464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x8E (20x8E.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 0.0707 0.0246 0.006 0.399 0.361 4.717 0.045 1.604 34.671 0.08 36848. 0.6108
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0.35 0.0187 0.0524 0.0693 0.0247 0.006 0.401 0.353 4.739 0.045 1.572 33.823 0.08 36865. 0.5899
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0.71 0.0373 0.1021 0.0678 0.0248 0.006 0.402 0.346 4.756 0.045 1.538 32.973 0.08 36884. 0.5688
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1.06 0.0560 0.1493 0.0662 0.0248 0.006 0.403 0.338 4.769 0.046 1.502 32.123 0.08 36904. 0.5477
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1.41 0.0746 0.1937 0.0646 0.0249 0.006 0.404 0.329 4.776 0.046 1.465 31.274 0.08 36925. 0.5265
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1.77 0.0933 0.2356 0.0628 0.0249 0.006 0.404 0.320 4.777 0.046 1.425 30.426 0.08 36947. 0.5053
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2.12 0.1119 0.2749 0.0610 0.0248 0.006 0.403 0.311 4.772 0.046 1.384 29.578 0.08 36971. 0.4841
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2.47 0.1306 0.3115 0.0591 0.0248 0.006 0.402 0.301 4.758 0.045 1.341 28.730 0.08 36996. 0.4627
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2.83 0.1492 0.3454 0.0571 0.0247 0.006 0.400 0.291 4.737 0.045 1.295 27.880 0.08 37022. 0.4414
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3.18 0.1679 0.3767 0.0550 0.0245 0.006 0.398 0.280 4.707 0.045 1.248 27.028 0.08 37050. 0.4200
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3.53 0.1865 0.4053 0.0528 0.0243 0.006 0.394 0.269 4.667 0.045 1.198 26.172 0.08 37079. 0.3985
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3.89 0.2052 0.4312 0.0505 0.0240 0.006 0.390 0.258 4.617 0.044 1.146 25.310 0.08 37110. 0.3769
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4.24 0.2238 0.4542 0.0482 0.0237 0.006 0.385 0.246 4.558 0.044 1.092 24.439 0.08 37143. 0.3553
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4.59 0.2425 0.4743 0.0457 0.0234 0.006 0.379 0.233 4.488 0.043 1.037 23.557 0.08 37177. 0.3337
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4.95 0.2611 0.4913 0.0432 0.0230 0.006 0.373 0.220 4.408 0.042 0.979 22.660 0.08 37212. 0.3120
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5.30 0.2798 0.5051 0.0406 0.0225 0.006 0.365 0.207 4.317 0.041 0.920 21.743 0.08 37250. 0.2902
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5.65 0.2985 0.5155 0.0379 0.0220 0.006 0.356 0.193 4.215 0.040 0.860 20.801 0.08 37289. 0.2683
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6.01 0.3171 0.5221 0.0352 0.0214 0.006 0.347 0.179 4.103 0.039 0.798 19.830 0.08 37329. 0.2464
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6.36 0.3358 0.5247 0.0324 0.0207 0.005 0.336 0.165 3.980 0.038 0.735 18.821 0.08 37371. 0.2244
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6.71 0.3544 0.5228 0.0295 0.0200 0.005 0.325 0.151 3.846 0.037 0.670 17.766 0.08 37415. 0.2023
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7.07 0.3731 0.5159 0.0266 0.0193 0.005 0.313 0.136 3.701 0.035 0.604 16.654 0.08 37461. 0.1801
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7.42 0.3917 0.5032 0.0237 0.0185 0.005 0.300 0.121 3.545 0.034 0.538 15.472 0.08 37509. 0.1578
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7.77 0.4104 0.4840 0.0207 0.0176 0.005 0.286 0.106 3.378 0.032 0.471 14.204 0.08 37558. 0.1355
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8.13 0.4290 0.4569 0.0178 0.0167 0.004 0.271 0.091 3.202 0.031 0.403 12.828 0.08 37609. 0.1132
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8.48 0.4477 0.4207 0.0148 0.0157 0.004 0.255 0.075 3.015 0.029 0.335 11.317 0.08 37662. 0.0911
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8.83 0.4663 0.3730 0.0117 0.0147 0.004 0.238 0.060 2.818 0.027 0.266 9.635 0.08 37716. 0.0692
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9.19 0.4850 0.3114 0.0087 0.0136 0.004 0.221 0.045 2.612 0.025 0.198 7.732 0.08 37773. 0.0479
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9.54 0.5036 0.2317 0.0057 0.0125 0.003 0.203 0.029 2.398 0.023 0.130 5.542 0.08 37831. 0.0278
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9.89 0.5223 0.1286 0.0028 0.0113 0.003 0.184 0.014 2.177 0.021 0.063 2.966 0.08 37891. 0.0104
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10.25 0.5409 -0.0072 -0.0001 0.0101 0.003 0.165 -0.001 1.947 0.019 -0.003 -0.160 0.08 37952. 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 0.0710 0.0224 0.046 1.457 1.448 34.487 0.165 6.442 19.048 0.16 73695. 0.6725
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0.71 0.0187 0.0576 0.0696 0.0226 0.047 1.466 1.420 34.690 0.166 6.314 18.560 0.16 73730. 0.6488
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1.42 0.0374 0.1122 0.0681 0.0227 0.047 1.473 1.389 34.858 0.166 6.179 18.074 0.16 73767. 0.6250
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2.12 0.0561 0.1638 0.0665 0.0228 0.047 1.479 1.357 34.985 0.167 6.036 17.592 0.16 73807. 0.6012
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2.83 0.0747 0.2124 0.0649 0.0228 0.047 1.482 1.323 35.067 0.167 5.885 17.114 0.16 73849. 0.5776
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3.54 0.0934 0.2582 0.0631 0.0228 0.047 1.483 1.288 35.097 0.168 5.727 16.640 0.16 73894. 0.5539
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4.25 0.1121 0.3011 0.0613 0.0228 0.047 1.482 1.250 35.071 0.167 5.561 16.169 0.16 73941. 0.5304
