427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x10.5PN (20x105PN.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 0.0885 0.0348 0.009 0.565 0.451 6.688 0.064 2.006 30.590 0.08 41723. 0.6027
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0.45 0.0238 0.0587 0.0871 0.0352 0.009 0.572 0.444 6.767 0.065 1.976 29.771 0.08 41749. 0.5821
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0.90 0.0475 0.1142 0.0856 0.0356 0.009 0.578 0.437 6.841 0.065 1.942 28.953 0.08 41778. 0.5613
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1.35 0.0713 0.1665 0.0841 0.0360 0.009 0.584 0.429 6.910 0.066 1.907 28.139 0.08 41809. 0.5405
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1.80 0.0950 0.2156 0.0824 0.0363 0.009 0.589 0.420 6.970 0.067 1.868 27.330 0.08 41843. 0.5196
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2.25 0.1188 0.2616 0.0805 0.0366 0.009 0.593 0.411 7.020 0.067 1.826 26.528 0.08 41880. 0.4987
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2.70 0.1425 0.3045 0.0786 0.0368 0.009 0.597 0.401 7.059 0.067 1.782 25.734 0.08 41919. 0.4778
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3.15 0.1663 0.3444 0.0764 0.0369 0.010 0.599 0.390 7.085 0.068 1.733 24.949 0.08 41961. 0.4569
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3.60 0.1900 0.3814 0.0742 0.0369 0.010 0.600 0.378 7.094 0.068 1.682 24.173 0.08 42006. 0.4361
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4.05 0.2138 0.4154 0.0717 0.0369 0.010 0.599 0.366 7.086 0.068 1.627 23.405 0.08 42054. 0.4152
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4.50 0.2375 0.4466 0.0691 0.0368 0.009 0.597 0.352 7.059 0.067 1.568 22.646 0.08 42105. 0.3944
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4.95 0.2613 0.4750 0.0664 0.0365 0.009 0.592 0.338 7.010 0.067 1.505 21.893 0.08 42159. 0.3736
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5.40 0.2850 0.5005 0.0634 0.0361 0.009 0.586 0.323 6.939 0.066 1.439 21.146 0.08 42216. 0.3529
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5.85 0.3088 0.5231 0.0604 0.0356 0.009 0.579 0.308 6.844 0.065 1.369 20.403 0.08 42276. 0.3321
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6.30 0.3325 0.5429 0.0572 0.0350 0.009 0.569 0.292 6.727 0.064 1.297 19.661 0.08 42340. 0.3115
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6.75 0.3563 0.5596 0.0539 0.0343 0.009 0.557 0.275 6.587 0.063 1.222 18.916 0.08 42406. 0.2909
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7.20 0.3801 0.5732 0.0505 0.0335 0.009 0.543 0.257 6.424 0.061 1.144 18.165 0.08 42476. 0.2703
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7.65 0.4038 0.5834 0.0469 0.0325 0.008 0.527 0.239 6.237 0.060 1.064 17.401 0.08 42550. 0.2497
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8.10 0.4276 0.5900 0.0433 0.0314 0.008 0.509 0.221 6.026 0.058 0.982 16.621 0.08 42626. 0.2291
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8.55 0.4513 0.5926 0.0396 0.0302 0.008 0.490 0.202 5.792 0.055 0.898 15.814 0.08 42706. 0.2085
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9.00 0.4751 0.5906 0.0358 0.0288 0.007 0.468 0.183 5.534 0.053 0.813 14.973 0.08 42789. 0.1878
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9.45 0.4988 0.5833 0.0320 0.0273 0.007 0.444 0.163 5.252 0.050 0.725 14.083 0.08 42876. 0.1668
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9.90 0.5226 0.5696 0.0281 0.0258 0.007 0.418 0.143 4.945 0.047 0.637 13.127 0.08 42966. 0.1457
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10.35 0.5463 0.5480 0.0241 0.0240 0.006 0.390 0.123 4.615 0.044 0.547 12.082 0.08 43059. 0.1243
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10.80 0.5701 0.5165 0.0201 0.0222 0.006 0.360 0.103 4.261 0.041 0.456 10.913 0.08 43156. 0.1025
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11.25 0.5938 0.4719 0.0161 0.0202 0.005 0.328 0.082 3.884 0.037 0.365 9.571 0.08 43256. 0.0804
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11.70 0.6176 0.4092 0.0120 0.0182 0.005 0.295 0.061 3.485 0.033 0.273 7.980 0.08 43359. 0.0580
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12.15 0.6413 0.3204 0.0080 0.0160 0.004 0.259 0.041 3.065 0.029 0.181 6.016 0.08 43466. 0.0356
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12.60 0.6651 0.1915 0.0039 0.0137 0.004 0.222 0.020 2.625 0.025 0.089 3.468 0.08 43576. 0.0144
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13.05 0.6888 -0.0049 -0.0001 0.0113 0.003 0.183 0.000 2.166 0.021 -0.002 -0.085 0.08 43687. 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 0.0889 0.0314 0.065 2.040 1.813 48.270 0.230 8.064 17.036 0.16 83444. 0.6730
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0.90 0.0239 0.0656 0.0875 0.0319 0.066 2.069 1.786 48.964 0.234 7.942 16.541 0.16 83497. 0.6485
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1.81 0.0477 0.1272 0.0861 0.0323 0.067 2.097 1.756 49.622 0.237 7.810 16.050 0.16 83556. 0.6239
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2.71 0.0716 0.1851 0.0845 0.0327 0.067 2.123 1.724 50.229 0.240 7.667 15.565 0.16 83618. 0.5995
