|
|
73.06 0.8036 0.7623 0.0242 0.0255 0.466 4.890 1.821 347.125 0.552 8.102 2.380 0.39 194077. 0.1178
|
|
75.98 0.8358 0.7222 0.0181 0.0210 0.383 4.019 1.364 285.312 0.454 6.066 2.168 0.39 194881. 0.0928
|
|
78.90 0.8679 0.6459 0.0120 0.0162 0.295 3.100 0.906 220.035 0.350 4.029 1.867 0.40 195711. 0.0652
|
|
81.83 0.9001 0.4828 0.0060 0.0112 0.203 2.135 0.450 151.593 0.241 2.001 1.346 0.40 196564. 0.0331
|
|
84.75 0.9322 -0.0068 0.0000 0.0059 0.107 1.129 -0.003 80.129 0.128 -0.014 -0.018 0.40 197421. 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 0.1181 0.0466 1.348 12.136 12.085 1005.043 1.371 53.756 5.454 0.44 212876. 0.6953
|
|
3.42 0.0322 0.0789 0.1172 0.0478 1.384 12.460 11.997 1031.948 1.408 53.362 5.273 0.44 213067. 0.6698
|
|
6.83 0.0644 0.1525 0.1162 0.0491 1.421 12.791 11.894 1059.369 1.445 52.905 5.093 0.44 213281. 0.6441
|
|
10.25 0.0966 0.2207 0.1151 0.0504 1.457 13.123 11.775 1086.832 1.483 52.377 4.914 0.44 213520. 0.6184
|
|
13.66 0.1288 0.2838 0.1137 0.0516 1.494 13.449 11.638 1113.806 1.519 51.766 4.739 0.44 213786. 0.5929
|
|
17.08 0.1610 0.3420 0.1122 0.0528 1.528 13.761 11.480 1139.698 1.555 51.061 4.569 0.44 214080. 0.5677
|
|
20.49 0.1932 0.3955 0.1104 0.0539 1.561 14.053 11.298 1163.846 1.588 50.252 4.403 0.45 214403. 0.5427
|
|
23.91 0.2254 0.4447 0.1084 0.0549 1.590 14.315 11.090 1185.553 1.617 49.329 4.243 0.45 214755. 0.5182
|
|
27.32 0.2576 0.4897 0.1061 0.0558 1.615 14.539 10.855 1204.085 1.643 48.281 4.089 0.45 215139. 0.4940
|
|
30.74 0.2898 0.5310 0.1035 0.0565 1.634 14.715 10.589 1218.691 1.663 47.100 3.941 0.45 215553. 0.4703
|
|
34.15 0.3220 0.5688 0.1006 0.0569 1.648 14.835 10.291 1228.616 1.676 45.776 3.799 0.45 215999. 0.4470
|
|
37.57 0.3542 0.6034 0.0973 0.0571 1.654 14.889 9.960 1233.104 1.682 44.304 3.664 0.45 216477. 0.4240
|
|
40.98 0.3864 0.6349 0.0938 0.0571 1.651 14.869 9.594 1231.408 1.680 42.676 3.534 0.45 216987. 0.4014
|
|
44.40 0.4186 0.6636 0.0898 0.0567 1.640 14.765 9.193 1222.822 1.668 40.889 3.410 0.45 217529. 0.3791
|
|
47.81 0.4508 0.6897 0.0856 0.0559 1.618 14.571 8.755 1206.743 1.646 38.942 3.291 0.45 218103. 0.3571
|
|
51.23 0.4830 0.7134 0.0809 0.0548 1.586 14.282 8.283 1182.811 1.614 36.845 3.176 0.45 218708. 0.3353
|
|
54.64 0.5152 0.7346 0.0760 0.0533 1.544 13.898 7.782 1151.019 1.570 34.613 3.066 0.45 219345. 0.3137
|
|
58.06 0.5474 0.7534 0.0709 0.0515 1.491 13.422 7.254 1111.571 1.516 32.267 2.960 0.45 220013. 0.2924
|
|
61.47 0.5796 0.7698 0.0655 0.0493 1.428 12.856 6.705 1064.716 1.452 29.825 2.856 0.45 220712. 0.2713
|
|
64.89 0.6118 0.7836 0.0600 0.0468 1.355 12.204 6.138 1010.674 1.379 27.302 2.755 0.45 221442. 0.2503
|
|
68.30 0.6440 0.7946 0.0543 0.0440 1.273 11.466 5.556 949.620 1.295 24.711 2.654 0.45 222203. 0.2294
|
|
71.72 0.6762 0.8022 0.0485 0.0409 1.182 10.646 4.960 881.699 1.203 22.062 2.552 0.45 222994. 0.2084
|
|
