575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
15x11 (15x11.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 0.1136 0.0557 0.003 0.214 0.183 2.538 0.024 0.815 32.758 0.06 26753. 0.5486
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0.44 0.0306 0.0608 0.1125 0.0566 0.003 0.218 0.181 2.581 0.025 0.807 31.889 0.06 26776. 0.5314
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0.87 0.0613 0.1183 0.1112 0.0576 0.004 0.222 0.179 2.624 0.025 0.798 31.013 0.06 26801. 0.5139
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1.31 0.0919 0.1725 0.1098 0.0585 0.004 0.225 0.177 2.667 0.025 0.788 30.135 0.06 26830. 0.4962
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1.74 0.1226 0.2233 0.1082 0.0594 0.004 0.229 0.175 2.707 0.026 0.777 29.260 0.06 26861. 0.4783
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2.18 0.1532 0.2708 0.1065 0.0602 0.004 0.232 0.172 2.744 0.026 0.764 28.392 0.06 26896. 0.4603
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2.61 0.1838 0.3152 0.1045 0.0609 0.004 0.235 0.169 2.777 0.027 0.750 27.532 0.06 26934. 0.4422
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3.05 0.2145 0.3564 0.1023 0.0616 0.004 0.237 0.165 2.806 0.027 0.734 26.684 0.06 26975. 0.4241
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3.48 0.2451 0.3945 0.0999 0.0621 0.004 0.239 0.161 2.828 0.027 0.717 25.849 0.06 27019. 0.4059
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3.92 0.2757 0.4297 0.0972 0.0624 0.004 0.240 0.157 2.843 0.027 0.698 25.027 0.06 27067. 0.3877
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4.35 0.3064 0.4621 0.0943 0.0625 0.004 0.241 0.152 2.849 0.027 0.677 24.218 0.06 27118. 0.3695
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4.79 0.3370 0.4916 0.0911 0.0625 0.004 0.241 0.147 2.846 0.027 0.654 23.423 0.06 27173. 0.3513
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5.22 0.3677 0.5183 0.0876 0.0622 0.004 0.239 0.141 2.832 0.027 0.629 22.638 0.06 27231. 0.3329
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5.66 0.3983 0.5422 0.0839 0.0616 0.004 0.237 0.135 2.807 0.027 0.602 21.863 0.06 27294. 0.3146
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6.09 0.4289 0.5634 0.0798 0.0608 0.004 0.234 0.129 2.768 0.026 0.573 21.093 0.06 27359. 0.2960
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6.53 0.4596 0.5817 0.0755 0.0596 0.004 0.230 0.122 2.717 0.026 0.542 20.325 0.06 27428. 0.2774
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6.96 0.4902 0.5969 0.0709 0.0582 0.004 0.224 0.114 2.653 0.025 0.509 19.555 0.06 27501. 0.2587
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7.40 0.5208 0.6090 0.0661 0.0565 0.003 0.218 0.107 2.577 0.025 0.474 18.777 0.06 27577. 0.2399
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7.83 0.5515 0.6176 0.0611 0.0546 0.003 0.210 0.099 2.488 0.024 0.439 17.983 0.06 27657. 0.2209
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8.27 0.5821 0.6222 0.0560 0.0524 0.003 0.202 0.090 2.388 0.023 0.402 17.165 0.06 27741. 0.2019
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8.70 0.6128 0.6224 0.0508 0.0500 0.003 0.192 0.082 2.277 0.022 0.364 16.312 0.06 27828. 0.1826
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9.14 0.6434 0.6173 0.0454 0.0473 0.003 0.182 0.073 2.155 0.021 0.326 15.408 0.06 27918. 0.1631
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9.57 0.6740 0.6059 0.0399 0.0444 0.003 0.171 0.064 2.023 0.019 0.286 14.435 0.06 28012. 0.1433
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10.01 0.7047 0.5865 0.0343 0.0413 0.003 0.159 0.055 1.880 0.018 0.246 13.366 0.06 28109. 0.1231
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10.44 0.7353 0.5569 0.0287 0.0379 0.002 0.146 0.046 1.727 0.016 0.206 12.162 0.06 28210. 0.1024
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10.88 0.7659 0.5134 0.0230 0.0343 0.002 0.132 0.037 1.564 0.015 0.165 10.765 0.06 28314. 0.0811
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11.32 0.7966 0.4506 0.0173 0.0305 0.002 0.118 0.028 1.391 0.013 0.124 9.084 0.06 28422. 0.0593
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11.75 0.8272 0.3589 0.0115 0.0265 0.002 0.102 0.019 1.209 0.012 0.083 6.967 0.06 28533. 0.0371
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12.19 0.8579 0.2210 0.0058 0.0224 0.001 0.086 0.009 1.019 0.010 0.041 4.138 0.06 28647. 0.0156
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12.62 0.8885 0.0021 0.0000 0.0180 0.001 0.069 0.000 0.822 0.008 0.000 0.038 0.06 28765. 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 0.1141 0.0500 0.024 0.771 0.736 18.240 0.087 3.275 18.310 0.12 53505. 0.6146
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0.88 0.0308 0.0683 0.1130 0.0511 0.025 0.786 0.729 18.610 0.089 3.244 17.772 0.12 53551. 0.5937
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1.75 0.0617 0.1324 0.1118 0.0521 0.025 0.802 0.721 18.981 0.091 3.208 17.234 0.12 53603. 0.5725
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2.63 0.0925 0.1925 0.1104 0.0531 0.026 0.818 0.712 19.344 0.092 3.168 16.699 0.12 53661. 0.5513
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3.51 0.1234 0.2485 0.1088 0.0540 0.026 0.832 0.702 19.693 0.094 3.123 16.169 0.12 53724. 0.5300
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4.38 0.1542 0.3006 0.1070 0.0549 0.027 0.846 0.691 20.020 0.096 3.072 15.648 0.12 53794. 0.5087
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5.26 0.1851 0.3489 0.1051 0.0557 0.027 0.859 0.678 20.316 0.097 3.016 15.136 0.12 53870. 0.4875
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6.13 0.2159 0.3936 0.1029 0.0564 0.028 0.869 0.664 20.572 0.098 2.953 14.636 0.12 53953. 0.4665
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7.01 0.2468 0.4348 0.1004 0.0570 0.028 0.878 0.648 20.779 0.099 2.883 14.149 0.12 54043. 0.4456
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7.89 0.2776 0.4728 0.0978 0.0574 0.028 0.884 0.631 20.927 0.100 2.806 13.674 0.12 54139. 0.4248
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8.76 0.3085 0.5075 0.0948 0.0576 0.028 0.888 0.612 21.007 0.100 2.722 13.211 0.12 54243. 0.4042
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9.64 0.3393 0.5393 0.0916 0.0576 0.028 0.888 0.591 21.008 0.100 2.629 12.761 0.12 54354. 0.3838
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10.52 0.3701 0.5681 0.0881 0.0574 0.028 0.884 0.568 20.920 0.100 2.528 12.323 0.12 54472. 0.3634
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11.39 0.4010 0.5941 0.0843 0.0569 0.028 0.876 0.544 20.736 0.099 2.419 11.895 0.12 54598. 0.3432
