apc_calc/data/PERFILES2/PER3_16x8E.dat

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102 KiB
Plaintext

16x8E (16x8E.dat)
v2022-0915
Simulation Date: 09/22/2022
AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
====== PERFORMANCE DATA (versus advance ratio and MPH) ======
DEFINITIONS:
J=V/nD (advance ratio)
Ct=T/(rho * n**2 * D**4) (thrust coef.)
Cp=P/(rho * n**3 * D**5) (power coef.)
Pe=Ct*J/Cp (efficiency)
V (model speed in MPH)
Mach (at prop tip)
Reyn (at 75% of span)
FOM (Figure of Merit)
PROP RPM = 1000
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 0.0843 0.0330 0.003 0.176 0.176 2.079 0.020 0.783 38.388 0.06 23826. 0.5905
0.33 0.0220 0.0548 0.0829 0.0333 0.003 0.177 0.173 2.096 0.020 0.770 37.461 0.06 23840. 0.5715
0.67 0.0440 0.1069 0.0814 0.0335 0.003 0.178 0.170 2.110 0.020 0.756 36.531 0.06 23855. 0.5523
1.00 0.0661 0.1562 0.0798 0.0337 0.003 0.179 0.167 2.123 0.020 0.741 35.600 0.06 23871. 0.5330
1.33 0.0881 0.2029 0.0781 0.0339 0.003 0.180 0.163 2.134 0.020 0.726 34.669 0.06 23889. 0.5135
1.67 0.1101 0.2468 0.0763 0.0340 0.003 0.181 0.159 2.142 0.020 0.709 33.740 0.06 23908. 0.4939
2.00 0.1321 0.2880 0.0744 0.0341 0.003 0.181 0.155 2.147 0.020 0.691 32.814 0.06 23928. 0.4742
2.34 0.1542 0.3266 0.0723 0.0341 0.003 0.182 0.151 2.148 0.021 0.672 31.890 0.06 23949. 0.4545
2.67 0.1762 0.3624 0.0701 0.0341 0.003 0.181 0.146 2.145 0.020 0.651 30.969 0.06 23972. 0.4346
3.00 0.1982 0.3956 0.0678 0.0340 0.003 0.181 0.142 2.138 0.020 0.630 30.050 0.06 23997. 0.4147
3.34 0.2202 0.4261 0.0654 0.0338 0.003 0.180 0.136 2.125 0.020 0.607 29.131 0.06 24023. 0.3947
3.67 0.2423 0.4539 0.0628 0.0335 0.003 0.178 0.131 2.108 0.020 0.583 28.210 0.06 24050. 0.3746
4.00 0.2643 0.4790 0.0601 0.0331 0.003 0.176 0.125 2.085 0.020 0.558 27.285 0.06 24079. 0.3544
4.34 0.2863 0.5011 0.0572 0.0327 0.003 0.174 0.119 2.056 0.020 0.531 26.351 0.06 24109. 0.3340
4.67 0.3083 0.5203 0.0542 0.0321 0.003 0.171 0.113 2.022 0.019 0.504 25.404 0.06 24141. 0.3135
5.01 0.3303 0.5363 0.0511 0.0315 0.003 0.167 0.107 1.981 0.019 0.475 24.439 0.06 24175. 0.2928
5.34 0.3524 0.5488 0.0479 0.0307 0.003 0.163 0.100 1.933 0.018 0.445 23.448 0.06 24210. 0.2719
5.67 0.3744 0.5576 0.0445 0.0299 0.003 0.159 0.093 1.880 0.018 0.413 22.423 0.06 24247. 0.2507
6.01 0.3964 0.5623 0.0410 0.0289 0.002 0.154 0.086 1.820 0.017 0.381 21.355 0.06 24285. 0.2292
6.34 0.4184 0.5624 0.0375 0.0279 0.002 0.148 0.078 1.754 0.017 0.348 20.233 0.06 24325. 0.2076
6.67 0.4405 0.5572 0.0338 0.0267 0.002 0.142 0.071 1.683 0.016 0.314 19.044 0.06 24367. 0.1856
7.01 0.4625 0.5459 0.0301 0.0255 0.002 0.136 0.063 1.606 0.015 0.280 17.770 0.06 24410. 0.1635
7.34 0.4845 0.5275 0.0264 0.0242 0.002 0.129 0.055 1.524 0.015 0.245 16.391 0.06 24455. 0.1410
7.67 0.5065 0.5006 0.0226 0.0228 0.002 0.121 0.047 1.436 0.014 0.210 14.880 0.06 24502. 0.1185
8.01 0.5286 0.4635 0.0187 0.0214 0.002 0.114 0.039 1.345 0.013 0.174 13.201 0.06 24550. 0.0958
8.34 0.5506 0.4135 0.0149 0.0198 0.002 0.105 0.031 1.248 0.012 0.138 11.307 0.06 24600. 0.0731
8.68 0.5726 0.3474 0.0111 0.0182 0.002 0.097 0.023 1.148 0.011 0.103 9.134 0.06 24652. 0.0509
9.01 0.5946 0.2604 0.0073 0.0166 0.001 0.088 0.015 1.044 0.010 0.067 6.593 0.06 24705. 0.0298
9.34 0.6166 0.1455 0.0035 0.0149 0.001 0.079 0.007 0.937 0.009 0.033 3.551 0.06 24760. 0.0112
9.68 0.6387 -0.0083 -0.0002 0.0132 0.001 0.070 0.000 0.828 0.008 -0.002 -0.195 0.06 24816. 0.0000
PROP RPM = 2000
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 0.0846 0.0301 0.020 0.641 0.706 15.161 0.072 3.142 21.134 0.13 47651. 0.6514
0.67 0.0221 0.0604 0.0832 0.0304 0.021 0.647 0.695 15.311 0.073 3.091 20.585 0.13 47679. 0.6293
1.34 0.0442 0.1177 0.0817 0.0307 0.021 0.653 0.682 15.449 0.074 3.036 20.038 0.13 47709. 0.6071
2.01 0.0663 0.1717 0.0801 0.0309 0.021 0.658 0.669 15.571 0.074 2.977 19.493 0.13 47742. 0.5848
2.68 0.0884 0.2226 0.0784 0.0311 0.021 0.662 0.655 15.675 0.075 2.913 18.954 0.13 47778. 0.5625
3.35 0.1105 0.2704 0.0766 0.0313 0.021 0.666 0.640 15.756 0.075 2.846 18.419 0.13 47816. 0.5403
4.02 0.1326 0.3152 0.0747 0.0314 0.021 0.668 0.624 15.811 0.075 2.774 17.890 0.13 47856. 0.5181
4.69 0.1547 0.3569 0.0726 0.0315 0.021 0.669 0.606 15.837 0.076 2.697 17.368 0.13 47900. 0.4960
5.36 0.1768 0.3958 0.0704 0.0314 0.021 0.669 0.588 15.829 0.076 2.616 16.851 0.13 47946. 0.4739
6.03 0.1989 0.4318 0.0681 0.0314 0.021 0.667 0.569 15.785 0.075 2.529 16.340 0.13 47995. 0.4519
6.70 0.2210 0.4649 0.0656 0.0312 0.021 0.663 0.548 15.700 0.075 2.438 15.835 0.13 48047. 0.4299
7.37 0.2431 0.4952 0.0630 0.0309 0.021 0.658 0.526 15.571 0.074 2.342 15.334 0.13 48102. 0.4080
8.04 0.2652 0.5227 0.0603 0.0306 0.021 0.651 0.504 15.396 0.074 2.240 14.836 0.13 48160. 0.3861
8.71 0.2873 0.5473 0.0574 0.0301 0.020 0.641 0.480 15.172 0.072 2.133 14.339 0.13 48221. 0.3642
9.38 0.3094 0.5689 0.0544 0.0296 0.020 0.630 0.455 14.896 0.071 2.022 13.841 0.13 48286. 0.3422
10.05 0.3315 0.5874 0.0513 0.0289 0.020 0.616 0.428 14.567 0.070 1.906 13.339 0.13 48353. 0.3202
10.72 0.3536 0.6027 0.0480 0.0282 0.019 0.599 0.401 14.182 0.068 1.784 12.829 0.13 48424. 0.2980
11.39 0.3757 0.6143 0.0446 0.0273 0.018 0.581 0.373 13.741 0.066 1.659 12.308 0.13 48498. 0.2756
12.05 0.3978 0.6220 0.0412 0.0263 0.018 0.560 0.344 13.247 0.063 1.529 11.770 0.13 48575. 0.2531
12.72 0.4199 0.6254 0.0376 0.0252 0.017 0.537 0.314 12.702 0.061 1.396 11.210 0.13 48656. 0.2303
13.39 0.4420 0.6236 0.0339 0.0240 0.016 0.512 0.283 12.106 0.058 1.261 10.621 0.13 48740. 0.2074
14.06 0.4641 0.6160 0.0302 0.0228 0.015 0.484 0.252 11.461 0.055 1.123 9.991 0.13 48827. 0.1841
14.73 0.4862 0.6013 0.0265 0.0214 0.014 0.455 0.221 10.769 0.051 0.983 9.309 0.13 48917. 0.1605