75.13 0.7084 0.8060 0.0425 0.0374 1.082 9.745 4.354 807.037 1.101 19.365 2.447 0.46 223816. 0.1872
|
|
78.55 0.7406 0.8045 0.0365 0.0336 0.973 8.763 3.738 725.767 0.990 16.628 2.336 0.46 224668. 0.1657
|
|
81.96 0.7728 0.7959 0.0304 0.0296 0.856 7.704 3.116 638.044 0.870 13.860 2.215 0.46 225550. 0.1434
|
|
85.38 0.8050 0.7765 0.0243 0.0252 0.730 6.569 2.489 544.072 0.742 11.069 2.075 0.46 226462. 0.1200
|
|
88.79 0.8372 0.7387 0.0182 0.0206 0.596 5.363 1.858 444.126 0.606 8.265 1.898 0.46 227403. 0.0949
|
|
92.21 0.8694 0.6647 0.0120 0.0157 0.454 4.088 1.227 338.581 0.462 5.460 1.644 0.46 228373. 0.0668
|
|
95.62 0.9016 0.5000 0.0059 0.0106 0.306 2.752 0.599 227.925 0.311 2.666 1.193 0.46 229372. 0.0339
|
|
99.04 0.9338 -0.0450 -0.0003 0.0052 0.150 1.355 -0.026 112.190 0.153 -0.114 -0.104 0.46 230362. 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 0.1187 0.0466 2.014 15.867 15.864 1501.841 1.793 70.563 4.791 0.51 243274. 0.6998
|
|
3.90 0.0322 0.0792 0.1179 0.0479 2.069 16.300 15.755 1542.783 1.842 70.076 4.632 0.51 243491. 0.6742
|
|
7.80 0.0643 0.1529 0.1169 0.0492 2.125 16.742 15.627 1584.604 1.891 69.509 4.473 0.51 243735. 0.6485
|
|
11.70 0.0965 0.2213 0.1158 0.0505 2.181 17.185 15.479 1626.585 1.942 68.849 4.316 0.51 244008. 0.6227
|
|
15.60 0.1287 0.2846 0.1145 0.0518 2.237 17.622 15.306 1667.915 1.991 68.080 4.162 0.51 244311. 0.5972
|
|
19.50 0.1608 0.3429 0.1130 0.0530 2.290 18.042 15.105 1707.672 2.038 67.188 4.012 0.51 244647. 0.5718
|
|
23.40 0.1930 0.3966 0.1113 0.0542 2.340 18.435 14.874 1744.848 2.083 66.159 3.866 0.51 245015. 0.5468
|
|
27.30 0.2252 0.4458 0.1093 0.0552 2.385 18.789 14.608 1778.364 2.123 64.978 3.726 0.51 245417. 0.5222
|
|
31.19 0.2574 0.4910 0.1070 0.0561 2.423 19.092 14.306 1807.090 2.157 63.631 3.591 0.51 245855. 0.4980
|
|
35.09 0.2895 0.5325 0.1045 0.0568 2.454 19.333 13.963 1829.881 2.184 62.106 3.461 0.51 246329. 0.4743
|
|
38.99 0.3217 0.5704 0.1016 0.0573 2.475 19.499 13.577 1845.579 2.203 60.392 3.337 0.51 246838. 0.4509
|
|
42.89 0.3539 0.6051 0.0984 0.0575 2.485 19.578 13.147 1853.032 2.212 58.479 3.218 0.51 247384. 0.4279
|
|
46.79 0.3860 0.6369 0.0948 0.0575 2.482 19.557 12.671 1851.105 2.210 56.359 3.105 0.51 247967. 0.4053
|
|
50.69 0.4182 0.6658 0.0909 0.0571 2.466 19.427 12.146 1838.727 2.195 54.026 2.996 0.51 248586. 0.3829
|
|
54.59 0.4504 0.6922 0.0866 0.0563 2.434 19.176 11.574 1814.979 2.166 51.480 2.892 0.51 249242. 0.3609
|
|
58.49 0.4825 0.7161 0.0820 0.0552 2.386 18.799 10.956 1779.296 2.124 48.731 2.793 0.51 249933. 0.3390
|
|
62.39 0.5147 0.7377 0.0770 0.0538 2.322 18.295 10.297 1731.652 2.067 45.802 2.697 0.51 250661. 0.3174
|
|
66.29 0.5469 0.7570 0.0719 0.0519 2.243 17.669 9.604 1672.354 1.996 42.719 2.605 0.52 251424. 0.2960
|
|
70.19 0.5791 0.7739 0.0664 0.0497 2.148 16.923 8.882 1601.788 1.912 39.507 2.515 0.52 252223. 0.2749
|
|