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12.27 0.4318 0.6173 0.0802 0.0561 0.027 0.864 0.517 20.447 0.098 2.301 11.477 0.12 54731. 0.3229
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13.14 0.4627 0.6377 0.0758 0.0550 0.027 0.847 0.489 20.049 0.096 2.176 11.066 0.12 54871. 0.3027
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14.02 0.4935 0.6552 0.0712 0.0536 0.026 0.826 0.459 19.544 0.093 2.043 10.660 0.12 55018. 0.2826
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14.90 0.5244 0.6698 0.0663 0.0519 0.025 0.800 0.428 18.933 0.090 1.904 10.256 0.12 55173. 0.2625
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15.77 0.5552 0.6812 0.0613 0.0500 0.024 0.770 0.396 18.222 0.087 1.760 9.851 0.12 55334. 0.2424
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16.65 0.5861 0.6891 0.0562 0.0478 0.023 0.736 0.362 17.412 0.083 1.612 9.440 0.12 55503. 0.2223
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17.53 0.6169 0.6929 0.0509 0.0453 0.022 0.698 0.328 16.506 0.079 1.460 9.018 0.12 55679. 0.2021
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18.40 0.6478 0.6920 0.0454 0.0425 0.021 0.655 0.293 15.505 0.074 1.304 8.578 0.12 55862. 0.1817
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19.28 0.6786 0.6853 0.0399 0.0395 0.019 0.609 0.258 14.412 0.069 1.146 8.109 0.12 56052. 0.1610
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20.15 0.7095 0.6712 0.0343 0.0363 0.018 0.559 0.222 13.228 0.063 0.985 7.596 0.12 56249. 0.1399
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21.03 0.7403 0.6472 0.0287 0.0328 0.016 0.505 0.185 11.955 0.057 0.823 7.019 0.12 56453. 0.1181
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21.91 0.7711 0.6091 0.0230 0.0291 0.014 0.448 0.148 10.596 0.051 0.659 6.342 0.12 56665. 0.0955
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22.78 0.8020 0.5499 0.0172 0.0251 0.012 0.387 0.111 9.154 0.044 0.494 5.506 0.12 56883. 0.0718
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23.66 0.8328 0.4561 0.0115 0.0209 0.010 0.323 0.074 7.633 0.036 0.329 4.397 0.12 57108. 0.0468
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24.54 0.8637 0.2986 0.0057 0.0166 0.008 0.255 0.037 6.040 0.029 0.164 2.776 0.12 57339. 0.0209
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25.41 0.8945 0.0021 0.0000 0.0120 0.006 0.185 0.000 4.381 0.021 0.001 0.019 0.12 57575. 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 0.1144 0.0478 0.079 1.655 1.662 58.758 0.187 7.391 12.827 0.18 80256. 0.6468
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1.32 0.0309 0.0719 0.1134 0.0488 0.081 1.692 1.646 60.046 0.191 7.321 12.433 0.18 80326. 0.6239
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2.64 0.0619 0.1392 0.1121 0.0499 0.082 1.728 1.628 61.337 0.195 7.242 12.039 0.18 80404. 0.6009
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3.96 0.0928 0.2020 0.1107 0.0509 0.084 1.764 1.608 62.606 0.199 7.152 11.649 0.18 80490. 0.5778
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5.27 0.1238 0.2604 0.1092 0.0519 0.086 1.798 1.585 63.829 0.203 7.051 11.265 0.18 80586. 0.5548
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6.59 0.1547 0.3147 0.1074 0.0528 0.087 1.831 1.560 64.978 0.207 6.938 10.888 0.18 80691. 0.5319
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7.91 0.1856 0.3648 0.1055 0.0537 0.089 1.860 1.531 66.024 0.210 6.811 10.520 0.18 80806. 0.5092
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9.23 0.2166 0.4111 0.1033 0.0544 0.090 1.886 1.500 66.936 0.213 6.670 10.161 0.18 80931. 0.4867
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10.55 0.2475 0.4538 0.1008 0.0550 0.091 1.907 1.464 67.680 0.215 6.513 9.813 0.18 81066. 0.4645
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11.87 0.2785 0.4929 0.0982 0.0555 0.091 1.922 1.425 68.224 0.217 6.340 9.476 0.18 81212. 0.4425
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13.18 0.3094 0.5288 0.0952 0.0557 0.092 1.931 1.382 68.534 0.218 6.149 9.149 0.18 81369. 0.4208
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14.50 0.3403 0.5616 0.0920 0.0557 0.092 1.932 1.335 68.575 0.218 5.940 8.832 0.18 81536. 0.3993
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15.82 0.3713 0.5914 0.0884 0.0555 0.092 1.925 1.284 68.314 0.217 5.712 8.526 0.18 81715. 0.3779
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17.14 0.4022 0.6183 0.0846 0.0550 0.091 1.908 1.229 67.718 0.216 5.465 8.229 0.18 81904. 0.3568
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18.46 0.4332 0.6425 0.0805 0.0543 0.090 1.881 1.169 66.762 0.213 5.198 7.940 0.18 82104. 0.3358
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19.78 0.4641 0.6639 0.0761 0.0532 0.088 1.843 1.105 65.431 0.208 4.914 7.658 0.18 82316. 0.3148
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21.10 0.4950 0.6827 0.0714 0.0518 0.085 1.795 1.037 63.728 0.203 4.613 7.382 0.18 82538. 0.2941
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22.41 0.5260 0.6986 0.0666 0.0501 0.083 1.737 0.967 61.662 0.196 4.299 7.110 0.18 82771. 0.2734
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23.73 0.5569 0.7115 0.0615 0.0482 0.079 1.669 0.893 59.244 0.189 3.973 6.839 0.18 83015. 0.2528
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25.05 0.5879 0.7212 0.0563 0.0459 0.076 1.591 0.818 56.483 0.180 3.638 6.567 0.18 83269. 0.2323
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26.37 0.6188 0.7271 0.0510 0.0434 0.072 1.504 0.740 53.387 0.170 3.293 6.290 0.18 83535. 0.2117
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27.69 0.6497 0.7288 0.0455 0.0406 0.067 1.408 0.661 49.961 0.159 2.942 6.004 0.18 83811. 0.1910
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29.01 0.6807 0.7250 0.0400 0.0376 0.062 1.302 0.581 46.210 0.147 2.584 5.702 0.18 84098. 0.1700
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30.32 0.7116 0.7144 0.0344 0.0343 0.057 1.187 0.499 42.142 0.134 2.221 5.374 0.18 84395. 0.1485
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31.64 0.7426 0.6944 0.0287 0.0307 0.051 1.064 0.417 37.761 0.120 1.854 5.006 0.18 84703. 0.1264
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32.96 0.7735 0.6609 0.0230 0.0269 0.044 0.932 0.334 33.079 0.105 1.484 4.574 0.18 85021. 0.1033
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34.28 0.8044 0.6062 0.0172 0.0228 0.038 0.792 0.250 28.105 0.089 1.112 4.033 0.18 85350. 0.0789
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35.60 0.8354 0.5147 0.0114 0.0186 0.031 0.644 0.166 22.858 0.073 0.739 3.298 0.18 85690. 0.0526
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36.92 0.8663 0.3500 0.0057 0.0141 0.023 0.489 0.083 17.358 0.055 0.368 2.163 0.19 86039. 0.0243
