16x6E (16x6E.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 0.0685 0.0253 0.002 0.135 0.143 1.593 0.015 0.637 40.741 0.06 23855. 0.5653 0.27 0.0176 0.0464 0.0671 0.0254 0.002 0.135 0.140 1.598 0.015 0.624 39.806 0.06 23866. 0.5467 0.53 0.0351 0.0906 0.0657 0.0254 0.002 0.135 0.137 1.601 0.015 0.610 38.863 0.06 23877. 0.5279 0.80 0.0527 0.1326 0.0642 0.0255 0.002 0.136 0.134 1.603 0.015 0.596 37.912 0.06 23889. 0.5090 1.06 0.0702 0.1724 0.0626 0.0255 0.002 0.136 0.131 1.604 0.015 0.581 36.954 0.06 23902. 0.4898 1.33 0.0878 0.2098 0.0609 0.0255 0.002 0.135 0.127 1.602 0.015 0.565 35.989 0.06 23915. 0.4706 1.60 0.1053 0.2450 0.0591 0.0254 0.002 0.135 0.123 1.599 0.015 0.549 35.016 0.06 23930. 0.4512 1.86 0.1229 0.2778 0.0573 0.0253 0.002 0.135 0.120 1.594 0.015 0.532 34.034 0.06 23945. 0.4316 2.13 0.1404 0.3082 0.0553 0.0252 0.002 0.134 0.116 1.586 0.015 0.514 33.042 0.06 23960. 0.4119 2.39 0.1580 0.3362 0.0533 0.0251 0.002 0.133 0.111 1.577 0.015 0.495 32.038 0.06 23977. 0.3921 2.66 0.1756 0.3617 0.0512 0.0249 0.002 0.132 0.107 1.565 0.015 0.476 31.021 0.06 23995. 0.3721 2.93 0.1931 0.3846 0.0491 0.0246 0.002 0.131 0.102 1.550 0.015 0.456 29.987 0.06 24013. 0.3520 3.19 0.2107 0.4049 0.0468 0.0244 0.002 0.130 0.098 1.533 0.015 0.435 28.933 0.06 24032. 0.3318 3.46 0.2282 0.4223 0.0445 0.0240 0.002 0.128 0.093 1.512 0.014 0.413 27.856 0.06 24052. 0.3113 3.72 0.2458 0.4367 0.0420 0.0237 0.002 0.126 0.088 1.489 0.014 0.391 26.751 0.06 24074. 0.2907 3.99 0.2633 0.4480 0.0395 0.0232 0.002 0.124 0.083 1.463 0.014 0.367 25.614 0.06 24096. 0.2700 4.26 0.2809 0.4560 0.0370 0.0228 0.002 0.121 0.077 1.434 0.014 0.344 24.439 0.06 24119. 0.2491 4.52 0.2984 0.4603 0.0344 0.0223 0.002 0.118 0.072 1.402 0.013 0.319 23.220 0.06 24143. 0.2281 4.79 0.3160 0.4607 0.0317 0.0217 0.002 0.116 0.066 1.367 0.013 0.294 21.951 0.06 24167. 0.2070 5.05 0.3336 0.4569 0.0289 0.0211 0.002 0.112 0.060 1.329 0.013 0.269 20.621 0.06 24193. 0.1859 5.32 0.3511 0.4483 0.0261 0.0205 0.002 0.109 0.055 1.288 0.012 0.243 19.220 0.06 24220. 0.1647 5.59 0.3687 0.4344 0.0233 0.0198 0.002 0.105 0.049 1.245 0.012 0.217 17.737 0.06 24248. 0.1435 5.85 0.3862 0.4145 0.0204 0.0190 0.002 0.101 0.043 1.198 0.011 0.190 16.156 0.06 24277. 0.1224 6.12 0.4038 0.3878 0.0175 0.0183 0.002 0.097 0.037 1.149 0.011 0.163 14.459 0.06 24307. 0.1015 6.38 0.4213 0.3533 0.0146 0.0174 0.001 0.093 0.031 1.097 0.010 0.136 12.624 0.06 24338. 0.0809 6.65 0.4389 0.3097 0.0117 0.0166 0.001 0.088 0.024 1.043 0.010 0.109 10.624 0.06 24371. 0.0609 6.92 0.4564 0.2554 0.0088 0.0157 0.001 0.083 0.018 0.986 0.009 0.081 8.425 0.06 24404. 0.0418 7.18 0.4740 0.1884 0.0059 0.0147 0.001 0.078 0.012 0.927 0.009 0.054 5.985 0.06 24438. 0.0243 7.45 0.4916 0.1060 0.0030 0.0138 0.001 0.073 0.006 0.865 0.008 0.028 3.248 0.06 24473. 0.0094 7.71 0.5091 0.0044 0.0001 0.0127 0.001 0.068 0.000 0.802 0.008 0.001 0.130 0.06 24509. 