74.09 0.6112 0.7883 0.0609 0.0472 2.039 16.062 8.135 1520.297 1.815 36.186 2.427 0.52 253057. 0.2539
|
|
77.99 0.6434 0.8000 0.0551 0.0443 1.915 15.089 7.368 1428.154 1.705 32.773 2.340 0.52 253926. 0.2329
|
|
81.89 0.6756 0.8086 0.0493 0.0411 1.778 14.005 6.583 1325.583 1.582 29.282 2.253 0.52 254829. 0.2119
|
|
85.79 0.7077 0.8135 0.0433 0.0376 1.626 12.813 5.784 1212.779 1.448 25.725 2.163 0.52 255768. 0.1908
|
|
89.68 0.7399 0.8135 0.0372 0.0338 1.462 11.516 4.972 1089.937 1.301 22.115 2.069 0.52 256740. 0.1692
|
|
93.58 0.7721 0.8068 0.0311 0.0297 1.284 10.114 4.150 957.296 1.143 18.461 1.966 0.52 257747. 0.1469
|
|
97.48 0.8042 0.7899 0.0249 0.0253 1.093 8.612 3.322 815.158 0.973 14.776 1.848 0.52 258787. 0.1235
|
|
101.38 0.8364 0.7558 0.0186 0.0206 0.890 7.015 2.489 663.937 0.793 11.072 1.701 0.53 259862. 0.0984
|
|
105.28 0.8686 0.6875 0.0124 0.0157 0.676 5.327 1.656 504.193 0.602 7.365 1.490 0.53 260969. 0.0703
|
|
109.18 0.9007 0.5323 0.0062 0.0105 0.451 3.557 0.826 336.664 0.402 3.672 1.112 0.53 262109. 0.0371
|
|
113.08 0.9329 -0.0003 0.0000 0.0050 0.217 1.707 0.000 161.601 0.193 -0.001 -0.001 0.53 263247. 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 0.1193 0.0468 2.879 20.162 20.189 2146.889 2.278 89.799 4.265 0.57 273666. 0.7028
|
|
4.39 0.0322 0.0793 0.1186 0.0481 2.959 20.722 20.060 2206.543 2.341 89.225 4.123 0.57 273910. 0.6773
|
|
8.78 0.0644 0.1532 0.1177 0.0494 3.041 21.296 19.908 2267.663 2.406 88.551 3.982 0.57 274184. 0.6516
|
|
13.17 0.0966 0.2218 0.1166 0.0508 3.123 21.874 19.730 2329.185 2.471 87.759 3.842 0.57 274491. 0.6259
|
|
17.56 0.1288 0.2852 0.1154 0.0521 3.205 22.445 19.521 2389.917 2.536 86.831 3.705 0.57 274832. 0.6003
|
|
21.95 0.1609 0.3436 0.1140 0.0534 3.283 22.995 19.277 2448.491 2.598 85.745 3.571 0.57 275209. 0.5750
|
|
26.34 0.1931 0.3973 0.1123 0.0546 3.357 23.510 18.993 2503.405 2.656 84.482 3.441 0.57 275623. 0.5500
|
|
30.72 0.2253 0.4467 0.1103 0.0557 3.424 23.977 18.665 2553.048 2.709 83.023 3.316 0.57 276077. 0.5254
|
|
35.11 0.2575 0.4919 0.1081 0.0566 3.481 24.378 18.289 2595.746 2.754 81.348 3.196 0.57 276570. 0.5012
|
|
39.50 0.2897 0.5335 0.1056 0.0573 3.527 24.697 17.860 2629.803 2.790 79.442 3.080 0.57 277104. 0.4774
|
|
43.89 0.3219 0.5715 0.1027 0.0578 3.558 24.920 17.376 2653.512 2.815 77.289 2.970 0.57 277679. 0.4540
|
|
48.28 0.3541 0.6064 0.0995 0.0581 3.574 25.030 16.834 2665.182 2.828 74.877 2.865 0.57 278295. 0.4311
|
|
52.67 0.3863 0.6383 0.0959 0.0581 3.571 25.011 16.231 2663.165 2.826 72.194 2.764 0.58 278952. 0.4084
|
|
57.06 0.4184 0.6675 0.0920 0.0577 3.548 24.849 15.565 2645.893 2.807 69.234 2.668 0.58 279651. 0.3861
|
|
61.45 0.4506 0.6941 0.0877 0.0569 3.503 24.531 14.837 2612.027 2.771 65.996 2.576 0.58 280390. 0.3639
|
|
65.84 0.4828 0.7183 0.0831 0.0558 3.434 24.049 14.050 2560.740 2.717 62.493 2.489 0.58 281170. 0.3421
|
|
70.23 0.5150 0.7402 0.0781 0.0543 3.342 23.403 13.209 2491.981 2.644 58.753 2.404 0.58 281991. 0.3204