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38.24 0.8972 -0.0007 0.0000 0.0094 0.016 0.328 0.000 11.626 0.037 0.000 -0.004 0.19 86394. 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 0.1148 0.0465 0.182 2.869 2.963 135.753 0.324 13.180 9.900 0.24 107005. 0.6666
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1.76 0.0310 0.0740 0.1137 0.0476 0.186 2.934 2.935 138.870 0.332 13.057 9.587 0.24 107099. 0.6425
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3.52 0.0620 0.1432 0.1125 0.0487 0.190 3.000 2.904 141.997 0.339 12.917 9.276 0.24 107203. 0.6184
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5.28 0.0930 0.2077 0.1111 0.0497 0.195 3.066 2.869 145.078 0.346 12.760 8.968 0.24 107319. 0.5942
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7.04 0.1240 0.2676 0.1096 0.0508 0.199 3.128 2.829 148.052 0.353 12.582 8.666 0.24 107446. 0.5701
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8.81 0.1550 0.3231 0.1078 0.0517 0.202 3.188 2.784 150.854 0.360 12.382 8.370 0.24 107587. 0.5463
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10.57 0.1860 0.3743 0.1059 0.0526 0.206 3.242 2.733 153.412 0.366 12.158 8.081 0.24 107740. 0.5226
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12.33 0.2170 0.4216 0.1037 0.0534 0.209 3.289 2.677 155.649 0.372 11.907 7.801 0.24 107908. 0.4993
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14.09 0.2479 0.4650 0.1013 0.0540 0.211 3.328 2.614 157.487 0.376 11.628 7.529 0.24 108089. 0.4762
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15.85 0.2789 0.5049 0.0986 0.0545 0.213 3.357 2.545 158.846 0.379 11.320 7.267 0.24 108284. 0.4535
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17.61 0.3099 0.5415 0.0956 0.0547 0.214 3.373 2.469 159.644 0.381 10.980 7.014 0.24 108493. 0.4311
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19.37 0.3409 0.5748 0.0924 0.0548 0.214 3.377 2.385 159.796 0.381 10.608 6.769 0.24 108718. 0.4089
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21.13 0.3719 0.6052 0.0888 0.0546 0.214 3.364 2.293 159.223 0.380 10.201 6.533 0.24 108956. 0.3870
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22.89 0.4029 0.6328 0.0850 0.0541 0.212 3.335 2.194 157.846 0.377 9.760 6.305 0.24 109210. 0.3653
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24.65 0.4339 0.6576 0.0809 0.0534 0.209 3.288 2.087 155.601 0.371 9.284 6.084 0.24 109478. 0.3438
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26.42 0.4649 0.6797 0.0764 0.0523 0.204 3.221 1.973 152.454 0.364 8.776 5.870 0.24 109760. 0.3225
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28.18 0.4959 0.6993 0.0718 0.0509 0.199 3.136 1.852 148.409 0.354 8.239 5.661 0.24 110058. 0.3014
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29.94 0.5269 0.7161 0.0669 0.0492 0.192 3.032 1.726 143.488 0.343 7.677 5.456 0.24 110370. 0.2804
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31.70 0.5579 0.7300 0.0618 0.0472 0.185 2.910 1.595 137.714 0.329 7.095 5.253 0.24 110696. 0.2595
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33.46 0.5889 0.7409 0.0566 0.0450 0.176 2.770 1.460 131.111 0.313 6.495 5.051 0.24 111037. 0.2388
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35.22 0.6199 0.7483 0.0512 0.0424 0.166 2.614 1.322 123.693 0.295 5.879 4.847 0.24 111392. 0.2180
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36.98 0.6509 0.7517 0.0457 0.0396 0.155 2.440 1.180 115.477 0.276 5.251 4.637 0.24 111761. 0.1971
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38.74 0.6819 0.7501 0.0402 0.0365 0.143 2.250 1.037 106.474 0.254 4.611 4.416 0.24 112145. 0.1759
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40.50 0.7129 0.7420 0.0345 0.0332 0.130 2.043 0.891 96.697 0.231 3.963 4.179 0.24 112543. 0.1543
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42.26 0.7438 0.7251 0.0288 0.0295 0.116 1.821 0.743 86.164 0.206 3.307 3.914 0.24 112955. 0.1320
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44.03 0.7748 0.6953 0.0230 0.0257 0.100 1.583 0.595 74.897 0.179 2.646 3.602 0.25 113381. 0.1087
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45.79 0.8058 0.6446 0.0173 0.0216 0.084 1.330 0.446 62.925 0.150 1.982 3.212 0.25 113821. 0.0839
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47.55 0.8368 0.5567 0.0115 0.0172 0.067 1.063 0.296 50.288 0.120 1.317 2.671 0.25 114274. 0.0568
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49.31 0.8678 0.3896 0.0057 0.0127 0.050 0.783 0.147 37.041 0.088 0.655 1.802 0.25 114741. 0.0270
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51.07 0.8988 -0.0031 0.0000 0.0080 0.031 0.491 -0.001 23.224 0.055 -0.003 -0.014 0.25 115214. 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 0.1152 0.0459 0.350 4.415 4.645 261.175 0.499 20.663 8.068 0.30 133753. 0.6802
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2.20 0.0310 0.0754 0.1141 0.0469 0.359 4.520 4.603 267.373 0.511 20.474 7.809 0.30 133870. 0.6553
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4.41 0.0621 0.1459 0.1129 0.0480 0.367 4.625 4.555 273.598 0.523 20.260 7.551 0.30 134000. 0.6304
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6.61 0.0931 0.2115 0.1116 0.0491 0.375 4.729 4.500 279.739 0.534 20.017 7.297 0.30 134145. 0.6055
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8.81 0.1241 0.2723 0.1100 0.0502 0.383 4.829 4.438 285.678 0.546 19.742 7.047 0.30 134305. 0.5807
|
|
11.02 0.1551 0.3286 0.1083 0.0511 0.391 4.924 4.369 291.281 0.556 19.432 6.803 0.30 134481. 0.5562
|
|
13.22 0.1862 0.3805 0.1064 0.0520 0.397 5.011 4.290 296.406 0.566 19.084 6.565 0.30 134673. 0.5320
|
|
15.42 0.2172 0.4284 0.1042 0.0528 0.404 5.087 4.203 300.903 0.575 18.694 6.335 0.30 134882. 0.5080
|
|
17.63 0.2482 0.4724 0.1018 0.0535 0.408 5.149 4.105 304.614 0.582 18.260 6.113 0.30 135109. 0.4845
|
|
19.83 0.2792 0.5128 0.0991 0.0540 0.412 5.196 3.997 307.379 0.587 17.779 5.898 0.30 135354. 0.4613
|
|
22.04 0.3103 0.5498 0.0961 0.0543 0.414 5.224 3.878 309.034 0.590 17.247 5.691 0.30 135616. 0.4384
|
|
24.24 0.3413 0.5836 0.0929 0.0543 0.415 5.231 3.747 309.416 0.591 16.664 5.492 0.30 135897. 0.4158
|
|
26.44 0.3723 0.6144 0.0893 0.0541 0.414 5.213 3.603 308.361 0.589 16.028 5.300 0.30 136196. 0.3936
|
|
28.65 0.4033 0.6424 0.0855 0.0537 0.410 5.168 3.448 305.716 0.584 15.336 5.115 0.30 136514. 0.3715
|
|
30.85 0.4344 0.6677 0.0813 0.0529 0.404 5.094 3.280 301.353 0.576 14.589 4.937 0.30 136850. 0.3497
|
|
33.05 0.4654 0.6903 0.0769 0.0518 0.396 4.990 3.101 295.203 0.564 13.792 4.764 0.30 137204. 0.3282
|
|
35.26 0.4964 0.7104 0.0722 0.0504 0.385 4.856 2.911 287.271 0.549 12.948 4.596 0.30 137577. 0.3068
|
|
