538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x12W (17x12W.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 0.1208 0.0568 0.006 0.403 0.318 4.773 0.046 1.414 30.203 0.07 36806. 0.5894
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0.48 0.0301 0.0623 0.1195 0.0578 0.007 0.410 0.314 4.853 0.046 1.398 29.382 0.07 36839. 0.5703
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0.97 0.0603 0.1211 0.1180 0.0587 0.007 0.417 0.311 4.931 0.047 1.381 28.560 0.07 36875. 0.5509
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1.45 0.0904 0.1764 0.1164 0.0596 0.007 0.423 0.306 5.007 0.048 1.362 27.740 0.07 36915. 0.5314
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1.93 0.1205 0.2284 0.1146 0.0605 0.007 0.429 0.301 5.078 0.048 1.341 26.926 0.07 36959. 0.5117
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2.42 0.1506 0.2769 0.1126 0.0612 0.007 0.435 0.296 5.142 0.049 1.317 26.121 0.07 37007. 0.4921
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2.90 0.1808 0.3222 0.1103 0.0619 0.007 0.439 0.290 5.199 0.050 1.291 25.328 0.07 37060. 0.4724
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3.39 0.2109 0.3643 0.1079 0.0625 0.007 0.443 0.284 5.245 0.050 1.263 24.547 0.07 37116. 0.4527
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3.87 0.2410 0.4034 0.1052 0.0629 0.007 0.446 0.277 5.279 0.050 1.231 23.781 0.07 37177. 0.4331
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4.35 0.2712 0.4394 0.1023 0.0631 0.007 0.448 0.269 5.299 0.051 1.197 23.028 0.07 37243. 0.4135
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4.84 0.3013 0.4726 0.0991 0.0632 0.007 0.448 0.261 5.303 0.051 1.159 22.290 0.07 37313. 0.3939
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5.32 0.3314 0.5029 0.0956 0.0630 0.007 0.447 0.251 5.289 0.051 1.119 21.565 0.07 37388. 0.3743
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5.80 0.3616 0.5305 0.0918 0.0626 0.007 0.444 0.242 5.254 0.050 1.074 20.851 0.07 37467. 0.3547
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6.29 0.3917 0.5553 0.0878 0.0619 0.007 0.439 0.231 5.197 0.050 1.027 20.147 0.07 37552. 0.3351
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6.77 0.4218 0.5774 0.0834 0.0609 0.007 0.432 0.219 5.117 0.049 0.976 19.451 0.07 37641. 0.3154
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7.25 0.4519 0.5966 0.0788 0.0597 0.007 0.424 0.207 5.012 0.048 0.922 18.759 0.07 37734. 0.2957
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7.74 0.4821 0.6129 0.0740 0.0582 0.007 0.413 0.195 4.885 0.047 0.865 18.067 0.07 37833. 0.2759
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8.22 0.5122 0.6261 0.0689 0.0564 0.006 0.400 0.181 4.734 0.045 0.806 17.370 0.07 37935. 0.2560
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8.71 0.5423 0.6359 0.0637 0.0543 0.006 0.386 0.168 4.562 0.044 0.745 16.662 0.07 38043. 0.2361
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9.19 0.5725 0.6419 0.0583 0.0520 0.006 0.369 0.153 4.369 0.042 0.683 15.934 0.07 38155. 0.2161
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9.67 0.6026 0.6436 0.0528 0.0495 0.006 0.351 0.139 4.154 0.040 0.618 15.177 0.07 38272. 0.1959
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10.16 0.6327 0.6401 0.0472 0.0467 0.005 0.331 0.124 3.919 0.037 0.553 14.377 0.07 38394. 0.1754
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10.64 0.6629 0.6305 0.0415 0.0436 0.005 0.310 0.109 3.664 0.035 0.486 13.518 0.07 38520. 0.1546
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11.12 0.6930 0.6131 0.0357 0.0404 0.005 0.286 0.094 3.389 0.032 0.418 12.573 0.07 38651. 0.1334
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11.61 0.7231 0.5855 0.0298 0.0369 0.004 0.262 0.078 3.094 0.030 0.349 11.505 0.07 38786. 0.1116
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12.09 0.7532 0.5438 0.0239 0.0331 0.004 0.235 0.063 2.781 0.027 0.280 10.260 0.07 38926. 0.0891
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12.57 0.7834 0.4820 0.0179 0.0292 0.003 0.207 0.047 2.449 0.023 0.210 8.744 0.07 39070. 0.0658
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13.06 0.8135 0.3892 0.0120 0.0250 0.003 0.177 0.031 2.099 0.020 0.140 6.798 0.07 39219. 0.0417
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13.54 0.8436 0.2445 0.0060 0.0206 0.002 0.147 0.016 1.733 0.017 0.070 4.118 0.07 39372. 0.0179
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14.03 0.8738 0.0018 0.0000 0.0161 0.002 0.114 0.000 1.353 0.013 0.000 0.029 0.07 39529. 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 0.1213 0.0519 0.047 1.474 1.277 34.872 0.167 5.679 16.606 0.13 73611. 0.6495
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0.97 0.0303 0.0687 0.1200 0.0529 0.048 1.502 1.263 35.551 0.170 5.618 16.114 0.13 73677. 0.6269
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1.95 0.0606 0.1333 0.1186 0.0539 0.049 1.531 1.248 36.220 0.173 5.550 15.624 0.13 73750. 0.6041
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2.92 0.0909 0.1938 0.1169 0.0549 0.049 1.558 1.231 36.868 0.176 5.474 15.140 0.13 73831. 0.5814
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3.89 0.1213 0.2502 0.1151 0.0558 0.050 1.584 1.212 37.482 0.179 5.389 14.662 0.13 73920. 0.5587
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4.87 0.1516 0.3027 0.1131 0.0566 0.051 1.608 1.190 38.045 0.182 5.295 14.193 0.13 74017. 0.5361
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5.84 0.1819 0.3515 0.1109 0.0574 0.052 1.629 1.167 38.545 0.184 5.191 13.734 0.13 74122. 0.5136
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6.81 0.2122 0.3968 0.1085 0.0580 0.052 1.647 1.141 38.963 0.186 5.077 13.286 0.13 74237. 0.4913
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7.79 0.2425 0.4386 0.1058 0.0585 0.053 1.660 1.113 39.284 0.188 4.950 12.850 0.13 74360. 0.4693
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8.76 0.2728 0.4771 0.1028 0.0588 0.053 1.669 1.082 39.490 0.189 4.812 12.425 0.13 74492. 0.4474
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9.73 0.3031 0.5125 0.0996 0.0589 0.053 1.672 1.048 39.564 0.189 4.661 12.013 0.14 74634. 0.4257
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10.70 0.3334 0.5449 0.0961 0.0588 0.053 1.669 1.011 39.488 0.189 4.497 11.612 0.14 74786. 0.4041