|
|
74.62 0.5472 0.7598 0.0728 0.0525 3.227 22.598 12.323 2406.208 2.553 54.811 2.323 0.58 282852. 0.2990
|
|
79.01 0.5794 0.7772 0.0674 0.0502 3.090 21.638 11.398 2303.994 2.445 50.700 2.244 0.58 283753. 0.2778
|
|
83.40 0.6116 0.7922 0.0617 0.0477 2.931 20.528 10.442 2185.867 2.319 46.446 2.167 0.58 284693. 0.2568
|
|
87.78 0.6438 0.8045 0.0559 0.0447 2.752 19.273 9.459 2052.233 2.177 42.072 2.090 0.58 285672. 0.2358
|
|
92.17 0.6759 0.8139 0.0500 0.0415 2.553 17.876 8.452 1903.423 2.020 37.596 2.014 0.58 286691. 0.2147
|
|
96.56 0.7081 0.8196 0.0439 0.0379 2.333 16.338 7.427 1739.722 1.846 33.033 1.936 0.59 287748. 0.1935
|
|
100.95 0.7403 0.8208 0.0377 0.0340 2.094 14.664 6.385 1561.425 1.657 28.399 1.855 0.59 288844. 0.1719
|
|
105.34 0.7725 0.8156 0.0315 0.0298 1.836 12.856 5.330 1368.869 1.452 23.707 1.766 0.59 289979. 0.1495
|
|
109.73 0.8047 0.8006 0.0252 0.0253 1.559 10.917 4.265 1162.497 1.233 18.972 1.664 0.59 291151. 0.1260
|
|
114.12 0.8369 0.7689 0.0189 0.0206 1.264 8.855 3.195 942.908 1.000 14.212 1.537 0.59 292362. 0.1008
|
|
118.51 0.8691 0.7039 0.0126 0.0155 0.953 6.677 2.124 710.919 0.754 9.446 1.355 0.59 293609. 0.0724
|
|
122.90 0.9013 0.5518 0.0062 0.0102 0.627 4.392 1.056 467.611 0.496 4.696 1.024 0.59 294892. 0.0386
|
|
127.29 0.9334 -0.0085 0.0000 0.0046 0.286 2.002 -0.007 213.183 0.226 -0.032 -0.015 0.60 296168. 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 0.1201 0.0471 3.978 25.072 25.073 2966.359 2.833 111.525 3.834 0.63 304053. 0.7040
|
|
4.88 0.0322 0.0793 0.1194 0.0485 4.090 25.778 24.928 3049.882 2.912 110.879 3.707 0.63 304323. 0.6788
|
|
9.76 0.0644 0.1532 0.1185 0.0498 4.205 26.505 24.756 3135.821 2.994 110.113 3.581 0.63 304626. 0.6534
|
|
14.64 0.0966 0.2217 0.1176 0.0512 4.322 27.239 24.552 3222.699 3.077 109.205 3.455 0.63 304966. 0.6279
|
|
19.51 0.1288 0.2851 0.1164 0.0526 4.437 27.967 24.309 3308.819 3.160 108.129 3.332 0.64 305344. 0.6025
|
|
24.39 0.1610 0.3435 0.1150 0.0539 4.549 28.672 24.023 3392.229 3.239 106.856 3.212 0.64 305763. 0.5774
|
|
29.27 0.1932 0.3972 0.1134 0.0552 4.654 29.336 23.687 3470.746 3.314 105.362 3.096 0.64 306223. 0.5525
|
|
34.15 0.2254 0.4466 0.1115 0.0563 4.750 29.938 23.295 3542.025 3.382 103.618 2.983 0.64 306728. 0.5280
|
|
39.03 0.2576 0.4919 0.1094 0.0573 4.833 30.459 22.842 3603.632 3.441 101.601 2.875 0.64 307276. 0.5039
|
|
43.91 0.2898 0.5335 0.1069 0.0581 4.899 30.877 22.322 3653.085 3.488 99.289 2.772 0.64 307870. 0.4802
|
|
48.79 0.3220 0.5716 0.1041 0.0586 4.946 31.171 21.731 3687.939 3.522 96.661 2.673 0.64 308510. 0.4569
|
|
53.67 0.3542 0.6066 0.1009 0.0589 4.970 31.322 21.066 3705.798 3.539 93.702 2.578 0.64 309197. 0.4340
|
|
58.54 0.3864 0.6387 0.0973 0.0589 4.968 31.310 20.323 3704.323 3.537 90.396 2.488 0.64 309929. 0.4114
|
|
63.42 0.4186 0.6680 0.0934 0.0585 4.937 31.115 19.500 3681.309 3.515 86.736 2.403 0.64 310707. 0.3891