15.40 0.5083 0.5779 0.0227 0.0199 0.013 0.424 0.189 10.032 0.048 0.842 8.558 0.13 49011. 0.1366
16.07 0.5304 0.5436 0.0188 0.0184 0.012 0.391 0.157 9.252 0.044 0.700 7.715 0.13 49108. 0.1122
16.74 0.5525 0.4951 0.0150 0.0167 0.011 0.356 0.125 8.432 0.040 0.558 6.745 0.13 49209. 0.0876
17.41 0.5746 0.4274 0.0112 0.0150 0.010 0.320 0.094 7.575 0.036 0.416 5.599 0.13 49313. 0.0628
18.08 0.5967 0.3329 0.0074 0.0133 0.009 0.283 0.062 6.687 0.032 0.275 4.199 0.13 49420. 0.0383
18.75 0.6188 0.1988 0.0037 0.0115 0.008 0.244 0.031 5.772 0.028 0.137 2.418 0.13 49531. 0.0156
19.42 0.6409 0.0019 0.0000 0.0096 0.006 0.204 0.000 4.835 0.023 0.001 0.022 0.13 49644. 0.0000
PROP RPM = 3000
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 0.0849 0.0289 0.066 1.383 1.595 49.078 0.156 7.094 14.740 0.19 71475. 0.6827
1.02 0.0224 0.0641 0.0835 0.0292 0.067 1.398 1.569 49.620 0.158 6.977 14.338 0.19 71518. 0.6586
2.04 0.0448 0.1245 0.0819 0.0295 0.067 1.412 1.540 50.119 0.160 6.851 13.939 0.19 71564. 0.6344
3.06 0.0673 0.1815 0.0803 0.0298 0.068 1.425 1.510 50.565 0.161 6.716 13.544 0.19 71615. 0.6104
4.08 0.0897 0.2351 0.0786 0.0300 0.068 1.435 1.477 50.944 0.162 6.572 13.154 0.19 71669. 0.5863
5.10 0.1121 0.2852 0.0768 0.0302 0.069 1.444 1.443 51.245 0.163 6.417 12.769 0.19 71727. 0.5624
6.11 0.1345 0.3321 0.0748 0.0303 0.069 1.450 1.406 51.453 0.164 6.252 12.390 0.19 71789. 0.5387
7.13 0.1569 0.3758 0.0727 0.0303 0.069 1.453 1.366 51.557 0.164 6.076 12.017 0.19 71855. 0.5150
8.15 0.1793 0.4163 0.0704 0.0303 0.069 1.452 1.324 51.541 0.164 5.888 11.649 0.19 71926. 0.4915
9.17 0.2018 0.4539 0.0680 0.0303 0.069 1.448 1.279 51.394 0.164 5.689 11.288 0.19 72001. 0.4682
10.19 0.2242 0.4884 0.0655 0.0301 0.069 1.440 1.232 51.102 0.163 5.479 10.933 0.19 72081. 0.4450
11.21 0.2466 0.5200 0.0629 0.0298 0.068 1.427 1.182 50.655 0.161 5.257 10.582 0.19 72166. 0.4219
12.23 0.2690 0.5487 0.0601 0.0295 0.067 1.410 1.129 50.040 0.159 5.023 10.235 0.19 72255. 0.3988
13.25 0.2914 0.5744 0.0571 0.0290 0.066 1.388 1.074 49.249 0.157 4.777 9.891 0.19 72349. 0.3759
14.27 0.3139 0.5971 0.0541 0.0284 0.065 1.360 1.016 48.273 0.154 4.520 9.547 0.19 72448. 0.3529
15.29 0.3363 0.6167 0.0508 0.0277 0.063 1.327 0.956 47.103 0.150 4.251 9.203 0.19 72552. 0.3299
16.30 0.3587 0.6329 0.0475 0.0269 0.061 1.288 0.893 45.732 0.146 3.971 8.855 0.19 72661. 0.3069
17.32 0.3811 0.6456 0.0440 0.0260 0.059 1.244 0.828 44.164 0.141 3.682 8.501 0.19 72775. 0.2837
18.34 0.4035 0.6544 0.0405 0.0250 0.057 1.195 0.761 42.405 0.135 3.384 8.138 0.19 72893. 0.2603
19.36 0.4259 0.6586 0.0368 0.0238 0.054 1.140 0.692 40.459 0.129 3.079 7.760 0.19 73017. 0.2368
20.38 0.4484 0.6578 0.0331 0.0226 0.051 1.080 0.622 38.332 0.122 2.767 7.362 0.19 73146. 0.2130
21.40 0.4708 0.6508 0.0293 0.0212 0.048 1.015 0.551 36.028 0.115 2.451 6.937 0.19 73281. 0.1889
22.42 0.4932 0.6364 0.0255 0.0198 0.045 0.945 0.479 33.554 0.107 2.131 6.475 0.19 73420. 0.1644
23.44 0.5156 0.6126 0.0216 0.0182 0.041 0.871 0.406 30.917 0.098 1.808 5.962 0.19 73564. 0.1394
24.46 0.5380 0.5765 0.0177 0.0166 0.038 0.792 0.333 28.126 0.090 1.483 5.377 0.19 73714. 0.1139
25.48 0.5605 0.5238 0.0139 0.0148 0.034 0.710 0.261 25.193 0.080 1.159 4.690 0.19 73869. 0.0878
26.49 0.5829 0.4475 0.0100 0.0130 0.030 0.624 0.188 22.133 0.070 0.836 3.852 0.19 74029. 0.0613
27.51 0.6053 0.3355 0.0062 0.0112 0.025 0.534 0.116 18.964 0.060 0.517 2.782 0.19 74194. 0.0348
28.53 0.6277 0.1658 0.0024 0.0092 0.021 0.442 0.046 15.705 0.050 0.204 1.326 0.19 74364. 0.0104
29.55 0.6501
PROP RPM = 4000
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 0.0852 0.0282 0.152 2.402 2.847 113.690 0.271 12.663 11.358 0.25 95298. 0.7028
1.36 0.0224 0.0657 0.0838 0.0286 0.154 2.430 2.800 115.014 0.275 12.456 11.043 0.25 95355. 0.6777
2.71 0.0448 0.1276 0.0823 0.0289 0.156 2.456 2.750 116.239 0.277 12.232 10.731 0.25 95417. 0.6526
4.07 0.0671 0.1859 0.0807 0.0291 0.157 2.479 2.696 117.335 0.280 11.993 10.423 0.25 95484. 0.6276
5.43 0.0895 0.2406 0.0790 0.0294 0.159 2.499 2.639 118.274 0.282 11.736 10.118 0.25 95556. 0.6028
6.78 0.1119 0.2919 0.0771 0.0296 0.160 2.515 2.577 119.026 0.284 11.461 9.819 0.25 95633. 0.5780
8.14 0.1343 0.3398 0.0751 0.0297 0.160 2.526 2.511 119.558 0.285 11.168 9.525 0.25 95716. 0.5535
9.49 0.1566 0.3844 0.0730 0.0298 0.161 2.532 2.440 119.840 0.286 10.855 9.237 0.25 95805. 0.5292
10.85 0.1790 0.4259 0.0708 0.0298 0.161 2.532 2.366 119.838 0.286 10.522 8.953 0.25 95899. 0.5050
12.21 0.2014 0.4643 0.0684 0.0297 0.160 2.526 2.286 119.521 0.285 10.169 8.676 0.25 95999. 0.4811
13.56 0.2238 0.4996 0.0659 0.0295 0.159 2.512 2.202 118.858 0.284 9.795 8.403 0.25 96105. 0.4573
14.92 0.2462 0.5321 0.0632 0.0293 0.158 2.490 2.113 117.820 0.281 9.399 8.135 0.25 96218. 0.4337
16.28 0.2685 0.5616 0.0604 0.0289 0.156 2.459 2.020 116.383 0.278 8.983 7.871 0.25 96337. 0.4102
17.63 0.2909 0.5882 0.0575 0.0284 0.154 2.420 1.921 114.522 0.273 8.546 7.610 0.25 96462. 0.3868
18.99 0.3133 0.6119 0.0544 0.0279 0.150 2.371 1.819 112.217 0.268 8.089 7.350 0.26 96593. 0.3635
20.34 0.3357 0.6325 0.0512 0.0272 0.147 2.313 1.711 109.443 0.261 7.611 7.092 0.26 96731. 0.3402
21.70 0.3581 0.6499 0.0479 0.0264 0.142 2.244 1.599 106.185 0.253 7.114 6.831 0.26 96876. 0.3168
23.06 0.3804 0.6639 0.0444 0.0254 0.137 2.165 1.484 102.449 0.245 6.599 6.568 0.26 97028. 0.2934
24.41 0.4028 0.6741 0.0408 0.0244 0.132 2.076 1.364 98.249 0.235 6.069 6.299 0.26 97186. 0.2698
25.77 0.4252 0.6801 0.0372 0.0232 0.126 1.978 1.242 93.597 0.223 5.526 6.020 0.26 97350. 0.2461
27.13 0.4476 0.6812 0.0334 0.0220 0.119 1.870 1.118 88.502 0.211 4.972 5.728 0.26 97522. 0.2221
28.48 0.4699 0.6765 0.0297 0.0206 0.111 1.753 0.991 82.978 0.198 4.409 5.418 0.26 97700. 0.1978