0.0001 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 0.0688 0.0227 0.015 0.483 0.575 11.423 0.055 2.556 22.817 0.13 47710. 0.6343 0.54 0.0177 0.0523 0.0674 0.0228 0.015 0.485 0.563 11.469 0.055 2.504 22.268 0.13 47731. 0.6128 1.07 0.0353 0.1019 0.0659 0.0229 0.015 0.486 0.551 11.504 0.055 2.450 21.717 0.13 47754. 0.5911 1.61 0.0530 0.1490 0.0644 0.0229 0.015 0.487 0.538 11.528 0.055 2.393 21.166 0.13 47778. 0.5693 2.14 0.0707 0.1935 0.0628 0.0229 0.015 0.488 0.524 11.538 0.055 2.333 20.615 0.13 47804. 0.5475 2.68 0.0883 0.2354 0.0611 0.0229 0.015 0.487 0.510 11.534 0.055 2.270 20.065 0.13 47831. 0.5256 3.21 0.1060 0.2748 0.0593 0.0229 0.015 0.487 0.495 11.514 0.055 2.204 19.515 0.13 47860. 0.5037 3.75 0.1237 0.3115 0.0574 0.0228 0.015 0.485 0.480 11.477 0.055 2.135 18.964 0.13 47890. 0.4818 4.28 0.1413 0.3457 0.0555 0.0227 0.015 0.483 0.464 11.422 0.055 2.062 18.413 0.13 47922. 0.4598 4.82 0.1590 0.3772 0.0535 0.0225 0.015 0.479 0.447 11.346 0.054 1.987 17.860 0.13 47956. 0.4378 5.35 0.1767 0.4061 0.0514 0.0223 0.015 0.475 0.429 11.249 0.054 1.909 17.304 0.13 47991. 0.4157 5.89 0.1943 0.4322 0.0492 0.0221 0.015 0.470 0.411 11.129 0.053 1.827 16.744 0.13 48028. 0.3936 6.42 0.2120 0.4556 0.0469 0.0218 0.015 0.464 0.392 10.986 0.052 1.743 16.178 0.13 48067. 0.3714 6.96 0.2297 0.4760 0.0445 0.0215 0.015 0.457 0.372 10.816 0.052 1.655 15.604 0.13 48108. 0.3491 7.49 0.2473 0.4935 0.0421 0.0211 0.014 0.449 0.352 10.621 0.051 1.564 15.019 0.13 48151. 0.3267 8.03 0.2650 0.5077 0.0396 0.0207 0.014 0.440 0.331 10.400 0.050 1.471 14.422 0.13 48195. 0.3042 8.57 0.2826 0.5185 0.0370 0.0202 0.014 0.429 0.309 10.153 0.048 1.375 13.809 0.13 48242. 0.2816 9.10 0.3003 0.5257 0.0344 0.0196 0.013 0.418 0.287 9.879 0.047 1.277 13.176 0.13 48290. 0.2589 9.64 0.3180 0.5288 0.0316 0.0190 0.013 0.405 0.264 9.580 0.046 1.176 12.518 0.13 48341. 0.2361 10.17 0.3356 0.5275 0.0289 0.0184 0.012 0.391 0.241 9.254 0.044 1.074 11.830 0.13 48393. 0.2131 10.71 0.3533 0.5212 0.0261 0.0177 0.012 0.376 0.218 8.902 0.043 0.969 11.105 0.13 48448. 0.1901 11.24 0.3710 0.5092 0.0232 0.0169 0.011 0.360 0.194 8.523 0.041 0.864 10.333 0.13 48504. 0.1670 11.78 0.3886 0.4907 0.0204 0.0161 0.011 0.343 0.170 8.118 0.039 0.757 9.504 0.13 48563. 0.1437 12.31 0.4063 0.4644 0.0175 0.0153 0.010 0.325 0.146 7.688 0.037 0.649 8.603 0.13 48623. 0.1205 12.85 0.4240 0.4288 0.0145 0.0144 0.010 0.306 0.121 7.234 0.035 0.540 7.613 0.13 48686. 0.0973 13.38 0.4416 0.3819 0.0116 0.0134 0.009 0.285 0.097 6.755 0.032 0.431 6.509 0.13 48751. 0.0743 13.92 0.4593 0.3208 0.0087 0.0124 0.008 0.264 0.073 6.255 0.030 0.322 5.257 0.13 48818. 0.0519 14.45 0.4770 0.2416 0.0058 0.0114 0.008 0.242 0.048 5.734 0.027 0.214 3.813 0.13 48888. 0.0307 14.99 0.4946 0.1387 0.0029 0.0103 0.007 0.220 0.024 5.194 0.025 0.107 2.110 0.13 48959. 