37.46 0.5274 0.7279 0.0673 0.0487 0.372 4.693 2.713 277.599 0.530 12.066 4.432 0.30 137968. 0.2856
|
|
39.66 0.5585 0.7427 0.0622 0.0467 0.357 4.501 2.507 266.235 0.508 11.151 4.271 0.30 138376. 0.2645
|
|
41.87 0.5895 0.7545 0.0569 0.0445 0.340 4.281 2.295 253.221 0.484 10.208 4.111 0.30 138803. 0.2436
|
|
44.07 0.6205 0.7630 0.0515 0.0419 0.320 4.033 2.077 238.588 0.456 9.241 3.949 0.30 139248. 0.2227
|
|
46.27 0.6515 0.7678 0.0460 0.0390 0.298 3.759 1.855 222.366 0.425 8.253 3.785 0.30 139711. 0.2017
|
|
48.48 0.6826 0.7678 0.0404 0.0359 0.274 3.458 1.629 204.578 0.391 7.248 3.613 0.30 140191. 0.1804
|
|
50.68 0.7136 0.7618 0.0347 0.0325 0.248 3.132 1.400 185.251 0.354 6.229 3.429 0.31 140690. 0.1587
|
|
52.88 0.7446 0.7474 0.0290 0.0289 0.220 2.779 1.169 164.418 0.314 5.198 3.224 0.31 141206. 0.1363
|
|
55.09 0.7756 0.7206 0.0232 0.0250 0.191 2.403 0.935 142.124 0.271 4.159 2.984 0.31 141740. 0.1129
|
|
57.29 0.8067 0.6737 0.0174 0.0208 0.159 2.002 0.700 118.427 0.226 3.115 2.682 0.31 142291. 0.0878
|
|
59.50 0.8377 0.5896 0.0115 0.0164 0.125 1.579 0.466 93.410 0.178 2.071 2.260 0.31 142859. 0.0603
|
|
61.70 0.8687 0.4228 0.0057 0.0118 0.090 1.136 0.232 67.178 0.128 1.030 1.563 0.31 143444. 0.0294
|
|
63.90 0.8997 -0.0028 0.0000 0.0070 0.053 0.673 -0.001 39.805 0.076 -0.004 -0.010 0.31 144034. 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 0.1156 0.0455 0.600 6.303 6.715 447.465 0.712 29.870 6.807 0.36 160498. 0.6900
|
|
2.67 0.0313 0.0770 0.1146 0.0466 0.615 6.458 6.655 458.451 0.730 29.602 6.584 0.36 160639. 0.6644
|
|
5.33 0.0626 0.1488 0.1134 0.0477 0.630 6.614 6.586 469.498 0.747 29.296 6.363 0.36 160797. 0.6388
|
|
8.00 0.0939 0.2155 0.1121 0.0488 0.644 6.768 6.508 480.406 0.765 28.949 6.145 0.36 160973. 0.6132
|
|
10.67 0.1252 0.2774 0.1105 0.0499 0.658 6.916 6.420 490.959 0.781 28.554 5.931 0.36 161167. 0.5878
|
|
13.34 0.1565 0.3345 0.1088 0.0509 0.672 7.056 6.319 500.918 0.797 28.107 5.722 0.36 161380. 0.5626
|
|
16.00 0.1878 0.3872 0.1068 0.0518 0.684 7.185 6.206 510.025 0.812 27.603 5.519 0.36 161614. 0.5378
|
|
18.67 0.2191 0.4356 0.1047 0.0526 0.695 7.297 6.079 518.005 0.824 27.038 5.323 0.36 161869. 0.5133
|
|
21.34 0.2504 0.4802 0.1022 0.0533 0.703 7.390 5.937 524.577 0.835 26.406 5.133 0.36 162145. 0.4892
|
|
24.00 0.2817 0.5210 0.0995 0.0538 0.710 7.458 5.779 529.448 0.843 25.704 4.951 0.36 162443. 0.4655
|
|
26.67 0.3129 0.5583 0.0965 0.0541 0.714 7.499 5.604 532.327 0.847 24.928 4.775 0.36 162763. 0.4422
|
|
29.34 0.3442 0.5925 0.0932 0.0541 0.715 7.507 5.412 532.918 0.848 24.075 4.607 0.36 163106. 0.4192
|
|
32.01 0.3755 0.6236 0.0896 0.0539 0.712 7.479 5.203 530.927 0.845 23.141 4.445 0.36 163470. 0.3966
|
|
34.67 0.4068 0.6519 0.0856 0.0534 0.705 7.411 4.974 526.082 0.837 22.126 4.289 0.36 163858. 0.3742
|
|
37.34 0.4381 0.6775 0.0814 0.0526 0.695 7.299 4.728 518.159 0.825 21.029 4.139 0.36 164267. 0.3520
|
|
40.01 0.4694 0.7004 0.0769 0.0515 0.680 7.143 4.464 507.047 0.807 19.858 3.994 0.36 164699. 0.3301
|
|
42.67 0.5007 0.7208 0.0721 0.0501 0.661 6.942 4.186 492.764 0.784 18.619 3.853 0.36 165153. 0.3084
|
|
45.34 0.5320 0.7387 0.0671 0.0483 0.638 6.697 3.895 475.389 0.757 17.325 3.716 0.36 165630. 0.2869
|
|
48.01 0.5633 0.7538 0.0619 0.0462 0.610 6.410 3.593 455.004 0.724 15.982 3.582 0.36 166128. 0.2656
|
|
50.68 0.5946 0.7661 0.0565 0.0439 0.579 6.081 3.282 431.684 0.687 14.598 3.448 0.36 166649. 0.2444
|
|
53.34 0.6259 0.7751 0.0510 0.0412 0.544 5.712 2.963 405.483 0.645 13.180 3.314 0.36 167191. 0.2232
|
|
56.01 0.6572 0.7803 0.0454 0.0382 0.505 5.303 2.638 376.451 0.599 11.732 3.178 0.36 167755. 0.2019
|
|
58.68 0.6885 0.7808 0.0397 0.0350 0.462 4.855 2.306 344.632 0.548 10.259 3.035 0.37 168341. 0.1803
|
|
61.34 0.7198 0.7752 0.0339 0.0315 0.416 4.368 1.971 310.075 0.493 8.766 2.883 0.37 168949. 0.1583
|
|
64.01 0.7511 0.7610 0.0281 0.0277 0.366 3.844 1.631 272.842 0.434 7.256 2.712 0.37 169578. 0.1355
|
|
66.68 0.7824 0.7337 0.0222 0.0237 0.312 3.283 1.289 233.016 0.371 5.735 2.510 0.37 170229. 0.1115
|
|
69.35 0.8137 0.6841 0.0163 0.0194 0.256 2.687 0.946 190.713 0.304 4.208 2.250 0.37 170900. 0.0856
|
|
72.01 0.8450 0.5910 0.0104 0.0148 0.196 2.058 0.603 146.088 0.233 2.682 1.872 0.37 171593. 0.0569
|
|
74.68 0.8762 0.3906 0.0045 0.0101 0.133 1.399 0.261 99.343 0.158 1.162 1.193 0.37 172305. 0.0239
|
|
77.35 0.9075
|
|
|
|
|
|
|
|
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 0.1161 0.0453 0.949 8.546 9.181 707.744 0.965 40.837 5.884 0.42 187239. 0.6974
|
|
3.09 0.0311 0.0771 0.1151 0.0464 0.973 8.759 9.102 725.371 0.990 40.485 5.691 0.42 187402. 0.6717
|
|
6.18 0.0621 0.1490 0.1140 0.0475 0.997 8.973 9.011 743.122 1.014 40.083 5.500 0.42 187585. 0.6459
|
|
9.27 0.0932 0.2158 0.1127 0.0487 1.020 9.185 8.908 760.681 1.038 39.624 5.312 0.42 187788. 0.6202
|
|
12.36 0.1243 0.2777 0.1112 0.0498 1.043 9.391 8.791 777.706 1.061 39.102 5.127 0.42 188012. 0.5946
|
|
15.44 0.1553 0.3349 0.1095 0.0508 1.065 9.585 8.658 793.817 1.083 38.510 4.947 0.42 188259. 0.5694
|
|
18.53 0.1864 0.3877 0.1076 0.0517 1.084 9.764 8.507 808.604 1.103 37.841 4.772 0.42 188529. 0.5445
|
|
21.62 0.2175 0.4363 0.1055 0.0526 1.102 9.921 8.338 821.633 1.121 37.088 4.603 0.42 188823. 0.5199
|
|
24.71 0.2485 0.4810 0.1031 0.0533 1.116 10.052 8.149 832.457 1.136 36.245 4.440 0.42 189142. 0.4958
|
|
27.80 0.2796 0.5220 0.1004 0.0538 1.127 10.150 7.938 840.615 1.147 35.306 4.283 0.42 189486. 0.4720
|
|
30.89 0.3106 0.5595 0.0975 0.0541 1.134 10.211 7.704 845.646 1.154 34.267 4.132 0.42 189855. 0.4486
|
|
33.98 0.3417 0.5939 0.0942 0.0542 1.136 10.228 7.447 847.082 1.156 33.123 3.987 0.42 190250. 0.4256
|
|
37.07 0.3728 0.6253 0.0906 0.0540 1.132 10.197 7.165 844.462 1.152 31.870 3.848 0.42 190671. 0.4030
|
|
40.15 0.4038 0.6539 0.0868 0.0536 1.123 10.111 6.858 837.352 1.142 30.505 3.715 0.42 191118. 0.3806
|
|
43.24 0.4349 0.6799 0.0826 0.0528 1.107 9.966 6.526 825.385 1.126 29.030 3.586 0.42 191590. 0.3584
|
|
46.33 0.4660 0.7033 0.0781 0.0517 1.084 9.761 6.171 808.363 1.103 27.450 3.463 0.42 192088. 0.3365
|
|
49.42 0.4970 0.7243 0.0733 0.0503 1.054 9.494 5.795 786.288 1.073 25.778 3.343 0.42 192612. 0.3148
|
|
52.51 0.5281 0.7428 0.0683 0.0486 1.018 9.168 5.402 759.279 1.036 24.027 3.227 0.42 193161. 0.2934
|
|
55.60 0.5592 0.7588 0.0632 0.0465 0.976 8.784 4.993 727.471 0.992 22.209 3.113 0.42 193735. 0.2721
|
|
58.69 0.5902 0.7720 0.0578 0.0442 0.927 8.343 4.571 690.981 0.943 20.334 3.001 0.42 194335. 0.2510
|
|
61.78 0.6213 0.7823 0.0524 0.0416 0.872 7.847 4.139 649.904 0.887 18.410 2.889 0.42 194960. 0.2299
|
|
64.86 0.6524 0.7891 0.0468 0.0387 0.810 7.297 3.697 604.315 0.824 16.445 2.775 0.43 195610. 0.2087