29.84 0.4923 0.6646 0.0258 0.0191 0.103 1.628 0.863 77.037 0.184 3.838 5.081 0.26 97886. 0.1731
31.19 0.5147 0.6437 0.0220 0.0176 0.095 1.494 0.734 70.698 0.169 3.264 4.707 0.26 98078. 0.1479
32.55 0.5371 0.6109 0.0181 0.0159 0.086 1.352 0.604 63.983 0.153 2.686 4.281 0.26 98277. 0.1220
33.91 0.5595 0.5616 0.0142 0.0141 0.076 1.203 0.474 56.919 0.136 2.109 3.778 0.26 98482. 0.0954
35.26 0.5818 0.4884 0.0103 0.0123 0.066 1.047 0.345 49.543 0.118 1.535 3.160 0.26 98695. 0.0681
36.62 0.6042 0.3781 0.0065 0.0104 0.056 0.885 0.218 41.898 0.100 0.968 2.355 0.26 98915. 0.0403
37.98 0.6266 0.2047 0.0028 0.0085 0.046 0.719 0.092 34.034 0.081 0.410 1.230 0.26 99141. 0.0137
39.33 0.6490
PROP RPM = 5000
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 0.0856 0.0279 0.294 3.705 4.471 219.192 0.419 19.885 9.251 0.32 119118. 0.7173
1.68 0.0222 0.0663 0.0842 0.0282 0.297 3.750 4.398 221.819 0.424 19.563 8.993 0.32 119190. 0.6917
3.36 0.0444 0.1288 0.0827 0.0285 0.301 3.791 4.320 224.254 0.428 19.217 8.738 0.32 119267. 0.6661
5.04 0.0666 0.1877 0.0811 0.0288 0.304 3.828 4.237 226.441 0.432 18.846 8.487 0.32 119350. 0.6407
6.73 0.0888 0.2430 0.0794 0.0290 0.306 3.860 4.148 228.326 0.436 18.448 8.239 0.32 119439. 0.6154
8.41 0.1110 0.2947 0.0776 0.0292 0.308 3.885 4.052 229.848 0.439 18.023 7.996 0.32 119535. 0.5903
10.09 0.1332 0.3431 0.0756 0.0294 0.310 3.904 3.950 230.946 0.441 17.568 7.757 0.32 119637. 0.5654
11.77 0.1554 0.3882 0.0736 0.0294 0.311 3.914 3.841 231.560 0.442 17.084 7.523 0.32 119747. 0.5407
13.45 0.1776 0.4302 0.0713 0.0294 0.311 3.915 3.725 231.625 0.442 16.568 7.294 0.32 119863. 0.5163
15.13 0.1998 0.4691 0.0690 0.0294 0.310 3.906 3.602 231.080 0.441 16.021 7.070 0.32 119987. 0.4920
16.82 0.2220 0.5050 0.0665 0.0292 0.308 3.886 3.471 229.866 0.439 15.441 6.850 0.32 120119. 0.4680
18.50 0.2442 0.5380 0.0639 0.0290 0.306 3.853 3.334 227.926 0.435 14.829 6.634 0.32 120258. 0.4442
20.18 0.2664 0.5682 0.0611 0.0286 0.302 3.807 3.189 225.210 0.430 14.184 6.422 0.32 120404. 0.4206
21.86 0.2886 0.5955 0.0582 0.0282 0.297 3.747 3.037 221.671 0.423 13.507 6.214 0.32 120559. 0.3971
23.54 0.3108 0.6200 0.0551 0.0276 0.291 3.673 2.877 217.267 0.415 12.799 6.007 0.32 120721. 0.3737
25.22 0.3330 0.6415 0.0519 0.0269 0.284 3.583 2.711 211.955 0.405 12.058 5.801 0.32 120892. 0.3503
26.91 0.3552 0.6600 0.0486 0.0262 0.276 3.477 2.538 205.696 0.393 11.287 5.596 0.32 121071. 0.3269
28.59 0.3774 0.6753 0.0452 0.0252 0.266 3.355 2.358 198.497 0.379 10.488 5.388 0.32 121257. 0.3034
30.27 0.3996 0.6870 0.0416 0.0242 0.255 3.218 2.173 190.384 0.364 9.666 5.177 0.32 121452. 0.2799
31.95 0.4218 0.6948 0.0380 0.0231 0.243 3.066 1.984 181.379 0.346 8.823 4.960 0.32 121655. 0.2562
33.63 0.4440 0.6980 0.0343 0.0218 0.230 2.899 1.790 171.502 0.328 7.962 4.734 0.32 121867. 0.2323
35.31 0.4662 0.6959 0.0305 0.0204 0.216 2.718 1.593 160.776 0.307 7.087 4.495 0.32 122087. 0.2081
37.00 0.4883 0.6873 0.0267 0.0190 0.200 2.523 1.394 149.225 0.285 6.201 4.237 0.32 122315. 0.1835
38.68 0.5105 0.6703 0.0228 0.0174 0.184 2.314 1.193 136.883 0.261 5.307 3.953 0.32 122552. 0.1584
40.36 0.5327 0.6424 0.0190 0.0157 0.166 2.093 0.991 123.790 0.236 4.408 3.631 0.32 122797. 0.1326
42.04 0.5549 0.5995 0.0151 0.0140 0.148 1.859 0.789 110.000 0.210 3.509 3.252 0.32 123050. 0.1059
43.72 0.5771 0.5344 0.0113 0.0122 0.128 1.616 0.588 95.579 0.183 2.613 2.788 0.32 123312. 0.0784
45.40 0.5993 0.4349 0.0074 0.0102 0.108 1.363 0.388 80.609 0.154 1.727 2.185 0.32 123583. 0.0499
47.09 0.6215 0.2764 0.0037 0.0083 0.087 1.102 0.192 65.187 0.124 0.856 1.339 0.32 123862. 0.0215
48.77 0.6437 0.0004 0.0000 0.0063 0.066 0.834 0.000 49.351 0.094 0.001 0.002 0.32 124143. 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 0.0861 0.0277 0.505 5.302 6.476 376.360 0.599 28.807 7.805 0.38 142937. 0.7284
2.02 0.0222 0.0672 0.0848 0.0280 0.511 5.367 6.372 380.992 0.606 28.343 7.586 0.38 143023. 0.7023
4.04 0.0444 0.1305 0.0833 0.0283 0.517 5.428 6.260 385.290 0.613 27.844 7.369 0.38 143115. 0.6762
6.06 0.0666 0.1900 0.0817 0.0286 0.522 5.482 6.139 389.152 0.619 27.308 7.156 0.38 143215. 0.6502
8.08 0.0889 0.2460 0.0799 0.0289 0.526 5.529 6.010 392.484 0.625 26.734 6.946 0.38 143323. 0.6245
10.10 0.1111 0.2983 0.0781 0.0291 0.530 5.567 5.872 395.180 0.629 26.119 6.740 0.38 143438. 0.5989
12.12 0.1333 0.3473 0.0761 0.0292 0.533 5.594 5.724 397.134 0.632 25.462 6.538 0.38 143562. 0.5736
14.14 0.1555 0.3929 0.0740 0.0293 0.534 5.610 5.567 398.236 0.634 24.760 6.340 0.38 143693. 0.5486
16.16 0.1777 0.4354 0.0718 0.0293 0.534 5.612 5.399 398.374 0.634 24.014 6.147 0.38 143834. 0.5238
18.17 0.1999 0.4747 0.0694 0.0292 0.533 5.599 5.221 397.442 0.633 23.222 5.958 0.38 143983. 0.4992
20.19 0.2221 0.5111 0.0669 0.0291 0.530 5.569 5.032 395.333 0.629 22.382 5.773 0.38 144141. 0.4749
22.21 0.2443 0.5446 0.0643 0.0288 0.526 5.521 4.833 391.950 0.624 21.495 5.592 0.38 144308. 0.4508
24.23 0.2666 0.5753 0.0615 0.0285 0.519 5.455 4.622 387.201 0.616 20.561 5.415 0.38 144485. 0.4269
26.25 0.2888 0.6031 0.0585 0.0280 0.511 5.367 4.402 381.006 0.606 19.579 5.240 0.38 144671. 0.4032
28.27 0.3110 0.6281 0.0555 0.0275 0.501 5.259 4.171 373.290 0.594 18.552 5.068 0.38 144866. 0.3796
30.29 0.3332 0.6503 0.0523 0.0268 0.488 5.127 3.929 363.976 0.579 17.478 4.897 0.38 145071. 0.3560
32.31 0.3554 0.6694 0.0489 0.0260 0.473 4.973 3.678 352.995 0.562 16.359 4.726 0.38 145286. 0.3324
34.33 0.3776 0.6854 0.0455 0.0250 0.456 4.795 3.417 340.360 0.542 15.200 4.554 0.38 145510. 0.3087
36.35 0.3998 0.6979 0.0419 0.0240 0.437 4.594 3.149 326.113 0.519 14.007 4.380 0.38 145745. 0.2850
38.37 0.4221 0.7066 0.0382 0.0228 0.416 4.371 2.874 310.293 0.494 12.783 4.201 0.38 145989. 0.2612