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4.95 0.1308 0.3411 0.0594 0.0228 0.047 1.478 1.211 34.983 0.167 5.387 15.702 0.16 73992. 0.5070
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5.66 0.1495 0.3783 0.0574 0.0227 0.047 1.472 1.170 34.826 0.166 5.204 15.238 0.16 74045. 0.4836
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6.37 0.1682 0.4127 0.0553 0.0225 0.046 1.462 1.127 34.595 0.165 5.013 14.777 0.16 74101. 0.4603
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7.08 0.1869 0.4443 0.0531 0.0223 0.046 1.449 1.082 34.283 0.164 4.814 14.318 0.16 74160. 0.4370
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7.79 0.2056 0.4731 0.0508 0.0221 0.045 1.432 1.035 33.888 0.162 4.606 13.859 0.16 74222. 0.4137
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8.49 0.2242 0.4990 0.0484 0.0217 0.045 1.412 0.987 33.407 0.160 4.390 13.400 0.16 74287. 0.3906
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9.20 0.2429 0.5220 0.0459 0.0214 0.044 1.388 0.937 32.839 0.157 4.167 12.939 0.16 74355. 0.3674
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9.91 0.2616 0.5420 0.0434 0.0209 0.043 1.360 0.885 32.181 0.154 3.937 12.475 0.16 74426. 0.3443
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10.62 0.2803 0.5587 0.0408 0.0205 0.042 1.328 0.832 31.432 0.150 3.700 12.004 0.16 74501. 0.3212
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11.33 0.2990 0.5722 0.0381 0.0199 0.041 1.293 0.777 30.590 0.146 3.457 11.524 0.16 74579. 0.2981
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12.03 0.3177 0.5820 0.0354 0.0193 0.040 1.253 0.721 29.655 0.142 3.208 11.032 0.16 74661. 0.2749
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12.74 0.3364 0.5879 0.0326 0.0186 0.038 1.210 0.664 28.624 0.137 2.954 10.525 0.16 74745. 0.2516
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13.45 0.3551 0.5894 0.0297 0.0179 0.037 1.162 0.606 27.499 0.131 2.696 9.996 0.16 74834. 0.2283
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14.16 0.3737 0.5859 0.0268 0.0171 0.035 1.111 0.547 26.278 0.125 2.433 9.440 0.16 74925. 0.2048
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14.86 0.3924 0.5767 0.0239 0.0162 0.033 1.055 0.487 24.962 0.119 2.166 8.849 0.16 75021. 0.1812
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15.57 0.4111 0.5607 0.0209 0.0153 0.032 0.995 0.426 23.553 0.112 1.897 8.213 0.16 75120. 0.1574
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16.28 0.4298 0.5365 0.0179 0.0144 0.030 0.932 0.365 22.052 0.105 1.626 7.517 0.16 75222. 0.1333
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16.99 0.4485 0.5021 0.0149 0.0133 0.027 0.865 0.304 20.462 0.098 1.353 6.742 0.16 75328. 0.1091
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17.70 0.4672 0.4547 0.0119 0.0122 0.025 0.794 0.243 18.788 0.090 1.080 5.861 0.16 75438. 0.0847
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18.40 0.4859 0.3900 0.0089 0.0111 0.023 0.720 0.182 17.035 0.081 0.808 4.834 0.16 75551. 0.0604
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19.11 0.5046 0.3018 0.0059 0.0099 0.020 0.643 0.121 15.209 0.073 0.537 3.602 0.16 75669. 0.0367
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19.82 0.5232 0.1796 0.0030 0.0087 0.018 0.563 0.061 13.318 0.064 0.270 2.067 0.16 75789. 0.0149
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20.53 0.5419 0.0041 0.0001 0.0074 0.015 0.480 0.001 11.356 0.054 0.005 0.046 0.16 75909. 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 0.0714 0.0216 0.150 3.155 3.275 111.981 0.356 14.568 13.266 0.24 110539. 0.7044
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1.06 0.0187 0.0603 0.0700 0.0217 0.151 3.175 3.210 112.706 0.359 14.278 12.918 0.24 110592. 0.6790
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2.13 0.0375 0.1174 0.0684 0.0219 0.152 3.192 3.141 113.310 0.361 13.972 12.574 0.24 110649. 0.6538
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3.19 0.0562 0.1713 0.0669 0.0219 0.153 3.205 3.068 113.774 0.362 13.648 12.233 0.24 110709. 0.6287
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4.26 0.0749 0.2221 0.0652 0.0220 0.153 3.214 2.992 114.079 0.363 13.308 11.896 0.24 110772. 0.6037
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5.32 0.0937 0.2698 0.0634 0.0220 0.153 3.218 2.911 114.207 0.364 12.950 11.562 0.24 110840. 0.5788
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6.39 0.1124 0.3146 0.0616 0.0220 0.153 3.216 2.827 114.139 0.363 12.573 11.233 0.24 110911. 0.5541
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7.45 0.1312 0.3563 0.0597 0.0220 0.153 3.208 2.738 113.856 0.362 12.179 10.908 0.24 110987. 0.5295
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8.52 0.1499 0.3952 0.0576 0.0219 0.152 3.193 2.645 113.335 0.361 11.765 10.586 0.24 111067. 0.5051
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9.58 0.1686 0.4312 0.0555 0.0217 0.151 3.171 2.548 112.554 0.358 11.332 10.267 0.24 111152. 0.4808
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10.65 0.1874 0.4644 0.0533 0.0215 0.150 3.141 2.446 111.493 0.355 10.880 9.951 0.24 111241. 0.4566
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11.71 0.2061 0.4947 0.0510 0.0212 0.148 3.103 2.340 110.140 0.351 10.408 9.637 0.24 111334. 0.4325
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12.77 0.2248 0.5222 0.0486 0.0209 0.145 3.057 2.230 108.488 0.345 9.920 9.324 0.24 111432. 0.4085