0.0120 15.52 0.5123 0.0023 0.0000 0.0092 0.006 0.196 0.000 4.635 0.022 0.002 0.034 0.13 49030. 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 0.0690 0.0216 0.049 1.033 1.298 36.655 0.117 5.772 16.058 0.19 71564. 0.6709 0.81 0.0177 0.0553 0.0676 0.0217 0.049 1.037 1.271 36.822 0.117 5.655 15.662 0.19 71596. 0.6476 1.61 0.0355 0.1079 0.0662 0.0218 0.050 1.041 1.244 36.954 0.118 5.532 15.266 0.19 71631. 0.6244 2.42 0.0532 0.1576 0.0646 0.0218 0.050 1.044 1.215 37.045 0.118 5.403 14.872 0.19 71667. 0.6011 3.22 0.0709 0.2046 0.0630 0.0218 0.050 1.045 1.184 37.090 0.118 5.267 14.480 0.19 71706. 0.5778 4.03 0.0886 0.2489 0.0613 0.0218 0.050 1.045 1.152 37.085 0.118 5.124 14.089 0.19 71747. 0.5546 4.84 0.1064 0.2904 0.0595 0.0218 0.050 1.043 1.118 37.025 0.118 4.974 13.700 0.19 71790. 0.5313 5.64 0.1241 0.3292 0.0576 0.0217 0.049 1.040 1.083 36.904 0.117 4.818 13.313 0.19 71836. 0.5081 6.45 0.1418 0.3654 0.0557 0.0216 0.049 1.035 1.046 36.718 0.117 4.655 12.927 0.19 71884. 0.4849 7.25 0.1596 0.3988 0.0536 0.0215 0.049 1.027 1.008 36.462 0.116 4.484 12.541 0.19 71935. 0.4618 8.06 0.1773 0.4294 0.0515 0.0213 0.048 1.018 0.968 36.131 0.115 4.307 12.155 0.19 71989. 0.4386 8.86 0.1950 0.4573 0.0493 0.0210 0.048 1.006 0.927 35.720 0.114 4.122 11.768 0.19 72045. 0.4155 9.67 0.2128 0.4824 0.0470 0.0207 0.047 0.992 0.884 35.224 0.112 3.931 11.379 0.19 72103. 0.3923 10.48 0.2305 0.5046 0.0446 0.0204 0.046 0.976 0.839 34.638 0.110 3.732 10.986 0.19 72165. 0.3690 11.28 0.2482 0.5237 0.0422 0.0200 0.046 0.957 0.793 33.961 0.108 3.526 10.588 0.19 72229. 0.3457 12.09 0.2659 0.5397 0.0396 0.0195 0.045 0.935 0.745 33.191 0.106 3.315 10.183 0.19 72296. 0.3224 12.89 0.2837 0.5522 0.0370 0.0190 0.043 0.911 0.696 32.328 0.103 3.097 9.769 0.19 72367. 0.2989 13.70 0.3014 0.5611 0.0344 0.0185 0.042 0.884 0.646 31.372 0.100 2.874 9.343 0.19 72440. 0.2754 14.51 0.3191 0.5661 0.0317 0.0178 0.041 0.854 0.595 30.323 0.097 2.647 8.901 0.19 72516. 0.2518 15.31 0.3369 0.5665 0.0289 0.0172 0.039 0.822 0.543 29.179 0.093 2.415 8.439 0.19 72595. 0.2280 16.12 0.3546 0.5619 0.0261 0.0164 0.037 0.787 0.490 27.940 0.089 2.179 7.953 0.19 72677. 0.2041 16.92 0.3723 0.5516 0.0232 0.0157 0.036 0.750 0.436 26.608 0.085 1.940 7.434 0.19 72763. 0.1801 17.73 0.3901 0.5344 0.0203 0.0148 0.034 0.710 0.382 25.183 0.080 1.698 6.875 0.19 72851. 0.1558 18.54 0.4078 0.5091 0.0174 0.0139 0.032 0.667 0.327 23.666 0.075 1.454 6.265 0.19 72943. 0.1313 19.34 0.4255 0.4737 0.0145 0.0130 0.030 0.622 0.272 22.062 0.070 1.209 5.586 0.19 73038. 0.1068 20.15 0.4432 0.4257 0.0115 0.0120 0.027 0.574 0.216 20.373 0.065 0.963 4.819 0.19 73136. 0.0822 20.95 0.4610 0.3613 0.0086 0.0110 0.025 0.524 0.161 18.605 0.059 0.718 3.933 0.19 73237. 0.0579 21.76 0.4787 0.2750 0.0057 0.0099 0.022 0.472 0.107 16.765 0.053 0.474 2.883 0.19 73342. 0.0345 22.57 0.4964 0.1582 0.0028 0.0087 0.020 0.419 0.052 14.859 0.047 0.233 1.600 0.19 73449. 