40.39 0.4443 0.7109 0.0345 0.0216 0.393 4.127 2.593 292.934 0.466 11.535 4.015 0.38 146243. 0.2371
42.41 0.4665 0.7100 0.0307 0.0202 0.368 3.861 2.308 274.074 0.436 10.265 3.819 0.38 146508. 0.2128
44.43 0.4887 0.7027 0.0268 0.0187 0.340 3.575 2.019 253.760 0.404 8.979 3.608 0.39 146782. 0.1880
46.45 0.5109 0.6873 0.0230 0.0171 0.311 3.269 1.727 232.048 0.369 7.681 3.375 0.39 147066. 0.1627
48.47 0.5331 0.6610 0.0191 0.0154 0.280 2.944 1.434 209.012 0.333 6.377 3.111 0.39 147361. 0.1366
50.49 0.5553 0.6196 0.0152 0.0136 0.248 2.603 1.140 184.745 0.294 5.072 2.800 0.39 147666. 0.1096
52.50 0.5776 0.5558 0.0113 0.0117 0.214 2.245 0.848 159.366 0.254 3.774 2.415 0.39 147981. 0.0816
54.52 0.5998 0.4560 0.0074 0.0098 0.178 1.874 0.560 133.021 0.212 2.489 1.908 0.39 148306. 0.0523
56.54 0.6220 0.2925 0.0037 0.0078 0.142 1.492 0.275 105.882 0.169 1.225 1.180 0.39 148641. 0.0227
58.56 0.6442 -0.0051 0.0000 0.0057 0.105 1.099 -0.003 77.993 0.124 -0.015 -0.020 0.39 148977. 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 0.0868 0.0277 0.800 7.206 8.878 596.824 0.814 39.491 6.747 0.44 166752. 0.7373
2.36 0.0222 0.0677 0.0854 0.0280 0.810 7.297 8.736 604.316 0.824 38.859 6.557 0.44 166852. 0.7108
4.71 0.0444 0.1316 0.0839 0.0283 0.820 7.381 8.583 611.266 0.834 38.179 6.369 0.44 166961. 0.6843
7.07 0.0666 0.1916 0.0823 0.0286 0.828 7.456 8.419 617.516 0.842 37.448 6.184 0.44 167078. 0.6580
9.42 0.0889 0.2480 0.0805 0.0289 0.835 7.521 8.243 622.908 0.850 36.664 6.002 0.44 167204. 0.6320
11.78 0.1111 0.3008 0.0787 0.0291 0.841 7.574 8.054 627.275 0.856 35.825 5.824 0.44 167339. 0.6061
14.14 0.1333 0.3501 0.0767 0.0292 0.845 7.612 7.852 630.445 0.860 34.927 5.649 0.44 167483. 0.5805
16.49 0.1555 0.3961 0.0746 0.0293 0.848 7.634 7.637 632.238 0.862 33.968 5.479 0.44 167637. 0.5552
18.85 0.1777 0.4390 0.0724 0.0293 0.848 7.637 7.407 632.478 0.863 32.947 5.312 0.44 167801. 0.5302
21.21 0.1999 0.4787 0.0700 0.0292 0.846 7.619 7.163 630.988 0.861 31.863 5.149 0.45 167975. 0.5054
23.56 0.2222 0.5155 0.0675 0.0291 0.842 7.578 6.905 627.601 0.856 30.713 4.990 0.45 168160. 0.4809
25.92 0.2444 0.5493 0.0648 0.0288 0.834 7.512 6.632 622.156 0.849 29.498 4.835 0.45 168356. 0.4566
28.27 0.2666 0.5804 0.0620 0.0285 0.824 7.420 6.344 614.507 0.838 28.218 4.682 0.45 168562. 0.4325
30.63 0.2888 0.6087 0.0590 0.0280 0.811 7.299 6.042 604.522 0.825 26.873 4.533 0.45 168780. 0.4086
32.99 0.3110 0.6342 0.0559 0.0274 0.794 7.149 5.725 592.082 0.808 25.463 4.385 0.45 169008. 0.3848
35.34 0.3332 0.6569 0.0527 0.0267 0.774 6.968 5.394 577.064 0.787 23.991 4.239 0.45 169248. 0.3611
37.70 0.3554 0.6766 0.0493 0.0259 0.750 6.754 5.049 559.354 0.763 22.456 4.094 0.45 169499. 0.3373
40.05 0.3777 0.6932 0.0458 0.0250 0.723 6.508 4.691 538.971 0.735 20.866 3.948 0.45 169761. 0.3136
42.41 0.3999 0.7065 0.0422 0.0239 0.692 6.230 4.323 515.979 0.704 19.228 3.800 0.45 170035. 0.2897
44.77 0.4221 0.7161 0.0386 0.0227 0.658 5.922 3.945 490.441 0.669 17.549 3.649 0.45 170320. 0.2658
47.12 0.4443 0.7214 0.0348 0.0214 0.620 5.583 3.560 462.414 0.631 15.834 3.492 0.45 170617. 0.2416
49.48 0.4665 0.7216 0.0310 0.0200 0.579 5.216 3.168 431.957 0.589 14.091 3.326 0.45 170925. 0.2171
51.84 0.4887 0.7156 0.0271 0.0185 0.535 4.820 2.771 399.145 0.545 12.325 3.149 0.45 171246. 0.1922
54.19 0.5110 0.7016 0.0232 0.0169 0.488 4.396 2.370 364.070 0.497 10.543 2.953 0.45 171578. 0.1667
56.55 0.5332 0.6769 0.0192 0.0151 0.438 3.947 1.968 326.850 0.446 8.752 2.731 0.45 171922. 0.1405
58.90 0.5554 0.6373 0.0153 0.0133 0.386 3.473 1.565 287.639 0.392 6.961 2.468 0.45 172277. 0.1132
61.26 0.5776 0.5749 0.0114 0.0114 0.331 2.978 1.164 246.627 0.336 5.178 2.141 0.45 172645. 0.0847
63.62 0.5998 0.4757 0.0075 0.0095 0.274 2.464 0.767 204.055 0.278 3.413 1.706 0.45 173024. 0.0548
65.97 0.6220 0.3090 0.0037 0.0074 0.215 1.934 0.377 160.202 0.219 1.678 1.068 0.45 173415. 0.0241
68.33 0.6442 -0.0068 -0.0001 0.0053 0.154 1.390 -0.006 115.113 0.157 -0.026 -0.023 0.45 173806. 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 0.0875 0.0277 1.198 9.439 11.694 893.411 1.066 52.016 5.937 0.51 190563. 0.7446
2.69 0.0222 0.0681 0.0861 0.0281 1.213 9.559 11.509 904.795 1.080 51.191 5.769 0.51 190678. 0.7178
5.38 0.0444 0.1323 0.0846 0.0284 1.228 9.671 11.309 915.356 1.093 50.302 5.604 0.51 190803. 0.6911
8.08 0.0666 0.1927 0.0830 0.0287 1.240 9.771 11.094 924.852 1.104 49.346 5.441 0.51 190937. 0.6646
10.77 0.0888 0.2493 0.0813 0.0290 1.251 9.858 10.863 933.043 1.114 48.319 5.281 0.51 191081. 0.6383
13.46 0.1111 0.3024 0.0794 0.0292 1.260 9.928 10.616 939.674 1.122 47.219 5.124 0.51 191236. 0.6123
16.15 0.1333 0.3520 0.0774 0.0293 1.267 9.979 10.351 944.484 1.127 46.041 4.971 0.51 191401. 0.5865
18.85 0.1555 0.3983 0.0753 0.0294 1.270 10.007 10.068 947.201 1.131 44.783 4.821 0.51 191578. 0.5610
21.54 0.1777 0.4414 0.0731 0.0294 1.271 10.011 9.767 947.560 1.131 43.442 4.675 0.51 191766. 0.5358
24.23 0.1999 0.4815 0.0707 0.0293 1.268 9.987 9.446 945.289 1.128 42.017 4.533 0.51 191965. 0.5109
26.92 0.2221 0.5186 0.0681 0.0292 1.261 9.933 9.106 940.134 1.122 40.506 4.393 0.51 192177. 0.4862
29.62 0.2443 0.5528 0.0654 0.0289 1.250 9.845 8.747 931.854 1.112 38.907 4.258 0.51 192401. 0.4618
32.31 0.2665 0.5842 0.0626 0.0286 1.234 9.722 8.368 920.226 1.098 37.222 4.125 0.51 192637. 0.4376
35.00 0.2888 0.6129 0.0596 0.0281 1.214 9.562 7.970 905.050 1.080 35.451 3.994 0.51 192886. 0.4135
37.69 0.3110 0.6388 0.0565 0.0275 1.188 9.362 7.553 886.146 1.058 33.595 3.866 0.51 193148. 0.3896
40.38 0.3332 0.6619 0.0532 0.0268 1.158 9.121 7.117 863.329 1.031 31.654 3.739 0.51 193422. 0.3658
43.08 0.3554 0.6822 0.0498 0.0260 1.122 8.837 6.662 836.427 0.998 29.632 3.613 0.51 193709. 0.3419