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13.84 0.2436 0.5467 0.0461 0.0205 0.143 3.001 2.116 106.529 0.339 9.414 9.011 0.24 111535. 0.3846
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14.90 0.2623 0.5683 0.0436 0.0201 0.140 2.937 1.999 104.255 0.332 8.892 8.697 0.24 111643. 0.3608
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15.97 0.2810 0.5867 0.0409 0.0196 0.136 2.864 1.878 101.661 0.324 8.355 8.381 0.24 111756. 0.3370
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17.03 0.2998 0.6019 0.0382 0.0190 0.132 2.782 1.755 98.740 0.314 7.804 8.060 0.24 111873. 0.3132
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18.10 0.3185 0.6135 0.0355 0.0184 0.128 2.690 1.628 95.489 0.304 7.241 7.732 0.24 111996. 0.2894
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19.16 0.3373 0.6213 0.0327 0.0177 0.123 2.589 1.498 91.904 0.293 6.665 7.395 0.24 112124. 0.2656
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20.23 0.3560 0.6248 0.0298 0.0170 0.118 2.479 1.367 87.982 0.280 6.079 7.046 0.24 112257. 0.2416
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21.29 0.3747 0.6234 0.0269 0.0161 0.112 2.359 1.233 83.724 0.267 5.483 6.679 0.24 112395. 0.2176
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22.36 0.3935 0.6163 0.0239 0.0153 0.106 2.229 1.097 79.131 0.252 4.880 6.289 0.24 112539. 0.1932
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23.42 0.4122 0.6025 0.0209 0.0143 0.100 2.091 0.960 74.207 0.236 4.270 5.868 0.24 112688. 0.1687
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24.49 0.4309 0.5803 0.0179 0.0133 0.092 1.943 0.822 68.960 0.220 3.656 5.406 0.24 112842. 0.1438
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25.55 0.4497 0.5474 0.0149 0.0122 0.085 1.786 0.683 63.400 0.202 3.039 4.887 0.24 113002. 0.1185
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26.61 0.4684 0.5006 0.0119 0.0111 0.077 1.621 0.544 57.543 0.183 2.421 4.291 0.24 113168. 0.0929
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27.68 0.4872 0.4346 0.0088 0.0099 0.069 1.448 0.406 51.407 0.164 1.806 3.582 0.24 113339. 0.0670
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28.74 0.5059 0.3410 0.0059 0.0087 0.060 1.268 0.269 45.017 0.143 1.195 2.706 0.24 113515. 0.0412
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29.81 0.5246 0.2051 0.0029 0.0074 0.051 1.082 0.133 38.398 0.122 0.591 1.570 0.24 113697. 0.0168
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30.87 0.5434 -0.0038 0.0000 0.0061 0.042 0.888 -0.002 31.508 0.100 -0.009 -0.028 0.24 113875. 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 0.0718 0.0212 0.349 5.503 5.861 260.414 0.622 26.070 10.208 0.32 147381. 0.7251
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1.42 0.0188 0.0619 0.0704 0.0213 0.352 5.540 5.745 262.184 0.626 25.552 9.938 0.32 147452. 0.6988
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2.84 0.0375 0.1205 0.0689 0.0215 0.354 5.571 5.621 263.661 0.629 25.004 9.670 0.32 147528. 0.6727
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4.26 0.0563 0.1758 0.0673 0.0215 0.355 5.595 5.491 264.797 0.632 24.426 9.406 0.32 147608. 0.6467
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5.68 0.0750 0.2279 0.0656 0.0216 0.356 5.611 5.354 265.552 0.634 23.816 9.145 0.32 147693. 0.6209
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7.10 0.0938 0.2768 0.0639 0.0216 0.357 5.618 5.210 265.877 0.635 23.176 8.888 0.32 147784. 0.5952
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8.52 0.1125 0.3227 0.0620 0.0216 0.356 5.615 5.059 265.729 0.634 22.502 8.635 0.32 147879. 0.5698
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9.95 0.1313 0.3656 0.0601 0.0216 0.355 5.601 4.900 265.057 0.633 21.796 8.385 0.32 147981. 0.5446
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11.37 0.1500 0.4055 0.0580 0.0215 0.354 5.574 4.734 263.810 0.630 21.055 8.139 0.32 148088. 0.5195
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12.79 0.1688 0.4426 0.0559 0.0213 0.351 5.535 4.559 261.933 0.625 20.280 7.895 0.32 148201. 0.4946
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14.21 0.1875 0.4768 0.0537 0.0211 0.348 5.481 4.377 259.379 0.619 19.470 7.654 0.32 148320. 0.4698
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15.63 0.2063 0.5081 0.0513 0.0208 0.343 5.412 4.188 256.116 0.611 18.626 7.416 0.32 148445. 0.4452
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17.05 0.2251 0.5366 0.0489 0.0205 0.338 5.328 3.991 252.124 0.602 17.750 7.179 0.32 148576. 0.4208
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18.47 0.2438 0.5622 0.0464 0.0201 0.332 5.227 3.787 247.385 0.591 16.844 6.943 0.32 148714. 0.3964
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19.89 0.2626 0.5849 0.0438 0.0197 0.324 5.111 3.577 241.881 0.577 15.910 6.707 0.32 148858. 0.3722
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21.31 0.2813 0.6045 0.0412 0.0192 0.316 4.978 3.361 235.597 0.562 14.948 6.470 0.32 149008. 0.3480
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22.73 0.3001 0.6209 0.0385 0.0186 0.306 4.829 3.139 228.518 0.546 13.962 6.230 0.32 149166. 0.3238
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24.15 0.3188 0.6339 0.0357 0.0180 0.296 4.662 2.912 220.632 0.527 12.952 5.986 0.32 149330. 0.2997
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25.57 0.3376 0.6431 0.0329 0.0172 0.284 4.478 2.680 211.931 0.506 11.921 5.736 0.32 149501. 0.2755