|
|
68.30 0.4508 0.6949 0.0890 0.0578 4.874 30.723 18.597 3634.867 3.471 82.720 2.321 0.64 311531. 0.3670
|
|
73.18 0.4830 0.7193 0.0844 0.0566 4.779 30.122 17.618 3563.825 3.403 78.363 2.242 0.64 312401. 0.3451
|
|
78.06 0.5152 0.7416 0.0793 0.0551 4.651 29.313 16.570 3468.097 3.312 73.703 2.167 0.64 313315. 0.3235
|
|
82.94 0.5474 0.7616 0.0740 0.0532 4.490 28.301 15.464 3348.345 3.197 68.782 2.095 0.64 314274. 0.3021
|
|
87.82 0.5796 0.7794 0.0685 0.0509 4.299 27.093 14.308 3205.415 3.061 63.643 2.025 0.65 315277. 0.2809
|
|
92.69 0.6118 0.7949 0.0628 0.0483 4.077 25.695 13.111 3040.070 2.903 58.320 1.956 0.65 316324. 0.2598
|
|
97.57 0.6440 0.8079 0.0569 0.0453 3.826 24.114 11.880 2852.917 2.724 52.842 1.889 0.65 317415. 0.2387
|
|
102.45 0.6762 0.8180 0.0508 0.0420 3.546 22.351 10.619 2644.436 2.525 47.232 1.821 0.65 318548. 0.2176
|
|
107.33 0.7084 0.8247 0.0447 0.0384 3.239 20.412 9.332 2415.034 2.306 41.510 1.753 0.65 319725. 0.1964
|
|
112.21 0.7406 0.8270 0.0384 0.0344 2.903 18.300 8.025 2165.121 2.068 35.694 1.681 0.65 320945. 0.1746
|
|
117.09 0.7728 0.8231 0.0321 0.0301 2.541 16.019 6.700 1895.180 1.810 29.803 1.604 0.65 322207. 0.1522
|
|
121.97 0.8050 0.8100 0.0257 0.0255 2.153 13.573 5.363 1605.822 1.533 23.855 1.515 0.66 323512. 0.1286
|
|
126.85 0.8372 0.7808 0.0192 0.0206 1.740 10.970 4.018 1297.886 1.239 17.872 1.404 0.66 324858. 0.1032
|
|
131.72 0.8694 0.7192 0.0128 0.0155 1.304 8.220 2.670 972.519 0.929 11.878 1.245 0.66 326245. 0.0746
|
|
136.60 0.9016 0.5709 0.0064 0.0100 0.847 5.336 1.327 631.259 0.603 5.902 0.953 0.66 327672. 0.0403
|
|
141.48 0.9338 -0.0121 -0.0001 0.0044 0.368 2.318 -0.012 274.258 0.262 -0.052 -0.019 0.66 329084. 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 0.1208 0.0480 5.396 30.918 30.526 4023.713 3.493 135.779 3.441 0.70 334434. 0.6972
|
|
5.37 0.0322 0.0784 0.1202 0.0494 5.545 31.771 30.370 4134.824 3.590 135.087 3.331 0.70 334729. 0.6733
|
|
10.74 0.0644 0.1516 0.1194 0.0507 5.699 32.652 30.184 4249.484 3.689 134.260 3.222 0.70 335061. 0.6491
|
|
16.10 0.0966 0.2198 0.1186 0.0521 5.855 33.545 29.961 4365.702 3.790 133.267 3.113 0.70 335433. 0.6248
|
|
21.47 0.1288 0.2829 0.1175 0.0535 6.009 34.433 29.693 4481.197 3.890 132.073 3.005 0.70 335848. 0.6006
|
|
26.84 0.1610 0.3413 0.1162 0.0548 6.160 35.294 29.371 4593.317 3.988 130.643 2.900 0.70 336307. 0.5764
|
|
32.21 0.1932 0.3951 0.1147 0.0561 6.302 36.107 28.988 4699.134 4.079 128.940 2.798 0.70 336813. 0.5525
|
|
37.58 0.2255 0.4446 0.1129 0.0573 6.431 36.848 28.536 4795.508 4.163 126.927 2.699 0.70 337368. 0.5287
|
|
42.94 0.2577 0.4901 0.1108 0.0583 6.543 37.491 28.006 4879.151 4.236 124.572 2.603 0.70 337972. 0.5053
|
|
48.31 0.2899 0.5320 0.1084 0.0591 6.634 38.010 27.393 4946.721 4.294 121.846 2.512 0.70 338626. 0.4821
|
|