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3.62 0.0955 0.2392 0.0828 0.0331 0.068 2.146 1.689 50.773 0.242 7.512 15.087 0.16 83687. 0.5752
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4.52 0.1193 0.2897 0.0810 0.0334 0.069 2.165 1.651 51.239 0.245 7.345 14.617 0.16 83760. 0.5511
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5.42 0.1432 0.3367 0.0790 0.0336 0.069 2.181 1.611 51.612 0.246 7.165 14.156 0.16 83839. 0.5271
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6.33 0.1671 0.3802 0.0768 0.0338 0.070 2.192 1.567 51.873 0.248 6.972 13.704 0.16 83924. 0.5034
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7.23 0.1910 0.4205 0.0746 0.0339 0.070 2.198 1.521 52.007 0.248 6.764 13.262 0.16 84014. 0.4798
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8.14 0.2148 0.4577 0.0721 0.0338 0.070 2.197 1.471 51.996 0.248 6.542 12.829 0.16 84111. 0.4564
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9.04 0.2387 0.4917 0.0695 0.0337 0.069 2.190 1.417 51.822 0.247 6.304 12.405 0.16 84214. 0.4333
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9.95 0.2626 0.5227 0.0667 0.0335 0.069 2.175 1.361 51.472 0.246 6.052 11.989 0.16 84323. 0.4103
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10.85 0.2864 0.5509 0.0638 0.0332 0.068 2.153 1.301 50.937 0.243 5.785 11.582 0.16 84438. 0.3875
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11.75 0.3103 0.5761 0.0607 0.0327 0.067 2.122 1.238 50.211 0.240 5.506 11.181 0.16 84560. 0.3649
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12.66 0.3342 0.5985 0.0575 0.0321 0.066 2.083 1.172 49.293 0.235 5.214 10.786 0.16 84688. 0.3426
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13.56 0.3580 0.6180 0.0541 0.0314 0.065 2.036 1.104 48.179 0.230 4.911 10.394 0.16 84822. 0.3204
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14.47 0.3819 0.6344 0.0507 0.0305 0.063 1.981 1.034 46.867 0.224 4.598 10.004 0.16 84964. 0.2984
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15.37 0.4058 0.6477 0.0471 0.0295 0.061 1.917 0.961 45.356 0.217 4.276 9.613 0.16 85111. 0.2765
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16.27 0.4297 0.6576 0.0435 0.0284 0.059 1.844 0.887 43.643 0.208 3.945 9.217 0.16 85266. 0.2547
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17.18 0.4535 0.6638 0.0398 0.0272 0.056 1.763 0.811 41.726 0.199 3.607 8.814 0.16 85427. 0.2329
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18.08 0.4774 0.6658 0.0360 0.0258 0.053 1.674 0.733 39.605 0.189 3.262 8.398 0.16 85595. 0.2110
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18.99 0.5013 0.6628 0.0321 0.0243 0.050 1.575 0.654 37.276 0.178 2.911 7.962 0.16 85770. 0.1890
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19.89 0.5251 0.6538 0.0282 0.0226 0.047 1.468 0.574 34.741 0.166 2.554 7.497 0.16 85951. 0.1667
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20.80 0.5490 0.6372 0.0242 0.0208 0.043 1.352 0.493 32.001 0.153 2.193 6.989 0.16 86140. 0.1440
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21.70 0.5729 0.6105 0.0202 0.0189 0.039 1.228 0.411 29.058 0.139 1.829 6.418 0.16 86335. 0.1207
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22.60 0.5967 0.5700 0.0161 0.0169 0.035 1.095 0.329 25.917 0.124 1.462 5.752 0.16 86537. 0.0967
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23.51 0.6206 0.5089 0.0121 0.0147 0.030 0.954 0.246 22.585 0.108 1.094 4.938 0.16 86746. 0.0718
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24.41 0.6445 0.4152 0.0080 0.0124 0.026 0.806 0.163 19.074 0.091 0.726 3.880 0.16 86961. 0.0460
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25.32 0.6683 0.2643 0.0040 0.0100 0.021 0.651 0.081 15.395 0.074 0.360 2.381 0.16 87183. 0.0199
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26.22 0.6922 -0.0058 -0.0001 0.0075 0.015 0.488 -0.001 11.539 0.055 -0.006 -0.051 0.16 87402. 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 0.0894 0.0301 0.209 4.401 4.101 156.215 0.497 18.240 11.906 0.24 125163. 0.7073
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1.36 0.0239 0.0688 0.0880 0.0306 0.213 4.470 4.039 158.656 0.505 17.966 11.547 0.24 125243. 0.6808
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2.72 0.0478 0.1334 0.0866 0.0310 0.216 4.535 3.972 160.974 0.512 17.668 11.192 0.24 125330. 0.6544
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4.08 0.0718 0.1939 0.0850 0.0315 0.219 4.596 3.900 163.123 0.519 17.346 10.843 0.24 125425. 0.6282
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5.44 0.0957 0.2503 0.0833 0.0318 0.221 4.650 3.821 165.056 0.525 16.997 10.501 0.24 125528. 0.6022
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6.80 0.1196 0.3029 0.0814 0.0322 0.224 4.697 3.737 166.723 0.531 16.620 10.165 0.24 125638. 0.5765
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8.16 0.1435 0.3518 0.0794 0.0324 0.225 4.735 3.645 168.070 0.535 16.214 9.838 0.24 125758. 0.5511
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9.52 0.1675 0.3970 0.0773 0.0326 0.227 4.763 3.547 169.039 0.538 15.777 9.518 0.24 125885. 0.5259