|
|
67.95 0.6834 0.7916 0.0411 0.0355 0.743 6.693 3.247 554.286 0.756 14.444 2.657 0.43 196285. 0.1873
|
|
71.04 0.7145 0.7887 0.0353 0.0320 0.670 6.036 2.791 499.891 0.682 12.415 2.533 0.43 196985. 0.1655
|
|
74.13 0.7455 0.7783 0.0295 0.0282 0.592 5.328 2.330 441.223 0.602 10.363 2.395 0.43 197709. 0.1430
|
|
77.22 0.7766 0.7565 0.0236 0.0242 0.507 4.569 1.864 378.407 0.516 8.293 2.235 0.43 198458. 0.1194
|
|
80.31 0.8077 0.7159 0.0177 0.0199 0.418 3.763 1.397 311.613 0.425 6.214 2.033 0.43 199232. 0.0940
|
|
83.40 0.8387 0.6391 0.0118 0.0154 0.323 2.911 0.929 241.073 0.329 4.132 1.748 0.43 200029. 0.0659
|
|
86.49 0.8698 0.4764 0.0059 0.0107 0.224 2.018 0.463 167.092 0.228 2.059 1.256 0.43 200850. 0.0334
|
|
89.58 0.9009 -0.0011 0.0000 0.0057 0.120 1.085 -0.001 89.832 0.123 -0.003 -0.003 0.43 201674. 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 0.1167 0.0453 1.416 11.157 12.051 1056.015 1.261 53.605 5.176 0.48 213977. 0.7029
|
|
3.53 0.0311 0.0775 0.1158 0.0464 1.452 11.441 11.952 1082.868 1.293 53.161 5.006 0.48 214163. 0.6770
|
|
7.06 0.0622 0.1498 0.1146 0.0476 1.488 11.727 11.837 1109.950 1.325 52.652 4.837 0.48 214372. 0.6510
|
|
10.60 0.0933 0.2170 0.1134 0.0487 1.524 12.010 11.706 1136.780 1.357 52.069 4.671 0.48 214604. 0.6251
|
|
14.13 0.1243 0.2792 0.1119 0.0498 1.559 12.286 11.556 1162.833 1.388 51.402 4.508 0.48 214861. 0.5994
|
|
17.66 0.1554 0.3367 0.1103 0.0509 1.592 12.547 11.385 1187.525 1.418 50.642 4.349 0.48 215143. 0.5740
|
|
21.19 0.1865 0.3897 0.1084 0.0519 1.623 12.786 11.192 1210.224 1.445 49.780 4.194 0.48 215452. 0.5489
|
|
24.73 0.2176 0.4385 0.1063 0.0527 1.650 12.998 10.973 1230.266 1.469 48.806 4.045 0.48 215789. 0.5242
|
|
28.26 0.2487 0.4834 0.1039 0.0534 1.672 13.175 10.727 1246.959 1.488 47.713 3.902 0.48 216154. 0.4999
|
|
31.79 0.2798 0.5246 0.1012 0.0540 1.689 13.308 10.452 1259.604 1.504 46.492 3.764 0.48 216548. 0.4760
|
|
35.32 0.3109 0.5624 0.0983 0.0543 1.700 13.391 10.148 1267.493 1.513 45.138 3.631 0.48 216971. 0.4525
|
|
38.86 0.3419 0.5970 0.0950 0.0544 1.703 13.417 9.812 1269.918 1.516 43.642 3.504 0.48 217423. 0.4294
|
|
42.39 0.3730 0.6286 0.0915 0.0543 1.698 13.378 9.443 1266.179 1.511 42.002 3.383 0.48 217906. 0.4066
|
|
45.92 0.4041 0.6575 0.0876 0.0538 1.684 13.266 9.041 1255.618 1.499 40.213 3.266 0.48 218417. 0.3841
|
|
49.45 0.4352 0.6837 0.0833 0.0530 1.660 13.076 8.605 1237.674 1.477 38.276 3.154 0.48 218958. 0.3619
|
|
52.99 0.4663 0.7074 0.0788 0.0520 1.625 12.806 8.138 1212.041 1.447 36.199 3.046 0.48 219529. 0.3399
|
|
56.52 0.4974 0.7288 0.0740 0.0505 1.581 12.454 7.644 1178.724 1.407 33.999 2.941 0.48 220129. 0.3181
|
|
60.05 0.5284 0.7477 0.0690 0.0488 1.526 12.022 7.125 1137.900 1.358 31.693 2.840 0.48 220758. 0.2966
|
|
63.58 0.5595 0.7642 0.0638 0.0467 1.461 11.514 6.587 1089.780 1.301 29.298 2.741 0.48 221416. 0.2752
|
|
67.12 0.5906 0.7780 0.0584 0.0443 1.387 10.930 6.031 1034.543 1.235 26.826 2.644 0.48 222103. 0.2540
|
|
70.65 0.6217 0.7889 0.0529 0.0417 1.304 10.273 5.461 972.335 1.161 24.290 2.547 0.49 222818. 0.2329
|
|
74.18 0.6528 0.7966 0.0472 0.0387 1.211 9.543 4.878 903.274 1.078 21.697 2.449 0.49 223562. 0.2116
|
|
77.71 0.6839 0.8002 0.0415 0.0355 1.110 8.742 4.285 827.467 0.988 19.058 2.349 0.49 224335. 0.1902
|
|
81.24 0.7150 0.7985 0.0357 0.0319 0.999 7.871 3.683 745.030 0.889 16.380 2.242 0.49 225136. 0.1683
|
|
84.78 0.7460 0.7897 0.0298 0.0281 0.880 6.932 3.073 656.101 0.783 13.671 2.125 0.49 225966. 0.1457
|
|
88.31 0.7771 0.7699 0.0238 0.0240 0.752 5.926 2.459 560.872 0.669 10.938 1.989 0.49 226823. 0.1220
|
|
91.84 0.8082 0.7318 0.0178 0.0197 0.616 4.856 1.842 459.599 0.549 8.192 1.818 0.49 227708. 0.0965
|
|
95.37 0.8393 0.6581 0.0119 0.0151 0.473 3.726 1.224 352.638 0.421 5.443 1.574 0.49 228621. 0.0681
|
|
98.91 0.8704 0.4972 0.0059 0.0103 0.322 2.541 0.608 240.457 0.287 2.704 1.147 0.49 229560. 0.0350
|
|
102.44 0.9015 -0.0078 0.0000 0.0053 0.165 1.302 -0.005 123.239 0.147 -0.021 -0.017 0.50 230498. 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 0.1174 0.0454 2.021 14.156 15.338 1507.388 1.599 68.223 4.615 0.54 240710. 0.7070
|
|
3.98 0.0311 0.0778 0.1164 0.0466 2.074 14.524 15.217 1546.501 1.641 67.686 4.463 0.54 240919. 0.6810
|
|
7.95 0.0622 0.1503 0.1154 0.0477 2.127 14.895 15.078 1586.017 1.683 67.067 4.312 0.54 241154. 0.6550
|
|
11.93 0.0933 0.2177 0.1142 0.0489 2.179 15.263 14.918 1625.238 1.724 66.353 4.163 0.54 241415. 0.6290
|
|
15.91 0.1244 0.2801 0.1127 0.0501 2.231 15.622 14.733 1663.391 1.765 65.533 4.017 0.54 241704. 0.6032
|
|
19.88 0.1555 0.3378 0.1111 0.0512 2.279 15.962 14.522 1699.614 1.803 64.594 3.875 0.54 242022. 0.5777
|
|
23.86 0.1866 0.3910 0.1093 0.0522 2.324 16.275 14.281 1732.975 1.839 63.522 3.738 0.54 242370. 0.5525
|
|
27.84 0.2177 0.4399 0.1072 0.0531 2.364 16.552 14.008 1762.490 1.870 62.306 3.605 0.54 242750. 0.5278
|
|
31.81 0.2488 0.4849 0.1048 0.0538 2.397 16.784 13.700 1787.145 1.896 60.935 3.477 0.54 243161. 0.5034
|
|
35.79 0.2799 0.5262 0.1022 0.0544 2.422 16.960 13.354 1805.913 1.916 59.399 3.354 0.54 243606. 0.4795
|
|
39.77 0.3111 0.5642 0.0992 0.0547 2.438 17.071 12.970 1817.759 1.929 57.689 3.236 0.54 244083. 0.4559
|
|
43.74 0.3422 0.5989 0.0960 0.0548 2.443 17.108 12.544 1821.658 1.933 55.797 3.123 0.54 244593. 0.4327
|
|
47.72 0.3733 0.6308 0.0924 0.0547 2.436 17.060 12.076 1816.594 1.927 53.716 3.015 0.54 245137. 0.4099
|
|
51.69 0.4044 0.6599 0.0885 0.0542 2.416 16.920 11.565 1801.610 1.912 51.443 2.912 0.54 245714. 0.3873
|
|
55.67 0.4355 0.6864 0.0843 0.0535 2.382 16.678 11.011 1775.900 1.884 48.977 2.812 0.54 246325. 0.3650
|
|
59.65 0.4666 0.7104 0.0797 0.0523 2.332 16.332 10.416 1739.003 1.845 46.330 2.717 0.54 246968. 0.3430
|
|
63.62 0.4977 0.7321 0.0749 0.0509 2.268 15.880 9.785 1690.928 1.794 43.522 2.625 0.54 247645. 0.3212
|
|
67.60 0.5288 0.7514 0.0698 0.0491 2.188 15.326 9.123 1631.934 1.732 40.577 2.535 0.54 248354. 0.2996
|
|
71.58 0.5599 0.7683 0.0645 0.0470 2.095 14.672 8.434 1562.336 1.658 37.515 2.449 0.54 249096. 0.2782
|
|
75.55 0.5910 0.7827 0.0591 0.0446 1.988 13.922 7.723 1482.402 1.573 34.353 2.363 0.54 249871. 0.2569
|
|
79.53 0.6221 0.7943 0.0535 0.0419 1.867 13.076 6.993 1392.350 1.477 31.107 2.278 0.55 250678. 0.2357
|
|
83.51 0.6532 0.8027 0.0478 0.0389 1.733 12.137 6.247 1292.352 1.371 27.788 2.193 0.55 251516. 0.2144
|
|
87.48 0.6843 0.8072 0.0420 0.0356 1.586 11.106 5.487 1182.567 1.255 24.408 2.105 0.55 252387. 0.1929
|
|
91.46 0.7154 0.8067 0.0361 0.0320 1.426 9.985 4.716 1063.162 1.128 20.977 2.012 0.55 253290. 0.1709
|
|
95.44 0.7465 0.7993 0.0301 0.0281 1.253 8.775 3.935 934.342 0.991 17.505 1.910 0.55 254225. 0.1482