0.0134 23.37 0.5142 -0.0050 -0.0001 0.0076 0.017 0.363 -0.001 12.877 0.041 -0.006 -0.049 0.19 73555. 0.0000 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 0.0693 0.0210 0.113 1.784 2.317 84.429 0.202 10.307 12.449 0.25 95417. 0.6949 1.08 0.0177 0.0572 0.0679 0.0211 0.114 1.793 2.270 84.843 0.203 10.099 12.137 0.25 95460. 0.6707 2.15 0.0355 0.1115 0.0665 0.0211 0.114 1.800 2.221 85.170 0.203 9.879 11.828 0.25 95506. 0.6464 3.23 0.0532 0.1629 0.0649 0.0212 0.115 1.805 2.169 85.400 0.204 9.648 11.520 0.25 95555. 0.6222 4.30 0.0710 0.2115 0.0633 0.0212 0.115 1.807 2.114 85.519 0.204 9.405 11.214 0.25 95607. 0.5980 5.38 0.0887 0.2572 0.0616 0.0212 0.115 1.807 2.057 85.517 0.204 9.150 10.911 0.25 95662. 0.5739 6.45 0.1065 0.3001 0.0598 0.0212 0.114 1.804 1.997 85.380 0.204 8.883 10.609 0.25 95720. 0.5498 7.53 0.1242 0.3402 0.0579 0.0211 0.114 1.798 1.934 85.098 0.203 8.604 10.310 0.25 95781. 0.5259 8.60 0.1419 0.3776 0.0559 0.0210 0.114 1.789 1.869 84.657 0.202 8.312 10.012 0.25 95845. 0.5019 9.68 0.1597 0.4122 0.0539 0.0209 0.113 1.776 1.800 84.045 0.201 8.008 9.716 0.25 95913. 0.4781 10.75 0.1774 0.4441 0.0517 0.0207 0.112 1.759 1.729 83.252 0.199 7.691 9.420 0.25 95984. 0.4543 11.83 0.1952 0.4732 0.0495 0.0204 0.110 1.738 1.655 82.266 0.196 7.362 9.125 0.25 96059. 0.4305 12.90 0.2129 0.4994 0.0472 0.0201 0.109 1.713 1.578 81.072 0.194 7.019 8.829 0.25 96138. 0.4067 13.98 0.2306 0.5228 0.0448 0.0198 0.107 1.683 1.498 79.659 0.190 6.664 8.531 0.25 96220. 0.3829 15.05 0.2484 0.5432 0.0424 0.0194 0.105 1.649 1.416 78.023 0.186 6.297 8.230 0.25 96306. 0.3591 16.13 0.2661 0.5604 0.0398 0.0189 0.102 1.609 1.331 76.162 0.182 5.919 7.925 0.25 96396. 0.3353 17.20 0.2839 0.5743 0.0372 0.0184 0.099 1.565 1.243 74.074 0.177 5.531 7.614 0.25 96490. 0.3114 18.28 0.3016 0.5846 0.0345 0.0178 0.096 1.516 1.154 71.759 0.171 5.133 7.295 0.26 96587. 0.2874 19.35 0.3194 0.5909 0.0318 0.0172 0.093 1.463 1.063 69.214 0.165 4.727 6.964 0.26 96689. 0.2633 20.43 0.3371 0.5929 0.0290 0.0165 0.089 1.404 0.970 66.437 0.159 4.313 6.620 0.26 96795. 0.2391 21.51 0.3548 0.5899 0.0262 0.0158 0.085 1.340 0.875 63.429 0.151 3.892 6.257 0.26 96904. 0.2146 22.58 0.3726 0.5811 0.0233 0.0149 0.081 1.272 0.779 60.191 0.144 3.465 5.871 0.26 97018. 0.1900 23.66 0.3903 0.5655 0.0204 0.0141 0.076 1.199 0.682 56.725 0.135 3.034 5.453 0.26 97137. 0.1652 24.73 0.4081 0.5416 0.0175 0.0132 0.071 1.121 0.584 53.036 0.127 2.598 4.996 0.26 97259. 0.1400 25.81 0.4258 0.5073 0.0145 0.0122 0.066 1.038 0.486 49.130 0.117 2.161 4.484 0.26 97386. 0.1146 26.88 0.4436 0.4597 0.0116 0.0112 0.060 0.951 0.387 45.018 0.107 1.722 3.901 0.26 97517. 0.0890 27.96 0.4613 0.3945 0.0086 0.0101 0.055 0.860 0.289 40.712 0.097 1.285 3.219 0.26 97652. 0.0634 29.03 0.4790 0.3048 0.0057 0.0090 0.049 0.766 0.191 36.230 0.086 0.851 2.395 0.26 97792. 