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27.00 0.3563 0.6481 0.0300 0.0165 0.271 4.277 2.444 202.409 0.483 10.871 5.477 0.32 149679. 0.2512
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28.42 0.3751 0.6484 0.0270 0.0156 0.258 4.058 2.204 192.066 0.459 9.804 5.205 0.32 149863. 0.2267
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29.84 0.3938 0.6432 0.0240 0.0147 0.243 3.823 1.961 180.905 0.432 8.724 4.917 0.32 150055. 0.2020
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31.26 0.4126 0.6312 0.0210 0.0137 0.227 3.570 1.716 168.937 0.403 7.631 4.606 0.32 150255. 0.1770
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32.68 0.4314 0.6109 0.0180 0.0127 0.209 3.300 1.468 156.180 0.373 6.531 4.264 0.32 150461. 0.1516
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34.10 0.4501 0.5798 0.0150 0.0116 0.191 3.015 1.220 142.662 0.341 5.426 3.879 0.32 150675. 0.1257
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35.52 0.4689 0.5343 0.0119 0.0104 0.172 2.714 0.971 128.417 0.307 4.321 3.431 0.32 150896. 0.0992
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36.94 0.4876 0.4684 0.0089 0.0092 0.152 2.398 0.724 113.495 0.271 3.219 2.892 0.32 151124. 0.0722
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38.36 0.5064 0.3722 0.0059 0.0080 0.131 2.070 0.478 97.954 0.234 2.126 2.213 0.32 151360. 0.0449
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39.78 0.5251 0.2273 0.0029 0.0067 0.110 1.730 0.235 81.859 0.195 1.046 1.303 0.32 151602. 0.0185
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41.20 0.5439 -0.0083 -0.0001 0.0053 0.087 1.375 -0.007 65.057 0.155 -0.029 -0.046 0.32 151837. 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 0.0724 0.0210 0.677 8.530 9.235 504.598 0.964 41.079 8.301 0.40 184219. 0.7401
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1.78 0.0188 0.0629 0.0710 0.0212 0.681 8.589 9.052 508.112 0.970 40.264 8.081 0.40 184308. 0.7133
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3.55 0.0375 0.1225 0.0695 0.0213 0.685 8.639 8.858 511.038 0.976 39.402 7.862 0.40 184402. 0.6865
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5.33 0.0563 0.1787 0.0679 0.0214 0.688 8.677 8.654 513.289 0.980 38.492 7.647 0.40 184503. 0.6600
|
|
7.11 0.0750 0.2316 0.0662 0.0214 0.690 8.702 8.438 514.775 0.983 37.533 7.435 0.40 184610. 0.6336
|
|
8.88 0.0938 0.2814 0.0644 0.0215 0.691 8.713 8.211 515.407 0.984 36.524 7.226 0.40 184724. 0.6075
|
|
10.66 0.1126 0.3281 0.0625 0.0215 0.691 8.707 7.973 515.093 0.984 35.464 7.021 0.40 184844. 0.5816
|
|
12.44 0.1313 0.3717 0.0606 0.0214 0.689 8.684 7.723 513.736 0.981 34.352 6.818 0.40 184971. 0.5559
|
|
14.21 0.1501 0.4124 0.0585 0.0213 0.686 8.642 7.461 511.235 0.976 33.186 6.619 0.40 185106. 0.5304
|
|
15.99 0.1688 0.4502 0.0564 0.0211 0.681 8.579 7.186 507.479 0.969 31.964 6.423 0.40 185247. 0.5051
|
|
17.77 0.1876 0.4851 0.0541 0.0209 0.674 8.492 6.899 502.372 0.959 30.688 6.229 0.40 185396. 0.4800
|
|
19.54 0.2064 0.5172 0.0518 0.0207 0.665 8.382 6.600 495.852 0.947 29.358 6.037 0.40 185553. 0.4551
|
|
21.32 0.2251 0.5465 0.0493 0.0203 0.654 8.247 6.290 487.876 0.932 27.978 5.848 0.40 185718. 0.4303
|
|
23.09 0.2439 0.5730 0.0468 0.0199 0.642 8.087 5.969 478.407 0.914 26.549 5.659 0.40 185890. 0.4056
|
|
24.87 0.2626 0.5965 0.0442 0.0195 0.627 7.901 5.638 467.410 0.893 25.076 5.471 0.40 186071. 0.3811
|
|
26.65 0.2814 0.6170 0.0416 0.0189 0.610 7.689 5.297 454.855 0.869 23.560 5.282 0.40 186259. 0.3566
|
|
28.42 0.3002 0.6344 0.0388 0.0184 0.591 7.450 4.947 440.712 0.842 22.004 5.091 0.40 186456. 0.3322
|
|
30.20 0.3189 0.6485 0.0360 0.0177 0.570 7.184 4.589 424.957 0.812 20.412 4.898 0.40 186662. 0.3078
|
|
31.98 0.3377 0.6589 0.0331 0.0170 0.547 6.890 4.223 407.573 0.778 18.786 4.700 0.40 186876. 0.2834
|
|
33.75 0.3564 0.6652 0.0302 0.0162 0.521 6.568 3.851 388.547 0.742 17.130 4.496 0.40 187099. 0.2588
|
|
35.53 0.3752 0.6670 0.0272 0.0153 0.493 6.219 3.473 367.879 0.703 15.447 4.282 0.40 187330. 0.2341
|
|
37.31 0.3940 0.6632 0.0242 0.0144 0.463 5.842 3.090 345.577 0.660 13.743 4.055 0.40 187570. 0.2091
|
|
39.08 0.4127 0.6529 0.0212 0.0134 0.431 5.438 2.702 321.662 0.614 12.020 3.811 0.40 187820. 0.1838
|
|
40.86 0.4315 0.6343 0.0181 0.0123 0.397 5.007 2.312 296.170 0.566 10.285 3.541 0.40 188078. 0.1580
|
|
42.64 0.4502 0.6049 0.0151 0.0112 0.361 4.550 1.921 269.155 0.514 8.542 3.236 0.40 188345. 0.1316
|
|
44.41 0.4690 0.5609 0.0120 0.0100 0.323 4.069 1.529 240.691 0.460 6.799 2.880 0.40 188622. 0.1045
|
|
46.19 0.4878 0.4956 0.0089 0.0088 0.283 3.565 1.138 210.875 0.403 5.062 2.448 0.40 188908. 0.0766
|
|
47.97 0.5065 0.3981 0.0059 0.0075 0.241 3.040 0.750 179.827 0.343 3.338 1.893 0.40 189202. 0.0481
|
|
49.74 0.5253 0.2463 0.0029 0.0062 0.198 2.496 0.368 147.676 0.282 1.636 1.129 0.40 189506. 0.0201
|
|
51.52 0.5440 -0.0132 -0.0001 0.0047 0.153 1.927 -0.015 114.013 0.218 -0.065 -0.058 0.40 189794. 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 0.0732 0.0210 1.169 12.284 13.440 872.019 1.388 59.781 6.991 0.48 221050. 0.7519
|
|
2.13 0.0188 0.0636 0.0718 0.0212 1.178 12.370 13.174 878.143 1.398 58.598 6.805 0.48 221158. 0.7246
|
|
4.26 0.0375 0.1237 0.0702 0.0213 1.184 12.442 12.893 883.228 1.406 57.347 6.621 0.48 221272. 0.6975
|
|
6.39 0.0563 0.1805 0.0686 0.0214 1.190 12.497 12.596 887.116 1.412 56.025 6.440 0.48 221394. 0.6705
|
|
8.53 0.0750 0.2341 0.0669 0.0214 1.193 12.533 12.283 889.650 1.416 54.633 6.262 0.48 221523. 0.6439