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11.68 0.3638 0.5745 0.0923 0.0584 0.053 1.658 0.971 39.243 0.187 4.318 11.221 0.14 74946. 0.3828
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12.65 0.3941 0.6012 0.0882 0.0578 0.052 1.640 0.928 38.814 0.185 4.126 10.841 0.14 75117. 0.3615
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13.62 0.4244 0.6253 0.0838 0.0569 0.051 1.614 0.881 38.190 0.182 3.921 10.469 0.14 75296. 0.3403
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14.60 0.4547 0.6466 0.0791 0.0556 0.050 1.579 0.832 37.368 0.178 3.703 10.105 0.14 75486. 0.3191
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15.57 0.4850 0.6652 0.0742 0.0541 0.049 1.536 0.781 36.352 0.174 3.474 9.745 0.14 75684. 0.2981
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16.54 0.5153 0.6809 0.0691 0.0523 0.047 1.485 0.728 35.145 0.168 3.236 9.389 0.14 75892. 0.2772
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17.52 0.5456 0.6936 0.0639 0.0502 0.045 1.426 0.672 33.754 0.161 2.990 9.032 0.14 76110. 0.2563
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18.49 0.5759 0.7029 0.0585 0.0479 0.043 1.360 0.615 32.181 0.154 2.737 8.671 0.14 76337. 0.2354
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19.46 0.6063 0.7083 0.0529 0.0453 0.041 1.286 0.557 30.430 0.145 2.477 8.301 0.14 76573. 0.2145
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20.44 0.6366 0.7092 0.0473 0.0424 0.038 1.205 0.497 28.503 0.136 2.213 7.916 0.14 76819. 0.1933
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21.41 0.6669 0.7046 0.0415 0.0393 0.035 1.116 0.437 26.402 0.126 1.944 7.507 0.14 77074. 0.1718
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22.38 0.6972 0.6928 0.0357 0.0359 0.032 1.020 0.376 24.130 0.115 1.671 7.061 0.14 77338. 0.1498
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23.36 0.7275 0.6714 0.0298 0.0323 0.029 0.917 0.314 21.689 0.104 1.395 6.557 0.14 77612. 0.1271
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24.33 0.7578 0.6362 0.0239 0.0284 0.026 0.807 0.251 19.085 0.091 1.116 5.965 0.14 77895. 0.1034
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25.30 0.7881 0.5797 0.0179 0.0243 0.022 0.690 0.188 16.323 0.078 0.837 5.226 0.14 78187. 0.0785
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26.27 0.8184 0.4872 0.0119 0.0200 0.018 0.567 0.125 13.413 0.064 0.556 4.229 0.14 78488. 0.0518
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27.25 0.8488 0.3252 0.0059 0.0154 0.014 0.438 0.062 10.364 0.049 0.277 2.723 0.14 78797. 0.0235
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28.22 0.8791 -0.0024 0.0000 0.0107 0.010 0.304 0.000 7.185 0.034 -0.001 -0.019 0.14 79111. 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 0.1217 0.0500 0.152 3.193 2.882 113.313 0.361 12.821 11.537 0.20 110413. 0.6781
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1.46 0.0304 0.0717 0.1205 0.0510 0.155 3.259 2.852 115.671 0.368 12.685 11.183 0.20 110513. 0.6537
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2.93 0.0608 0.1390 0.1190 0.0521 0.158 3.325 2.818 118.003 0.376 12.533 10.831 0.20 110623. 0.6293
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4.39 0.0912 0.2017 0.1174 0.0530 0.161 3.388 2.780 120.264 0.383 12.364 10.483 0.20 110745. 0.6050
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5.85 0.1215 0.2602 0.1156 0.0540 0.164 3.449 2.737 122.410 0.390 12.174 10.142 0.20 110878. 0.5808
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7.32 0.1519 0.3146 0.1136 0.0549 0.167 3.505 2.690 124.391 0.396 11.964 9.808 0.20 111024. 0.5568
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8.78 0.1823 0.3649 0.1114 0.0556 0.169 3.554 2.637 126.153 0.402 11.730 9.482 0.20 111183. 0.5330
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10.24 0.2127 0.4115 0.1089 0.0563 0.171 3.596 2.579 127.642 0.406 11.472 9.165 0.20 111356. 0.5095
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11.71 0.2431 0.4546 0.1062 0.0568 0.173 3.629 2.515 128.799 0.410 11.188 8.858 0.20 111541. 0.4863
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13.17 0.2735 0.4942 0.1033 0.0572 0.174 3.650 2.445 129.564 0.412 10.876 8.560 0.20 111741. 0.4634
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14.63 0.3039 0.5306 0.1000 0.0573 0.174 3.659 2.369 129.877 0.413 10.535 8.272 0.20 111955. 0.4407
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16.10 0.3343 0.5640 0.0965 0.0572 0.174 3.653 2.285 129.675 0.413 10.164 7.993 0.20 112183. 0.4183
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17.56 0.3646 0.5945 0.0927 0.0569 0.173 3.632 2.195 128.896 0.410 9.762 7.723 0.20 112425. 0.3960
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19.02 0.3950 0.6222 0.0886 0.0562 0.171 3.592 2.097 127.486 0.406 9.328 7.461 0.20 112682. 0.3740
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20.49 0.4254 0.6472 0.0842 0.0553 0.168 3.533 1.992 125.403 0.399 8.862 7.206 0.20 112953. 0.3521
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21.95 0.4558 0.6696 0.0795 0.0541 0.164 3.455 1.882 122.639 0.390 8.369 6.959 0.20 113238. 0.3304
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23.41 0.4862 0.6893 0.0746 0.0526 0.160 3.358 1.765 119.202 0.379 7.851 6.716 0.20 113537. 0.3089
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24.88 0.5166 0.7064 0.0694 0.0508 0.154 3.243 1.644 115.110 0.366 7.312 6.478 0.20 113851. 0.2875
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26.34 0.5470 0.7206 0.0641 0.0487 0.148 3.110 1.519 110.376 0.351 6.755 6.241 0.20 114179. 0.2662
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27.80 0.5773 0.7317 0.0587 0.0463 0.141 2.959 1.390 105.013 0.334 6.182 6.003 0.21 114521. 0.2450
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29.26 0.6077 0.7392 0.0531 0.0437 0.133 2.790 1.258 99.030 0.315 5.596 5.762 0.21 114877. 0.2237
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30.73 0.6381 0.7427 0.0475 0.0408 0.124 2.604 1.123 92.434 0.294 4.997 5.513 0.21 115247. 0.2023
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32.19 0.6685 0.7410 0.0417 0.0376 0.114 2.401 0.987 85.232 0.271 4.389 5.251 0.21 115631. 0.1806
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33.65 0.6989 0.7329 0.0358 0.0342 0.104 2.182 0.848 77.432 0.246 3.772 4.967 0.21 116030. 0.1583