0.0384 30.11 0.4968 0.1796 0.0028 0.0078 0.042 0.667 0.095 31.588 0.075 0.422 1.361 0.26 97935. 0.0154 31.18 0.5145 -0.0027 0.0000 0.0066 0.036 0.565 -0.001 26.755 0.064 -0.005 -0.020 0.26 98076. 0.0000 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 0.0697 0.0206 0.217 2.741 3.640 162.119 0.310 16.192 10.185 0.32 119268. 0.7126 1.36 0.0180 0.0592 0.0683 0.0207 0.219 2.755 3.566 162.954 0.311 15.861 9.925 0.32 119323. 0.6873 2.72 0.0359 0.1153 0.0668 0.0208 0.219 2.766 3.487 163.613 0.312 15.512 9.668 0.32 119381. 0.6621 4.08 0.0539 0.1684 0.0652 0.0209 0.220 2.774 3.405 164.074 0.313 15.144 9.412 0.32 119443. 0.6369 5.44 0.0718 0.2185 0.0635 0.0209 0.220 2.778 3.318 164.309 0.314 14.757 9.159 0.32 119509. 0.6118 6.80 0.0898 0.2656 0.0618 0.0209 0.220 2.777 3.227 164.295 0.314 14.352 8.908 0.32 119579. 0.5868 8.16 0.1077 0.3098 0.0600 0.0209 0.220 2.772 3.131 164.007 0.313 13.926 8.659 0.32 119653. 0.5619 9.52 0.1257 0.3511 0.0580 0.0208 0.219 2.763 3.031 163.420 0.312 13.481 8.412 0.32 119731. 0.5371 10.88 0.1436 0.3896 0.0560 0.0207 0.218 2.747 2.926 162.508 0.310 13.016 8.167 0.32 119813. 0.5124 12.24 0.1616 0.4253 0.0540 0.0205 0.216 2.726 2.817 161.247 0.308 12.531 7.924 0.32 119899. 0.4878 13.60 0.1795 0.4581 0.0518 0.0203 0.214 2.698 2.703 159.614 0.305 12.025 7.682 0.32 119990. 0.4632 14.96 0.1975 0.4881 0.0495 0.0200 0.211 2.664 2.585 157.582 0.301 11.499 7.441 0.32 120085. 0.4387 16.32 0.2155 0.5152 0.0472 0.0197 0.208 2.622 2.462 155.125 0.296 10.952 7.199 0.32 120186. 0.4143 17.68 0.2334 0.5393 0.0447 0.0194 0.204 2.573 2.335 152.219 0.291 10.385 6.957 0.32 120290. 0.3898 19.04 0.2514 0.5604 0.0422 0.0189 0.200 2.516 2.203 148.856 0.284 9.799 6.712 0.32 120400. 0.3654 20.40 0.2693 0.5783 0.0396 0.0184 0.194 2.452 2.067 145.034 0.277 9.195 6.465 0.32 120515. 0.3409 21.76 0.2873 0.5927 0.0369 0.0179 0.189 2.379 1.928 140.748 0.269 8.575 6.213 0.32 120634. 0.3163 23.12 0.3052 0.6035 0.0342 0.0173 0.182 2.299 1.785 135.994 0.260 7.940 5.954 0.32 120759. 0.2917 24.48 0.3232 0.6103 0.0314 0.0166 0.175 2.211 1.639 130.769 0.250 7.292 5.686 0.32 120889. 0.2670 25.84 0.3411 0.6126 0.0286 0.0159 0.168 2.114 1.491 125.070 0.239 6.631 5.407 0.32 121024. 0.2421 27.20 0.3591 0.6096 0.0257 0.0151 0.159 2.010 1.340 118.898 0.227 5.960 5.112 0.32 121164. 0.2170 28.56 0.3771 0.6006 0.0227 0.0143 0.151 1.898 1.187 112.254 0.214 5.280 4.796 0.32 121310. 0.1916 29.92 0.3950 0.5843 0.0198 0.0134 0.141 1.777 1.032 105.146 0.201 4.592 4.454 0.32 121460. 0.1660 31.28 0.4130 0.5589 0.0168 0.0124 0.131 1.650 0.877 97.583 0.186 3.900 4.075 0.32 121617. 0.1399 32.65 0.4309 0.5220 0.0138 0.0114 0.120 1.514 0.720 89.581 0.171 3.204 3.647 0.32 121779. 0.1135 34.01 0.4489 0.4697 0.0108 0.0103 0.109 1.372 0.564 81.164 0.155 2.508 3.151 0.32 121946. 0.0868 35.37 0.4668 0.3965 0.0078 0.0092 0.097 1.223 0.408 72.361 0.138 1.815 2.557 0.32 122119. 