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10.87 0.1914 0.4389 0.0750 0.0327 0.227 4.777 3.442 169.570 0.540 15.308 9.206 0.24 126022. 0.5010
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12.23 0.2153 0.4774 0.0725 0.0327 0.227 4.778 3.329 169.601 0.540 14.805 8.902 0.24 126167. 0.4765
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13.59 0.2392 0.5128 0.0699 0.0326 0.227 4.763 3.208 169.073 0.538 14.268 8.606 0.24 126322. 0.4522
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14.95 0.2632 0.5452 0.0671 0.0324 0.225 4.732 3.079 167.939 0.535 13.697 8.317 0.24 126487. 0.4282
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16.31 0.2871 0.5746 0.0641 0.0320 0.223 4.682 2.944 166.166 0.529 13.094 8.035 0.24 126660. 0.4045
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17.67 0.3110 0.6012 0.0610 0.0316 0.220 4.613 2.801 163.736 0.521 12.460 7.760 0.24 126844. 0.3810
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19.03 0.3349 0.6249 0.0578 0.0310 0.215 4.526 2.653 160.635 0.511 11.799 7.490 0.24 127037. 0.3579
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20.39 0.3589 0.6458 0.0544 0.0303 0.210 4.419 2.498 156.857 0.499 11.113 7.224 0.24 127240. 0.3350
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21.75 0.3828 0.6638 0.0510 0.0294 0.204 4.294 2.339 152.393 0.485 10.404 6.961 0.24 127452. 0.3124
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23.11 0.4067 0.6788 0.0474 0.0284 0.197 4.148 2.175 147.233 0.469 9.674 6.700 0.24 127675. 0.2899
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24.47 0.4306 0.6905 0.0437 0.0273 0.190 3.983 2.006 141.371 0.450 8.925 6.437 0.24 127908. 0.2675
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25.83 0.4546 0.6988 0.0400 0.0260 0.181 3.798 1.834 134.800 0.429 8.159 6.172 0.24 128151. 0.2452
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27.19 0.4785 0.7032 0.0361 0.0246 0.171 3.593 1.659 127.512 0.406 7.377 5.900 0.24 128404. 0.2229
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28.55 0.5024 0.7029 0.0322 0.0230 0.160 3.367 1.480 119.504 0.380 6.582 5.616 0.24 128667. 0.2004
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29.91 0.5263 0.6970 0.0283 0.0214 0.149 3.121 1.298 110.775 0.353 5.775 5.316 0.24 128941. 0.1777
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31.27 0.5503 0.6839 0.0243 0.0195 0.136 2.855 1.115 101.329 0.323 4.958 4.989 0.24 129224. 0.1545
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32.62 0.5742 0.6611 0.0202 0.0176 0.122 2.569 0.929 91.176 0.290 4.133 4.622 0.24 129519. 0.1307
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33.98 0.5981 0.6246 0.0162 0.0155 0.108 2.263 0.742 80.332 0.256 3.303 4.192 0.24 129823. 0.1060
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35.34 0.6220 0.5670 0.0121 0.0133 0.092 1.939 0.555 68.825 0.219 2.470 3.659 0.24 130138. 0.0800
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36.70 0.6460 0.4739 0.0080 0.0109 0.076 1.597 0.368 56.692 0.180 1.638 2.946 0.24 130463. 0.0524
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38.06 0.6699 0.3133 0.0040 0.0085 0.059 1.239 0.182 43.980 0.140 0.810 1.878 0.24 130796. 0.0235
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39.42 0.6938 -0.0104 -0.0001 0.0059 0.041 0.862 -0.004 30.602 0.097 -0.018 -0.060 0.24 131119. 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 0.0899 0.0295 0.487 7.671 7.338 363.016 0.867 32.639 9.168 0.32 166877. 0.7286
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1.82 0.0240 0.0707 0.0886 0.0300 0.495 7.797 7.229 368.978 0.881 32.153 8.886 0.32 166984. 0.7009
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3.63 0.0479 0.1371 0.0871 0.0305 0.502 7.916 7.110 374.646 0.894 31.625 8.608 0.32 167101. 0.6734
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5.45 0.0719 0.1991 0.0856 0.0309 0.509 8.028 6.981 379.907 0.907 31.051 8.335 0.32 167228. 0.6461
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7.26 0.0959 0.2569 0.0839 0.0313 0.516 8.128 6.841 384.649 0.918 30.430 8.067 0.32 167365. 0.6190
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9.08 0.1199 0.3107 0.0820 0.0316 0.521 8.215 6.690 388.751 0.928 29.759 7.806 0.32 167514. 0.5924
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10.90 0.1438 0.3607 0.0800 0.0319 0.526 8.285 6.528 392.081 0.936 29.034 7.551 0.32 167673. 0.5660
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12.71 0.1678 0.4070 0.0779 0.0321 0.529 8.336 6.352 394.499 0.942 28.254 7.303 0.32 167844. 0.5400
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14.53 0.1918 0.4498 0.0755 0.0322 0.531 8.365 6.164 395.860 0.945 27.416 7.062 0.32 168027. 0.5144
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16.34 0.2158 0.4893 0.0731 0.0322 0.531 8.368 5.961 396.014 0.945 26.516 6.828 0.32 168223. 0.4891
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18.16 0.2397 0.5255 0.0704 0.0321 0.529 8.343 5.745 394.819 0.943 25.555 6.600 0.32 168430. 0.4641