53.68 0.3221 0.5704 0.1056 0.0596 6.698 38.380 26.691 4994.859 4.336 118.721 2.424 0.70 339332. 0.4592
|
|
59.05 0.3543 0.6056 0.1025 0.0599 6.732 38.575 25.894 5020.236 4.358 115.177 2.339 0.70 340088. 0.4366
|
|
64.41 0.3865 0.6379 0.0989 0.0599 6.731 38.570 24.999 5019.562 4.358 111.196 2.259 0.70 340896. 0.4142
|
|
69.78 0.4187 0.6675 0.0950 0.0596 6.691 38.340 24.003 4989.695 4.332 106.766 2.182 0.70 341755. 0.3920
|
|
75.15 0.4509 0.6946 0.0906 0.0588 6.608 37.865 22.906 4927.866 4.278 101.887 2.108 0.71 342664. 0.3700
|
|
80.52 0.4831 0.7194 0.0859 0.0577 6.480 37.131 21.712 4832.285 4.195 96.576 2.038 0.71 343623. 0.3483
|
|
85.89 0.5153 0.7420 0.0808 0.0562 6.306 36.135 20.431 4702.705 4.083 90.878 1.971 0.71 344632. 0.3266
|
|
91.25 0.5475 0.7624 0.0755 0.0542 6.088 34.885 19.076 4540.044 3.941 84.849 1.906 0.71 345689. 0.3052
|
|
96.62 0.5797 0.7807 0.0699 0.0519 5.827 33.390 17.658 4345.527 3.772 78.542 1.843 0.71 346796. 0.2840
|
|
101.99 0.6119 0.7967 0.0641 0.0492 5.525 31.660 16.187 4120.263 3.577 72.001 1.782 0.71 347950. 0.2629
|
|
107.36 0.6441 0.8103 0.0581 0.0462 5.183 29.699 14.672 3865.134 3.355 65.261 1.722 0.71 349152. 0.2419
|
|
112.73 0.6764 0.8212 0.0519 0.0428 4.802 27.515 13.119 3580.827 3.109 58.354 1.662 0.71 350402. 0.2207
|
|
118.09 0.7086 0.8288 0.0456 0.0390 4.382 25.110 11.534 3267.906 2.837 51.303 1.601 0.72 351699. 0.1994
|
|
123.46 0.7408 0.8322 0.0393 0.0349 3.925 22.490 9.921 2926.927 2.541 44.130 1.537 0.72 353042. 0.1776
|
|
128.83 0.7730 0.8297 0.0328 0.0306 3.431 19.660 8.287 2558.578 2.221 36.860 1.469 0.72 354433. 0.1551
|
|
134.20 0.8052 0.8183 0.0263 0.0258 2.902 16.626 6.635 2163.793 1.878 29.514 1.391 0.72 355869. 0.1314
|
|
139.56 0.8374 0.7913 0.0197 0.0208 2.339 13.400 4.973 1743.892 1.514 22.119 1.293 0.72 357352. 0.1058
|
|
144.93 0.8696 0.7324 0.0131 0.0155 1.744 9.995 3.306 1300.767 1.129 14.705 1.153 0.72 358879. 0.0769
|
|
150.30 0.9018 0.5865 0.0065 0.0100 1.122 6.432 1.643 837.037 0.727 7.307 0.890 0.73 360450. 0.0418
|
|
155.67 0.9340 -0.0147 -0.0001 0.0042 0.474 2.715 -0.017 353.357 0.307 -0.075 -0.022 0.73 361998. 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 0.1215 0.0505 7.361 38.660 36.542 5488.742 4.368 162.538 3.020 0.76 364808. 0.6694
|
|
5.86 0.0322 0.0752 0.1210 0.0518 7.550 39.657 36.384 5630.256 4.480 161.836 2.931 0.76 365127. 0.6484
|
|
11.71 0.0644 0.1459 0.1203 0.0531 7.746 40.685 36.194 5776.249 4.597 160.989 2.842 0.76 365487. 0.6270
|
|
17.57 0.0966 0.2120 0.1196 0.0545 7.944 41.725 35.962 5923.917 4.714 159.960 2.753 0.76 365891. 0.6055
|
|
23.42 0.1288 0.2738 0.1186 0.0558 8.140 42.754 35.680 6070.015 4.830 158.704 2.666 0.76 366341. 0.5840
|
|
29.28 0.1610 0.3312 0.1175 0.0571 8.329 43.746 35.336 6210.794 4.942 157.173 2.581 0.76 366840. 0.5625
|
|
35.13 0.1932 0.3846 0.1161 0.0583 8.505 44.672 34.918 6342.230 5.047 155.316 2.497 0.76 367390. 0.5412
|
|