|
|
10.66 0.0938 0.2844 0.0651 0.0215 1.194 12.547 11.953 890.676 1.418 53.167 6.087 0.48 221660. 0.6174
|
|
12.79 0.1125 0.3316 0.0632 0.0215 1.194 12.538 11.607 890.028 1.417 51.626 5.915 0.48 221804. 0.5912
|
|
14.92 0.1313 0.3758 0.0612 0.0214 1.190 12.503 11.243 887.541 1.413 50.009 5.746 0.48 221958. 0.5652
|
|
17.05 0.1501 0.4171 0.0592 0.0213 1.184 12.439 10.862 883.036 1.405 48.313 5.579 0.48 222119. 0.5395
|
|
19.18 0.1688 0.4554 0.0570 0.0211 1.175 12.345 10.463 876.319 1.395 46.538 5.415 0.48 222290. 0.5139
|
|
21.32 0.1876 0.4909 0.0547 0.0209 1.163 12.217 10.045 867.219 1.380 44.681 5.254 0.48 222469. 0.4885
|
|
23.45 0.2063 0.5236 0.0524 0.0206 1.147 12.053 9.610 855.624 1.362 42.746 5.094 0.48 222658. 0.4633
|
|
25.58 0.2251 0.5536 0.0499 0.0203 1.128 11.854 9.159 841.459 1.339 40.737 4.937 0.48 222856. 0.4383
|
|
27.71 0.2438 0.5807 0.0473 0.0199 1.106 11.617 8.691 824.659 1.312 38.659 4.780 0.48 223064. 0.4135
|
|
29.84 0.2626 0.6050 0.0447 0.0194 1.080 11.342 8.209 805.162 1.281 36.514 4.624 0.48 223281. 0.3887
|
|
31.97 0.2814 0.6263 0.0420 0.0189 1.050 11.029 7.713 782.913 1.246 34.306 4.468 0.48 223508. 0.3641
|
|
34.10 0.3001 0.6446 0.0392 0.0183 1.016 10.676 7.204 757.862 1.206 32.041 4.311 0.48 223744. 0.3395
|
|
36.24 0.3189 0.6596 0.0364 0.0176 0.979 10.283 6.682 729.966 1.162 29.722 4.152 0.48 223991. 0.3149
|
|
38.37 0.3376 0.6710 0.0335 0.0169 0.938 9.850 6.150 699.195 1.113 27.354 3.989 0.48 224249. 0.2902
|
|
40.50 0.3564 0.6785 0.0305 0.0160 0.892 9.375 5.608 665.528 1.059 24.942 3.822 0.48 224516. 0.2655
|
|
42.63 0.3751 0.6815 0.0275 0.0152 0.843 8.860 5.057 628.963 1.001 22.491 3.646 0.48 224794. 0.2406
|
|
44.76 0.3939 0.6791 0.0245 0.0142 0.791 8.305 4.498 589.515 0.938 20.008 3.461 0.48 225082. 0.2153
|
|
46.89 0.4127 0.6703 0.0214 0.0132 0.734 7.709 3.934 547.221 0.871 17.498 3.261 0.48 225382. 0.1897
|
|
49.02 0.4314 0.6533 0.0183 0.0121 0.673 7.074 3.365 502.145 0.799 14.970 3.040 0.48 225692. 0.1636
|
|
51.16 0.4502 0.6256 0.0152 0.0110 0.609 6.401 2.795 454.384 0.723 12.431 2.790 0.48 226013. 0.1368
|
|
53.29 0.4689 0.5831 0.0121 0.0097 0.542 5.692 2.223 404.067 0.643 9.890 2.496 0.48 226345. 0.1092
|
|
55.42 0.4877 0.5188 0.0090 0.0085 0.471 4.950 1.654 351.367 0.559 7.358 2.135 0.48 226688. 0.0806
|
|
57.55 0.5064 0.4206 0.0059 0.0071 0.398 4.177 1.090 296.499 0.472 4.847 1.667 0.48 227041. 0.0510
|
|
59.68 0.5252 0.2633 0.0029 0.0058 0.321 3.377 0.532 239.693 0.381 2.366 1.007 0.48 227405. 0.0215
|
|
61.81 0.5440 -0.0185 -0.0001 0.0043 0.241 2.536 -0.027 180.031 0.287 -0.121 -0.068 0.48 227745. 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 0.0742 0.0212 1.870 16.836 18.532 1394.301 1.902 82.432 6.029 0.56 257874. 0.7614
|
|
2.49 0.0187 0.0639 0.0727 0.0213 1.883 16.954 18.167 1404.064 1.915 80.808 5.869 0.56 258000. 0.7339
|
|
4.97 0.0375 0.1244 0.0712 0.0214 1.894 17.051 17.781 1412.126 1.926 79.088 5.711 0.56 258134. 0.7065
|
|
7.46 0.0562 0.1816 0.0695 0.0215 1.902 17.125 17.372 1418.230 1.935 77.272 5.556 0.56 258277. 0.6794
|
|
9.94 0.0750 0.2355 0.0678 0.0216 1.907 17.172 16.942 1422.127 1.940 75.357 5.403 0.56 258429. 0.6525
|
|
12.43 0.0937 0.2862 0.0660 0.0216 1.909 17.189 16.488 1423.563 1.942 73.340 5.253 0.56 258589. 0.6258
|
|
14.91 0.1125 0.3338 0.0641 0.0216 1.907 17.173 16.012 1422.276 1.940 71.220 5.106 0.56 258759. 0.5994
|
|
17.40 0.1312 0.3784 0.0621 0.0215 1.902 17.122 15.511 1417.999 1.934 68.994 4.962 0.56 258938. 0.5733
|
|
19.88 0.1500 0.4201 0.0600 0.0214 1.891 17.031 14.987 1410.444 1.924 66.660 4.819 0.56 259128. 0.5474
|
|
22.37 0.1687 0.4589 0.0578 0.0212 1.876 16.896 14.437 1399.302 1.909 64.215 4.680 0.56 259328. 0.5216
|
|
24.85 0.1875 0.4949 0.0555 0.0210 1.856 16.715 13.862 1384.292 1.888 61.658 4.542 0.56 259538. 0.4961
|
|
27.34 0.2062 0.5281 0.0531 0.0207 1.831 16.485 13.263 1365.226 1.862 58.992 4.406 0.56 259759. 0.4708
|
|
29.82 0.2250 0.5586 0.0506 0.0204 1.800 16.204 12.640 1341.986 1.831 56.223 4.272 0.56 259990. 0.4456
|
|
32.31 0.2437 0.5863 0.0480 0.0200 1.763 15.872 11.996 1314.466 1.793 53.357 4.139 0.56 260233. 0.4206
|
|
34.79 0.2624 0.6112 0.0454 0.0195 1.720 15.487 11.331 1282.570 1.750 50.399 4.007 0.56 260487. 0.3957
|
|
37.28 0.2812 0.6333 0.0426 0.0189 1.671 15.047 10.646 1246.208 1.700 47.355 3.875 0.56 260752. 0.3709
|
|
39.76 0.2999 0.6523 0.0398 0.0183 1.616 14.554 9.944 1205.301 1.644 44.230 3.742 0.56 261029. 0.3462
|
|
42.25 0.3187 0.6682 0.0369 0.0176 1.555 14.004 9.225 1159.783 1.582 41.031 3.608 0.56 261317. 0.3215
|
|
44.74 0.3374 0.6806 0.0340 0.0168 1.488 13.398 8.490 1109.603 1.514 37.763 3.470 0.56 261617. 0.2967
|
|
47.22 0.3562 0.6892 0.0310 0.0160 1.414 12.735 7.741 1054.730 1.439 34.434 3.329 0.56 261930. 0.2717
|
|
49.71 0.3749 0.6933 0.0279 0.0151 1.335 12.016 6.981 995.159 1.358 31.051 3.182 0.56 262254. 0.2466
|
|
52.19 0.3937 0.6923 0.0249 0.0141 1.248 11.240 6.210 930.916 1.270 27.622 3.026 0.56 262591. 0.2212
|
|
54.68 0.4124 0.6849 0.0217 0.0131 1.156 10.409 5.431 862.061 1.176 24.156 2.857 0.56 262940. 0.1954
|
|
57.16 0.4312 0.6695 0.0186 0.0120 1.058 9.523 4.646 788.699 1.076 20.664 2.672 0.56 263301. 0.1689
|
|
59.65 0.4499 0.6435 0.0154 0.0108 0.953 8.585 3.857 710.986 0.970 17.157 2.461 0.56 263676. 0.1418
|
|
62.13 0.4687 0.6025 0.0123 0.0096 0.844 7.597 3.068 629.134 0.858 13.647 2.212 0.56 264063. 0.1137
|
|
64.62 0.4874 0.5395 0.0091 0.0083 0.729 6.562 2.282 543.426 0.741 10.150 1.905 0.56 264463. 0.0844