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19.98 0.2637 0.5587 0.0676 0.0319 0.526 8.287 5.515 392.157 0.936 24.532 6.379 0.32 168650. 0.4395
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21.79 0.2877 0.5889 0.0646 0.0316 0.520 8.198 5.272 387.950 0.926 23.451 6.164 0.32 168883. 0.4152
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23.61 0.3116 0.6163 0.0615 0.0311 0.512 8.075 5.017 382.150 0.912 22.316 5.955 0.32 169128. 0.3913
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25.43 0.3356 0.6409 0.0582 0.0305 0.503 7.918 4.751 374.727 0.895 21.130 5.750 0.32 169387. 0.3677
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27.24 0.3596 0.6627 0.0548 0.0298 0.490 7.727 4.474 365.660 0.873 19.900 5.549 0.32 169659. 0.3444
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29.06 0.3836 0.6818 0.0513 0.0289 0.476 7.500 4.188 354.927 0.847 18.628 5.352 0.32 169944. 0.3213
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30.87 0.4075 0.6979 0.0477 0.0279 0.459 7.237 3.894 342.508 0.818 17.319 5.156 0.32 170242. 0.2985
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32.69 0.4315 0.7109 0.0440 0.0267 0.440 6.939 3.592 328.383 0.784 15.976 4.961 0.32 170554. 0.2758
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34.51 0.4555 0.7207 0.0402 0.0254 0.419 6.604 3.283 312.534 0.746 14.602 4.764 0.32 170879. 0.2532
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36.32 0.4795 0.7267 0.0364 0.0240 0.396 6.232 2.968 294.945 0.704 13.200 4.564 0.32 171218. 0.2306
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38.14 0.5034 0.7283 0.0324 0.0224 0.370 5.824 2.647 275.606 0.658 11.773 4.356 0.32 171570. 0.2079
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39.95 0.5274 0.7246 0.0285 0.0207 0.341 5.378 2.321 254.517 0.608 10.326 4.137 0.32 171936. 0.1849
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41.77 0.5514 0.7141 0.0244 0.0189 0.311 4.896 1.992 231.685 0.553 8.860 3.900 0.32 172316. 0.1615
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43.59 0.5753 0.6943 0.0203 0.0169 0.278 4.377 1.659 207.134 0.494 7.380 3.633 0.32 172710. 0.1373
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45.40 0.5993 0.6610 0.0162 0.0147 0.243 3.823 1.324 180.908 0.432 5.891 3.321 0.32 173118. 0.1121
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47.22 0.6233 0.6065 0.0121 0.0125 0.205 3.235 0.989 153.072 0.365 4.398 2.930 0.32 173539. 0.0855
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49.03 0.6473 0.5149 0.0080 0.0101 0.166 2.614 0.653 123.721 0.295 2.906 2.395 0.32 173974. 0.0568
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50.85 0.6712 0.3479 0.0039 0.0076 0.125 1.964 0.320 92.968 0.222 1.423 1.560 0.32 174420. 0.0259
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52.67 0.6952 -0.0269 -0.0002 0.0049 0.081 1.277 -0.016 60.416 0.144 -0.069 -0.117 0.33 174837. 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 0.0907 0.0293 0.944 11.894 11.560 703.601 1.344 51.420 7.452 0.40 208584. 0.7434
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2.27 0.0240 0.0719 0.0894 0.0298 0.960 12.096 11.390 715.549 1.367 50.665 7.220 0.40 208719. 0.7149
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4.54 0.0480 0.1392 0.0879 0.0303 0.975 12.288 11.205 726.914 1.388 49.842 6.992 0.40 208865. 0.6867
|
|
6.81 0.0719 0.2021 0.0863 0.0307 0.989 12.467 11.004 737.472 1.408 48.948 6.768 0.40 209025. 0.6587
|
|
9.08 0.0959 0.2608 0.0846 0.0311 1.002 12.628 10.786 747.000 1.427 47.978 6.549 0.40 209197. 0.6311
|
|
11.35 0.1199 0.3153 0.0828 0.0315 1.013 12.767 10.550 755.254 1.442 46.928 6.336 0.40 209383. 0.6038
|
|
13.62 0.1439 0.3660 0.0808 0.0317 1.022 12.881 10.295 761.976 1.455 45.794 6.128 0.40 209583. 0.5769
|
|
15.89 0.1678 0.4129 0.0786 0.0319 1.028 12.964 10.021 766.889 1.465 44.572 5.927 0.40 209797. 0.5504
|
|
18.16 0.1918 0.4563 0.0763 0.0321 1.032 13.011 9.725 769.701 1.470 43.257 5.731 0.40 210027. 0.5243
|
|
20.43 0.2158 0.4964 0.0738 0.0321 1.033 13.018 9.408 770.118 1.471 41.845 5.541 0.40 210271. 0.4986
|
|
22.71 0.2398 0.5332 0.0711 0.0320 1.030 12.980 9.068 767.858 1.467 40.336 5.357 0.40 210531. 0.4732
|
|
24.98 0.2637 0.5670 0.0683 0.0318 1.023 12.893 8.707 762.684 1.457 38.728 5.178 0.40 210807. 0.4483
|
|
27.25 0.2877 0.5978 0.0653 0.0314 1.012 12.753 8.325 754.436 1.441 37.028 5.005 0.40 211098. 0.4236
|
|
29.52 0.3117 0.6258 0.0622 0.0310 0.996 12.560 7.923 743.018 1.419 35.241 4.836 0.40 211406. 0.3994
|
|
31.79 0.3357 0.6511 0.0589 0.0303 0.977 12.313 7.503 728.372 1.391 33.374 4.672 0.40 211730. 0.3755
|
|
34.06 0.3596 0.6737 0.0554 0.0296 0.953 12.010 7.068 710.453 1.357 31.436 4.512 0.40 212070. 0.3519
|
|
36.33 0.3836 0.6935 0.0519 0.0287 0.924 11.651 6.617 689.219 1.316 29.433 4.355 0.40 212427. 0.3286
|
|
38.60 0.4076 0.7106 0.0483 0.0277 0.891 11.235 6.153 664.631 1.269 27.370 4.199 0.40 212800. 0.3056
|
|
40.87 0.4316 0.7247 0.0445 0.0265 0.854 10.762 5.677 636.647 1.216 25.252 4.045 0.40 213191. 0.2827
|
|
43.14 0.4556 0.7356 0.0407 0.0252 0.812 10.231 5.190 605.231 1.156 23.086 3.890 0.40 213598. 0.2600
|
|