|
|
99.41 0.7776 0.7814 0.0241 0.0240 1.068 7.479 3.148 796.376 0.845 14.002 1.793 0.55 255191. 0.1244
|
|
103.39 0.8087 0.7456 0.0180 0.0196 0.871 6.101 2.356 649.644 0.689 10.480 1.645 0.55 256189. 0.0988
|
|
107.37 0.8398 0.6748 0.0120 0.0149 0.663 4.646 1.563 494.660 0.525 6.954 1.434 0.55 257217. 0.0701
|
|
111.34 0.8709 0.5156 0.0059 0.0100 0.445 3.119 0.773 332.111 0.352 3.440 1.056 0.56 258275. 0.0363
|
|
115.32 0.9020 -0.0185 -0.0001 0.0049 0.217 1.523 -0.013 162.145 0.172 -0.058 -0.037 0.56 259325. 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 0.1181 0.0456 2.787 17.567 19.052 2078.429 1.985 84.744 4.158 0.59 267437. 0.7099
|
|
4.42 0.0311 0.0779 0.1172 0.0468 2.861 18.032 18.912 2133.397 2.037 84.120 4.021 0.60 267669. 0.6840
|
|
8.83 0.0622 0.1504 0.1162 0.0480 2.936 18.503 18.749 2189.074 2.090 83.394 3.885 0.60 267930. 0.6580
|
|
13.25 0.0933 0.2179 0.1150 0.0493 3.010 18.971 18.559 2244.459 2.143 82.553 3.751 0.60 268219. 0.6321
|
|
17.67 0.1244 0.2803 0.1137 0.0504 3.082 19.427 18.340 2298.464 2.195 81.578 3.619 0.60 268540. 0.6063
|
|
22.08 0.1555 0.3380 0.1121 0.0516 3.151 19.862 18.088 2349.852 2.244 80.455 3.491 0.60 268893. 0.5808
|
|
26.50 0.1866 0.3912 0.1103 0.0526 3.215 20.263 17.798 2397.299 2.289 79.165 3.367 0.60 269280. 0.5557
|
|
30.92 0.2177 0.4402 0.1083 0.0535 3.271 20.618 17.467 2439.392 2.329 77.694 3.248 0.60 269702. 0.5310
|
|
35.34 0.2488 0.4853 0.1059 0.0543 3.319 20.917 17.092 2474.690 2.363 76.026 3.133 0.60 270160. 0.5066
|
|
39.75 0.2799 0.5267 0.1033 0.0549 3.355 21.145 16.670 2501.731 2.389 74.149 3.022 0.60 270654. 0.4827
|
|
44.17 0.3110 0.5648 0.1004 0.0553 3.378 21.292 16.198 2519.064 2.406 72.050 2.917 0.60 271184. 0.4592
|
|
48.59 0.3420 0.5997 0.0972 0.0554 3.386 21.344 15.675 2525.248 2.411 69.721 2.815 0.60 271752. 0.4360
|
|
53.00 0.3731 0.6317 0.0936 0.0553 3.378 21.290 15.097 2518.864 2.405 67.152 2.719 0.60 272358. 0.4132
|
|
57.42 0.4042 0.6610 0.0897 0.0548 3.351 21.119 14.465 2498.583 2.386 64.339 2.626 0.60 273000. 0.3907
|
|
61.84 0.4353 0.6877 0.0854 0.0541 3.303 20.820 13.778 2463.272 2.352 61.283 2.537 0.60 273679. 0.3684
|
|
66.25 0.4664 0.7121 0.0808 0.0529 3.235 20.389 13.038 2412.271 2.304 57.995 2.452 0.60 274395. 0.3463
|
|
70.67 0.4975 0.7341 0.0759 0.0515 3.145 19.825 12.253 2345.578 2.240 54.502 2.369 0.60 275148. 0.3244
|
|
75.09 0.5286 0.7538 0.0708 0.0497 3.035 19.132 11.428 2263.566 2.162 50.833 2.290 0.60 275937. 0.3028
|
|
79.51 0.5597 0.7712 0.0655 0.0475 2.906 18.313 10.570 2166.681 2.069 47.014 2.213 0.60 276762. 0.2814
|
|
83.92 0.5908 0.7862 0.0600 0.0451 2.756 17.372 9.683 2055.326 1.963 43.069 2.137 0.61 277623. 0.2601
|
|
88.34 0.6219 0.7984 0.0544 0.0423 2.588 16.311 8.771 1929.811 1.843 39.015 2.062 0.61 278520. 0.2388
|
|
92.76 0.6530 0.8076 0.0486 0.0393 2.401 15.133 7.839 1790.387 1.710 34.869 1.986 0.61 279453. 0.2175
|
|
97.17 0.6841 0.8130 0.0427 0.0359 2.196 13.839 6.889 1637.278 1.563 30.644 1.909 0.61 280421. 0.1960
|
|
101.59 0.7152 0.8137 0.0367 0.0323 1.972 12.431 5.925 1470.717 1.404 26.352 1.827 0.61 281424. 0.1740
|
|
106.01 0.7463 0.8078 0.0307 0.0283 1.731 10.912 4.948 1290.987 1.233 22.007 1.738 0.61 282463. 0.1513
|
|
110.42 0.7774 0.7919 0.0246 0.0241 1.473 9.285 3.962 1098.467 1.049 17.622 1.636 0.61 283536. 0.1274
|
|
114.84 0.8085 0.7590 0.0184 0.0196 1.198 7.554 2.970 893.676 0.853 13.212 1.508 0.61 284644. 0.1016
|
|
119.26 0.8396 0.6922 0.0123 0.0149 0.908 5.725 1.977 677.334 0.647 8.795 1.324 0.62 285786. 0.0728
|
|
123.68 0.8707 0.5388 0.0061 0.0099 0.604 3.807 0.987 450.399 0.430 4.390 0.994 0.62 286961. 0.0386
|
|
128.09 0.9018 0.0011 0.0000 0.0047 0.286 1.802 0.001 213.153 0.204 0.004 0.002 0.62 288129. 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 0.1189 0.0460 3.743 21.449 23.207 2791.386 2.423 103.224 3.771 0.65 294159. 0.7106
|
|
4.86 0.0311 0.0777 0.1181 0.0473 3.843 22.021 23.049 2865.885 2.488 102.524 3.648 0.65 294414. 0.6851
|
|
9.72 0.0622 0.1503 0.1171 0.0485 3.945 22.603 22.865 2941.635 2.554 101.704 3.526 0.65 294699. 0.6595
|
|
14.58 0.0933 0.2177 0.1160 0.0497 4.046 23.184 22.649 3017.279 2.619 100.744 3.405 0.65 295017. 0.6338
|
|
19.44 0.1244 0.2801 0.1147 0.0510 4.146 23.753 22.397 3091.321 2.684 99.622 3.286 0.66 295369. 0.6084
|
|
24.30 0.1555 0.3378 0.1132 0.0521 4.240 24.297 22.104 3162.072 2.745 98.317 3.171 0.66 295758. 0.5831
|
|
29.16 0.1867 0.3910 0.1115 0.0532 4.328 24.801 21.764 3227.676 2.802 96.807 3.058 0.66 296184. 0.5581
|
|
34.03 0.2178 0.4401 0.1095 0.0542 4.407 25.250 21.374 3286.135 2.853 95.070 2.950 0.66 296648. 0.5335
|
|
38.89 0.2489 0.4852 0.1072 0.0550 4.473 25.629 20.928 3335.403 2.896 93.089 2.846 0.66 297153. 0.5093
|
|
43.75 0.2800 0.5267 0.1046 0.0556 4.524 25.921 20.424 3373.410 2.929 90.845 2.746 0.66 297698. 0.4855
|
|
48.61 0.3111 0.5648 0.1017 0.0560 4.557 26.111 19.857 3398.114 2.950 88.324 2.650 0.66 298283. 0.4620
|
|
53.47 0.3422 0.5998 0.0985 0.0562 4.570 26.183 19.225 3407.536 2.958 85.513 2.559 0.66 298910. 0.4389
|
|
58.33 0.3733 0.6320 0.0949 0.0561 4.559 26.123 18.526 3399.750 2.951 82.403 2.472 0.66 299578. 0.4161
|
|
63.19 0.4044 0.6615 0.0910 0.0556 4.523 25.917 17.758 3372.955 2.928 78.987 2.388 0.66 300286. 0.3936
|
|
68.05 0.4355 0.6885 0.0867 0.0548 4.460 25.553 16.921 3325.604 2.887 75.266 2.308 0.66 301036. 0.3714
|
|
72.91 0.4666 0.7131 0.0821 0.0537 4.367 25.025 16.019 3256.789 2.827 71.254 2.231 0.66 301826. 0.3493
|
|
77.77 0.4977 0.7355 0.0771 0.0522 4.246 24.331 15.060 3166.486 2.749 66.985 2.157 0.66 302656. 0.3275
|
|
82.63 0.5288 0.7556 0.0720 0.0504 4.097 23.476 14.050 3055.222 2.652 62.493 2.086 0.66 303526. 0.3058
|
|
87.49 0.5600 0.7734 0.0666 0.0482 3.921 22.465 12.998 2923.643 2.538 57.813 2.016 0.66 304436. 0.2844
|
|
92.35 0.5911 0.7889 0.0610 0.0457 3.718 21.302 11.909 2772.316 2.407 52.973 1.948 0.67 305386. 0.2630
|
|
97.22 0.6222 0.8018 0.0553 0.0429 3.489 19.991 10.791 2601.692 2.259 47.997 1.881 0.67 306374. 0.2417
|
|
102.08 0.6533 0.8116 0.0494 0.0398 3.235 18.534 9.646 2412.121 2.094 42.904 1.814 0.67 307402. 0.2204
|
|
106.94 0.6844 0.8180 0.0434 0.0363 2.955 16.935 8.478 2203.913 1.913 37.711 1.745 0.67 308469. 0.1987
|
|
111.80 0.7155 0.8197 0.0374 0.0326 2.652 15.194 7.292 1977.387 1.717 32.433 1.673 0.67 309574. 0.1767
|
|
116.66 0.7466 0.8152 0.0312 0.0286 2.324 13.316 6.090 1732.930 1.504 27.087 1.594 0.67 310719. 0.1539
|
|
121.52 0.7777 0.8009 0.0250 0.0243 1.973 11.303 4.876 1471.054 1.277 21.689 1.503 0.67 311901. 0.1299
|
|
126.38 0.8088 0.7702 0.0187 0.0197 1.599 9.163 3.655 1192.464 1.035 16.257 1.390 0.68 313121. 0.1040
|
|