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35.12 0.7293 0.7158 0.0299 0.0305 0.093 1.945 0.708 69.047 0.220 3.148 4.649 0.21 116442. 0.1354
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36.58 0.7597 0.6856 0.0239 0.0265 0.081 1.693 0.566 60.092 0.191 2.519 4.275 0.21 116868. 0.1114
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38.04 0.7900 0.6345 0.0179 0.0223 0.068 1.425 0.424 50.589 0.161 1.887 3.804 0.21 117308. 0.0858
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39.51 0.8204 0.5463 0.0119 0.0179 0.054 1.143 0.282 40.568 0.129 1.255 3.154 0.21 117762. 0.0580
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40.97 0.8508 0.3801 0.0059 0.0133 0.040 0.847 0.140 30.069 0.096 0.624 2.116 0.21 118228. 0.0274
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42.43 0.8812 -0.0035 0.0000 0.0084 0.026 0.538 -0.001 19.106 0.061 -0.004 -0.019 0.21 118697. 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 0.1222 0.0490 0.353 5.566 5.143 263.404 0.629 22.878 8.857 0.27 147213. 0.6953
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1.95 0.0304 0.0735 0.1209 0.0501 0.361 5.687 5.090 269.117 0.642 22.640 8.579 0.27 147345. 0.6700
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3.91 0.0609 0.1422 0.1195 0.0511 0.368 5.806 5.030 274.773 0.656 22.373 8.303 0.27 147493. 0.6446
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5.86 0.0913 0.2064 0.1179 0.0522 0.376 5.922 4.963 280.268 0.669 22.075 8.031 0.27 147655. 0.6194
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7.82 0.1217 0.2661 0.1161 0.0531 0.383 6.033 4.888 285.492 0.682 21.741 7.765 0.27 147834. 0.5943
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9.77 0.1522 0.3214 0.1141 0.0540 0.389 6.135 4.804 290.324 0.693 21.368 7.505 0.27 148029. 0.5694
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11.72 0.1826 0.3727 0.1119 0.0548 0.395 6.226 4.711 294.636 0.703 20.955 7.252 0.27 148242. 0.5449
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13.68 0.2130 0.4201 0.1095 0.0555 0.400 6.303 4.608 298.294 0.712 20.497 7.007 0.27 148472. 0.5207
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15.63 0.2434 0.4639 0.1068 0.0560 0.404 6.364 4.495 301.157 0.719 19.992 6.769 0.27 148721. 0.4968
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17.58 0.2739 0.5041 0.1038 0.0564 0.406 6.404 4.370 303.081 0.724 19.437 6.540 0.27 148988. 0.4732
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19.54 0.3043 0.5412 0.1006 0.0566 0.408 6.422 4.233 303.919 0.726 18.830 6.318 0.27 149274. 0.4500
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21.49 0.3347 0.5751 0.0970 0.0565 0.407 6.414 4.085 303.520 0.725 18.169 6.104 0.27 149579. 0.4271
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23.45 0.3652 0.6062 0.0932 0.0561 0.405 6.376 3.923 301.735 0.720 17.451 5.897 0.27 149903. 0.4044
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25.40 0.3956 0.6345 0.0891 0.0555 0.400 6.306 3.749 298.429 0.712 16.675 5.698 0.27 150246. 0.3819
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27.35 0.4260 0.6601 0.0846 0.0546 0.394 6.202 3.562 293.506 0.701 15.844 5.505 0.27 150608. 0.3596
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29.31 0.4565 0.6832 0.0799 0.0534 0.385 6.063 3.364 286.940 0.685 14.962 5.317 0.27 150990. 0.3376
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31.26 0.4869 0.7037 0.0750 0.0519 0.374 5.890 3.156 278.752 0.665 14.036 5.135 0.27 151390. 0.3158
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33.21 0.5173 0.7216 0.0698 0.0501 0.361 5.684 2.939 268.980 0.642 13.073 4.956 0.27 151810. 0.2941
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35.17 0.5477 0.7369 0.0645 0.0479 0.346 5.444 2.715 257.659 0.615 12.076 4.779 0.27 152248. 0.2726
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37.12 0.5782 0.7491 0.0590 0.0456 0.328 5.173 2.485 244.815 0.584 11.051 4.603 0.27 152706. 0.2512
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39.08 0.6086 0.7581 0.0534 0.0429 0.309 4.870 2.249 230.469 0.550 10.002 4.426 0.27 153182. 0.2297
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41.03 0.6390 0.7633 0.0477 0.0399 0.288 4.535 2.008 214.640 0.512 8.932 4.244 0.27 153677. 0.2082
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42.98 0.6695 0.7638 0.0419 0.0367 0.265 4.170 1.764 197.343 0.471 7.844 4.053 0.27 154191. 0.1863
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44.94 0.6999 0.7582 0.0360 0.0332 0.240 3.774 1.516 178.600 0.426 6.741 3.849 0.28 154724. 0.1640
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46.89 0.7303 0.7443 0.0300 0.0295 0.212 3.348 1.265 158.438 0.378 5.626 3.621 0.28 155275. 0.1410
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48.85 0.7608 0.7180 0.0240 0.0255 0.184 2.893 1.012 136.895 0.327 4.501 3.353 0.28 155845. 0.1168
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50.80 0.7912 0.6715 0.0180 0.0212 0.153 2.409 0.758 114.025 0.272 3.372 3.015 0.28 156433. 0.0909
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52.75 0.8216 0.5878 0.0120 0.0167 0.121 1.900 0.504 89.904 0.215 2.241 2.542 0.28 157039. 0.0624
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54.71 0.8520 0.4215 0.0059 0.0120 0.087 1.366 0.250 64.627 0.154 1.114 1.758 0.28 157663. 0.0304
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56.66 0.8825 -0.0056 0.0000 0.0071 0.051 0.807 -0.002 38.205 0.091 -0.008 -0.022 0.28 158286. 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 0.1227 0.0485 0.683 8.611 8.072 509.364 0.973 35.905 7.188 0.34 184008. 0.7069
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2.44 0.0305 0.0746 0.1215 0.0496 0.698 8.803 7.990 520.750 0.995 35.540 6.959 0.34 184174. 0.6810
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4.89 0.0609 0.1443 0.1201 0.0507 0.713 8.994 7.898 532.037 1.016 35.129 6.733 0.34 184358. 0.6550
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7.33 0.0914 0.2092 0.1185 0.0517 0.728 9.179 7.794 543.016 1.037 34.668 6.510 0.34 184561. 0.6292
|
|
9.78 0.1218 0.2697 0.1167 0.0527 0.742 9.356 7.678 553.466 1.057 34.152 6.292 0.34 184785. 0.6036
|
|
12.22 0.1523 0.3257 0.1148 0.0537 0.755 9.520 7.548 563.148 1.076 33.575 6.080 0.34 185029. 0.5782
|
|