45.41 0.4795 0.7430 0.0368 0.0238 0.765 9.642 4.693 570.354 1.089 20.876 3.732 0.40 214022. 0.2372
|
|
47.68 0.5035 0.7463 0.0329 0.0222 0.713 8.993 4.188 531.993 1.016 18.627 3.570 0.40 214463. 0.2144
|
|
49.95 0.5275 0.7446 0.0288 0.0204 0.657 8.286 3.674 490.148 0.936 16.343 3.400 0.40 214921. 0.1912
|
|
52.22 0.5515 0.7364 0.0247 0.0185 0.597 7.520 3.155 444.834 0.850 14.032 3.217 0.40 215397. 0.1676
|
|
54.49 0.5754 0.7194 0.0206 0.0165 0.531 6.696 2.630 396.098 0.756 11.697 3.011 0.40 215889. 0.1433
|
|
56.76 0.5994 0.6895 0.0165 0.0143 0.461 5.816 2.102 344.025 0.657 9.348 2.771 0.40 216399. 0.1178
|
|
59.03 0.6234 0.6390 0.0123 0.0120 0.387 4.881 1.572 288.747 0.551 6.991 2.469 0.40 216926. 0.0908
|
|
61.30 0.6474 0.5515 0.0082 0.0096 0.309 3.896 1.043 230.452 0.440 4.638 2.052 0.40 217469. 0.0615
|
|
63.57 0.6713 0.3853 0.0040 0.0071 0.227 2.863 0.516 169.366 0.323 2.296 1.383 0.41 218028. 0.0291
|
|
65.84 0.6953 -0.0166 -0.0001 0.0044 0.140 1.770 -0.013 104.682 0.200 -0.059 -0.057 0.41 218547. 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 0.0916 0.0293 1.632 17.141 16.816 1216.766 1.937 74.799 6.269 0.48 250283. 0.7542
|
|
2.72 0.0240 0.0725 0.0903 0.0298 1.660 17.439 16.574 1237.975 1.970 73.720 6.072 0.48 250445. 0.7253
|
|
5.45 0.0479 0.1404 0.0888 0.0303 1.687 17.724 16.309 1258.153 2.002 72.542 5.879 0.48 250621. 0.6966
|
|
8.17 0.0719 0.2039 0.0873 0.0308 1.712 17.988 16.020 1276.903 2.032 71.258 5.691 0.48 250813. 0.6682
|
|
10.90 0.0959 0.2630 0.0856 0.0312 1.735 18.226 15.707 1293.831 2.059 69.864 5.506 0.48 251020. 0.6402
|
|
13.62 0.1198 0.3180 0.0837 0.0315 1.755 18.433 15.367 1308.512 2.083 68.353 5.327 0.48 251244. 0.6126
|
|
16.34 0.1438 0.3691 0.0817 0.0318 1.771 18.602 15.000 1320.488 2.102 66.718 5.152 0.48 251485. 0.5854
|
|
19.07 0.1678 0.4165 0.0796 0.0320 1.783 18.726 14.603 1329.274 2.116 64.953 4.983 0.48 251743. 0.5586
|
|
21.79 0.1918 0.4603 0.0772 0.0322 1.789 18.797 14.175 1334.361 2.124 63.052 4.818 0.48 252019. 0.5322
|
|
24.51 0.2157 0.5007 0.0747 0.0322 1.791 18.809 13.716 1335.229 2.125 61.010 4.659 0.48 252313. 0.5063
|
|
27.24 0.2397 0.5380 0.0720 0.0321 1.785 18.755 13.225 1331.383 2.119 58.823 4.505 0.48 252626. 0.4807
|
|
29.96 0.2637 0.5722 0.0692 0.0319 1.773 18.629 12.701 1322.406 2.105 56.493 4.356 0.48 252958. 0.4555
|
|
32.69 0.2876 0.6035 0.0662 0.0315 1.754 18.426 12.146 1308.008 2.082 54.026 4.212 0.48 253308. 0.4306
|
|
35.41 0.3116 0.6321 0.0630 0.0311 1.727 18.144 11.563 1288.024 2.050 51.431 4.072 0.48 253678. 0.4062
|
|
38.13 0.3356 0.6579 0.0597 0.0304 1.693 17.783 10.953 1262.347 2.009 48.719 3.936 0.48 254067. 0.3821
|
|
40.86 0.3595 0.6811 0.0562 0.0297 1.651 17.340 10.320 1230.904 1.959 45.902 3.803 0.48 254476. 0.3584
|
|
43.58 0.3835 0.7017 0.0527 0.0288 1.601 16.815 9.665 1193.623 1.900 42.988 3.672 0.48 254905. 0.3350
|
|
46.30 0.4075 0.7195 0.0490 0.0277 1.543 16.206 8.990 1150.435 1.831 39.986 3.544 0.48 255354. 0.3118
|
|
49.03 0.4315 0.7345 0.0452 0.0266 1.477 15.514 8.297 1101.270 1.753 36.905 3.417 0.48 255822. 0.2888
|
|
51.75 0.4554 0.7465 0.0413 0.0252 1.403 14.736 7.588 1046.066 1.665 33.752 3.290 0.48 256311. 0.2659
|
|
54.48 0.4794 0.7551 0.0374 0.0237 1.321 13.873 6.865 984.769 1.567 30.534 3.162 0.48 256820. 0.2430
|
|
57.20 0.5034 0.7598 0.0334 0.0221 1.230 12.923 6.128 917.344 1.460 27.258 3.030 0.48 257350. 0.2201
|
|
59.92 0.5273 0.7598 0.0293 0.0203 1.132 11.886 5.380 843.785 1.343 23.931 2.892 0.48 257900. 0.1968
|
|
62.65 0.5513 0.7536 0.0252 0.0184 1.025 10.764 4.623 764.120 1.216 20.563 2.744 0.48 258470. 0.1731
|
|
65.37 0.5753 0.7392 0.0210 0.0164 0.910 9.557 3.858 678.431 1.080 17.161 2.579 0.48 259062. 0.1486
|
|
68.10 0.5992 0.7125 0.0168 0.0141 0.787 8.267 3.088 586.865 0.934 13.736 2.387 0.48 259673. 0.1230
|
|
70.82 0.6232 0.6659 0.0126 0.0118 0.657 6.898 2.316 489.653 0.779 10.299 2.145 0.49 260305. 0.0958
|
|
73.54 0.6472 0.5831 0.0084 0.0093 0.519 5.453 1.544 387.125 0.616 6.866 1.809 0.49 260957. 0.0659
|
|
76.27 0.6711 0.4207 0.0042 0.0067 0.375 3.940 0.776 279.682 0.445 3.451 1.258 0.49 261627. 0.0325
|
|
78.99 0.6951 0.0043 0.0000 0.0040 0.223 2.340 0.005 166.109 0.264 0.020 0.013 0.49 262257. 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 0.0927 0.0296 2.611 23.509 23.171 1947.015 2.656 103.066 5.398 0.56 291970. 0.7623
|
|
3.18 0.0240 0.0730 0.0914 0.0301 2.658 23.930 22.844 1981.829 2.704 101.611 5.228 0.56 292160. 0.7331
|
|
6.37 0.0480 0.1413 0.0900 0.0306 2.702 24.330 22.486 2014.941 2.749 100.017 5.062 0.56 292367. 0.7042
|
|
9.55 0.0720 0.2051 0.0884 0.0311 2.743 24.701 22.095 2045.710 2.791 98.276 4.899 0.56 292592. 0.6756
|
|
12.73 0.0960 0.2646 0.0867 0.0315 2.781 25.036 21.668 2073.478 2.829 96.380 4.740 0.56 292836. 0.6473
|
|
15.91 0.1200 0.3199 0.0849 0.0318 2.813 25.327 21.205 2097.551 2.861 94.320 4.585 0.56 293098. 0.6195
|
|
19.10 0.1441 0.3713 0.0829 0.0321 2.839 25.564 20.703 2117.182 2.888 92.086 4.435 0.56 293381. 0.5921
|
|
22.28 0.1681 0.4190 0.0807 0.0324 2.859 25.738 20.160 2131.585 2.908 89.671 4.290 0.56 293684. 0.5651
|
|