|
|
67.10 0.5061 0.4411 0.0060 0.0069 0.609 5.484 1.502 454.211 0.620 6.679 1.500 0.56 264875. 0.0539
|
|
69.59 0.5249 0.2795 0.0029 0.0055 0.485 4.369 0.731 361.868 0.494 3.252 0.916 0.56 265299. 0.0230
|
|
72.07 0.5436 -0.0238 -0.0002 0.0040 0.355 3.195 -0.044 264.573 0.361 -0.196 -0.075 0.56 265688. 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 0.0754 0.0215 2.829 22.287 24.593 2109.448 2.518 109.389 5.288 0.63 294688. 0.7693
|
|
2.84 0.0187 0.0640 0.0739 0.0216 2.848 22.441 24.111 2124.028 2.535 107.245 5.149 0.63 294833. 0.7417
|
|
5.67 0.0375 0.1247 0.0723 0.0217 2.864 22.567 23.600 2135.975 2.550 104.975 5.011 0.63 294987. 0.7143
|
|
8.51 0.0562 0.1820 0.0707 0.0218 2.876 22.662 23.061 2144.899 2.560 102.575 4.877 0.63 295152. 0.6871
|
|
11.35 0.0749 0.2360 0.0689 0.0219 2.884 22.720 22.492 2150.418 2.567 100.044 4.744 0.63 295326. 0.6601
|
|
14.19 0.0936 0.2870 0.0671 0.0219 2.886 22.738 21.892 2152.151 2.569 97.378 4.614 0.63 295510. 0.6334
|
|
17.02 0.1124 0.3348 0.0652 0.0219 2.883 22.712 21.262 2149.697 2.566 94.573 4.486 0.64 295705. 0.6069
|
|
19.86 0.1311 0.3797 0.0631 0.0218 2.873 22.638 20.600 2142.653 2.558 91.627 4.361 0.64 295912. 0.5807
|
|
22.70 0.1498 0.4217 0.0610 0.0217 2.857 22.510 19.905 2130.593 2.543 88.537 4.237 0.64 296129. 0.5546
|
|
25.54 0.1685 0.4608 0.0588 0.0215 2.834 22.325 19.177 2113.052 2.522 85.299 4.116 0.64 296358. 0.5289
|
|
28.37 0.1873 0.4972 0.0564 0.0213 2.802 22.077 18.415 2089.587 2.494 81.911 3.997 0.64 296600. 0.5033
|
|
31.21 0.2060 0.5309 0.0540 0.0210 2.762 21.764 17.621 2059.917 2.459 78.378 3.880 0.64 296853. 0.4778
|
|
34.05 0.2247 0.5619 0.0515 0.0206 2.714 21.383 16.796 2023.853 2.416 74.708 3.764 0.64 297118. 0.4526
|
|
36.89 0.2434 0.5901 0.0488 0.0202 2.657 20.932 15.941 1981.241 2.365 70.907 3.649 0.64 297396. 0.4275
|
|
39.72 0.2622 0.6157 0.0461 0.0197 2.591 20.412 15.059 1931.940 2.306 66.982 3.535 0.64 297687. 0.4025
|
|
42.56 0.2809 0.6384 0.0434 0.0191 2.516 19.819 14.151 1875.820 2.239 62.943 3.422 0.64 297990. 0.3776
|
|
45.40 0.2996 0.6582 0.0405 0.0184 2.431 19.152 13.218 1812.760 2.164 58.795 3.307 0.64 298307. 0.3528
|
|
48.24 0.3184 0.6749 0.0376 0.0177 2.337 18.412 12.263 1742.666 2.080 54.547 3.192 0.64 298637. 0.3279
|
|
51.07 0.3371 0.6883 0.0346 0.0169 2.233 17.596 11.288 1665.459 1.988 50.207 3.074 0.64 298980. 0.3030
|
|
53.91 0.3558 0.6979 0.0315 0.0161 2.120 16.705 10.293 1581.096 1.887 45.785 2.953 0.64 299337. 0.2779
|
|
56.75 0.3745 0.7032 0.0284 0.0152 1.998 15.738 9.283 1489.573 1.778 41.290 2.827 0.64 299708. 0.2527
|
|
59.58 0.3933 0.7035 0.0253 0.0141 1.865 14.696 8.258 1390.926 1.660 36.733 2.693 0.64 300093. 0.2270
|
|
62.42 0.4120 0.6975 0.0221 0.0131 1.724 13.579 7.223 1285.250 1.534 32.127 2.549 0.64 300492. 0.2010
|
|
65.26 0.4307 0.6837 0.0189 0.0119 1.573 12.390 6.179 1172.708 1.400 27.484 2.390 0.64 300905. 0.1743
|
|
68.10 0.4494 0.6594 0.0157 0.0107 1.413 11.131 5.130 1053.532 1.258 22.820 2.209 0.64 301332. 0.1468
|
|
70.93 0.4682 0.6202 0.0125 0.0094 1.245 9.805 4.081 928.053 1.108 18.152 1.995 0.64 301774. 0.1182
|
|
73.77 0.4869 0.5588 0.0093 0.0081 1.068 8.417 3.035 796.700 0.951 13.499 1.728 0.64 302230. 0.0883
|
|
76.61 0.5056 0.4608 0.0061 0.0067 0.885 6.973 1.997 660.014 0.788 8.881 1.372 0.64 302701. 0.0569
|
|
79.45 0.5243 0.2958 0.0030 0.0053 0.695 5.479 0.971 518.576 0.619 4.319 0.849 0.64 303184. 0.0246
|
|
82.28 0.5431 -0.0281 -0.0002 0.0038 0.495 3.900 -0.063 369.151 0.441 -0.282 -0.078 0.64 303619. 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 0.0768 0.0219 4.112 28.794 31.735 3065.985 3.253 141.156 4.695 0.71 331487. 0.7759
|
|
3.19 0.0187 0.0639 0.0753 0.0220 4.139 28.988 31.118 3086.655 3.275 138.413 4.573 0.71 331652. 0.7484
|
|
6.37 0.0374 0.1244 0.0738 0.0222 4.162 29.145 30.464 3103.419 3.293 135.503 4.452 0.71 331827. 0.7210
|
|
9.56 0.0561 0.1817 0.0721 0.0223 4.178 29.261 29.772 3115.697 3.306 132.427 4.334 0.71 332013. 0.6938
|
|
12.75 0.0748 0.2357 0.0703 0.0223 4.188 29.329 29.042 3122.946 3.314 129.179 4.218 0.71 332211. 0.6669
|
|
15.93 0.0935 0.2867 0.0685 0.0223 4.190 29.344 28.272 3124.599 3.315 125.755 4.104 0.71 332420. 0.6402
|
|
19.12 0.1122 0.3347 0.0665 0.0223 4.184 29.302 27.462 3120.085 3.311 122.152 3.992 0.71 332641. 0.6138
|
|
22.31 0.1309 0.3797 0.0644 0.0222 4.169 29.196 26.611 3108.820 3.299 118.366 3.882 0.71 332874. 0.5876
|
|
25.50 0.1496 0.4219 0.0623 0.0221 4.144 29.021 25.718 3090.194 3.279 114.392 3.775 0.71 333120. 0.5616
|
|
28.68 0.1683 0.4614 0.0600 0.0219 4.108 28.771 24.781 3063.544 3.251 110.226 3.669 0.72 333379. 0.5358
|
|
31.87 0.1870 0.4981 0.0576 0.0216 4.061 28.439 23.801 3028.225 3.213 105.866 3.565 0.72 333652. 0.5102
|
|
35.06 0.2057 0.5321 0.0552 0.0213 4.001 28.022 22.778 2983.803 3.166 101.317 3.463 0.72 333938. 0.4848
|
|
38.24 0.2244 0.5636 0.0526 0.0209 3.929 27.517 21.715 2930.011 3.109 96.587 3.361 0.72 334237. 0.4596
|
|
41.43 0.2431 0.5924 0.0499 0.0205 3.844 26.922 20.613 2866.635 3.042 91.688 3.262 0.72 334551. 0.4344
|
|
44.62 0.2618 0.6185 0.0472 0.0200 3.746 26.235 19.476 2793.478 2.964 86.627 3.162 0.72 334879. 0.4094
|
|
47.80 0.2805 0.6419 0.0443 0.0194 3.635 25.454 18.304 2710.357 2.876 81.416 3.063 0.72 335221. 0.3845
|
|
50.99 0.2992 0.6625 0.0414 0.0187 3.510 24.578 17.101 2617.112 2.777 76.063 2.964 0.72 335578. 0.3596
|
|
54.18 0.3178 0.6801 0.0384 0.0180 3.371 23.606 15.868 2513.604 2.667 70.580 2.863 0.72 335949. 0.3346