14.66 0.1827 0.3775 0.1126 0.0545 0.767 9.666 7.404 571.807 1.092 32.933 5.873 0.34 185295. 0.5532
|
|
17.11 0.2132 0.4254 0.1101 0.0552 0.777 9.791 7.244 579.174 1.106 32.220 5.673 0.34 185584. 0.5285
|
|
19.55 0.2436 0.4696 0.1074 0.0557 0.784 9.889 7.067 584.972 1.117 31.433 5.479 0.34 185895. 0.5042
|
|
21.99 0.2741 0.5103 0.1045 0.0561 0.790 9.955 6.872 588.914 1.125 30.567 5.293 0.34 186230. 0.4803
|
|
24.44 0.3045 0.5478 0.1012 0.0563 0.792 9.986 6.659 590.706 1.128 29.618 5.113 0.34 186588. 0.4567
|
|
26.88 0.3350 0.5821 0.0977 0.0562 0.791 9.974 6.426 590.049 1.127 28.582 4.940 0.34 186970. 0.4334
|
|
29.33 0.3654 0.6136 0.0939 0.0559 0.787 9.917 6.173 586.647 1.120 27.457 4.773 0.34 187376. 0.4105
|
|
31.77 0.3959 0.6423 0.0897 0.0553 0.778 9.809 5.899 580.235 1.108 26.241 4.612 0.34 187806. 0.3877
|
|
34.21 0.4263 0.6684 0.0852 0.0544 0.765 9.646 5.606 570.619 1.090 24.937 4.456 0.34 188260. 0.3653
|
|
36.66 0.4568 0.6920 0.0805 0.0531 0.748 9.428 5.295 557.741 1.065 23.552 4.306 0.34 188738. 0.3430
|
|
39.10 0.4872 0.7131 0.0755 0.0516 0.726 9.156 4.968 541.645 1.034 22.097 4.160 0.34 189240. 0.3210
|
|
41.55 0.5177 0.7317 0.0704 0.0498 0.701 8.831 4.627 522.402 0.998 20.582 4.017 0.34 189765. 0.2992
|
|
43.99 0.5481 0.7477 0.0650 0.0476 0.671 8.454 4.275 500.081 0.955 19.015 3.877 0.34 190315. 0.2775
|
|
46.43 0.5786 0.7610 0.0595 0.0452 0.637 8.025 3.913 474.735 0.907 17.403 3.738 0.34 190887. 0.2560
|
|
48.88 0.6090 0.7711 0.0539 0.0425 0.599 7.546 3.542 446.405 0.853 15.753 3.599 0.34 191484. 0.2344
|
|
51.32 0.6395 0.7776 0.0481 0.0396 0.557 7.017 3.163 415.125 0.793 14.070 3.456 0.34 192104. 0.2128
|
|
53.76 0.6699 0.7797 0.0422 0.0363 0.511 6.439 2.778 380.929 0.728 12.358 3.308 0.34 192747. 0.1909
|
|
56.21 0.7004 0.7762 0.0363 0.0328 0.461 5.813 2.388 343.857 0.657 10.622 3.150 0.34 193414. 0.1685
|
|
58.65 0.7308 0.7649 0.0303 0.0290 0.408 5.138 1.993 303.964 0.581 8.867 2.975 0.35 194104. 0.1454
|
|
61.10 0.7613 0.7418 0.0243 0.0249 0.350 4.418 1.596 261.326 0.499 7.098 2.770 0.35 194817. 0.1211
|
|
63.54 0.7917 0.6994 0.0182 0.0206 0.290 3.652 1.196 216.051 0.413 5.320 2.511 0.35 195554. 0.0951
|
|
65.98 0.8222 0.6206 0.0121 0.0160 0.226 2.845 0.796 168.288 0.321 3.541 2.145 0.35 196312. 0.0663
|
|
68.43 0.8526 0.4572 0.0060 0.0113 0.159 1.999 0.397 118.229 0.226 1.767 1.524 0.35 197093. 0.0333
|
|
70.87 0.8831 0.0001 0.0000 0.0063 0.088 1.113 0.000 65.867 0.126 0.000 0.000 0.35 197870. 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 0.1234 0.0483 1.176 12.352 11.684 876.842 1.396 51.972 6.044 0.40 220797. 0.7152
|
|
2.94 0.0305 0.0753 0.1222 0.0495 1.203 12.635 11.569 896.948 1.428 51.458 5.850 0.40 220996. 0.6888
|
|
5.87 0.0610 0.1456 0.1208 0.0506 1.230 12.917 11.438 916.907 1.459 50.878 5.658 0.40 221217. 0.6625
|
|
8.81 0.0914 0.2112 0.1192 0.0516 1.256 13.190 11.292 936.339 1.490 50.225 5.470 0.40 221462. 0.6363
|
|
11.74 0.1219 0.2721 0.1175 0.0526 1.280 13.451 11.127 954.859 1.520 49.491 5.285 0.40 221731. 0.6103
|
|
14.68 0.1524 0.3285 0.1155 0.0536 1.304 13.693 10.942 972.039 1.547 48.668 5.106 0.40 222025. 0.5846
|
|
17.61 0.1829 0.3808 0.1134 0.0544 1.324 13.910 10.735 987.428 1.572 47.750 4.931 0.40 222345. 0.5593
|
|
20.55 0.2134 0.4290 0.1109 0.0552 1.342 14.095 10.505 1000.550 1.592 46.728 4.762 0.40 222692. 0.5343
|
|
23.48 0.2439 0.4735 0.1082 0.0557 1.356 14.241 10.251 1010.914 1.609 45.598 4.599 0.40 223067. 0.5098
|
|
26.42 0.2743 0.5146 0.1053 0.0561 1.365 14.341 9.971 1018.017 1.620 44.351 4.443 0.40 223470. 0.4856
|
|
29.36 0.3048 0.5523 0.1020 0.0563 1.370 14.388 9.663 1021.340 1.626 42.983 4.291 0.41 223901. 0.4618
|
|
32.29 0.3353 0.5870 0.0985 0.0563 1.368 14.374 9.327 1020.358 1.624 41.487 4.146 0.41 224361. 0.4383
|
|
35.23 0.3658 0.6187 0.0946 0.0559 1.361 14.292 8.961 1014.551 1.615 39.860 4.006 0.41 224850. 0.4152
|
|
38.16 0.3963 0.6478 0.0904 0.0553 1.346 14.136 8.566 1003.451 1.597 38.100 3.872 0.41 225367. 0.3923
|
|
41.10 0.4267 0.6742 0.0860 0.0544 1.323 13.900 8.141 986.716 1.570 36.210 3.742 0.41 225914. 0.3696
|
|
44.03 0.4572 0.6982 0.0812 0.0532 1.293 13.583 7.689 964.242 1.535 34.202 3.617 0.41 226489. 0.3472
|
|
46.97 0.4877 0.7198 0.0762 0.0516 1.255 13.187 7.215 936.104 1.490 32.091 3.496 0.41 227093. 0.3250
|
|
49.91 0.5182 0.7390 0.0710 0.0498 1.210 12.713 6.720 902.429 1.436 29.892 3.378 0.41 227725. 0.3031
|
|
52.84 0.5487 0.7556 0.0656 0.0476 1.158 12.162 6.209 863.337 1.374 27.617 3.262 0.41 228386. 0.2814
|
|
55.78 0.5791 0.7696 0.0600 0.0452 1.098 11.536 5.683 818.922 1.303 25.276 3.147 0.41 229075. 0.2597
|
|
58.71 0.6096 0.7806 0.0543 0.0424 1.032 10.837 5.144 769.258 1.224 22.878 3.033 0.41 229793. 0.2381
|
|
61.65 0.6401 0.7882 0.0485 0.0394 0.958 10.064 4.594 714.405 1.137 20.432 2.916 0.41 230539. 0.2164
|
|
64.58 0.6706 0.7916 0.0426 0.0361 0.878 9.219 4.034 654.422 1.042 17.944 2.796 0.41 231313. 0.1944
|
|
67.52 0.7011 0.7897 0.0366 0.0325 0.790 8.303 3.467 589.380 0.938 15.421 2.668 0.41 232115. 0.1720
|
|
70.45 0.7316 0.7804 0.0305 0.0286 0.696 7.316 2.893 519.374 0.827 12.869 2.527 0.41 232945. 0.1488
|
|
73.39 0.7620 0.7599 0.0244 0.0245 0.596 6.262 2.315 444.540 0.708 10.296 2.362 0.42 233802. 0.1244
|
|
76.33 0.7925 0.7207 0.0183 0.0201 0.490 5.143 1.734 365.069 0.581 7.711 2.154 0.42 234688. 0.0982
|
|
79.26 0.8230 0.6455 0.0122 0.0155 0.377 3.962 1.152 281.225 0.448 5.123 1.858 0.42 235600. 0.0690
|
|
82.20 0.8535 0.4836 0.0060 0.0107 0.259 2.724 0.572 193.348 0.308 2.544 1.342 0.42 236538. 0.0351
|
|
85.13 0.8840 -0.0106 -0.0001 0.0056 0.136 1.427 -0.006 101.311 0.161 -0.028 -0.028 0.42 237464. 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 0.1241 0.0484 1.869 16.825 16.000 1393.446 1.901 71.167 5.208 0.47 257579. 0.7211
|
|
3.45 0.0307 0.0762 0.1229 0.0495 1.913 17.223 15.846 1426.380 1.946 70.484 5.039 0.47 257813. 0.6944
|
|
6.90 0.0614 0.1474 0.1216 0.0507 1.957 17.618 15.672 1459.106 1.990 69.708 4.872 0.47 258073. 0.6676
|
|
10.35 0.0921 0.2137 0.1200 0.0518 1.999 18.003 15.474 1490.999 2.034 68.830 4.707 0.47 258361. 0.6410
|
|
13.81 0.1229 0.2752 0.1183 0.0528 2.040 18.370 15.251 1521.402 2.075 67.838 4.547 0.47 258678. 0.6147
|
|
17.26 0.1536 0.3322 0.1164 0.0538 2.078 18.711 15.000 1549.606 2.114 66.722 4.391 0.47 259025. 0.5887
|
|