25.46 0.1921 0.4631 0.0783 0.0325 2.870 25.839 19.574 2139.930 2.919 87.064 4.149 0.56 294008. 0.5385
|
|
28.65 0.2161 0.5039 0.0758 0.0325 2.872 25.856 18.943 2141.376 2.921 84.259 4.012 0.56 294354. 0.5123
|
|
31.83 0.2401 0.5415 0.0731 0.0324 2.863 25.781 18.267 2135.113 2.913 81.252 3.881 0.56 294721. 0.4866
|
|
35.01 0.2641 0.5761 0.0702 0.0322 2.844 25.604 17.546 2120.461 2.893 78.044 3.753 0.56 295110. 0.4612
|
|
38.20 0.2881 0.6078 0.0672 0.0318 2.812 25.320 16.781 2096.951 2.861 74.642 3.630 0.56 295521. 0.4362
|
|
41.38 0.3121 0.6368 0.0639 0.0313 2.768 24.926 15.976 2064.312 2.816 71.062 3.510 0.56 295955. 0.4116
|
|
44.56 0.3361 0.6631 0.0606 0.0307 2.712 24.420 15.135 2022.382 2.759 67.319 3.394 0.56 296412. 0.3874
|
|
47.74 0.3601 0.6868 0.0571 0.0299 2.643 23.800 14.260 1971.045 2.689 63.427 3.281 0.56 296892. 0.3635
|
|
50.93 0.3841 0.7079 0.0534 0.0290 2.562 23.065 13.354 1910.198 2.606 59.399 3.171 0.56 297394. 0.3400
|
|
54.11 0.4081 0.7264 0.0497 0.0279 2.467 22.214 12.421 1839.729 2.510 55.249 3.062 0.56 297920. 0.3166
|
|
57.29 0.4322 0.7422 0.0459 0.0267 2.360 21.246 11.463 1759.529 2.400 50.987 2.955 0.56 298470. 0.2935
|
|
60.48 0.4562 0.7550 0.0420 0.0253 2.239 20.159 10.482 1669.502 2.278 46.624 2.848 0.56 299043. 0.2705
|
|
63.66 0.4802 0.7646 0.0379 0.0238 2.105 18.952 9.481 1569.564 2.141 42.170 2.740 0.56 299639. 0.2475
|
|
66.84 0.5042 0.7704 0.0339 0.0222 1.957 17.625 8.461 1459.660 1.991 37.635 2.629 0.56 300260. 0.2244
|
|
70.02 0.5282 0.7717 0.0297 0.0203 1.797 16.177 7.425 1339.779 1.828 33.029 2.514 0.56 300904. 0.2010
|
|
73.21 0.5522 0.7671 0.0255 0.0184 1.623 14.610 6.377 1209.974 1.651 28.363 2.390 0.56 301572. 0.1771
|
|
76.39 0.5762 0.7545 0.0213 0.0163 1.435 12.924 5.317 1070.374 1.460 23.650 2.253 0.56 302264. 0.1524
|
|
79.57 0.6002 0.7299 0.0170 0.0140 1.235 11.123 4.250 921.226 1.257 18.904 2.092 0.57 302980. 0.1266
|
|
82.76 0.6242 0.6858 0.0127 0.0116 1.023 9.212 3.179 762.909 1.041 14.142 1.890 0.57 303720. 0.0989
|
|
85.94 0.6482 0.6049 0.0084 0.0090 0.799 7.196 2.110 595.968 0.813 9.383 1.605 0.57 304484. 0.0684
|
|
89.12 0.6722 0.4399 0.0042 0.0064 0.565 5.084 1.045 421.062 0.574 4.649 1.126 0.57 305268. 0.0338
|
|
92.31 0.6962 -0.0255 -0.0001 0.0036 0.315 2.833 -0.033 234.618 0.320 -0.145 -0.063 0.57 305961. 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 0.0941 0.0300 3.952 31.139 30.711 2947.315 3.518 136.602 4.726 0.63 333643. 0.7684
|
|
3.64 0.0240 0.0731 0.0928 0.0305 4.025 31.710 30.291 3001.327 3.583 134.733 4.578 0.63 333861. 0.7391
|
|
7.28 0.0481 0.1415 0.0914 0.0311 4.094 32.253 29.828 3052.726 3.644 132.676 4.432 0.63 334099. 0.7101
|
|
10.92 0.0721 0.2054 0.0899 0.0315 4.158 32.758 29.321 3100.484 3.701 130.420 4.289 0.63 334357. 0.6814
|
|
14.57 0.0961 0.2650 0.0882 0.0320 4.216 33.213 28.767 3143.575 3.752 127.955 4.151 0.63 334637. 0.6531
|
|
18.21 0.1202 0.3205 0.0863 0.0324 4.266 33.607 28.162 3180.920 3.797 125.266 4.016 0.64 334939. 0.6252
|
|
21.85 0.1442 0.3721 0.0843 0.0327 4.307 33.929 27.505 3211.372 3.833 122.344 3.885 0.64 335264. 0.5977
|
|
25.49 0.1682 0.4200 0.0821 0.0329 4.336 34.165 26.793 3233.710 3.860 119.174 3.758 0.64 335613. 0.5707
|
|
29.13 0.1923 0.4643 0.0797 0.0330 4.354 34.302 26.022 3246.668 3.875 115.747 3.635 0.64 335986. 0.5441
|
|
32.77 0.2163 0.5053 0.0772 0.0330 4.357 34.326 25.191 3248.964 3.878 112.051 3.517 0.64 336383. 0.5179
|
|
36.41 0.2403 0.5431 0.0745 0.0329 4.344 34.225 24.299 3239.365 3.867 108.082 3.402 0.64 336805. 0.4920
|
|
40.06 0.2644 0.5780 0.0715 0.0327 4.314 33.987 23.345 3216.811 3.840 103.839 3.292 0.64 337253. 0.4666
|
|
43.70 0.2884 0.6101 0.0684 0.0324 4.265 33.604 22.333 3180.590 3.797 99.336 3.185 0.64 337726. 0.4416
|
|
47.34 0.3124 0.6395 0.0652 0.0318 4.198 33.072 21.266 3130.288 3.737 94.589 3.081 0.64 338224. 0.4169
|
|
50.98 0.3365 0.6662 0.0617 0.0312 4.111 32.390 20.149 3065.676 3.659 89.621 2.981 0.64 338749. 0.3926
|
|
54.62 0.3605 0.6905 0.0582 0.0304 4.005 31.554 18.986 2986.596 3.565 84.451 2.883 0.64 339300. 0.3686
|
|
58.26 0.3845 0.7122 0.0545 0.0294 3.879 30.564 17.783 2892.906 3.453 79.099 2.788 0.64 339877. 0.3449
|
|
61.90 0.4086 0.7313 0.0507 0.0283 3.734 29.419 16.542 2784.451 3.324 73.580 2.695 0.64 340481. 0.3215
|
|
65.55 0.4326 0.7478 0.0468 0.0271 3.569 28.115 15.267 2661.079 3.176 67.910 2.602 0.64 341111. 0.2983
|
|
69.19 0.4566 0.7614 0.0428 0.0257 3.383 26.653 13.962 2522.644 3.011 62.102 2.510 0.64 341769. 0.2752
|
|
72.83 0.4807 0.7720 0.0387 0.0241 3.177 25.029 12.628 2369.027 2.828 56.171 2.418 0.64 342453. 0.2521
|
|
76.47 0.5047 0.7789 0.0345 0.0224 2.950 23.245 11.270 2200.150 2.626 50.129 2.323 0.64 343165. 0.2288
|
|
80.11 0.5287 0.7815 0.0303 0.0205 2.703 21.300 9.890 2015.999 2.406 43.990 2.225 0.64 343903. 0.2053
|
|
83.75 0.5528 0.7784 0.0260 0.0185 2.436 19.193 8.491 1816.653 2.168 37.770 2.120 0.64 344669. 0.1813
|
|
87.40 0.5768 0.7677 0.0217 0.0163 2.149 16.929 7.078 1602.316 1.913 31.485 2.004 0.65 345463. 0.1564
|
|
91.04 0.6008 0.7454 0.0173 0.0140 1.842 14.510 5.655 1373.360 1.639 25.153 1.868 0.65 346283. 0.1303