|
|
57.37 0.3365 0.6944 0.0354 0.0171 3.218 22.537 14.608 2399.735 2.546 64.976 2.761 0.72 336336. 0.3096
|
|
60.55 0.3552 0.7050 0.0323 0.0163 3.051 21.370 13.324 2275.458 2.414 59.264 2.656 0.72 336737. 0.2844
|
|
63.74 0.3739 0.7115 0.0291 0.0153 2.871 20.105 12.018 2140.786 2.271 53.456 2.546 0.72 337154. 0.2590
|
|
66.93 0.3926 0.7131 0.0259 0.0143 2.676 18.743 10.694 1995.806 2.118 47.566 2.430 0.72 337587. 0.2332
|
|
70.11 0.4113 0.7085 0.0227 0.0131 2.468 17.287 9.355 1840.691 1.953 41.610 2.305 0.72 338035. 0.2068
|
|
73.30 0.4300 0.6962 0.0194 0.0120 2.247 15.737 8.005 1675.727 1.778 35.605 2.167 0.72 338499. 0.1798
|
|
76.49 0.4487 0.6735 0.0161 0.0107 2.013 14.100 6.648 1501.326 1.593 29.570 2.008 0.72 338979. 0.1519
|
|
79.67 0.4674 0.6358 0.0128 0.0094 1.768 12.378 5.290 1318.057 1.399 23.528 1.820 0.72 339475. 0.1228
|
|
82.86 0.4861 0.5754 0.0095 0.0080 1.511 10.581 3.935 1126.661 1.195 17.503 1.584 0.72 339987. 0.0922
|
|
86.05 0.5048 0.4775 0.0063 0.0066 1.245 8.716 2.590 928.068 0.985 11.521 1.266 0.72 340515. 0.0598
|
|
89.24 0.5235 0.3094 0.0031 0.0052 0.970 6.793 1.261 723.297 0.767 5.610 0.791 0.72 341058. 0.0261
|
|
92.42 0.5422 -0.0294 -0.0002 0.0036 0.680 4.764 -0.081 507.263 0.538 -0.360 -0.072 0.72 341541. 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 0.0787 0.0228 5.875 37.026 40.122 4380.631 4.183 178.464 4.154 0.79 368267. 0.7720
|
|
3.53 0.0186 0.0628 0.0772 0.0229 5.901 37.191 39.352 4400.117 4.202 175.038 4.056 0.79 368452. 0.7466
|
|
7.06 0.0373 0.1226 0.0756 0.0230 5.920 37.315 38.534 4414.825 4.216 171.401 3.959 0.79 368648. 0.7210
|
|
10.60 0.0559 0.1794 0.0739 0.0230 5.933 37.393 37.669 4423.985 4.225 167.550 3.862 0.79 368857. 0.6954
|
|
14.13 0.0746 0.2333 0.0721 0.0231 5.936 37.417 36.754 4426.827 4.227 163.481 3.766 0.79 369078. 0.6698
|
|
17.66 0.0932 0.2842 0.0702 0.0230 5.931 37.380 35.788 4422.547 4.223 159.187 3.670 0.79 369313. 0.6442
|
|
21.19 0.1119 0.3322 0.0682 0.0230 5.914 37.277 34.771 4410.312 4.212 154.664 3.576 0.79 369560. 0.6186
|
|
24.73 0.1305 0.3775 0.0661 0.0229 5.886 37.099 33.702 4389.263 4.191 149.906 3.483 0.79 369821. 0.5932
|
|
28.26 0.1492 0.4200 0.0639 0.0227 5.845 36.839 32.579 4358.486 4.162 144.910 3.390 0.79 370096. 0.5677
|
|
31.79 0.1678 0.4598 0.0616 0.0225 5.789 36.488 31.401 4316.997 4.122 139.670 3.299 0.79 370386. 0.5424
|
|
35.32 0.1865 0.4969 0.0592 0.0222 5.718 36.039 30.166 4263.835 4.072 134.181 3.209 0.79 370690. 0.5171
|
|
38.85 0.2051 0.5314 0.0566 0.0219 5.630 35.486 28.878 4198.401 4.009 128.448 3.120 0.80 371009. 0.4919
|
|
42.39 0.2238 0.5633 0.0540 0.0215 5.525 34.825 27.537 4120.212 3.935 122.485 3.031 0.80 371343. 0.4667
|
|
45.92 0.2424 0.5926 0.0513 0.0210 5.403 34.053 26.147 4028.872 3.847 116.302 2.944 0.80 371692. 0.4416
|
|
49.45 0.2611 0.6192 0.0485 0.0204 5.262 33.167 24.711 3924.060 3.747 109.913 2.856 0.80 372058. 0.4166
|
|
52.98 0.2797 0.6431 0.0456 0.0198 5.103 32.166 23.231 3805.611 3.634 103.331 2.769 0.80 372438. 0.3915
|
|
56.52 0.2984 0.6642 0.0426 0.0191 4.926 31.048 21.710 3673.352 3.508 96.566 2.681 0.80 372835. 0.3664
|
|
60.05 0.3170 0.6821 0.0395 0.0184 4.730 29.813 20.151 3527.223 3.368 89.632 2.591 0.80 373248. 0.3413
|
|
63.58 0.3357 0.6967 0.0364 0.0175 4.516 28.461 18.557 3367.260 3.215 82.544 2.500 0.80 373677. 0.3159
|
|
67.11 0.3543 0.7075 0.0332 0.0166 4.283 26.993 16.932 3193.611 3.050 75.314 2.405 0.80 374123. 0.2903
|
|
70.64 0.3730 0.7138 0.0300 0.0157 4.032 25.412 15.278 3006.557 2.871 67.959 2.305 0.80 374586. 0.2643
|
|
74.18 0.3916 0.7148 0.0267 0.0146 3.764 23.721 13.601 2806.477 2.680 60.496 2.198 0.80 375066. 0.2378
|
|
77.71 0.4103 0.7090 0.0233 0.0135 3.479 21.925 11.903 2593.940 2.477 52.944 2.081 0.80 375562. 0.2107
|
|
81.24 0.4289 0.6947 0.0200 0.0123 3.178 20.029 10.190 2369.713 2.263 45.326 1.950 0.80 376077. 0.1827
|
|
84.77 0.4476 0.6686 0.0166 0.0111 2.863 18.044 8.468 2134.784 2.039 37.664 1.799 0.80 376608. 0.1536
|
|
88.30 0.4662 0.6262 0.0132 0.0098 2.535 15.978 6.742 1890.350 1.805 29.987 1.618 0.80 377158. 0.1232
|
|
91.84 0.4849 0.5596 0.0098 0.0085 2.196 13.844 5.019 1637.879 1.564 22.325 1.390 0.80 377725. 0.0914
|
|
95.37 0.5035 0.4548 0.0065 0.0072 1.849 11.656 3.307 1379.072 1.317 14.711 1.088 0.80 378309. 0.0580
|
|
98.90 0.5222 0.2846 0.0032 0.0058 1.496 9.430 1.615 1115.722 1.065 7.182 0.656 0.80 378910. 0.0245
|
|
102.43 0.5408 -0.0213 -0.0002 0.0044 1.128 7.108 -0.088 840.914 0.803 -0.391 -0.047 0.81 379461. 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 0.0809 0.0259 8.861 50.773 49.928 6607.695 5.736 222.081 3.427 0.87 405020. 0.7105
|
|
3.89 0.0187 0.0575 0.0794 0.0258 8.835 50.624 48.990 6588.394 5.720 217.907 3.373 0.87 405226. 0.6926
|
|
7.77 0.0373 0.1130 0.0778 0.0257 8.801 50.426 47.991 6562.623 5.697 213.463 3.317 0.87 405446. 0.6741
|
|
11.66 0.0560 0.1667 0.0761 0.0255 8.757 50.174 46.931 6529.739 5.669 208.748 3.260 0.87 405679. 0.6552
|
|
15.55 0.0746 0.2183 0.0742 0.0254 8.702 49.861 45.808 6489.029 5.633 203.753 3.202 0.87 405925. 0.6358
|
|
19.44 0.0933 0.2678 0.0723 0.0252 8.636 49.482 44.621 6439.739 5.590 198.473 3.143 0.87 406187. 0.6159
|
|
23.32 0.1119 0.3152 0.0703 0.0250 8.557 49.031 43.368 6381.068 5.540 192.901 3.083 0.87 406462. 0.5956
|
|
27.21 0.1306 0.3604 0.0682 0.0247 8.465 48.502 42.049 6312.174 5.480 187.032 3.021 0.87 406753. 0.5748
|
|
31.10 0.1493 0.4034 0.0659 0.0244 8.357 47.886 40.661 6232.083 5.410 180.860 2.959 0.87 407060. 0.5536