131.24 0.8399 0.7063 0.0125 0.0148 1.204 6.901 2.431 898.177 0.780 10.813 1.228 0.68 314379. 0.0749
|
|
136.10 0.8710 0.5555 0.0062 0.0097 0.791 4.530 1.210 589.602 0.512 5.383 0.931 0.68 315673. 0.0401
|
|
140.96 0.9022 -0.0068 0.0000 0.0044 0.358 2.052 -0.006 267.101 0.232 -0.029 -0.011 0.68 316952. 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 0.1197 0.0471 4.972 26.116 27.809 3707.759 2.951 123.697 3.402 0.71 320875. 0.7018
|
|
5.30 0.0311 0.0766 0.1190 0.0483 5.101 26.791 27.641 3803.671 3.027 122.945 3.296 0.71 321151. 0.6778
|
|
10.61 0.0622 0.1483 0.1181 0.0495 5.232 27.479 27.440 3901.277 3.105 122.055 3.190 0.71 321461. 0.6537
|
|
15.91 0.0933 0.2152 0.1171 0.0508 5.362 28.166 27.204 3998.795 3.182 121.001 3.086 0.71 321806. 0.6295
|
|
21.21 0.1245 0.2774 0.1159 0.0520 5.491 28.838 26.923 4094.303 3.258 119.756 2.983 0.71 322190. 0.6054
|
|
26.52 0.1556 0.3350 0.1145 0.0532 5.613 29.482 26.594 4185.612 3.331 118.289 2.882 0.71 322613. 0.5813
|
|
31.82 0.1867 0.3883 0.1128 0.0542 5.727 30.078 26.208 4270.338 3.398 116.574 2.784 0.72 323078. 0.5575
|
|
37.12 0.2178 0.4376 0.1109 0.0552 5.828 30.611 25.760 4345.930 3.458 114.581 2.688 0.72 323585. 0.5338
|
|
42.43 0.2489 0.4830 0.1087 0.0560 5.914 31.060 25.244 4409.743 3.509 112.286 2.597 0.72 324136. 0.5103
|
|
47.73 0.2800 0.5248 0.1061 0.0566 5.980 31.408 24.655 4459.079 3.548 109.665 2.508 0.72 324732. 0.4871
|
|
53.03 0.3111 0.5633 0.1033 0.0570 6.023 31.634 23.989 4491.258 3.574 106.701 2.423 0.72 325372. 0.4641
|
|
58.34 0.3423 0.5986 0.1000 0.0572 6.039 31.721 23.241 4503.615 3.584 103.377 2.341 0.72 326057. 0.4414
|
|
63.64 0.3734 0.6311 0.0965 0.0571 6.026 31.650 22.410 4493.524 3.576 99.681 2.262 0.72 326788. 0.4189
|
|
68.95 0.4045 0.6609 0.0925 0.0566 5.979 31.403 21.494 4458.471 3.548 95.605 2.187 0.72 327563. 0.3966
|
|
74.25 0.4356 0.6882 0.0882 0.0558 5.895 30.965 20.493 4396.263 3.498 91.152 2.114 0.72 328383. 0.3744
|
|
79.55 0.4667 0.7131 0.0836 0.0547 5.774 30.326 19.410 4305.496 3.426 86.338 2.045 0.72 329247. 0.3524
|
|
84.86 0.4978 0.7359 0.0786 0.0532 5.613 29.484 18.256 4185.981 3.331 81.201 1.978 0.72 330156. 0.3306
|
|
90.16 0.5289 0.7564 0.0733 0.0513 5.416 28.445 17.039 4038.396 3.214 75.787 1.914 0.72 331107. 0.3090
|
|
95.46 0.5600 0.7747 0.0679 0.0491 5.181 27.214 15.769 3863.650 3.075 70.139 1.851 0.73 332102. 0.2875
|
|
100.77 0.5912 0.7907 0.0622 0.0465 4.912 25.797 14.454 3662.541 2.915 64.290 1.790 0.73 333140. 0.2662
|
|
106.07 0.6223 0.8042 0.0564 0.0436 4.607 24.200 13.100 3435.716 2.734 58.271 1.729 0.73 334221. 0.2449
|
|
111.37 0.6534 0.8149 0.0504 0.0404 4.269 22.424 11.714 3183.662 2.533 52.105 1.669 0.73 335345. 0.2234
|
|
116.68 0.6845 0.8221 0.0443 0.0369 3.898 20.474 10.300 2906.788 2.313 45.813 1.607 0.73 336510. 0.2018
|
|
121.98 0.7156 0.8249 0.0381 0.0331 3.494 18.352 8.861 2605.555 2.073 39.415 1.543 0.73 337718. 0.1796
|
|
127.28 0.7467 0.8216 0.0319 0.0290 3.058 16.063 7.403 2280.589 1.815 32.929 1.472 0.73 338967. 0.1567
|
|
132.59 0.7778 0.8089 0.0255 0.0245 2.592 13.614 5.930 1932.770 1.538 26.376 1.392 0.74 340259. 0.1326
|
|
137.89 0.8090 0.7798 0.0191 0.0199 2.096 11.012 4.446 1563.356 1.244 19.776 1.290 0.74 341591. 0.1064
|
|
143.19 0.8401 0.7173 0.0127 0.0149 1.575 8.270 2.958 1174.121 0.934 13.156 1.143 0.74 342964. 0.0769
|
|
148.50 0.8712 0.5663 0.0063 0.0097 1.029 5.406 1.472 767.473 0.611 6.547 0.870 0.74 344376. 0.0413
|
|
153.80 0.9023 -0.0097 0.0000 0.0044 0.462 2.426 -0.011 344.425 0.274 -0.049 -0.014 0.74 345767. 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 0.1205 0.0497 6.673 32.352 32.857 4975.936 3.655 146.147 2.995 0.77 347584. 0.6716
|
|
5.74 0.0311 0.0733 0.1199 0.0509 6.832 33.122 32.684 5094.384 3.742 145.377 2.910 0.77 347881. 0.6508
|
|
11.49 0.0622 0.1423 0.1191 0.0521 6.993 33.902 32.477 5214.365 3.830 144.456 2.825 0.77 348214. 0.6298
|
|
17.23 0.0933 0.2071 0.1182 0.0533 7.152 34.676 32.228 5333.410 3.918 143.350 2.741 0.77 348586. 0.6086
|
|
22.98 0.1244 0.2677 0.1171 0.0544 7.307 35.427 31.930 5448.854 4.003 142.024 2.658 0.77 349000. 0.5875
|
|
28.72 0.1555 0.3244 0.1158 0.0555 7.453 36.135 31.573 5557.809 4.083 140.438 2.577 0.77 349457. 0.5664
|
|
34.47 0.1866 0.3774 0.1142 0.0565 7.586 36.782 31.150 5657.229 4.156 138.556 2.497 0.77 349959. 0.5453
|
|
40.21 0.2178 0.4267 0.1124 0.0574 7.703 37.346 30.652 5743.988 4.219 136.340 2.420 0.78 350509. 0.5242
|
|
45.96 0.2489 0.4726 0.1103 0.0581 7.798 37.807 30.071 5814.912 4.271 133.757 2.346 0.78 351106. 0.5032
|
|
51.70 0.2800 0.5152 0.1078 0.0586 7.868 38.145 29.401 5866.831 4.310 130.775 2.273 0.78 351752. 0.4821
|
|
57.44 0.3111 0.5547 0.1050 0.0589 7.907 38.338 28.635 5896.609 4.331 127.370 2.203 0.78 352447. 0.4611
|
|
63.19 0.3422 0.5913 0.1019 0.0589 7.914 38.368 27.770 5901.202 4.335 123.520 2.134 0.78 353191. 0.4400
|
|
68.93 0.3733 0.6250 0.0983 0.0587 7.882 38.215 26.801 5877.607 4.317 119.211 2.068 0.78 353984. 0.4188
|
|
74.68 0.4044 0.6561 0.0944 0.0582 7.809 37.859 25.727 5822.921 4.277 114.433 2.004 0.78 354827. 0.3976
|
|
80.42 0.4355 0.6845 0.0900 0.0573 7.690 37.284 24.548 5734.521 4.212 109.187 1.942 0.78 355718. 0.3763
|
|
86.17 0.4666 0.7106 0.0853 0.0560 7.524 36.479 23.268 5610.610 4.121 103.496 1.881 0.78 356656. 0.3549
|
|
91.91 0.4977 0.7342 0.0803 0.0544 7.310 35.440 21.898 5450.785 4.004 97.403 1.822 0.78 357643. 0.3336
|
|
97.65 0.5288 0.7556 0.0750 0.0525 7.048 34.170 20.451 5255.590 3.861 90.965 1.765 0.78 358677. 0.3122
|
|
103.40 0.5599 0.7747 0.0695 0.0502 6.740 32.677 18.937 5025.881 3.692 84.232 1.709 0.79 359757. 0.2909
|
|
109.14 0.5911 0.7914 0.0637 0.0476 6.387 30.964 17.367 4762.434 3.498 77.250 1.654 0.79 360884. 0.2696
|
|
114.89 0.6222 0.8057 0.0578 0.0446 5.989 29.036 15.750 4465.921 3.280 70.055 1.600 0.79 362057. 0.2483
|
|
120.63 0.6533 0.8170 0.0517 0.0413 5.548 26.897 14.091 4136.966 3.039 62.677 1.545 0.79 363276. 0.2269
|
|
126.38 0.6844 0.8249 0.0455 0.0377 5.064 24.552 12.397 3776.288 2.774 55.141 1.489 0.79 364540. 0.2051
|
|
132.12 0.7155 0.8283 0.0391 0.0338 4.539 22.008 10.672 3384.889 2.486 47.469 1.430 0.79 365850. 0.1827
|
|
137.87 0.7466 0.8251 0.0327 0.0296 3.975 19.272 8.922 2964.176 2.177 39.683 1.365 0.80 367205. 0.1595
|
|
143.61 0.7777 0.8116 0.0262 0.0251 3.374 16.359 7.151 2516.081 1.848 31.807 1.289 0.80 368604. 0.1348
|
|
149.35 0.8088 0.7799 0.0197 0.0204 2.740 13.284 5.365 2043.173 1.501 23.865 1.191 0.80 370048. 0.1079
|
|
155.10 0.8399 0.7112 0.0131 0.0155 2.077 10.071 3.572 1548.897 1.138 15.887 1.046 0.80 371536. 0.0773
|
|
160.84 0.8710 0.5482 0.0065 0.0104 1.391 6.746 1.778 1037.578 0.762 7.910 0.777 0.80 373066. 0.0406