40.99 0.2254 0.4342 0.1144 0.0594 8.663 45.502 34.416 6460.139 5.141 153.084 2.416 0.76 367994. 0.5199
|
|
46.84 0.2576 0.4802 0.1125 0.0603 8.798 46.208 33.820 6560.337 5.221 150.432 2.338 0.76 368652. 0.4987
|
|
52.70 0.2898 0.5228 0.1101 0.0611 8.903 46.760 33.120 6638.708 5.283 147.317 2.263 0.76 369367. 0.4776
|
|
58.55 0.3221 0.5622 0.1074 0.0615 8.973 47.130 32.308 6691.242 5.325 143.706 2.190 0.77 370138. 0.4565
|
|
64.41 0.3543 0.5986 0.1043 0.0617 9.004 47.290 31.378 6714.015 5.343 139.568 2.120 0.77 370965. 0.4354
|
|
70.27 0.3865 0.6321 0.1008 0.0616 8.989 47.214 30.324 6703.163 5.334 134.882 2.052 0.77 371848. 0.4144
|
|
76.12 0.4187 0.6629 0.0969 0.0612 8.924 46.874 29.144 6654.915 5.296 129.634 1.986 0.77 372787. 0.3933
|
|
81.98 0.4509 0.6911 0.0926 0.0604 8.805 46.247 27.837 6565.832 5.225 123.820 1.923 0.77 373782. 0.3721
|
|
87.83 0.4831 0.7169 0.0878 0.0592 8.627 45.314 26.408 6433.458 5.120 117.462 1.862 0.77 374831. 0.3509
|
|
93.69 0.5153 0.7404 0.0827 0.0575 8.391 44.073 24.868 6257.255 4.979 110.613 1.803 0.77 375935. 0.3297
|
|
99.54 0.5475 0.7616 0.0773 0.0555 8.097 42.530 23.234 6038.124 4.805 103.344 1.745 0.77 377092. 0.3085
|
|
105.40 0.5797 0.7806 0.0716 0.0531 7.748 40.693 21.520 5777.409 4.598 95.720 1.689 0.77 378301. 0.2874
|
|
111.25 0.6119 0.7974 0.0656 0.0504 7.344 38.572 19.739 5476.262 4.358 87.799 1.635 0.78 379564. 0.2664
|
|
117.11 0.6441 0.8117 0.0595 0.0472 6.887 36.173 17.901 5135.601 4.087 79.626 1.581 0.78 380878. 0.2453
|
|
122.97 0.6763 0.8233 0.0533 0.0437 6.378 33.501 16.016 4756.221 3.785 71.239 1.527 0.78 382243. 0.2242
|
|
128.82 0.7085 0.8318 0.0468 0.0399 5.819 30.561 14.089 4338.940 3.453 62.668 1.473 0.78 383660. 0.2027
|
|
134.68 0.7407 0.8360 0.0403 0.0357 5.210 27.363 12.127 3884.807 3.091 53.942 1.416 0.78 385128. 0.1808
|
|
140.53 0.7729 0.8342 0.0337 0.0312 4.553 23.915 10.136 3395.282 2.702 45.085 1.354 0.78 386646. 0.1581
|
|
146.39 0.8051 0.8230 0.0270 0.0264 3.852 20.232 8.122 2872.434 2.286 36.126 1.282 0.79 388215. 0.1340
|
|
152.24 0.8373 0.7951 0.0203 0.0213 3.110 16.335 6.091 2319.080 1.845 27.095 1.191 0.79 389833. 0.1078
|
|
158.10 0.8695 0.7326 0.0135 0.0160 2.332 12.249 4.053 1739.052 1.384 18.026 1.057 0.79 391500. 0.0780
|
|
163.95 0.9017 0.5776 0.0067 0.0105 1.525 8.011 2.015 1137.341 0.905 8.962 0.804 0.79 393214. 0.0418
|
|
169.81 0.9340 -0.0142 -0.0001 0.0048 0.693 3.638 -0.022 516.486 0.411 -0.096 -0.019 0.79 394904. 0.0000
|
|
|
|
|
|
|
|
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 0.1221 0.0557 10.332 50.095 43.091 7704.866 5.660 191.668 2.537 0.83 395176. 0.6107
|
|
6.36 0.0323 0.0689 0.1216 0.0570 10.569 51.243 42.937 7881.505 5.789 190.983 2.471 0.83 395519. 0.5938
|
|
12.72 0.0646 0.1341 0.1211 0.0583 10.814 52.428 42.752 8063.736 5.923 190.159 2.405 0.83 395907. 0.5766
|
|
19.07 0.0968 0.1956 0.1205 0.0597 11.060 53.622 42.525 8247.321 6.058 189.149 2.339 0.83 396342. 0.5593