|
|
34.98 0.1679 0.4442 0.0635 0.0240 8.233 47.177 39.204 6139.719 5.330 174.380 2.896 0.87 407382. 0.5320
|
|
38.87 0.1866 0.4826 0.0611 0.0236 8.092 46.364 37.676 6033.886 5.238 167.584 2.832 0.87 407720. 0.5100
|
|
42.76 0.2052 0.5187 0.0585 0.0231 7.930 45.440 36.079 5913.639 5.134 160.478 2.767 0.87 408074. 0.4876
|
|
46.64 0.2239 0.5522 0.0558 0.0226 7.752 44.417 34.414 5780.565 5.018 153.075 2.700 0.87 408446. 0.4647
|
|
50.53 0.2426 0.5827 0.0530 0.0221 7.559 43.309 32.687 5636.397 4.893 145.391 2.630 0.88 408834. 0.4412
|
|
54.42 0.2612 0.6103 0.0501 0.0214 7.347 42.097 30.900 5478.637 4.756 137.443 2.558 0.88 409238. 0.4172
|
|
58.31 0.2799 0.6347 0.0471 0.0208 7.118 40.784 29.057 5307.779 4.608 129.246 2.483 0.88 409661. 0.3927
|
|
62.19 0.2985 0.6553 0.0440 0.0201 6.874 39.387 27.162 5125.950 4.450 120.815 2.403 0.88 410100. 0.3675
|
|
66.08 0.3172 0.6712 0.0409 0.0193 6.620 37.932 25.217 4936.521 4.285 112.164 2.317 0.88 410557. 0.3413
|
|
69.97 0.3358 0.6827 0.0376 0.0185 6.348 36.373 23.227 4733.633 4.109 103.316 2.226 0.88 411032. 0.3147
|
|
73.85 0.3545 0.6893 0.0344 0.0177 6.056 34.702 21.198 4516.255 3.921 94.288 2.129 0.88 411526. 0.2876
|
|
77.74 0.3732 0.6902 0.0310 0.0168 5.747 32.928 19.133 4285.413 3.720 85.102 2.025 0.88 412037. 0.2599
|
|
81.63 0.3918 0.6840 0.0276 0.0158 5.421 31.063 17.037 4042.656 3.510 75.779 1.911 0.88 412567. 0.2315
|
|
85.52 0.4105 0.6693 0.0242 0.0148 5.081 29.116 14.915 3789.268 3.290 66.344 1.785 0.88 413115. 0.2023
|
|
89.40 0.4291 0.6439 0.0207 0.0138 4.730 27.100 12.775 3526.866 3.062 56.824 1.643 0.88 413683. 0.1723
|
|
93.29 0.4478 0.6050 0.0172 0.0127 4.368 25.029 10.623 3257.369 2.828 47.251 1.479 0.88 414269. 0.1414
|
|
97.18 0.4664 0.5485 0.0137 0.0117 4.000 22.921 8.467 2983.004 2.590 37.660 1.287 0.88 414875. 0.1099
|
|
101.06 0.4851 0.4690 0.0102 0.0106 3.629 20.794 6.315 2706.164 2.349 28.091 1.059 0.88 415500. 0.0780
|
|
104.95 0.5038 0.3590 0.0068 0.0095 3.258 18.667 4.179 2429.322 2.109 18.588 0.780 0.88 416144. 0.0468
|
|
108.84 0.5224 0.2077 0.0034 0.0084 2.889 16.556 2.068 2154.639 1.870 9.197 0.435 0.88 416806. 0.0184
|
|
112.73 0.5411 -0.0052 -0.0001 0.0073 2.509 14.374 -0.043 1870.694 1.624 -0.192 -0.010 0.89 417449. 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 0.0824 0.0323 14.360 75.424 60.525 10708.284 8.521 269.214 2.564 0.95 441782. 0.5851
|
|
4.34 0.0191 0.0483 0.0810 0.0320 14.247 74.828 59.454 10623.678 8.454 264.451 2.538 0.95 442010. 0.5742
|
|
8.67 0.0382 0.0956 0.0794 0.0317 14.111 74.119 58.301 10522.933 8.374 259.322 2.513 0.95 442255. 0.5629
|
|
13.01 0.0573 0.1419 0.0777 0.0314 13.954 73.293 57.064 10405.718 8.281 253.822 2.487 0.95 442515. 0.5513
|
|
17.35 0.0763 0.1872 0.0759 0.0310 13.775 72.349 55.742 10271.701 8.174 247.939 2.461 0.95 442792. 0.5391
|
|
21.69 0.0954 0.2315 0.0740 0.0305 13.572 71.285 54.331 10120.642 8.054 241.664 2.435 0.95 443086. 0.5266
|
|
26.02 0.1145 0.2747 0.0720 0.0300 13.346 70.100 52.830 9952.316 7.920 234.988 2.408 0.95 443397. 0.5134
|
|
30.36 0.1336 0.3167 0.0698 0.0294 13.097 68.791 51.238 9766.547 7.772 227.906 2.380 0.95 443726. 0.4997
|
|
34.70 0.1527 0.3575 0.0675 0.0288 12.824 67.358 49.553 9563.069 7.610 220.411 2.350 0.95 444073. 0.4854
|
|
39.03 0.1718 0.3969 0.0651 0.0282 12.527 65.797 47.773 9341.455 7.434 212.496 2.320 0.95 444438. 0.4704
|
|
43.37 0.1908 0.4349 0.0625 0.0274 12.205 64.104 45.898 9101.046 7.242 204.154 2.287 0.95 444822. 0.4547
|
|
47.71 0.2099 0.4713 0.0598 0.0266 11.857 62.275 43.929 8841.495 7.036 195.394 2.254 0.95 445225. 0.4382
|
|
52.05 0.2290 0.5060 0.0570 0.0258 11.483 60.313 41.870 8562.943 6.814 186.238 2.218 0.95 445647. 0.4210
|
|
56.38 0.2481 0.5385 0.0541 0.0249 11.091 58.252 39.727 8270.346 6.581 176.707 2.179 0.95 446088. 0.4029
|
|
60.72 0.2672 0.5678 0.0511 0.0240 10.695 56.176 37.504 7975.524 6.347 166.820 2.133 0.96 446549. 0.3832
|
|
65.06 0.2863 0.5937 0.0480 0.0231 10.288 54.038 35.208 7672.019 6.105 156.605 2.081 0.96 447030. 0.3624
|
|
69.39 0.3053 0.6154 0.0447 0.0222 9.876 51.873 32.843 7364.650 5.861 146.087 2.023 0.96 447530. 0.3401
|
|
73.73 0.3244 0.6309 0.0414 0.0213 9.478 49.782 30.414 7067.797 5.624 135.283 1.952 0.96 448050. 0.3158
|
|
78.07 0.3435 0.6338 0.0380 0.0206 9.170 48.164 27.921 6838.112 5.442 124.191 1.852 0.96 448591. 0.2871
|
|
82.41 0.3626 0.6287 0.0346 0.0199 8.869 46.582 25.376 6613.472 5.263 112.874 1.740 0.96 449152. 0.2572
|
|
86.74 0.3817 0.6160 0.0310 0.0192 8.558 44.947 22.790 6381.355 5.078 101.372 1.620 0.96 449734. 0.2269
|
|
91.08 0.4008 0.5946 0.0275 0.0185 8.239 43.276 20.171 6144.126 4.889 89.721 1.489 0.96 450337. 0.1962
|
|
95.42 0.4198 0.5633 0.0239 0.0178 7.918 41.587 17.528 5904.291 4.698 77.965 1.347 0.96 450961. 0.1654
|
|
99.75 0.4389 0.5207 0.0203 0.0171 7.597 39.905 14.872 5665.420 4.508 66.150 1.191 0.96 451606. 0.1347
|
|
104.09 0.4580 0.4657 0.0166 0.0164 7.280 38.237 12.216 5428.684 4.320 54.335 1.021 0.96 452273. 0.1047
|
|
108.43 0.4771 0.3972 0.0130 0.0157 6.968 36.598 9.573 5196.039 4.135 42.580 0.836 0.96 452962. 0.0759
|
|
112.77 0.4962 0.3140 0.0095 0.0150 6.664 35.000 6.959 4969.083 3.954 30.952 0.635 0.96 453673. 0.0492
|
|
117.10 0.5153 0.2151 0.0060 0.0143 6.368 33.447 4.387 4748.594 3.779 19.515 0.419 0.96 454408. 0.0258
|
|
121.44 0.5343 0.0993 0.0025 0.0137 6.076 31.915 1.864 4531.058 3.606 8.291 0.187 0.97 455170. 0.0075
|
|
125.78 0.5534
|
|
|
|
|
|
|