45.77 0.3776 0.6995 0.0463 0.0250 1.080 8.510 6.190 805.459 0.961 27.535 3.486 0.51 194009. 0.3181
48.46 0.3998 0.7134 0.0427 0.0239 1.033 8.141 5.705 770.526 0.920 25.375 3.358 0.51 194323. 0.2941
51.15 0.4220 0.7238 0.0390 0.0227 0.981 7.731 5.207 731.720 0.873 23.160 3.228 0.51 194649. 0.2701
53.85 0.4442 0.7300 0.0352 0.0214 0.924 7.281 4.698 689.127 0.823 20.898 3.092 0.51 194988. 0.2458
56.54 0.4664 0.7312 0.0313 0.0200 0.862 6.792 4.181 642.840 0.767 18.598 2.950 0.51 195341. 0.2212
59.23 0.4887 0.7264 0.0274 0.0184 0.795 6.265 3.657 592.968 0.708 16.268 2.798 0.51 195707. 0.1962
61.92 0.5109 0.7138 0.0234 0.0168 0.724 5.702 3.128 539.653 0.644 13.916 2.629 0.51 196087. 0.1706
64.62 0.5331 0.6907 0.0194 0.0150 0.648 5.104 2.597 483.077 0.577 11.552 2.438 0.51 196480. 0.1441
67.31 0.5553 0.6527 0.0155 0.0131 0.568 4.474 2.065 423.471 0.505 9.186 2.212 0.52 196886. 0.1166
70.00 0.5775 0.5920 0.0115 0.0112 0.484 3.815 1.536 361.128 0.431 6.832 1.929 0.52 197307. 0.0877
72.69 0.5997 0.4936 0.0076 0.0092 0.397 3.132 1.012 296.414 0.354 4.502 1.549 0.52 197740. 0.0571
75.38 0.6219 0.3244 0.0037 0.0071 0.308 2.427 0.497 229.759 0.274 2.212 0.982 0.52 198187. 0.0254
78.08 0.6441 -0.0085 -0.0001 0.0050 0.216 1.703 -0.009 161.197 0.192 -0.039 -0.025 0.52 198632. 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 0.0884 0.0279 1.717 12.027 14.947 1280.597 1.359 66.484 5.294 0.57 214369. 0.7506
3.03 0.0222 0.0683 0.0870 0.0283 1.739 12.182 14.713 1297.116 1.376 65.441 5.145 0.57 214499. 0.7237
6.06 0.0444 0.1327 0.0855 0.0286 1.760 12.326 14.459 1312.433 1.393 64.316 4.997 0.57 214640. 0.6968
9.08 0.0666 0.1932 0.0839 0.0289 1.778 12.455 14.187 1326.198 1.407 63.104 4.852 0.57 214791. 0.6702
12.11 0.0888 0.2501 0.0821 0.0292 1.794 12.566 13.894 1338.063 1.420 61.801 4.710 0.57 214954. 0.6438
15.14 0.1110 0.3033 0.0803 0.0294 1.807 12.656 13.580 1347.659 1.430 60.403 4.570 0.57 215128. 0.6177
18.17 0.1332 0.3531 0.0783 0.0295 1.817 12.722 13.243 1354.607 1.437 58.906 4.434 0.57 215315. 0.5918
21.19 0.1554 0.3997 0.0762 0.0296 1.822 12.758 12.883 1358.513 1.441 57.306 4.301 0.57 215514. 0.5662
24.22 0.1776 0.4430 0.0739 0.0296 1.822 12.763 12.500 1358.988 1.442 55.599 4.172 0.57 215726. 0.5409
27.25 0.1998 0.4833 0.0715 0.0296 1.818 12.731 12.091 1355.644 1.438 53.782 4.046 0.57 215952. 0.5159
30.28 0.2220 0.5206 0.0689 0.0294 1.808 12.661 11.658 1348.113 1.430 51.855 3.922 0.57 216191. 0.4911
33.30 0.2442 0.5551 0.0662 0.0291 1.792 12.547 11.200 1336.043 1.418 49.816 3.802 0.57 216443. 0.4666
36.33 0.2664 0.5869 0.0633 0.0288 1.769 12.388 10.716 1319.116 1.400 47.664 3.685 0.57 216710. 0.4423
39.36 0.2886 0.6159 0.0603 0.0283 1.739 12.181 10.207 1297.042 1.376 45.402 3.569 0.57 216990. 0.4182
42.39 0.3108 0.6422 0.0572 0.0277 1.703 11.923 9.674 1269.560 1.347 43.030 3.456 0.57 217285. 0.3942
45.41 0.3330 0.6658 0.0539 0.0270 1.658 11.612 9.116 1236.408 1.312 40.550 3.344 0.57 217594. 0.3703
48.44 0.3552 0.6866 0.0505 0.0261 1.606 11.245 8.535 1197.334 1.270 37.963 3.233 0.57 217917. 0.3464
51.47 0.3774 0.7044 0.0469 0.0251 1.545 10.822 7.932 1152.358 1.223 35.281 3.122 0.58 218255. 0.3224
54.50 0.3996 0.7191 0.0432 0.0240 1.477 10.346 7.310 1101.626 1.169 32.516 3.010 0.58 218608. 0.2984
57.52 0.4218 0.7302 0.0394 0.0228 1.402 9.817 6.673 1045.272 1.109 29.680 2.895 0.58 218975. 0.2743
60.55 0.4441 0.7373 0.0356 0.0214 1.319 9.236 6.022 983.421 1.043 26.784 2.777 0.58 219357. 0.2499
63.58 0.4663 0.7395 0.0317 0.0200 1.229 8.604 5.359 916.206 0.972 23.838 2.653 0.58 219754. 0.2252
66.61 0.4885 0.7358 0.0277 0.0184 1.132 7.924 4.688 843.788 0.895 20.852 2.520 0.58 220166. 0.2001
69.64 0.5107 0.7246 0.0237 0.0167 1.028 7.197 4.010 766.374 0.813 17.838 2.373 0.58 220593. 0.1743
72.66 0.5329 0.7030 0.0197 0.0149 0.918 6.426 3.329 684.224 0.726 14.808 2.207 0.58 221035. 0.1477
75.69 0.5551 0.6667 0.0156 0.0130 0.801 5.613 2.647 597.676 0.634 11.776 2.009 0.58 221492. 0.1199
78.72 0.5773 0.6077 0.0116 0.0111 0.680 4.763 1.969 507.158 0.538 8.757 1.761 0.58 221965. 0.0906
81.75 0.5995 0.5103 0.0077 0.0090 0.554 3.881 1.297 413.204 0.438 5.770 1.424 0.58 222452. 0.0595
84.77 0.6217 0.3393 0.0038 0.0069 0.424 2.972 0.637 316.440 0.336 2.833 0.913 0.58 222954. 0.0267
87.80 0.6439 -0.0099 -0.0001 0.0047 0.291 2.037 -0.012 216.875 0.230 -0.055 -0.026 0.58 223454. 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 0.0894 0.0282 2.381 15.004 18.666 1775.197 1.695 83.025 4.769 0.63 238169. 0.7556
3.36 0.0222 0.0683 0.0880 0.0286 2.412 15.200 18.377 1798.336 1.717 81.740 4.635 0.63 238314. 0.7287
6.72 0.0444 0.1327 0.0865 0.0289 2.440 15.381 18.065 1819.781 1.738 80.351 4.502 0.63 238471. 0.7018
10.09 0.0666 0.1933 0.0849 0.0292 2.466 15.544 17.728 1839.036 1.756 78.854 4.372 0.63 238640. 0.6751
13.45 0.0888 0.2502 0.0831 0.0295 2.488 15.684 17.366 1855.614 1.772 77.242 4.245 0.63 238821. 0.6487
16.81 0.1109 0.3036 0.0813 0.0297 2.506 15.797 16.976 1869.000 1.785 75.511 4.120 0.64 239016. 0.6225
20.17 0.1331 0.3535 0.0793 0.0299 2.519 15.879 16.559 1878.660 1.794 73.654 3.998 0.64 239224. 0.5966
23.53 0.1553 0.4002 0.0771 0.0299 2.527 15.924 16.112 1884.046 1.799 71.667 3.879 0.64 239446. 0.5710
26.90 0.1775 0.4437 0.0749 0.0300 2.527 15.929 15.635 1884.611 1.800 69.545 3.763 0.64 239683. 0.5457
30.26 0.1997 0.4842 0.0724 0.0299 2.521 15.889 15.127 1879.818 1.795 67.286 3.650 0.64 239934. 0.5206
33.62 0.2219 0.5217 0.0698 0.0297 2.507 15.799 14.588 1869.150 1.785 64.887 3.540 0.64 240200. 0.4958
36.98 0.2441 0.5565 0.0671 0.0294 2.484 15.655 14.017 1852.118 1.769 62.346 3.433 0.64 240481. 0.4713
40.34 0.2663 0.5886 0.0642 0.0291 2.452 15.453 13.413 1828.275 1.746 59.663 3.328 0.64 240778. 0.4469