|
|
25.43 0.1291 0.2535 0.1197 0.0610 11.301 54.792 42.243 8427.235 6.190 187.899 2.274 0.83 396827. 0.5419
|
|
31.79 0.1614 0.3080 0.1187 0.0622 11.530 55.899 41.894 8597.559 6.315 186.344 2.210 0.83 397366. 0.5246
|
|
38.15 0.1937 0.3593 0.1175 0.0633 11.736 56.902 41.460 8751.882 6.429 184.416 2.149 0.83 397961. 0.5074
|
|
44.51 0.2259 0.4077 0.1160 0.0643 11.913 57.760 40.928 8883.792 6.526 182.047 2.090 0.83 398615. 0.4902
|
|
50.86 0.2582 0.4533 0.1141 0.0650 12.052 58.433 40.281 8987.320 6.602 179.169 2.033 0.83 399330. 0.4732
|
|
57.22 0.2905 0.4963 0.1119 0.0655 12.146 58.887 39.506 9057.208 6.653 175.723 1.978 0.83 400106. 0.4560
|
|
63.58 0.3228 0.5368 0.1093 0.0657 12.189 59.094 38.592 9088.992 6.676 171.658 1.926 0.83 400945. 0.4388
|
|
69.94 0.3551 0.5749 0.1063 0.0657 12.175 59.028 37.530 9078.812 6.669 166.935 1.875 0.83 401847. 0.4212
|
|
76.29 0.3873 0.6105 0.1029 0.0653 12.100 58.666 36.314 9023.114 6.628 161.523 1.825 0.83 402810. 0.4034
|
|
82.65 0.4196 0.6438 0.0990 0.0645 11.960 57.986 34.938 8918.551 6.551 155.404 1.777 0.83 403835. 0.3852
|
|
89.01 0.4519 0.6747 0.0946 0.0634 11.750 56.969 33.402 8762.062 6.436 148.574 1.729 0.83 404921. 0.3665
|
|
95.37 0.4842 0.7032 0.0898 0.0619 11.468 55.600 31.713 8551.642 6.282 141.059 1.682 0.83 406066. 0.3474
|
|
101.73 0.5165 0.7294 0.0847 0.0599 11.113 53.882 29.884 8287.292 6.088 132.925 1.636 0.84 407271. 0.3279
|
|
108.08 0.5487 0.7532 0.0791 0.0577 10.689 51.822 27.935 7970.454 5.855 124.255 1.590 0.84 408533. 0.3081
|
|
114.44 0.5810 0.7747 0.0733 0.0550 10.196 49.433 25.884 7603.101 5.585 115.132 1.544 0.84 409854. 0.2881
|
|
120.80 0.6133 0.7937 0.0673 0.0520 9.638 46.727 23.747 7186.916 5.279 105.629 1.499 0.84 411230. 0.2678
|
|
127.16 0.6456 0.8100 0.0610 0.0486 9.016 43.712 21.539 6723.210 4.939 95.804 1.453 0.84 412664. 0.2473
|
|
133.52 0.6778 0.8230 0.0546 0.0450 8.335 40.411 19.268 6215.406 4.566 85.702 1.406 0.84 414153. 0.2263
|
|
139.87 0.7101 0.8319 0.0480 0.0410 7.597 36.831 16.943 5664.823 4.161 75.363 1.357 0.85 415697. 0.2048
|
|
146.23 0.7424 0.8348 0.0413 0.0367 6.807 33.001 14.572 5075.711 3.728 64.818 1.302 0.85 417297. 0.1823
|
|
152.59 0.7747 0.8300 0.0345 0.0322 5.963 28.909 12.163 4446.396 3.266 54.101 1.241 0.85 418951. 0.1587
|
|
158.95 0.8070 0.8125 0.0275 0.0274 5.071 24.588 9.722 3781.775 2.778 43.246 1.166 0.85 420659. 0.1333
|
|
165.30 0.8392 0.7727 0.0206 0.0223 4.141 20.077 7.259 3088.026 2.268 32.289 1.066 0.85 422421. 0.1053
|
|
171.66 0.8715 0.6881 0.0136 0.0172 3.182 15.427 4.783 2372.688 1.743 21.274 0.914 0.86 424236. 0.0733
|
|
178.02 0.9038 0.4962 0.0065 0.0119 2.206 10.694 2.306 1644.749 1.208 10.255 0.636 0.86 426101. 0.0354
|
|
184.38 0.9361 -0.0722 -0.0005 0.0065 1.214 5.886 -0.178 905.240 0.665 -0.793 -0.089 0.86 427901. 0.0000
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