20.71 0.1843 0.3848 0.1142 0.0547 2.112 19.016 14.719 1574.848 2.148 65.470 4.239 0.47 259404. 0.5630
|
|
24.16 0.2150 0.4335 0.1117 0.0554 2.141 19.275 14.405 1596.340 2.178 64.073 4.093 0.47 259814. 0.5377
|
|
27.61 0.2457 0.4784 0.1090 0.0560 2.163 19.480 14.056 1613.265 2.201 62.522 3.952 0.47 260257. 0.5129
|
|
31.06 0.2764 0.5197 0.1060 0.0564 2.179 19.619 13.670 1624.784 2.217 60.806 3.816 0.47 260734. 0.4884
|
|
34.51 0.3072 0.5577 0.1028 0.0566 2.186 19.682 13.246 1630.042 2.224 58.918 3.686 0.47 261244. 0.4644
|
|
37.96 0.3379 0.5926 0.0992 0.0565 2.183 19.660 12.781 1628.167 2.221 56.850 3.561 0.47 261789. 0.4406
|
|
41.42 0.3686 0.6246 0.0952 0.0562 2.170 19.541 12.275 1618.314 2.208 54.597 3.440 0.47 262368. 0.4172
|
|
44.87 0.3993 0.6539 0.0910 0.0555 2.145 19.316 11.726 1599.713 2.182 52.156 3.325 0.47 262981. 0.3941
|
|
48.32 0.4300 0.6807 0.0864 0.0546 2.108 18.979 11.136 1571.828 2.144 49.532 3.213 0.48 263628. 0.3712
|
|
51.77 0.4607 0.7050 0.0815 0.0533 2.058 18.529 10.509 1534.518 2.093 46.743 3.106 0.48 264309. 0.3486
|
|
55.22 0.4915 0.7269 0.0764 0.0517 1.995 17.966 9.850 1487.924 2.030 43.811 3.002 0.48 265024. 0.3262
|
|
58.67 0.5222 0.7464 0.0711 0.0497 1.921 17.294 9.163 1432.260 1.954 40.756 2.902 0.48 265772. 0.3040
|
|
62.12 0.5529 0.7634 0.0656 0.0475 1.834 16.515 8.452 1367.726 1.866 37.595 2.803 0.48 266555. 0.2821
|
|
65.58 0.5836 0.7778 0.0599 0.0449 1.736 15.630 7.721 1294.474 1.766 34.344 2.705 0.48 267371. 0.2602
|
|
69.03 0.6143 0.7892 0.0541 0.0421 1.626 14.642 6.973 1212.628 1.654 31.014 2.608 0.48 268220. 0.2384
|
|
72.48 0.6450 0.7973 0.0482 0.0390 1.505 13.551 6.209 1122.284 1.531 27.616 2.509 0.48 269103. 0.2164
|
|
75.93 0.6758 0.8012 0.0421 0.0355 1.373 12.359 5.432 1023.545 1.396 24.160 2.407 0.48 270019. 0.1942
|
|
79.38 0.7065 0.7998 0.0360 0.0318 1.229 11.067 4.644 916.531 1.250 20.656 2.298 0.48 270968. 0.1714
|
|
82.83 0.7372 0.7907 0.0298 0.0278 1.075 9.677 3.847 801.408 1.093 17.113 2.177 0.48 271950. 0.1478
|
|
86.28 0.7679 0.7699 0.0236 0.0236 0.910 8.192 3.044 678.414 0.925 13.541 2.035 0.48 272965. 0.1229
|
|
89.73 0.7986 0.7288 0.0174 0.0190 0.735 6.615 2.238 547.884 0.747 9.954 1.853 0.49 274013. 0.0959
|
|
93.19 0.8293 0.6464 0.0111 0.0142 0.550 4.954 1.431 410.278 0.560 6.366 1.582 0.49 275092. 0.0655
|
|
96.64 0.8601 0.4531 0.0049 0.0092 0.357 3.214 0.628 266.179 0.363 2.792 1.070 0.49 276201. 0.0293
|
|
100.09 0.8908
|
|
|
|
|
|
|
|
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 0.1250 0.0486 2.802 22.075 21.042 2089.370 2.494 93.597 4.568 0.54 294353. 0.7254
|
|
3.93 0.0306 0.0762 0.1238 0.0498 2.869 22.607 20.850 2139.708 2.554 92.743 4.420 0.54 294619. 0.6986
|
|
7.86 0.0612 0.1473 0.1225 0.0509 2.937 23.136 20.631 2189.809 2.614 91.768 4.273 0.54 294915. 0.6719
|
|
11.79 0.0918 0.2135 0.1211 0.0521 3.002 23.653 20.382 2238.723 2.672 90.659 4.129 0.54 295242. 0.6454
|
|
15.73 0.1225 0.2750 0.1194 0.0532 3.065 24.146 20.099 2285.442 2.728 89.401 3.989 0.54 295603. 0.6190
|
|
19.66 0.1531 0.3320 0.1175 0.0542 3.123 24.605 19.779 2328.875 2.780 87.978 3.852 0.54 295998. 0.5931
|
|
23.59 0.1837 0.3847 0.1153 0.0551 3.175 25.017 19.419 2367.864 2.826 86.376 3.720 0.54 296429. 0.5674
|
|
27.52 0.2143 0.4334 0.1129 0.0559 3.220 25.369 19.016 2401.194 2.866 84.581 3.592 0.54 296896. 0.5422
|
|
31.45 0.2449 0.4783 0.1103 0.0565 3.256 25.649 18.566 2427.632 2.898 82.581 3.469 0.54 297401. 0.5174
|
|
35.38 0.2755 0.5197 0.1073 0.0569 3.280 25.842 18.067 2445.909 2.920 80.363 3.350 0.54 297944. 0.4930
|
|
39.31 0.3062 0.5579 0.1040 0.0571 3.292 25.935 17.517 2454.740 2.930 77.916 3.237 0.54 298526. 0.4689
|
|
43.25 0.3368 0.5930 0.1005 0.0571 3.289 25.915 16.913 2452.812 2.928 75.230 3.128 0.54 299146. 0.4453
|
|
47.18 0.3674 0.6252 0.0965 0.0567 3.271 25.767 16.254 2438.846 2.911 72.298 3.023 0.54 299806. 0.4219
|
|
51.11 0.3980 0.6548 0.0923 0.0561 3.234 25.480 15.538 2411.682 2.879 69.115 2.922 0.54 300504. 0.3988
|
|
55.04 0.4286 0.6818 0.0877 0.0551 3.179 25.045 14.768 2370.482 2.830 65.688 2.826 0.54 301240. 0.3759
|
|
58.97 0.4592 0.7065 0.0828 0.0538 3.104 24.459 13.948 2314.993 2.763 62.040 2.733 0.54 302016. 0.3533
|
|
62.90 0.4899 0.7288 0.0777 0.0522 3.011 23.724 13.084 2245.417 2.680 58.199 2.643 0.54 302830. 0.3309
|
|
66.83 0.5205 0.7489 0.0724 0.0503 2.899 22.843 12.183 2162.088 2.581 54.191 2.556 0.55 303682. 0.3088
|
|
70.77 0.5511 0.7665 0.0668 0.0480 2.770 21.821 11.250 2065.320 2.465 50.042 2.471 0.55 304573. 0.2869
|
|
74.70 0.5817 0.7816 0.0611 0.0455 2.622 20.659 10.290 1955.359 2.334 45.770 2.387 0.55 305501. 0.2650
|
|
78.63 0.6123 0.7940 0.0553 0.0426 2.457 19.360 9.306 1832.392 2.187 41.392 2.303 0.55 306467. 0.2432
|
|
82.56 0.6429 0.8032 0.0493 0.0395 2.275 17.925 8.301 1696.582 2.025 36.922 2.219 0.55 307471. 0.2213
|
|
86.49 0.6736 0.8086 0.0432 0.0360 2.076 16.356 7.278 1548.075 1.848 32.373 2.132 0.55 308513. 0.1991
|
|
90.42 0.7042 0.8090 0.0371 0.0323 1.860 14.655 6.241 1387.052 1.656 27.758 2.041 0.55 309592. 0.1765
|
|
94.36 0.7348 0.8024 0.0308 0.0282 1.628 12.824 5.191 1213.755 1.449 23.089 1.940 0.55 310709. 0.1530
|
|
98.29 0.7654 0.7852 0.0245 0.0239 1.379 10.867 4.132 1028.530 1.228 18.380 1.822 0.55 311863. 0.1282
|
|
102.22 0.7960 0.7497 0.0182 0.0193 1.116 8.789 3.068 831.864 0.993 13.648 1.673 0.55 313053. 0.1014
|
|
106.15 0.8266 0.6771 0.0119 0.0145 0.837 6.597 2.003 624.433 0.745 8.910 1.455 0.56 314280. 0.0713
|
|
110.08 0.8572 0.5062 0.0056 0.0095 0.546 4.301 0.942 407.107 0.486 4.188 1.049 0.56 315540. 0.0352
|
|
114.01 0.8879
|
|
|
|
|
|
|
|
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 0.1260 0.0490 4.021 28.158 26.840 2998.297 3.181 119.384 4.060 0.61 331116. 0.7282
|
|
4.41 0.0305 0.0759 0.1249 0.0502 4.120 28.850 26.610 3071.989 3.259 118.363 3.929 0.61 331413. 0.7016
|
|
8.82 0.0610 0.1468 0.1236 0.0514 4.218 29.541 26.347 3145.507 3.337 117.191 3.799 0.61 331745. 0.6750
|
|
13.23 0.0915 0.2129 0.1222 0.0526 4.315 30.216 26.045 3217.442 3.414 115.848 3.672 0.61 332111. 0.6486
|
|
17.63 0.1221 0.2742 0.1206 0.0537 4.407 30.863 25.700 3286.312 3.487 114.314 3.547 0.61 332515. 0.6225
|
|
22.04 0.1526 0.3311 0.1188 0.0547 4.493 31.466 25.308 3350.501 3.555 112.569 3.426 0.61 332958. 0.5966
|
|
26.45 0.1831 0.3837 0.1167 0.0557 4.571 32.009 24.864 3408.302 3.616 110.593 3.309 0.61 333441. 0.5711