43.71 0.2885 0.6179 0.0612 0.0286 2.410 15.191 12.779 1797.221 1.716 56.840 3.225 0.64 241090. 0.4228
47.07 0.3106 0.6446 0.0580 0.0279 2.358 14.864 12.113 1758.600 1.679 53.880 3.124 0.64 241418. 0.3988
50.43 0.3328 0.6687 0.0547 0.0272 2.296 14.471 11.417 1712.045 1.635 50.782 3.025 0.64 241761. 0.3748
53.79 0.3550 0.6900 0.0512 0.0263 2.222 14.007 10.690 1657.208 1.583 47.550 2.926 0.64 242121. 0.3508
57.15 0.3772 0.7084 0.0476 0.0253 2.138 13.474 9.936 1594.103 1.522 44.197 2.827 0.64 242497. 0.3268
60.52 0.3994 0.7237 0.0439 0.0242 2.042 12.872 9.159 1522.935 1.454 40.739 2.728 0.64 242889. 0.3027
63.88 0.4216 0.7355 0.0400 0.0229 1.936 12.204 8.361 1443.893 1.379 37.191 2.627 0.64 243298. 0.2785
67.24 0.4438 0.7434 0.0361 0.0216 1.820 11.471 7.546 1357.152 1.296 33.566 2.522 0.64 243722. 0.2541
70.60 0.4660 0.7467 0.0322 0.0201 1.694 10.674 6.717 1262.901 1.206 29.878 2.412 0.64 244163. 0.2293
73.96 0.4882 0.7442 0.0281 0.0185 1.557 9.816 5.876 1161.368 1.109 26.138 2.295 0.64 244621. 0.2040
77.33 0.5103 0.7342 0.0241 0.0167 1.412 8.899 5.027 1052.837 1.005 22.362 2.166 0.64 245095. 0.1781
80.69 0.5325 0.7142 0.0200 0.0149 1.257 7.925 4.174 937.678 0.895 18.565 2.019 0.64 245586. 0.1513
84.05 0.5547 0.6795 0.0159 0.0130 1.095 6.900 3.319 816.362 0.780 14.765 1.844 0.64 246094. 0.1232
87.41 0.5769 0.6223 0.0118 0.0110 0.925 5.828 2.469 689.491 0.658 10.980 1.624 0.65 246619. 0.0936
90.77 0.5991 0.5262 0.0078 0.0089 0.748 4.715 1.626 557.815 0.533 7.234 1.322 0.65 247160. 0.0618
94.13 0.6213 0.3538 0.0038 0.0067 0.566 3.569 0.798 422.217 0.403 3.550 0.857 0.65 247717. 0.0281
97.50 0.6435 -0.0112 -0.0001 0.0045 0.379 2.389 -0.016 282.666 0.270 -0.073 -0.026 0.65 248270. 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 0.0906 0.0286 3.216 18.426 22.888 2398.043 2.082 101.805 4.329 0.70 261961. 0.7595
3.69 0.0222 0.0682 0.0892 0.0290 3.258 18.667 22.540 2429.401 2.109 100.257 4.208 0.70 262121. 0.7327
7.39 0.0443 0.1325 0.0877 0.0294 3.297 18.891 22.163 2458.497 2.134 98.580 4.089 0.70 262294. 0.7059
11.08 0.0665 0.1930 0.0861 0.0297 3.332 19.092 21.756 2484.637 2.157 96.770 3.972 0.70 262481. 0.6793
14.78 0.0887 0.2499 0.0844 0.0299 3.362 19.264 21.317 2507.132 2.176 94.817 3.856 0.70 262681. 0.6530
18.47 0.1108 0.3032 0.0825 0.0302 3.386 19.404 20.844 2525.258 2.192 92.716 3.744 0.70 262896. 0.6269
22.17 0.1330 0.3532 0.0805 0.0303 3.404 19.504 20.337 2538.277 2.204 90.459 3.634 0.70 263126. 0.6010
25.86 0.1552 0.3999 0.0783 0.0304 3.413 19.559 19.793 2545.447 2.210 88.041 3.527 0.70 263371. 0.5754
29.56 0.1774 0.4435 0.0760 0.0304 3.414 19.563 19.212 2546.023 2.210 85.455 3.423 0.70 263632. 0.5502
33.25 0.1995 0.4842 0.0736 0.0303 3.405 19.511 18.592 2539.274 2.204 82.699 3.321 0.70 263910. 0.5251
36.95 0.2217 0.5219 0.0710 0.0301 3.385 19.398 17.933 2524.501 2.192 79.768 3.222 0.70 264203. 0.5004
40.64 0.2439 0.5569 0.0682 0.0299 3.354 19.218 17.235 2501.045 2.171 76.661 3.126 0.70 264513. 0.4759
44.34 0.2660 0.5893 0.0653 0.0295 3.310 18.966 16.497 2468.300 2.143 73.379 3.031 0.70 264840. 0.4515
48.03 0.2882 0.6190 0.0622 0.0290 3.253 18.639 15.720 2425.724 2.106 69.922 2.939 0.70 265184. 0.4274
51.73 0.3104 0.6461 0.0590 0.0283 3.182 18.233 14.904 2372.840 2.060 66.294 2.849 0.70 265546. 0.4034
55.42 0.3325 0.6706 0.0556 0.0276 3.097 17.743 14.050 2309.167 2.005 62.496 2.760 0.70 265925. 0.3794
59.12 0.3547 0.6924 0.0521 0.0267 2.996 17.167 13.159 2234.229 1.940 58.531 2.671 0.70 266321. 0.3554
62.81 0.3769 0.7113 0.0484 0.0256 2.881 16.505 12.233 2148.025 1.865 54.414 2.583 0.70 266735. 0.3313
66.51 0.3991 0.7273 0.0446 0.0245 2.750 15.758 11.279 2050.839 1.780 50.167 2.494 0.70 267166. 0.3072
70.20 0.4212 0.7399 0.0408 0.0232 2.606 14.929 10.298 1942.926 1.687 45.806 2.404 0.70 267616. 0.2829
73.90 0.4434 0.7487 0.0368 0.0218 2.447 14.019 9.296 1824.535 1.584 41.350 2.311 0.71 268083. 0.2584
77.59 0.4656 0.7529 0.0327 0.0202 2.274 13.031 8.276 1695.925 1.472 36.812 2.213 0.71 268568. 0.2335
81.29 0.4877 0.7516 0.0287 0.0186 2.089 11.967 7.242 1557.412 1.352 32.210 2.109 0.71 269072. 0.2081
84.98 0.5099 0.7429 0.0245 0.0168 1.890 10.830 6.196 1409.406 1.224 27.562 1.994 0.71 269593. 0.1820
88.68 0.5321 0.7244 0.0204 0.0150 1.680 9.624 5.145 1252.438 1.087 22.886 1.863 0.71 270133. 0.1550
92.37 0.5542 0.6914 0.0162 0.0130 1.458 8.354 4.093 1087.198 0.944 18.203 1.707 0.71 270691. 0.1267
96.07 0.5764 0.6358 0.0120 0.0109 1.226 7.027 3.044 914.569 0.794 13.539 1.510 0.71 271267. 0.0966
99.76 0.5986 0.5408 0.0079 0.0088 0.987 5.653 2.006 735.669 0.639 8.921 1.237 0.71 271862. 0.0642
103.46 0.6208 0.3669 0.0039 0.0066 0.740 4.240 0.984 551.830 0.479 4.378 0.809 0.71 272474. 0.0294
107.15 0.6429 -0.0122 -0.0001 0.0043 0.487 2.790 -0.021 363.079 0.315 -0.092 -0.026 0.71 273081. 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 0.0920 0.0295 4.298 22.575 27.660 3205.032 2.550 123.031 3.914 0.76 285743. 0.7550
4.03 0.0221 0.0673 0.0906 0.0298 4.347 22.833 27.249 3241.763 2.580 121.205 3.813 0.76 285918. 0.7299
8.05 0.0443 0.1310 0.0891 0.0301 4.393 23.073 26.804 3275.790 2.607 119.223 3.711 0.76 286108. 0.7046
12.08 0.0664 0.1912 0.0875 0.0304 4.434 23.288 26.321 3306.274 2.631 117.076 3.611 0.76 286313. 0.6794
16.10 0.0886 0.2479 0.0858 0.0306 4.469 23.472 25.799 3332.352 2.652 114.756 3.512 0.76 286532. 0.6541
20.13 0.1107 0.3012 0.0839 0.0308 4.497 23.618 25.237 3353.100 2.668 112.253 3.414 0.76 286768. 0.6289
24.15 0.1328 0.3513 0.0819 0.0310 4.516 23.719 24.631 3367.554 2.680 109.559 3.318 0.76 287019. 0.6038
28.18 0.1550 0.3981 0.0797 0.0310 4.526 23.770 23.981 3374.715 2.686 106.666 3.223 0.76 287288. 0.5788