|
|
94.68 0.6249 0.7039 0.0130 0.0115 1.516 11.943 4.226 1130.376 1.349 18.798 1.696 0.65 347131. 0.1023
|
|
98.32 0.6489 0.6258 0.0086 0.0089 1.172 9.236 2.798 874.207 1.044 12.447 1.452 0.65 348006. 0.0713
|
|
101.96 0.6729 0.4609 0.0042 0.0062 0.812 6.401 1.377 605.870 0.723 6.126 1.031 0.65 348903. 0.0355
|
|
105.60 0.6970 -0.0536 -0.0002 0.0032 0.424 3.339 -0.081 315.990 0.377 -0.359 -0.116 0.65 349608. 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 0.0957 0.0308 5.791 40.553 39.542 4318.101 4.582 175.885 4.154 0.71 375297. 0.7663
|
|
4.11 0.0241 0.0726 0.0945 0.0314 5.892 41.262 39.025 4393.594 4.662 173.582 4.029 0.71 375544. 0.7384
|
|
8.22 0.0482 0.1407 0.0931 0.0319 5.988 41.936 38.451 4465.421 4.738 171.031 3.906 0.71 375813. 0.7105
|
|
12.33 0.0723 0.2045 0.0916 0.0324 6.078 42.563 37.819 4532.159 4.809 168.217 3.785 0.71 376106. 0.6829
|
|
16.43 0.0964 0.2642 0.0899 0.0328 6.158 43.128 37.123 4592.343 4.873 165.122 3.666 0.71 376424. 0.6554
|
|
20.54 0.1205 0.3198 0.0880 0.0332 6.228 43.618 36.360 4644.425 4.928 161.730 3.551 0.71 376767. 0.6282
|
|
24.65 0.1446 0.3716 0.0860 0.0335 6.285 44.015 35.527 4686.732 4.973 158.026 3.438 0.71 377136. 0.6012
|
|
28.76 0.1687 0.4197 0.0838 0.0337 6.326 44.304 34.621 4717.483 5.005 153.993 3.329 0.72 377532. 0.5746
|
|
32.87 0.1928 0.4643 0.0814 0.0338 6.349 44.466 33.637 4734.781 5.024 149.616 3.222 0.72 377956. 0.5483
|
|
36.98 0.2169 0.5056 0.0789 0.0338 6.352 44.484 32.573 4736.687 5.026 144.883 3.119 0.72 378407. 0.5223
|
|
41.08 0.2410 0.5438 0.0761 0.0337 6.331 44.340 31.427 4721.302 5.009 139.786 3.019 0.72 378887. 0.4966
|
|
45.19 0.2651 0.5790 0.0731 0.0335 6.285 44.017 30.199 4686.983 4.973 134.325 2.922 0.72 379395. 0.4712
|
|
49.30 0.2892 0.6114 0.0700 0.0331 6.212 43.506 28.893 4632.574 4.915 128.516 2.829 0.72 379933. 0.4461
|
|
53.41 0.3133 0.6412 0.0666 0.0326 6.112 42.800 27.514 4557.381 4.836 122.384 2.738 0.72 380499. 0.4214
|
|
57.52 0.3374 0.6684 0.0631 0.0319 5.982 41.895 26.070 4461.021 4.733 115.957 2.651 0.72 381095. 0.3970
|
|
61.63 0.3615 0.6931 0.0595 0.0310 5.824 40.789 24.565 4343.242 4.608 109.263 2.565 0.72 381720. 0.3730
|
|
65.74 0.3856 0.7153 0.0557 0.0300 5.637 39.480 23.005 4203.848 4.460 102.326 2.482 0.72 382375. 0.3493
|
|
69.84 0.4098 0.7350 0.0518 0.0289 5.421 37.966 21.396 4042.661 4.289 95.169 2.401 0.72 383060. 0.3258
|
|
73.95 0.4339 0.7522 0.0478 0.0276 5.176 36.246 19.742 3859.471 4.095 87.811 2.320 0.72 383775. 0.3024
|
|
78.06 0.4580 0.7666 0.0437 0.0261 4.900 34.317 18.047 3654.081 3.877 80.271 2.240 0.72 384520. 0.2792
|
|
82.17 0.4821 0.7780 0.0395 0.0245 4.595 32.178 16.314 3426.317 3.635 72.567 2.160 0.72 385296. 0.2559
|
|
86.28 0.5062 0.7859 0.0352 0.0227 4.259 29.828 14.549 3176.082 3.370 64.715 2.078 0.72 386102. 0.2325
|
|
90.39 0.5303 0.7896 0.0309 0.0207 3.893 27.267 12.755 2903.373 3.081 56.733 1.993 0.72 386939. 0.2088
|
|
94.49 0.5544 0.7878 0.0265 0.0186 3.498 24.496 10.936 2608.336 2.768 48.643 1.902 0.73 387806. 0.1845
|
|
98.60 0.5785 0.7784 0.0220 0.0164 3.073 21.519 9.097 2291.326 2.431 40.464 1.801 0.73 388705. 0.1593
|
|
102.71 0.6026 0.7576 0.0175 0.0140 2.619 18.341 7.244 1952.988 2.072 32.222 1.682 0.73 389634. 0.1329
|
|
106.82 0.6267 0.7173 0.0130 0.0114 2.138 14.973 5.384 1594.371 1.692 23.948 1.532 0.73 390593. 0.1043
|
|
110.93 0.6508 0.6387 0.0085 0.0087 1.632 11.429 3.524 1217.000 1.291 15.676 1.313 0.73 391583. 0.0723
|
|
115.04 0.6749 0.4651 0.0041 0.0059 1.103 7.727 1.673 822.755 0.873 7.442 0.922 0.73 392598. 0.0350
|
|
119.15 0.6990
|
|
|
|
|
|
|
|
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 0.0976 0.0336 8.646 54.497 49.777 6447.615 6.157 221.407 3.502 0.79 416926. 0.7248
|
|
4.55 0.0240 0.0681 0.0964 0.0340 8.760 55.212 49.173 6532.243 6.238 218.721 3.414 0.79 417199. 0.7024
|
|
9.10 0.0481 0.1328 0.0951 0.0344 8.864 55.870 48.497 6610.116 6.312 215.717 3.328 0.79 417498. 0.6799
|
|
13.65 0.0721 0.1941 0.0936 0.0348 8.957 56.457 47.746 6679.488 6.378 212.373 3.242 0.79 417824. 0.6573
|
|
18.21 0.0961 0.2520 0.0920 0.0351 9.037 56.957 46.912 6738.674 6.435 208.665 3.158 0.79 418177. 0.6345
|
|
22.76 0.1202 0.3067 0.0902 0.0353 9.100 57.356 45.992 6785.937 6.480 204.572 3.074 0.79 418559. 0.6116
|
|
27.31 0.1442 0.3582 0.0882 0.0355 9.145 57.639 44.980 6819.431 6.512 200.071 2.992 0.79 418970. 0.5887
|
|
31.86 0.1682 0.4065 0.0860 0.0356 9.169 57.790 43.872 6837.181 6.529 195.143 2.910 0.79 419411. 0.5656
|
|
36.41 0.1922 0.4518 0.0837 0.0356 9.169 57.788 42.664 6837.030 6.529 189.768 2.830 0.79 419883. 0.5424
|
|
40.96 0.2163 0.4941 0.0811 0.0355 9.141 57.617 41.351 6816.725 6.509 183.929 2.751 0.80 420386. 0.5191
|
|
45.51 0.2403 0.5335 0.0783 0.0353 9.084 57.255 39.932 6773.974 6.469 177.616 2.674 0.80 420920. 0.4957
|
|
50.06 0.2643 0.5701 0.0753 0.0349 8.994 56.687 38.406 6706.725 6.404 170.829 2.597 0.80 421486. 0.4722
|
|
54.62 0.2884 0.6039 0.0721 0.0344 8.869 55.899 36.778 6613.486 6.315 163.587 2.522 0.80 422084. 0.4488
|
|