|
|
30.86 0.2136 0.4323 0.1143 0.0565 4.637 32.475 24.363 3457.929 3.669 108.368 3.196 0.61 333965. 0.5460
|
|
35.27 0.2441 0.4773 0.1117 0.0571 4.690 32.847 23.803 3497.581 3.711 105.877 3.087 0.61 334531. 0.5213
|
|
39.68 0.2746 0.5187 0.1088 0.0576 4.728 33.109 23.180 3525.418 3.741 103.104 2.982 0.61 335141. 0.4970
|
|
44.08 0.3052 0.5570 0.1055 0.0578 4.747 33.242 22.490 3539.587 3.756 100.036 2.882 0.61 335793. 0.4731
|
|
48.49 0.3357 0.5922 0.1020 0.0578 4.745 33.229 21.731 3538.207 3.754 96.658 2.786 0.61 336489. 0.4495
|
|
52.90 0.3662 0.6246 0.0981 0.0575 4.720 33.052 20.899 3519.432 3.734 92.960 2.693 0.61 337228. 0.4262
|
|
57.31 0.3967 0.6545 0.0938 0.0569 4.669 32.697 19.995 3481.579 3.694 88.938 2.605 0.61 338011. 0.4032
|
|
61.72 0.4272 0.6818 0.0893 0.0559 4.591 32.150 19.020 3423.404 3.632 84.599 2.520 0.61 338838. 0.3804
|
|
66.13 0.4577 0.7068 0.0844 0.0546 4.485 31.409 17.979 3344.490 3.549 79.970 2.438 0.61 339707. 0.3579
|
|
70.53 0.4882 0.7296 0.0792 0.0530 4.352 30.476 16.881 3245.106 3.443 75.086 2.359 0.61 340620. 0.3356
|
|
74.94 0.5188 0.7501 0.0738 0.0511 4.192 29.355 15.734 3125.761 3.317 69.985 2.283 0.61 341575. 0.3135
|
|
79.35 0.5493 0.7683 0.0683 0.0488 4.006 28.051 14.545 2986.935 3.169 64.697 2.209 0.61 342573. 0.2916
|
|
83.76 0.5798 0.7842 0.0625 0.0462 3.794 26.568 13.320 2829.002 3.002 59.247 2.136 0.62 343613. 0.2698
|
|
88.17 0.6103 0.7974 0.0566 0.0433 3.557 24.908 12.063 2652.260 2.814 53.658 2.063 0.62 344695. 0.2480
|
|
92.58 0.6408 0.8076 0.0506 0.0401 3.295 23.074 10.779 2456.940 2.607 47.947 1.990 0.62 345820. 0.2262
|
|
96.98 0.6713 0.8143 0.0445 0.0366 3.008 21.067 9.472 2243.271 2.380 42.132 1.915 0.62 346986. 0.2040
|
|
101.39 0.7019 0.8163 0.0382 0.0329 2.697 18.891 8.145 2011.505 2.134 36.227 1.837 0.62 348194. 0.1814
|
|
105.80 0.7324 0.8120 0.0319 0.0288 2.363 16.547 6.801 1761.979 1.870 30.251 1.751 0.62 349444. 0.1580
|
|
110.21 0.7629 0.7981 0.0256 0.0244 2.005 14.042 5.445 1495.171 1.586 24.219 1.652 0.62 350736. 0.1334
|
|
114.62 0.7934 0.7676 0.0192 0.0198 1.625 11.380 4.081 1211.759 1.286 18.152 1.528 0.62 352068. 0.1068
|
|
119.03 0.8239 0.7039 0.0127 0.0149 1.224 8.571 2.714 912.689 0.968 12.074 1.349 0.63 353440. 0.0769
|
|
123.43 0.8544 0.5536 0.0063 0.0098 0.804 5.627 1.351 599.200 0.636 6.011 1.023 0.63 354851. 0.0412
|
|
127.84 0.8849 -0.0116 -0.0001 0.0044 0.362 2.536 -0.012 270.086 0.287 -0.055 -0.021 0.63 356218. 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 0.1270 0.0497 5.591 35.242 33.422 4169.511 3.982 148.660 3.636 0.67 367867. 0.7276
|
|
4.90 0.0305 0.0756 0.1260 0.0509 5.729 36.112 33.158 4272.457 4.080 147.489 3.520 0.67 368197. 0.7017
|
|
9.80 0.0611 0.1463 0.1249 0.0521 5.868 36.983 32.853 4375.537 4.178 146.132 3.406 0.67 368564. 0.6757
|
|
14.70 0.0916 0.2122 0.1235 0.0533 6.003 37.839 32.501 4476.800 4.275 144.562 3.293 0.67 368970. 0.6498
|
|
19.60 0.1221 0.2735 0.1220 0.0545 6.134 38.662 32.094 4574.140 4.368 142.753 3.182 0.67 369419. 0.6241
|
|
24.50 0.1526 0.3303 0.1202 0.0556 6.256 39.432 31.627 4665.241 4.455 140.675 3.075 0.67 369911. 0.5986
|
|
29.40 0.1832 0.3829 0.1182 0.0565 6.367 40.128 31.093 4747.632 4.534 138.304 2.971 0.67 370449. 0.5734
|
|
34.30 0.2137 0.4315 0.1159 0.0574 6.462 40.729 30.488 4818.738 4.602 135.613 2.870 0.67 371032. 0.5485
|
|
39.20 0.2442 0.4765 0.1133 0.0581 6.539 41.212 29.807 4875.918 4.656 132.581 2.773 0.67 371664. 0.5240
|
|
44.10 0.2748 0.5180 0.1104 0.0586 6.593 41.555 29.044 4916.501 4.695 129.187 2.679 0.67 372343. 0.4999
|
|
49.00 0.3053 0.5564 0.1072 0.0588 6.622 41.735 28.196 4937.789 4.715 125.414 2.590 0.68 373070. 0.4761
|
|
53.90 0.3358 0.5918 0.1036 0.0588 6.621 41.730 27.258 4937.094 4.715 121.244 2.504 0.68 373846. 0.4526
|
|
58.80 0.3663 0.6244 0.0997 0.0585 6.587 41.516 26.229 4911.783 4.690 116.665 2.422 0.68 374671. 0.4294
|
|
63.70 0.3969 0.6544 0.0954 0.0579 6.517 41.074 25.106 4859.495 4.640 111.670 2.343 0.68 375544. 0.4064
|
|
68.60 0.4274 0.6820 0.0908 0.0569 6.408 40.389 23.891 4778.448 4.563 106.267 2.268 0.68 376466. 0.3837
|
|
73.50 0.4579 0.7074 0.0859 0.0556 6.260 39.455 22.592 4668.039 4.458 100.490 2.195 0.68 377436. 0.3612
|
|
78.40 0.4884 0.7305 0.0807 0.0539 6.073 38.277 21.220 4528.668 4.325 94.385 2.125 0.68 378453. 0.3389
|
|
83.30 0.5190 0.7514 0.0752 0.0519 5.848 36.861 19.784 4361.100 4.165 88.000 2.058 0.68 379518. 0.3168
|
|
88.20 0.5495 0.7702 0.0695 0.0496 5.587 35.212 18.294 4166.052 3.978 81.373 1.992 0.68 380630. 0.2949
|
|
93.10 0.5800 0.7866 0.0637 0.0470 5.289 33.336 16.758 3944.095 3.766 74.538 1.927 0.68 381789. 0.2731
|
|
98.00 0.6106 0.8005 0.0577 0.0440 4.956 31.237 15.181 3695.665 3.529 67.523 1.863 0.68 382994. 0.2513
|
|
102.90 0.6411 0.8115 0.0516 0.0407 4.588 28.916 13.568 3421.102 3.267 60.350 1.799 0.69 384247. 0.2294
|
|
107.80 0.6716 0.8191 0.0453 0.0372 4.185 26.377 11.925 3120.736 2.980 53.042 1.733 0.69 385545. 0.2072
|
|
112.70 0.7021 0.8223 0.0390 0.0333 3.748 23.623 10.256 2794.935 2.669 45.617 1.664 0.69 386890. 0.1845
|
|
117.61 0.7327 0.8195 0.0326 0.0291 3.278 20.659 8.565 2444.164 2.334 38.097 1.589 0.69 388282. 0.1610
|
|
122.51 0.7632 0.8074 0.0261 0.0246 2.775 17.488 6.858 2069.091 1.976 30.504 1.503 0.69 389718. 0.1363
|
|
127.41 0.7937 0.7794 0.0195 0.0199 2.240 14.121 5.140 1670.701 1.595 22.862 1.395 0.69 391201. 0.1095
|
|
132.31 0.8243 0.7190 0.0130 0.0149 1.677 10.569 3.418 1250.445 1.194 15.201 1.240 0.70 392728. 0.0793
|
|
137.21 0.8548 0.5720 0.0065 0.0097 1.087 6.849 1.699 810.276 0.774 7.556 0.951 0.70 394296. 0.0429
|
|
142.11 0.8853 -0.0196 -0.0001 0.0041 0.467 2.943 -0.024 348.234 0.333 -0.108 -0.031 0.70 395801. 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 0.1282 0.0515 7.718 44.222 40.807 5755.158 4.996 181.507 3.216 0.74 404606. 0.7112
|
|
5.39 0.0305 0.0738 0.1273 0.0527 7.897 45.250 40.520 5888.913 5.112 180.232 3.121 0.74 404965. 0.6877
|
|
10.78 0.0611 0.1430 0.1262 0.0539 8.076 46.276 40.183 6022.517 5.228 178.735 3.026 0.74 405367. 0.6641
|
|
16.17 0.0916 0.2079 0.1250 0.0551 8.252 47.281 39.789 6153.327 5.342 176.981 2.933 0.74 405813. 0.6404
|
|
21.56 0.1221 0.2686 0.1236 0.0562 8.420 48.244 39.329 6278.580 5.451 174.934 2.841 0.74 406305. 0.6168
|
|