32.20 0.1771 0.4420 0.0774 0.0310 4.524 23.762 23.284 3373.553 2.685 103.568 3.131 0.76 287574. 0.5540
36.23 0.1993 0.4828 0.0749 0.0309 4.510 23.688 22.540 3363.053 2.676 100.259 3.040 0.76 287877. 0.5293
40.25 0.2214 0.5209 0.0723 0.0307 4.482 23.541 21.748 3342.204 2.660 96.737 2.951 0.76 288198. 0.5048
44.28 0.2435 0.5561 0.0695 0.0304 4.439 23.315 20.908 3310.058 2.634 92.998 2.865 0.76 288538. 0.4804
48.30 0.2657 0.5888 0.0666 0.0300 4.379 23.002 20.019 3265.732 2.599 89.044 2.780 0.76 288895. 0.4562
52.33 0.2878 0.6189 0.0634 0.0295 4.303 22.599 19.082 3208.417 2.553 84.875 2.698 0.76 289271. 0.4321
56.36 0.3100 0.6464 0.0602 0.0289 4.207 22.098 18.097 3137.415 2.497 80.495 2.616 0.77 289666. 0.4082
60.38 0.3321 0.6713 0.0567 0.0281 4.093 21.497 17.065 3052.087 2.429 75.907 2.536 0.77 290080. 0.3842
64.41 0.3542 0.6936 0.0532 0.0271 3.958 20.791 15.988 2951.826 2.349 71.114 2.457 0.77 290513. 0.3602
68.43 0.3764 0.7132 0.0494 0.0261 3.804 19.980 14.868 2836.623 2.257 66.133 2.377 0.77 290965. 0.3362
72.46 0.3985 0.7298 0.0456 0.0249 3.630 19.066 13.712 2706.900 2.154 60.990 2.298 0.77 291436. 0.3120
76.48 0.4207 0.7431 0.0416 0.0236 3.437 18.053 12.524 2563.079 2.040 55.706 2.216 0.77 291926. 0.2876
80.51 0.4428 0.7526 0.0376 0.0221 3.226 16.944 11.309 2405.576 1.914 50.302 2.132 0.77 292436. 0.2630
84.53 0.4649 0.7575 0.0335 0.0206 2.997 15.741 10.071 2234.853 1.778 44.798 2.044 0.77 292965. 0.2379
88.56 0.4871 0.7567 0.0293 0.0189 2.751 14.450 8.815 2051.483 1.633 39.211 1.949 0.77 293513. 0.2122
92.58 0.5092 0.7484 0.0251 0.0171 2.489 13.074 7.546 1856.195 1.477 33.565 1.844 0.77 294081. 0.1858
96.61 0.5314 0.7298 0.0208 0.0152 2.213 11.621 6.268 1649.915 1.313 27.881 1.723 0.77 294669. 0.1582
100.64 0.5535 0.6961 0.0166 0.0132 1.923 10.099 4.988 1433.827 1.141 22.186 1.578 0.77 295277. 0.1292
104.66 0.5756 0.6387 0.0123 0.0111 1.622 8.519 3.711 1209.408 0.962 16.509 1.392 0.77 295905. 0.0983
108.69 0.5978 0.5404 0.0081 0.0090 1.312 6.892 2.447 978.460 0.779 10.882 1.134 0.78 296552. 0.0651
112.71 0.6199 0.3623 0.0040 0.0068 0.996 5.234 1.201 743.080 0.591 5.343 0.733 0.78 297219. 0.0295
116.74 0.6421 -0.0113 -0.0001 0.0046 0.675 3.546 -0.025 503.435 0.401 -0.109 -0.022 0.78 297880. 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 0.0936 0.0318 5.888 28.547 33.032 4390.663 3.225 146.927 3.412 0.83 309511. 0.7192
4.36 0.0221 0.0638 0.0922 0.0320 5.928 28.743 32.558 4420.846 3.247 144.819 3.340 0.83 309702. 0.6990
8.71 0.0442 0.1248 0.0908 0.0322 5.964 28.915 32.042 4447.245 3.267 142.522 3.268 0.83 309909. 0.6784
13.07 0.0664 0.1831 0.0892 0.0323 5.993 29.056 31.481 4468.925 3.283 140.026 3.195 0.83 310132. 0.6574
17.43 0.0885 0.2385 0.0875 0.0324 6.014 29.160 30.872 4484.942 3.294 137.319 3.122 0.83 310371. 0.6362
21.78 0.1106 0.2912 0.0856 0.0325 6.027 29.221 30.213 4494.292 3.301 134.389 3.049 0.83 310627. 0.6146
26.14 0.1327 0.3411 0.0836 0.0325 6.029 29.231 29.502 4495.939 3.303 131.226 2.976 0.83 310902. 0.5929
30.50 0.1548 0.3882 0.0814 0.0325 6.020 29.185 28.737 4488.790 3.297 127.820 2.904 0.83 311194. 0.5708
34.85 0.1769 0.4326 0.0791 0.0323 5.997 29.074 27.914 4471.723 3.285 124.163 2.831 0.83 311505. 0.5486
39.21 0.1991 0.4743 0.0766 0.0321 5.959 28.891 27.034 4443.602 3.264 120.249 2.759 0.83 311836. 0.5262
43.56 0.2212 0.5134 0.0739 0.0319 5.905 28.629 26.096 4403.280 3.234 116.073 2.688 0.83 312185. 0.5036
47.92 0.2433 0.5498 0.0711 0.0315 5.833 28.280 25.097 4349.644 3.195 111.633 2.617 0.83 312554. 0.4808
52.28 0.2654 0.5836 0.0681 0.0310 5.742 27.838 24.040 4281.618 3.145 106.928 2.547 0.83 312943. 0.4579
56.63 0.2875 0.6149 0.0649 0.0304 5.630 27.295 22.923 4198.185 3.084 101.961 2.477 0.83 313353. 0.4348
60.99 0.3096 0.6435 0.0616 0.0296 5.496 26.647 21.748 4098.463 3.011 96.736 2.407 0.83 313782. 0.4116
65.35 0.3318 0.6694 0.0581 0.0288 5.341 25.894 20.516 3982.601 2.925 91.256 2.337 0.83 314231. 0.3881
69.70 0.3539 0.6924 0.0545 0.0278 5.162 25.026 19.228 3849.067 2.827 85.525 2.266 0.83 314701. 0.3644
74.06 0.3760 0.7123 0.0507 0.0267 4.959 24.042 17.887 3697.865 2.716 79.562 2.194 0.83 315192. 0.3403
78.42 0.3981 0.7290 0.0468 0.0255 4.733 22.948 16.502 3529.539 2.593 73.399 2.121 0.83 315703. 0.3159
82.77 0.4202 0.7420 0.0427 0.0242 4.485 21.745 15.077 3344.487 2.457 67.062 2.045 0.83 316235. 0.2912
87.13 0.4424 0.7506 0.0386 0.0227 4.215 20.437 13.618 3143.268 2.309 60.575 1.965 0.83 316787. 0.2659
91.49 0.4645 0.7541 0.0344 0.0212 3.925 19.028 12.132 2926.668 2.150 53.963 1.880 0.83 317361. 0.2402
95.84 0.4866 0.7509 0.0301 0.0195 3.615 17.528 10.622 2695.869 1.980 47.248 1.787 0.83 317955. 0.2136
100.20 0.5087 0.7389 0.0258 0.0177 3.289 15.945 9.095 2452.365 1.801 40.455 1.682 0.84 318570. 0.1860
104.56 0.5308 0.7148 0.0214 0.0159 2.947 14.290 7.557 2197.903 1.614 33.613 1.559 0.84 319207. 0.1572
108.91 0.5529 0.6733 0.0170 0.0140 2.594 12.577 6.014 1934.486 1.421 26.752 1.410 0.84 319865. 0.1268
113.27 0.5751 0.6056 0.0127 0.0120 2.232 10.822 4.475 1664.541 1.223 19.907 1.220 0.84 320544. 0.0946
117.62 0.5972 0.4959 0.0084 0.0101 1.865 9.043 2.949 1390.880 1.022 13.118 0.962 0.84 321245. 0.0606
121.98 0.6193 0.3140 0.0041 0.0081 1.497 7.259 1.446 1116.527 0.820 6.430 0.587 0.84 321966. 0.0259
126.34 0.6414 -0.0104 -0.0001 0.0061 1.128 5.470 -0.035 841.270 0.618 -0.155 -0.019 0.84 322684. 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 0.0951 0.0366 8.466 38.114 38.932 6313.084 4.306 173.169 2.797 0.89 333273. 0.6400
4.77 0.0225 0.0577 0.0938 0.0366 8.476 38.158 38.394 6320.385 4.311 170.778 2.755 0.89 333483. 0.6261
9.55 0.0450 0.1136 0.0924 0.0366 8.475 38.157 37.804 6320.176 4.311 168.151 2.713 0.89 333710. 0.6117