0.0599 36.73 0.4848 0.2928 0.0049 0.0080 0.085 1.068 0.253 63.207 0.121 1.127 1.819 0.32 122298. 0.0336 38.09 0.5027 0.1422 0.0019 0.0068 0.072 0.908 0.101 53.736 0.103 0.449 0.852 0.32 122480. 0.0099 39.45 0.5207 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 0.0702 0.0204 0.372 3.909 5.277 277.523 0.442 23.470 8.624 0.38 143117. 0.7265 1.63 0.0179 0.0599 0.0688 0.0205 0.374 3.930 5.169 278.977 0.444 22.993 8.404 0.38 143183. 0.7007 3.25 0.0358 0.1167 0.0672 0.0206 0.376 3.946 5.056 280.126 0.446 22.489 8.186 0.38 143253. 0.6751 4.88 0.0536 0.1704 0.0657 0.0207 0.377 3.957 4.937 280.926 0.447 21.959 7.971 0.38 143327. 0.6495 6.50 0.0715 0.2211 0.0640 0.0207 0.377 3.963 4.812 281.336 0.448 21.402 7.757 0.38 143406. 0.6240 8.13 0.0894 0.2689 0.0622 0.0207 0.377 3.963 4.680 281.313 0.448 20.817 7.546 0.38 143490. 0.5987 9.75 0.1073 0.3137 0.0604 0.0207 0.377 3.956 4.542 280.811 0.447 20.205 7.337 0.38 143578. 0.5735 11.38 0.1252 0.3557 0.0585 0.0206 0.375 3.941 4.398 279.789 0.445 19.563 7.130 0.38 143671. 0.5484 13.00 0.1430 0.3948 0.0565 0.0205 0.373 3.919 4.247 278.203 0.443 18.893 6.925 0.38 143769. 0.5234 14.63 0.1609 0.4311 0.0544 0.0203 0.370 3.888 4.090 276.010 0.439 18.193 6.721 0.38 143873. 0.4985 16.25 0.1788 0.4646 0.0522 0.0201 0.366 3.848 3.926 273.169 0.435 17.464 6.519 0.38 143981. 0.4737 17.88 0.1967 0.4953 0.0500 0.0198 0.362 3.798 3.756 269.636 0.429 16.707 6.318 0.38 144095. 0.4490 19.51 0.2146 0.5231 0.0476 0.0195 0.356 3.738 3.579 265.364 0.422 15.919 6.117 0.38 144215. 0.4244 21.13 0.2324 0.5480 0.0452 0.0192 0.349 3.667 3.395 260.311 0.414 15.102 5.916 0.38 144340. 0.3998 22.76 0.2503 0.5700 0.0426 0.0187 0.341 3.585 3.205 254.460 0.405 14.257 5.713 0.38 144471. 0.3751 24.38 0.2682 0.5888 0.0400 0.0182 0.332 3.491 3.010 247.808 0.394 13.387 5.509 0.38 144608. 0.3505 26.01 0.2861 0.6044 0.0374 0.0177 0.322 3.386 2.809 240.346 0.383 12.494 5.301 0.38 144751. 0.3258 27.63 0.3040 0.6164 0.0346 0.0171 0.311 3.269 2.603 232.067 0.369 11.579 5.088 0.38 144899. 0.3011 29.26 0.3218 0.6244 0.0318 0.0164 0.299 3.141 2.393 222.965 0.355 10.645 4.868 0.38 145054. 0.2762 30.88 0.3397 0.6282 0.0290 0.0157 0.286 3.001 2.179 213.034 0.339 9.693 4.640 0.38 145215. 0.2512 32.51 0.3576 0.6269 0.0261 0.0149 0.271 2.849 1.962 202.276 0.322 8.725 4.398 0.38 145382. 0.2259 34.13 0.3755 0.6197 0.0232 0.0140 0.256 2.686 1.741 190.693 0.303 7.744 4.141 0.38 145556. 0.2004 35.76 0.3934 0.6055 0.0202 0.0131 0.239 2.512 1.518 178.295 0.284 6.753 3.862 0.38 145736. 0.1745 37.39 0.4112 0.5824 0.0172 0.0121 0.221 2.326 1.293 165.102 0.263 5.753 3.553 0.38 145922. 0.1482 39.01 0.4291 0.5480 0.0142 0.0111 0.203 2.129 1.068 151.139 0.241 4.749 3.204 0.38 146115. 0.1214 40.64 0.4470 0.4986 0.0112 0.0100 0.183 1.922 0.842 136.445 0.217 3.745 2.799 0.38 146314. 