26.95 0.1527 0.3251 0.1219 0.0572 8.576 49.140 38.794 6395.242 5.552 172.555 2.751 0.74 406846. 0.5932
|
|
32.35 0.1832 0.3777 0.1199 0.0582 8.717 49.946 38.176 6500.084 5.643 169.808 2.664 0.74 407437. 0.5698
|
|
37.74 0.2137 0.4266 0.1177 0.0590 8.837 50.635 37.468 6589.792 5.721 166.660 2.579 0.74 408081. 0.5465
|
|
43.13 0.2443 0.4720 0.1152 0.0596 8.933 51.182 36.663 6660.971 5.783 163.078 2.497 0.74 408776. 0.5233
|
|
48.52 0.2748 0.5141 0.1123 0.0600 8.999 51.560 35.755 6710.233 5.825 159.037 2.417 0.74 409526. 0.5003
|
|
53.91 0.3053 0.5530 0.1091 0.0603 9.031 51.744 34.738 6734.125 5.846 154.513 2.340 0.74 410329. 0.4774
|
|
59.30 0.3358 0.5889 0.1056 0.0602 9.024 51.706 33.607 6729.125 5.842 149.485 2.265 0.74 411186. 0.4546
|
|
64.69 0.3664 0.6221 0.1017 0.0599 8.974 51.418 32.360 6691.683 5.809 143.939 2.193 0.74 412097. 0.4319
|
|
70.08 0.3969 0.6526 0.0974 0.0592 8.875 50.855 30.995 6618.429 5.746 137.866 2.124 0.75 413061. 0.4094
|
|
75.47 0.4274 0.6807 0.0927 0.0582 8.726 49.996 29.513 6506.649 5.649 131.274 2.057 0.75 414079. 0.3869
|
|
80.86 0.4580 0.7065 0.0877 0.0569 8.522 48.832 27.924 6355.181 5.517 124.205 1.993 0.75 415149. 0.3646
|
|
86.25 0.4885 0.7301 0.0824 0.0552 8.266 47.366 26.240 6164.327 5.351 116.717 1.931 0.75 416272. 0.3424
|
|
91.64 0.5190 0.7515 0.0769 0.0531 7.959 45.603 24.476 5934.957 5.152 108.869 1.871 0.75 417447. 0.3203
|
|
97.04 0.5496 0.7708 0.0711 0.0507 7.601 43.552 22.643 5667.951 4.920 100.714 1.812 0.75 418674. 0.2985
|
|
102.43 0.5801 0.7878 0.0652 0.0480 7.193 41.217 20.750 5364.085 4.657 92.294 1.755 0.75 419953. 0.2767
|
|
107.82 0.6106 0.8024 0.0591 0.0450 6.737 38.604 18.804 5023.975 4.361 83.642 1.698 0.75 421282. 0.2548
|
|
113.21 0.6412 0.8143 0.0528 0.0416 6.233 35.715 16.814 4648.108 4.035 74.789 1.641 0.75 422663. 0.2329
|
|
118.60 0.6717 0.8229 0.0464 0.0379 5.682 32.557 14.784 4237.051 3.678 65.760 1.583 0.76 424094. 0.2107
|
|
123.99 0.7022 0.8272 0.0400 0.0339 5.085 29.133 12.721 3791.517 3.291 56.581 1.522 0.76 425576. 0.1879
|
|
129.38 0.7328 0.8255 0.0334 0.0296 4.442 25.453 10.629 3312.473 2.876 47.276 1.455 0.76 427109. 0.1642
|
|
134.77 0.7633 0.8145 0.0267 0.0251 3.757 21.525 8.514 2801.343 2.432 37.872 1.379 0.76 428691. 0.1392
|
|
140.16 0.7938 0.7873 0.0201 0.0202 3.031 17.367 6.385 2260.184 1.962 28.398 1.281 0.76 430323. 0.1121
|
|
145.55 0.8244 0.7265 0.0133 0.0151 2.269 13.000 4.247 1691.867 1.469 18.891 1.139 0.76 432004. 0.0812
|
|
150.94 0.8549 0.5760 0.0066 0.0098 1.475 8.453 2.111 1100.163 0.955 9.391 0.870 0.77 433731. 0.0438
|
|
156.33 0.8854 -0.0215 -0.0001 0.0043 0.648 3.714 -0.033 483.298 0.420 -0.149 -0.031 0.77 435379. 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 0.1293 0.0561 10.910 57.305 48.982 8135.844 6.474 217.870 2.731 0.81 441329. 0.6616
|
|
5.88 0.0305 0.0686 0.1285 0.0572 11.132 58.467 48.687 8300.775 6.606 216.561 2.660 0.81 441717. 0.6426
|
|
11.76 0.0611 0.1336 0.1276 0.0583 11.349 59.611 48.337 8463.260 6.735 215.002 2.590 0.81 442151. 0.6235
|
|
17.64 0.0916 0.1950 0.1265 0.0594 11.559 60.711 47.919 8619.350 6.859 213.146 2.522 0.81 442634. 0.6043
|
|
23.52 0.1221 0.2531 0.1252 0.0604 11.754 61.737 47.424 8765.009 6.975 210.942 2.454 0.81 443169. 0.5850
|
|
29.41 0.1527 0.3079 0.1236 0.0613 11.930 62.660 46.839 8896.124 7.079 208.338 2.388 0.81 443758. 0.5658
|
|
35.29 0.1832 0.3595 0.1218 0.0621 12.081 63.452 46.152 9008.587 7.169 205.285 2.324 0.81 444402. 0.5465
|
|
41.17 0.2137 0.4081 0.1197 0.0627 12.201 64.084 45.354 9098.340 7.240 201.733 2.261 0.81 445104. 0.5271
|
|
47.05 0.2443 0.4537 0.1173 0.0631 12.286 64.529 44.434 9161.402 7.290 197.641 2.200 0.81 445864. 0.5076
|
|
52.93 0.2748 0.4966 0.1145 0.0634 12.329 64.758 43.384 9193.993 7.316 192.971 2.140 0.81 446684. 0.4880
|
|
58.81 0.3053 0.5368 0.1114 0.0634 12.327 64.747 42.197 9192.466 7.315 187.691 2.082 0.81 447563. 0.4682
|
|
64.69 0.3359 0.5743 0.1079 0.0631 12.275 64.471 40.867 9153.190 7.284 181.776 2.025 0.81 448502. 0.4481
|
|
70.57 0.3664 0.6093 0.1040 0.0625 12.166 63.902 39.390 9072.396 7.220 175.205 1.969 0.81 449500. 0.4278
|
|
76.45 0.3969 0.6417 0.0997 0.0617 11.997 63.015 37.763 8946.433 7.119 167.969 1.915 0.81 450557. 0.4073
|
|
82.34 0.4275 0.6717 0.0950 0.0605 11.764 61.787 35.989 8772.196 6.981 160.079 1.861 0.81 451672. 0.3864
|
|
88.22 0.4580 0.6993 0.0900 0.0589 11.463 60.210 34.079 8548.239 6.802 151.581 1.808 0.82 452846. 0.3654
|
|
94.10 0.4885 0.7246 0.0846 0.0570 11.097 58.285 32.048 8274.944 6.585 142.548 1.757 0.82 454076. 0.3442
|
|
99.98 0.5191 0.7477 0.0790 0.0548 10.666 56.021 29.913 7953.510 6.329 133.053 1.706 0.82 455363. 0.3230
|
|
105.86 0.5496 0.7684 0.0731 0.0523 10.172 53.425 27.690 7585.035 6.036 123.165 1.656 0.82 456706. 0.3016
|
|
111.74 0.5801 0.7868 0.0670 0.0494 9.615 50.504 25.390 7170.206 5.706 112.936 1.606 0.82 458105. 0.2802
|
|
117.62 0.6107 0.8025 0.0608 0.0462 8.998 47.263 23.024 6710.174 5.340 102.413 1.556 0.82 459560. 0.2585
|
|
123.50 0.6412 0.8151 0.0544 0.0428 8.323 43.716 20.600 6206.490 4.939 91.628 1.505 0.82 461070. 0.2365
|
|
129.39 0.6717 0.8239 0.0478 0.0390 7.590 39.865 18.124 5659.767 4.504 80.616 1.452 0.83 462635. 0.2140
|
|
135.27 0.7023 0.8277 0.0412 0.0349 6.800 35.716 15.604 5070.711 4.035 69.406 1.396 0.83 464255. 0.1909
|
|
141.15 0.7328 0.8243 0.0344 0.0306 5.957 31.286 13.046 4441.867 3.535 58.028 1.332 0.83 465930. 0.1666
|
|
147.03 0.7633 0.8094 0.0276 0.0260 5.065 26.603 10.457 3776.942 3.006 46.514 1.256 0.83 467659. 0.1406
|
|
152.91 0.7939 0.7744 0.0207 0.0212 4.131 21.698 7.846 3080.509 2.451 34.898 1.155 0.83 469441. 0.1120
|
|
158.79 0.8244 0.6990 0.0138 0.0163 3.163 16.612 5.221 2358.500 1.877 23.224 1.004 0.83 471277. 0.0794
|
|
164.67 0.8549 0.5250 0.0068 0.0112 2.170 11.397 2.594 1618.073 1.288 11.540 0.727 0.84 473162. 0.0406
|
|
170.55 0.8854 -0.0165 -0.0001 0.0059 1.153 6.055 -0.042 859.605 0.684 -0.186 -0.022 0.84 474986. 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 0.1298 0.0643 15.912 77.147 57.707 11865.549 8.716 256.680 2.206 0.87 478061. 0.5801
|
|
6.42 0.0308 0.0607 0.1292 0.0655 16.196 78.522 57.424 12077.031 8.871 255.424 2.157 0.87 478478. 0.5657
|
|
12.85 0.0616 0.1187 0.1284 0.0666 16.472 79.862 57.084 12283.166 9.023 253.912 2.108 0.87 478945. 0.5513
|
|