|
|
166.59 0.9021 -0.0088 -0.0001 0.0051 0.687 3.329 -0.014 511.953 0.376 -0.061 -0.012 0.80 374576. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1212 0.0550 9.215 41.484 38.318 6871.294 4.687 170.437 2.529 0.83 374286. 0.6125
|
|
6.19 0.0311 0.0669 0.1206 0.0561 9.407 42.352 38.148 7015.114 4.785 169.684 2.467 0.83 374603. 0.5959
|
|
12.38 0.0622 0.1304 0.1200 0.0573 9.602 43.226 37.944 7159.848 4.884 168.777 2.404 0.83 374959. 0.5792
|
|
18.57 0.0934 0.1906 0.1192 0.0584 9.792 44.083 37.697 7301.677 4.980 167.674 2.342 0.83 375357. 0.5624
|
|
24.76 0.1245 0.2475 0.1183 0.0595 9.972 44.896 37.394 7436.365 5.072 166.330 2.281 0.83 375799. 0.5456
|
|
30.94 0.1556 0.3014 0.1171 0.0605 10.137 45.639 37.026 7559.404 5.156 164.692 2.222 0.83 376289. 0.5288
|
|
37.13 0.1867 0.3523 0.1157 0.0613 10.281 46.284 36.581 7666.327 5.229 162.711 2.164 0.83 376829. 0.5120
|
|
43.32 0.2179 0.4005 0.1140 0.0620 10.397 46.807 36.046 7752.897 5.288 160.334 2.109 0.83 377419. 0.4953
|
|
49.51 0.2490 0.4461 0.1120 0.0625 10.480 47.183 35.413 7815.278 5.331 157.517 2.055 0.84 378063. 0.4784
|
|
55.70 0.2801 0.4892 0.1096 0.0628 10.527 47.394 34.671 7850.159 5.355 154.218 2.003 0.84 378759. 0.4614
|
|
61.89 0.3112 0.5298 0.1069 0.0628 10.533 47.420 33.814 7854.435 5.357 150.403 1.953 0.84 379510. 0.4442
|
|
68.08 0.3423 0.5680 0.1038 0.0626 10.494 47.243 32.833 7825.103 5.337 146.042 1.903 0.84 380314. 0.4266
|
|
74.27 0.3735 0.6038 0.1003 0.0621 10.405 46.845 31.726 7759.200 5.292 141.115 1.855 0.84 381172. 0.4086
|
|
80.46 0.4046 0.6372 0.0964 0.0612 10.264 46.210 30.488 7654.011 5.221 135.609 1.807 0.84 382083. 0.3902
|
|
86.65 0.4357 0.6683 0.0921 0.0600 10.067 45.323 29.120 7507.225 5.121 129.524 1.759 0.84 383047. 0.3714
|
|
92.83 0.4668 0.6969 0.0874 0.0585 9.813 44.178 27.627 7317.431 4.991 122.886 1.712 0.84 384063. 0.3521
|
|
99.02 0.4979 0.7232 0.0823 0.0567 9.501 42.773 26.023 7084.839 4.833 115.750 1.666 0.84 385130. 0.3324
|
|
105.21 0.5291 0.7471 0.0769 0.0545 9.133 41.118 24.322 6810.594 4.645 108.185 1.620 0.84 386248. 0.3125
|
|
111.40 0.5602 0.7686 0.0713 0.0520 8.711 39.217 22.539 6495.816 4.431 100.252 1.574 0.85 387416. 0.2923
|
|
117.59 0.5913 0.7875 0.0654 0.0491 8.236 37.077 20.685 6141.256 4.189 92.005 1.528 0.85 388634. 0.2718
|
|
123.78 0.6224 0.8037 0.0594 0.0460 7.708 34.701 18.770 5747.831 3.921 83.489 1.481 0.85 389901. 0.2510
|
|
129.97 0.6536 0.8162 0.0531 0.0425 7.134 32.120 16.803 5320.168 3.629 74.738 1.433 0.85 391218. 0.2297
|
|
136.16 0.6847 0.8239 0.0468 0.0389 6.517 29.340 14.790 4859.752 3.315 65.785 1.380 0.85 392584. 0.2077
|
|
142.35 0.7158 0.8256 0.0403 0.0349 5.856 26.366 12.738 4367.170 2.979 56.657 1.323 0.85 393998. 0.1847
|
|
148.53 0.7469 0.8187 0.0337 0.0307 5.154 23.202 10.653 3843.058 2.621 47.383 1.257 0.86 395460. 0.1605
|
|
154.72 0.7780 0.7984 0.0270 0.0263 4.414 19.871 8.541 3291.289 2.245 37.990 1.177 0.86 396970. 0.1346
|
|
160.91 0.8092 0.7547 0.0203 0.0217 3.644 16.404 6.409 2717.025 1.853 28.507 1.070 0.86 398528. 0.1060
|
|
167.10 0.8403 0.6666 0.0135 0.0170 2.851 12.837 4.266 2126.344 1.450 18.975 0.910 0.86 400133. 0.0735
|
|
173.29 0.8714 0.4790 0.0067 0.0122 2.047 9.215 2.122 1526.375 1.041 9.439 0.631 0.86 401783. 0.0359
|
|
179.48 0.9025 -0.0063 -0.0001 0.0074 1.237 5.568 -0.016 922.232 0.629 -0.072 -0.008 0.87 403430. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1208 0.0620 12.783 53.712 43.865 9532.149 6.068 195.110 2.087 0.89 401023. 0.5408
|
|
6.65 0.0312 0.0595 0.1204 0.0632 13.026 54.735 43.707 9713.715 6.184 194.410 2.041 0.89 401359. 0.5278
|
|
13.31 0.0625 0.1163 0.1199 0.0644 13.274 55.775 43.519 9898.326 6.301 193.572 1.994 0.89 401736. 0.5146
|
|
19.96 0.0937 0.1704 0.1193 0.0655 13.519 56.804 43.289 10080.810 6.418 192.550 1.948 0.89 402158. 0.5013
|
|
26.61 0.1249 0.2219 0.1185 0.0667 13.752 57.785 43.006 10254.917 6.528 191.291 1.902 0.89 402627. 0.4880
|
|
33.27 0.1561 0.2710 0.1175 0.0677 13.964 58.677 42.656 10413.263 6.629 189.732 1.858 0.89 403147. 0.4747
|
|
39.92 0.1874 0.3177 0.1163 0.0686 14.145 59.435 42.222 10547.759 6.715 187.805 1.816 0.89 403721. 0.4615
|
|
46.57 0.2186 0.3625 0.1148 0.0693 14.282 60.012 41.690 10650.251 6.780 185.437 1.775 0.89 404351. 0.4484
|
|
53.23 0.2498 0.4055 0.1131 0.0697 14.367 60.368 41.043 10713.335 6.820 182.559 1.738 0.90 405039. 0.4355
|
|
59.88 0.2810 0.4468 0.1109 0.0698 14.390 60.467 40.267 10730.992 6.832 179.107 1.702 0.90 405786. 0.4225
|
|
66.53 0.3123 0.4866 0.1084 0.0696 14.347 60.286 39.349 10698.821 6.811 175.026 1.668 0.90 406592. 0.4093
|
|
73.19 0.3435 0.5249 0.1055 0.0690 14.233 59.807 38.281 10613.732 6.757 170.273 1.636 0.90 407458. 0.3959
|
|
79.84 0.3747 0.5616 0.1021 0.0681 14.046 59.018 37.054 10473.732 6.668 164.815 1.605 0.90 408384. 0.3821
|
|
86.49 0.4059 0.5968 0.0982 0.0668 13.782 57.912 35.664 10277.438 6.543 158.634 1.574 0.90 409367. 0.3677
|
|
93.15 0.4372 0.6302 0.0940 0.0652 13.443 56.487 34.112 10024.700 6.382 151.730 1.543 0.90 410409. 0.3526
|
|
99.80 0.4684 0.6618 0.0893 0.0632 13.030 54.750 32.404 9716.322 6.186 144.133 1.513 0.90 411507. 0.3368
|
|
106.45 0.4996 0.6914 0.0842 0.0608 12.544 52.709 30.555 9354.114 5.955 135.907 1.482 0.90 412661. 0.3204
|
|
113.11 0.5308 0.7190 0.0787 0.0581 11.990 50.381 28.582 8940.957 5.692 127.132 1.450 0.91 413870. 0.3032
|
|
119.76 0.5621 0.7443 0.0730 0.0551 11.372 47.784 26.504 8480.120 5.399 117.889 1.418 0.91 415134. 0.2855
|
|
126.41 0.5933 0.7671 0.0670 0.0519 10.694 44.934 24.336 7974.365 5.077 108.248 1.384 0.91 416451. 0.2671
|
|
133.07 0.6245 0.7873 0.0609 0.0483 9.957 41.840 22.093 7425.261 4.727 98.269 1.350 0.91 417821. 0.2481
|
|
139.72 0.6558 0.8034 0.0545 0.0445 9.174 38.548 19.782 6840.969 4.355 87.990 1.312 0.91 419244. 0.2282
|
|
146.37 0.6870 0.8128 0.0480 0.0405 8.360 35.128 17.410 6234.153 3.969 77.441 1.267 0.91 420720. 0.2068
|
|
153.03 0.7182 0.8088 0.0413 0.0366 7.557 31.756 14.980 5635.591 3.588 66.631 1.206 0.92 422247. 0.1825
|
|
159.68 0.7494 0.7916 0.0345 0.0326 6.727 28.267 12.507 5016.474 3.194 55.630 1.131 0.92 423826. 0.1564
|
|
166.33 0.7807 0.7555 0.0276 0.0285 5.871 24.671 10.001 4378.327 2.787 44.485 1.036 0.92 425456. 0.1282
|
|
172.99 0.8119 0.6893 0.0206 0.0243 5.002 21.017 7.474 3729.835 2.374 33.245 0.909 0.92 427137. 0.0972
|
|
179.64 0.8431 0.5730 0.0136 0.0200 4.130 17.354 4.941 3079.740 1.961 21.976 0.728 0.92 428868. 0.0633
|
|
186.29 0.8743 0.3680 0.0067 0.0158 3.268 13.732 2.421 2436.954 1.551 10.768 0.451 0.93 430648. 0.0274
|
|
192.95 0.9056 -0.0148 -0.0002 0.0117 2.420 10.169 -0.070 1804.719 1.149 -0.310 -0.018 0.93 432443. 0.0000
|
|
|
|
|
|
|