59.17 0.3124 0.6351 0.0687 0.0338 8.708 54.883 35.054 6493.365 6.201 155.920 2.449 0.80 422714. 0.4253
|
|
63.72 0.3364 0.6637 0.0652 0.0330 8.510 53.636 33.243 6345.787 6.060 147.866 2.376 0.80 423376. 0.4019
|
|
68.27 0.3605 0.6898 0.0615 0.0321 8.275 52.153 31.354 6170.299 5.892 139.460 2.305 0.80 424071. 0.3786
|
|
72.82 0.3845 0.7133 0.0576 0.0311 8.001 50.430 29.392 5966.415 5.698 130.736 2.234 0.80 424799. 0.3554
|
|
77.37 0.4085 0.7343 0.0537 0.0299 7.689 48.462 27.366 5733.597 5.475 121.723 2.165 0.80 425559. 0.3322
|
|
81.92 0.4326 0.7527 0.0496 0.0285 7.337 46.244 25.280 5471.243 5.225 112.447 2.096 0.80 426353. 0.3091
|
|
86.47 0.4566 0.7683 0.0454 0.0270 6.945 43.776 23.141 5179.160 4.946 102.932 2.027 0.80 427179. 0.2860
|
|
91.03 0.4806 0.7809 0.0411 0.0253 6.513 41.051 20.953 4856.836 4.638 93.200 1.957 0.80 428039. 0.2628
|
|
95.58 0.5046 0.7899 0.0367 0.0235 6.040 38.070 18.721 4504.075 4.301 83.273 1.885 0.80 428933. 0.2393
|
|
100.13 0.5287 0.7948 0.0323 0.0215 5.526 34.831 16.451 4120.943 3.935 73.172 1.811 0.80 429860. 0.2155
|
|
104.68 0.5527 0.7941 0.0277 0.0193 4.973 31.342 14.146 3708.088 3.541 62.923 1.730 0.81 430821. 0.1909
|
|
109.23 0.5767 0.7855 0.0232 0.0170 4.381 27.612 11.815 3266.804 3.120 52.552 1.640 0.81 431815. 0.1654
|
|
113.78 0.6008 0.7649 0.0186 0.0146 3.753 23.658 9.462 2798.984 2.673 42.088 1.533 0.81 432844. 0.1384
|
|
118.33 0.6248 0.7238 0.0139 0.0120 3.094 19.501 7.097 2307.241 2.203 31.568 1.395 0.81 433905. 0.1090
|
|
122.88 0.6488 0.6438 0.0093 0.0093 2.407 15.172 4.729 1794.979 1.714 21.036 1.195 0.81 435000. 0.0762
|
|
127.44 0.6729 0.4740 0.0046 0.0066 1.698 10.702 2.368 1266.177 1.209 10.535 0.848 0.81 436123. 0.0383
|
|
131.99 0.6969 -0.0094 0.0000 0.0037 0.952 6.003 -0.025 710.259 0.678 -0.113 -0.016 0.81 437119. 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 0.0993 0.0401 13.740 78.727 61.274 10245.703 8.894 272.549 2.713 0.87 458542. 0.6230
|
|
5.02 0.0241 0.0586 0.0983 0.0404 13.853 79.374 60.619 10329.923 8.968 269.635 2.662 0.87 458840. 0.6080
|
|
10.04 0.0482 0.1149 0.0970 0.0407 13.945 79.902 59.877 10398.686 9.027 266.331 2.612 0.87 459168. 0.5929
|
|
15.06 0.0723 0.1692 0.0957 0.0409 14.012 80.286 59.037 10448.719 9.071 262.599 2.563 0.87 459525. 0.5777
|
|
20.07 0.0964 0.2213 0.0942 0.0410 14.050 80.505 58.094 10477.193 9.095 258.401 2.515 0.87 459914. 0.5624
|
|
25.09 0.1204 0.2715 0.0924 0.0410 14.056 80.539 57.037 10481.641 9.099 253.701 2.468 0.87 460336. 0.5469
|
|
30.11 0.1445 0.3198 0.0905 0.0409 14.027 80.373 55.860 10460.024 9.081 248.466 2.422 0.87 460791. 0.5311
|
|
35.13 0.1686 0.3661 0.0884 0.0407 13.960 79.991 54.556 10410.324 9.037 242.665 2.377 0.87 461280. 0.5151
|
|
40.15 0.1927 0.4105 0.0861 0.0404 13.854 79.384 53.119 10331.259 8.969 236.272 2.332 0.87 461804. 0.4987
|
|
45.17 0.2168 0.4529 0.0835 0.0400 13.707 78.539 51.544 10221.347 8.873 229.267 2.287 0.87 462362. 0.4818
|
|
50.19 0.2409 0.4933 0.0808 0.0394 13.516 77.445 49.828 10078.940 8.750 221.633 2.242 0.88 462956. 0.4644
|
|
55.20 0.2650 0.5317 0.0778 0.0387 13.280 76.091 47.970 9902.688 8.597 213.369 2.197 0.88 463586. 0.4465
|
|
60.22 0.2891 0.5681 0.0745 0.0379 12.997 74.472 45.975 9691.991 8.414 204.499 2.152 0.88 464251. 0.4280
|
|
65.24 0.3132 0.6022 0.0711 0.0370 12.669 72.590 43.854 9447.027 8.201 195.063 2.106 0.88 464952. 0.4091
|
|
70.26 0.3372 0.6342 0.0675 0.0359 12.295 70.448 41.617 9168.249 7.959 185.112 2.059 0.88 465688. 0.3897
|
|
75.28 0.3613 0.6638 0.0637 0.0347 11.876 68.049 39.275 8856.051 7.688 174.693 2.011 0.88 466461. 0.3698
|
|
80.30 0.3854 0.6911 0.0597 0.0333 11.413 65.393 36.837 8510.490 7.388 163.852 1.963 0.88 467270. 0.3496
|
|
85.32 0.4095 0.7159 0.0556 0.0318 10.904 62.480 34.314 8131.320 7.059 152.626 1.914 0.88 468114. 0.3289
|
|
90.33 0.4336 0.7380 0.0514 0.0302 10.350 59.304 31.712 7717.973 6.700 141.054 1.864 0.88 468996. 0.3079
|
|
95.35 0.4577 0.7574 0.0471 0.0284 9.749 55.859 29.039 7269.680 6.311 129.166 1.812 0.88 469913. 0.2864
|
|
100.37 0.4818 0.7731 0.0426 0.0266 9.106 52.175 26.302 6790.186 5.895 116.991 1.757 0.88 470867. 0.2644
|
|
105.39 0.5059 0.7845 0.0381 0.0246 8.421 48.251 23.507 6279.577 5.451 104.557 1.698 0.88 471858. 0.2415
|
|
110.41 0.5300 0.7875 0.0335 0.0225 7.723 44.250 20.656 5758.782 4.999 91.879 1.627 0.88 472886. 0.2169
|
|
115.43 0.5541 0.7811 0.0288 0.0204 6.998 40.095 17.759 5218.122 4.530 78.994 1.544 0.89 473950. 0.1909
|
|
120.45 0.5781 0.7635 0.0240 0.0182 6.237 35.735 14.825 4650.710 4.037 65.942 1.446 0.89 475052. 0.1633
|
|
125.46 0.6022 0.7287 0.0192 0.0159 5.446 31.205 11.862 4061.063 3.525 52.764 1.325 0.89 476190. 0.1339
|
|
130.48 0.6263 0.6671 0.0144 0.0135 4.633 26.547 8.883 3454.965 2.999 39.510 1.166 0.89 477365. 0.1020
|
|
135.50 0.6504 0.5598 0.0096 0.0111 3.807 21.815 5.899 2839.080 2.465 26.237 0.942 0.89 478576. 0.0671
|
|
140.52 0.6745 0.3681 0.0047 0.0087 2.978 17.062 2.925 2220.454 1.928 13.012 0.598 0.89 479818. 0.0300
|
|
145.54 0.6986 -0.0146 -0.0001 0.0062 2.120 12.149 -0.080 1581.128 1.373 -0.354 -0.023 0.89 480959. 0.0000
|
|
|
|
|
|
|