19.27 0.0923 0.1740 0.1275 0.0676 16.732 81.121 56.672 12476.827 9.165 252.079 2.060 0.87 479466. 0.5369
|
|
25.69 0.1231 0.2268 0.1263 0.0686 16.965 82.250 56.172 12650.451 9.293 249.854 2.014 0.87 480045. 0.5225
|
|
32.12 0.1539 0.2773 0.1250 0.0694 17.159 83.195 55.566 12795.794 9.399 247.159 1.970 0.88 480684. 0.5083
|
|
38.54 0.1847 0.3256 0.1233 0.0700 17.307 83.910 54.838 12905.770 9.480 243.919 1.927 0.88 481386. 0.4940
|
|
44.96 0.2155 0.3719 0.1214 0.0703 17.400 84.359 53.972 12974.836 9.531 240.067 1.887 0.88 482153. 0.4798
|
|
51.38 0.2463 0.4163 0.1191 0.0705 17.430 84.509 52.954 12997.866 9.548 235.539 1.848 0.88 482986. 0.4655
|
|
57.81 0.2770 0.4588 0.1164 0.0703 17.394 84.334 51.772 12971.024 9.528 230.280 1.810 0.88 483886. 0.4509
|
|
64.23 0.3078 0.4995 0.1134 0.0699 17.288 83.816 50.415 12891.322 9.469 224.246 1.774 0.88 484853. 0.4360
|
|
70.65 0.3386 0.5383 0.1099 0.0691 17.106 82.937 48.876 12756.161 9.370 217.400 1.738 0.88 485887. 0.4206
|
|
77.08 0.3694 0.5752 0.1060 0.0681 16.847 81.680 47.148 12562.784 9.228 209.715 1.702 0.88 486988. 0.4046
|
|
83.50 0.4002 0.6101 0.1017 0.0667 16.506 80.024 45.228 12308.187 9.041 201.174 1.667 0.88 488154. 0.3880
|
|
89.92 0.4309 0.6430 0.0970 0.0650 16.079 77.957 43.119 11990.143 8.807 191.792 1.631 0.88 489385. 0.3708
|
|
96.35 0.4617 0.6739 0.0918 0.0629 15.568 75.479 40.834 11609.063 8.528 181.629 1.595 0.88 490680. 0.3529
|
|
102.77 0.4925 0.7026 0.0864 0.0605 14.976 72.608 38.395 11167.470 8.203 170.780 1.559 0.88 492038. 0.3345
|
|
109.19 0.5233 0.7291 0.0806 0.0578 14.307 69.364 35.823 10668.530 7.837 159.343 1.523 0.89 493458. 0.3156
|
|
115.62 0.5541 0.7532 0.0745 0.0548 13.564 65.761 33.139 10114.425 7.430 147.401 1.486 0.89 494940. 0.2961
|
|
122.04 0.5848 0.7749 0.0683 0.0515 12.748 61.805 30.355 9506.005 6.983 135.020 1.448 0.89 496484. 0.2762
|
|
128.46 0.6156 0.7939 0.0618 0.0479 11.860 57.500 27.486 8843.756 6.496 122.256 1.410 0.89 498088. 0.2558
|
|
134.89 0.6464 0.8084 0.0552 0.0441 10.918 52.935 24.539 8141.743 5.981 109.148 1.367 0.89 499753. 0.2344
|
|
141.31 0.6772 0.8158 0.0484 0.0402 9.940 48.194 21.522 7412.552 5.445 95.729 1.317 0.89 501478. 0.2115
|
|
147.73 0.7080 0.8131 0.0415 0.0361 8.936 43.322 18.442 6663.209 4.895 82.032 1.255 0.90 503262. 0.1866
|
|
154.15 0.7388 0.7986 0.0344 0.0319 7.883 38.218 15.314 5878.117 4.318 68.115 1.182 0.90 505106. 0.1601
|
|
160.58 0.7695 0.7657 0.0273 0.0275 6.792 32.929 12.145 5064.716 3.720 54.022 1.088 0.90 507009. 0.1312
|
|
167.00 0.8003 0.7021 0.0201 0.0229 5.676 27.520 8.949 4232.725 3.109 39.806 0.959 0.90 508970. 0.0993
|
|
173.42 0.8311 0.5836 0.0129 0.0184 4.550 22.060 5.742 3392.871 2.492 25.540 0.768 0.90 510989. 0.0637
|
|
179.85 0.8619 0.3556 0.0057 0.0139 3.428 16.619 2.542 2556.109 1.878 11.307 0.451 0.91 513061. 0.0249
|
|
186.27 0.8927
|
|
|
|
|
|
|
|
PROP RPM = 14000
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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 0.1275 0.0721 22.275 100.283 65.759 16610.484 11.330 292.495 1.796 0.94 514955. 0.5041
|
|
6.92 0.0308 0.0534 0.1270 0.0732 22.619 101.830 65.488 16866.721 11.505 291.293 1.761 0.94 515395. 0.4933
|
|
13.83 0.0615 0.1047 0.1264 0.0743 22.963 103.381 65.168 17123.689 11.680 289.868 1.726 0.94 515887. 0.4824
|
|
20.75 0.0923 0.1538 0.1256 0.0754 23.298 104.890 64.783 17373.670 11.850 288.157 1.691 0.94 516436. 0.4712
|
|
27.66 0.1231 0.2009 0.1247 0.0764 23.615 106.315 64.320 17609.697 12.011 286.095 1.657 0.94 517045. 0.4599
|
|
34.58 0.1539 0.2460 0.1237 0.0774 23.900 107.599 63.760 17822.246 12.156 283.602 1.623 0.94 517716. 0.4485
|
|
41.49 0.1846 0.2891 0.1223 0.0781 24.140 108.677 63.083 18000.867 12.278 280.591 1.589 0.94 518454. 0.4370
|
|
48.41 0.2154 0.3305 0.1208 0.0787 24.319 109.484 62.268 18134.600 12.369 276.969 1.557 0.94 519261. 0.4254
|
|
55.33 0.2462 0.3703 0.1189 0.0790 24.423 109.953 61.295 18212.211 12.422 272.642 1.527 0.94 520139. 0.4137
|
|
62.24 0.2770 0.4085 0.1166 0.0791 24.436 110.014 60.143 18222.275 12.429 267.516 1.497 0.94 521090. 0.4019
|
|
69.16 0.3077 0.4454 0.1140 0.0788 24.344 109.596 58.790 18153.129 12.382 261.498 1.469 0.95 522115. 0.3899
|
|
76.07 0.3385 0.4810 0.1110 0.0781 24.129 108.631 57.217 17993.184 12.273 254.500 1.442 0.95 523215. 0.3777
|
|
82.99 0.3693 0.5156 0.1075 0.0770 23.779 107.056 55.406 17732.369 12.095 246.444 1.417 0.95 524389. 0.3652
|
|
89.90 0.4001 0.5492 0.1035 0.0754 23.286 104.835 53.345 17364.496 11.844 237.280 1.393 0.95 525638. 0.3523
|
|
96.82 0.4308 0.5818 0.0990 0.0733 22.648 101.961 51.035 16888.406 11.519 227.004 1.371 0.95 526959. 0.3390
|
|
103.74 0.4616 0.6133 0.0940 0.0708 21.870 98.458 48.489 16308.311 11.124 215.677 1.349 0.95 528353. 0.3251
|
|
110.65 0.4924 0.6436 0.0887 0.0679 20.964 94.381 45.731 15632.901 10.663 203.412 1.327 0.95 529817. 0.3106
|
|
117.57 0.5232 0.6726 0.0830 0.0646 19.944 89.790 42.790 14872.577 10.144 190.331 1.305 0.95 531349. 0.2955
|
|
124.48 0.5539 0.6999 0.0770 0.0609 18.824 84.745 39.692 14036.791 9.574 176.550 1.283 0.96 532950. 0.2797
|
|
131.40 0.5847 0.7254 0.0707 0.0570 17.610 79.281 36.457 13131.832 8.957 162.163 1.259 0.96 534617. 0.2632
|
|
138.32 0.6155 0.7486 0.0642 0.0528 16.309 73.424 33.104 12161.697 8.295 147.245 1.235 0.96 536350. 0.2459
|
|
145.23 0.6463 0.7690 0.0575 0.0483 14.931 67.220 29.647 11134.053 7.594 131.871 1.208 0.96 538148. 0.2276
|
|
152.15 0.6770 0.7817 0.0506 0.0438 13.544 60.973 26.096 10099.433 6.889 116.075 1.172 0.96 540011. 0.2072
|
|
159.06 0.7078 0.7731 0.0435 0.0398 12.309 55.417 22.437 9179.132 6.261 99.798 1.109 0.96 541938. 0.1818
|
|
165.98 0.7386 0.7429 0.0363 0.0361 11.140 50.150 18.699 8306.745 5.666 83.175 1.021 0.97 543927. 0.1528
|
|
172.89 0.7694 0.6901 0.0289 0.0323 9.967 44.871 14.919 7432.205 5.069 66.360 0.910 0.97 545979. 0.1217
|
|
179.81 0.8001 0.6058 0.0216 0.0285 8.805 39.641 11.125 6566.047 4.479 49.485 0.769 0.97 548094. 0.0887
|
|
186.73 0.8309 0.4775 0.0143 0.0248 7.670 34.531 7.356 5719.659 3.901 32.720 0.583 0.97 550269. 0.0548
|
|
193.64 0.8617 0.2872 0.0071 0.0213 6.570 29.580 3.655 4899.558 3.342 16.256 0.338 0.98 552503. 0.0224
|
|
200.56 0.8925 0.0021 0.0000 0.0178 5.492 24.726 0.022 4095.508 2.794 0.096 0.002 0.98 554778. 0.0000
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