0.0942 42.26 0.4649 0.4281 0.0082 0.0089 0.162 1.706 0.617 121.070 0.193 2.744 2.311 0.38 146520. 0.0666 43.89 0.4828 0.3269 0.0052 0.0077 0.141 1.480 0.394 105.078 0.167 1.751 1.699 0.39 146733. 0.0391 45.51 0.5006 0.1770 0.0023 0.0065 0.119 1.247 0.173 88.528 0.141 0.770 0.887 0.39 146950. 0.0135 47.14 0.5185 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 0.0707 0.0203 0.589 5.302 7.239 439.086 0.599 32.197 7.477 0.44 166963. 0.7378 1.88 0.0178 0.0602 0.0693 0.0205 0.592 5.330 7.093 441.389 0.602 31.548 7.288 0.44 167040. 0.7118 3.77 0.0355 0.1172 0.0678 0.0205 0.594 5.352 6.939 443.206 0.605 30.863 7.101 0.44 167121. 0.6860 5.65 0.0533 0.1713 0.0662 0.0206 0.596 5.367 6.777 444.467 0.606 30.143 6.915 0.44 167208. 0.6602 7.53 0.0710 0.2223 0.0646 0.0206 0.597 5.374 6.606 445.107 0.607 29.385 6.732 0.44 167300. 0.6346 9.42 0.0888 0.2704 0.0628 0.0206 0.597 5.374 6.428 445.057 0.607 28.591 6.551 0.44 167396. 0.6091 11.30 0.1065 0.3156 0.0610 0.0206 0.596 5.364 6.240 444.248 0.606 27.758 6.371 0.44 167499. 0.5837 13.18 0.1243 0.3579 0.0591 0.0205 0.594 5.344 6.045 442.611 0.604 26.886 6.194 0.44 167607. 0.5585 15.06 0.1420 0.3975 0.0571 0.0204 0.590 5.314 5.840 440.079 0.600 25.975 6.019 0.44 167721. 0.5334 16.95 0.1598 0.4343 0.0550 0.0202 0.585 5.272 5.626 436.584 0.596 25.025 5.845 0.44 167840. 0.5084 18.83 0.1775 0.4683 0.0528 0.0200 0.579 5.217 5.404 432.062 0.589 24.035 5.673 0.44 167966. 0.4836 20.71 0.1953 0.4995 0.0505 0.0198 0.572 5.149 5.172 426.442 0.582 23.005 5.501 0.45 168098. 0.4588 22.60 0.2131 0.5280 0.0482 0.0194 0.563 5.067 4.932 419.653 0.572 21.936 5.330 0.45 168236. 0.4341 24.48 0.2308 0.5537 0.0458 0.0191 0.552 4.970 4.682 411.624 0.562 20.826 5.159 0.45 168381. 0.4094 26.36 0.2486 0.5764 0.0432 0.0186 0.540 4.858 4.424 402.326 0.549 19.679 4.988 0.45 168532. 0.3847 28.25 0.2663 0.5962 0.0406 0.0182 0.525 4.730 4.158 391.751 0.534 18.497 4.815 0.45 168690. 0.3601 30.13 0.2841 0.6128 0.0380 0.0176 0.509 4.587 3.886 379.886 0.518 17.283 4.639 0.45 168855. 0.3354 32.01 0.3018 0.6259 0.0352 0.0170 0.492 4.428 3.606 366.721 0.500 16.040 4.460 0.45 169027. 0.3106 33.89 0.3196 0.6353 0.0324 0.0163 0.472 4.253 3.320 352.244 0.481 14.770 4.276 0.45 169205. 0.2857 35.78 0.3373 0.6406 0.0296 0.0156 0.451 4.062 3.029 336.448 0.459 13.475 4.084 0.45 169391. 0.2607 37.66 0.3551 0.6411 0.0267 0.0148 0.428 3.856 2.734 319.330 0.436 12.159 3.883 0.45 169584. 0.2354 39.54 0.3728 0.6360 0.0238 0.0139 0.404 3.633 2.434 300.897 0.410 10.825 3.668 0.45 169784. 0.2099 41.43 0.3906 0.6241 0.0208 0.0130 0.377 3.395 2.130 281.162 0.384 9.476 3.437 0.45 169991. 0.1839 43.31 0.4083 0.6039 0.0178 0.0121 0.349 3.141 1.824 260.153 0.355 8.115 3.181 0.45 170206. 0.1576 45.19 0.4261 0.5730 0.0148 0.0110 0.319 2.873 1.517 237.909 0.325 6.748 2.892 0.45 170428. 0.1306 47.08 0.4439 0.5277 0.0118 0.0099 0.288 2.590 1.209 214.488 0.293 5.378 2.557 0.45 170658. 