14.32 0.0675 0.1677 0.0908 0.0366 8.464 38.105 37.157 6311.517 4.305 165.275 2.670 0.89 333955. 0.5969
19.10 0.0900 0.2199 0.0890 0.0365 8.440 37.996 36.451 6293.484 4.293 162.134 2.627 0.89 334220. 0.5817
23.87 0.1125 0.2703 0.0872 0.0363 8.402 37.825 35.682 6265.144 4.273 158.713 2.583 0.89 334504. 0.5659
28.65 0.1350 0.3188 0.0851 0.0361 8.349 37.585 34.847 6225.528 4.246 154.999 2.539 0.89 334808. 0.5496
33.42 0.1575 0.3654 0.0829 0.0358 8.279 37.272 33.943 6173.657 4.211 150.977 2.494 0.89 335133. 0.5328
38.19 0.1801 0.4099 0.0805 0.0354 8.192 36.879 32.967 6108.501 4.167 146.639 2.448 0.89 335478. 0.5154
42.97 0.2026 0.4523 0.0780 0.0349 8.085 36.399 31.919 6029.004 4.112 141.974 2.401 0.89 335846. 0.4975
47.74 0.2251 0.4927 0.0752 0.0344 7.958 35.826 30.795 5934.092 4.048 136.977 2.354 0.89 336235. 0.4790
52.52 0.2476 0.5308 0.0723 0.0337 7.808 35.153 29.596 5822.671 3.972 131.645 2.305 0.89 336646. 0.4600
57.29 0.2701 0.5667 0.0692 0.0330 7.635 34.375 28.322 5693.741 3.884 125.977 2.256 0.89 337079. 0.4403
62.06 0.2926 0.6002 0.0659 0.0321 7.438 33.485 26.973 5546.325 3.783 119.978 2.206 0.89 337535. 0.4201
66.84 0.3151 0.6313 0.0624 0.0312 7.214 32.478 25.551 5379.523 3.669 113.652 2.154 0.89 338013. 0.3994
71.61 0.3376 0.6595 0.0588 0.0301 6.966 31.361 24.057 5194.590 3.543 107.006 2.101 0.89 338514. 0.3778
76.39 0.3601 0.6842 0.0549 0.0289 6.696 30.144 22.492 4992.877 3.406 100.045 2.043 0.89 339037. 0.3554
81.16 0.3826 0.7051 0.0510 0.0277 6.404 28.832 20.864 4775.623 3.257 92.802 1.982 0.90 339584. 0.3319
85.94 0.4051 0.7216 0.0469 0.0263 6.091 27.423 19.181 4542.201 3.098 85.315 1.915 0.90 340153. 0.3076
90.71 0.4276 0.7316 0.0426 0.0249 5.769 25.971 17.449 4301.824 2.934 77.612 1.840 0.90 340745. 0.2818
95.48 0.4501 0.7344 0.0383 0.0235 5.434 24.466 15.675 4052.406 2.764 69.724 1.754 0.90 341360. 0.2547
100.26 0.4726 0.7298 0.0339 0.0219 5.081 22.873 13.869 3788.564 2.584 61.687 1.660 0.90 341998. 0.2268
105.03 0.4952 0.7156 0.0294 0.0203 4.710 21.205 12.035 3512.309 2.396 53.533 1.554 0.90 342660. 0.1977
109.81 0.5177 0.6891 0.0249 0.0187 4.327 19.479 10.183 3226.442 2.201 45.295 1.432 0.90 343344. 0.1675
114.58 0.5402 0.6461 0.0203 0.0170 3.935 17.716 8.321 2934.490 2.002 37.013 1.286 0.90 344052. 0.1361
119.36 0.5627 0.5807 0.0158 0.0153 3.540 15.936 6.459 2639.571 1.800 28.730 1.110 0.90 344784. 0.1034
124.13 0.5852 0.4849 0.0113 0.0136 3.145 14.159 4.608 2345.298 1.600 20.496 0.891 0.90 345540. 0.0702
128.90 0.6077 0.3468 0.0068 0.0119 2.757 12.410 2.781 2055.524 1.402 12.370 0.614 0.91 346318. 0.0375
133.68 0.6302 0.1486 0.0024 0.0103 2.378 10.706 0.991 1773.367 1.210 4.410 0.254 0.91 347119. 0.0093
138.45 0.6527
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 0.0951 0.0426 12.130 50.968 44.707 9045.229 5.758 198.856 2.242 0.95 357073. 0.5497
5.16 0.0227 0.0501 0.0940 0.0427 12.148 51.045 44.166 9058.753 5.767 196.453 2.211 0.95 357295. 0.5390
10.33 0.0454 0.0988 0.0927 0.0427 12.147 51.039 43.564 9057.786 5.766 193.773 2.181 0.95 357536. 0.5280
15.49 0.0682 0.1461 0.0913 0.0426 12.123 50.939 42.895 9040.101 5.755 190.795 2.152 0.95 357798. 0.5169
20.65 0.0909 0.1923 0.0897 0.0424 12.074 50.734 42.152 9003.668 5.732 187.494 2.123 0.95 358081. 0.5056
25.82 0.1136 0.2371 0.0880 0.0421 11.998 50.413 41.332 8946.694 5.696 183.847 2.095 0.95 358385. 0.4940
30.98 0.1363 0.2808 0.0860 0.0418 11.892 49.968 40.430 8867.686 5.645 179.831 2.068 0.95 358713. 0.4822
36.14 0.1590 0.3234 0.0839 0.0413 11.755 49.392 39.440 8765.467 5.580 175.429 2.041 0.95 359064. 0.4700
41.30 0.1817 0.3647 0.0816 0.0407 11.585 48.680 38.360 8639.077 5.500 170.624 2.014 0.95 359438. 0.4574
46.47 0.2045 0.4048 0.0791 0.0400 11.382 47.827 37.186 8487.821 5.404 165.402 1.987 0.95 359837. 0.4444
51.63 0.2272 0.4437 0.0764 0.0391 11.146 46.833 35.916 8311.305 5.291 159.755 1.960 0.95 360260. 0.4308
56.79 0.2499 0.4811 0.0735 0.0382 10.875 45.695 34.550 8109.387 5.163 153.679 1.932 0.96 360707. 0.4166
61.96 0.2726 0.5172 0.0704 0.0371 10.570 44.415 33.088 7882.257 5.018 147.176 1.904 0.96 361180. 0.4016
67.12 0.2953 0.5515 0.0671 0.0359 10.232 42.995 31.532 7630.185 4.858 140.252 1.874 0.96 361677. 0.3860
72.28 0.3180 0.5841 0.0636 0.0346 9.861 41.435 29.883 7353.420 4.681 132.917 1.843 0.96 362199. 0.3695
77.45 0.3408 0.6146 0.0599 0.0332 9.457 39.736 28.143 7051.944 4.489 125.181 1.810 0.96 362746. 0.3522
82.61 0.3635 0.6419 0.0560 0.0317 9.030 37.944 26.315 6733.811 4.287 117.051 1.773 0.96 363317. 0.3335
87.77 0.3862 0.6654 0.0519 0.0301 8.585 36.075 24.409 6402.197 4.076 108.569 1.729 0.96 363914. 0.3133
92.94 0.4089 0.6835 0.0477 0.0286 8.133 34.174 22.433 6064.727 3.861 99.781 1.678 0.96 364535. 0.2914
98.10 0.4316 0.6952 0.0434 0.0270 7.675 32.250 20.398 5723.363 3.644 90.731 1.617 0.96 365182. 0.2677
103.26 0.4544 0.6914 0.0390 0.0256 7.290 30.633 18.305 5436.456 3.461 81.422 1.527 0.96 365853. 0.2396
108.42 0.4771 0.6759 0.0344 0.0243 6.917 29.065 16.172 5158.079 3.284 71.931 1.422 0.96 366550. 0.2097
113.59 0.4998 0.6491 0.0298 0.0230 6.537 27.468 14.010 4874.652 3.103 62.315 1.304 0.96 367272. 0.1789
118.75 0.5225 0.6088 0.0252 0.0216 6.154 25.858 11.832 4588.883 2.921 52.627 1.169 0.97 368018. 0.1475
123.91 0.5452 0.5524 0.0205 0.0203 5.773 24.255 9.651 4304.566 2.740 42.928 1.017 0.97 368791. 0.1159
129.08 0.5679 0.4772 0.0159 0.0190 5.398 22.682 7.483 4025.339 2.563 33.286 0.843 0.97 369589. 0.0846
134.24 0.5907 0.3800 0.0114 0.0177 5.035 21.158 5.346 3754.857 2.390 23.778 0.646 0.97 370413. 0.0548
139.40 0.6134 0.2583 0.0069 0.0165 4.687 19.693 3.256 3494.839 2.225 14.483 0.423 0.97 371264. 0.0280
144.57 0.6361 0.1087 0.0026 0.0153 4.351 18.284 1.227 3244.781 2.066 5.458 0.172 0.97 372146. 0.0070
149.73 0.6588