0.1031 48.96 0.4616 0.4623 0.0088 0.0088 0.255 2.294 0.902 189.968 0.259 4.013 2.154 0.45 170896. 0.0750 50.84 0.4794 0.3672 0.0058 0.0076 0.221 1.986 0.597 164.446 0.224 2.657 1.648 0.45 171140. 0.0467 52.72 0.4971 0.2249 0.0029 0.0064 0.185 1.667 0.296 138.025 0.188 1.317 0.973 0.45 171392. 0.0194 54.61 0.5149 -0.0046 0.0000 0.0051 0.148 1.333 -0.005 110.400 0.151 -0.021 -0.019 0.45 171632. 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 0.0714 0.0204 0.880 6.933 9.543 656.172 0.783 42.448 6.597 0.51 190806. 0.7473 2.15 0.0178 0.0607 0.0700 0.0205 0.885 6.969 9.351 659.604 0.787 41.593 6.430 0.51 190894. 0.7211 4.31 0.0355 0.1183 0.0684 0.0206 0.888 6.997 9.148 662.294 0.791 40.690 6.265 0.51 190988. 0.6949 6.46 0.0533 0.1728 0.0668 0.0206 0.891 7.017 8.934 664.135 0.793 39.740 6.102 0.51 191087. 0.6689 8.61 0.0711 0.2243 0.0652 0.0206 0.892 7.026 8.710 665.025 0.794 38.742 5.940 0.51 191193. 0.6429 10.77 0.0888 0.2729 0.0634 0.0206 0.892 7.024 8.474 664.863 0.794 37.694 5.781 0.51 191304. 0.6172 12.92 0.1066 0.3186 0.0616 0.0206 0.890 7.011 8.227 663.544 0.792 36.595 5.624 0.51 191422. 0.5916 15.07 0.1244 0.3614 0.0596 0.0205 0.886 6.983 7.969 660.962 0.789 35.445 5.468 0.51 191546. 0.5661 17.23 0.1421 0.4014 0.0576 0.0204 0.881 6.942 7.699 657.016 0.784 34.244 5.315 0.51 191676. 0.5408 19.38 0.1599 0.4387 0.0555 0.0202 0.874 6.884 7.417 651.604 0.778 32.990 5.163 0.51 191814. 0.5156 21.53 0.1777 0.4732 0.0533 0.0200 0.864 6.811 7.123 644.626 0.769 31.683 5.012 0.51 191958. 0.4905 23.69 0.1954 0.5049 0.0510 0.0197 0.853 6.719 6.818 635.980 0.759 30.325 4.862 0.51 192109. 0.4656 25.84 0.2132 0.5340 0.0486 0.0194 0.839 6.609 6.500 625.555 0.747 28.913 4.713 0.51 192268. 0.4407 28.00 0.2310 0.5602 0.0462 0.0190 0.822 6.479 6.171 613.243 0.732 27.448 4.564 0.51 192434. 0.4158 30.15 0.2487 0.5835 0.0436 0.0186 0.803 6.329 5.830 599.002 0.715 25.934 4.415 0.51 192607. 0.3909 32.30 0.2665 0.6039 0.0410 0.0181 0.782 6.158 5.480 582.816 0.696 24.373 4.264 0.51 192788. 0.3661 34.46 0.2843 0.6211 0.0383 0.0175 0.757 5.966 5.119 564.669 0.674 22.770 4.112 0.51 192977. 0.3412 36.61 0.3020 0.6350 0.0355 0.0169 0.730 5.753 4.750 544.542 0.650 21.129 3.957 0.51 193174. 0.3162 38.76 0.3198 0.6452 0.0327 0.0162 0.701 5.520 4.373 522.420 0.624 19.451 3.797 0.51 193379. 0.2912 40.92 0.3376 0.6513 0.0298 0.0155 0.668 5.265 3.989 498.291 0.595 17.742 3.631 0.51 193591. 0.2659 43.07 0.3553 0.6526 0.0269 0.0147 0.633 4.988 3.598 472.152 0.564 16.004 3.456 0.51 193812. 0.2404 45.22 0.3731 0.6485 0.0240 0.0138 0.595 4.691 3.202 444.011 0.530 14.242 3.271 0.51 194041. 0.2146 47.38 0.3909 0.6376 0.0210 0.0128 0.555 4.373 2.801 413.892 0.494 12.460 3.070 0.51 194279. 0.1884 49.53 0.4086 0.6184 0.0179 0.0119 0.512 4.034 2.397 381.835 0.456 10.664 2.848 0.51 194525. 0.1617 51.68 0.4264 0.5883 0.0149 0.0108 0.467 3.676 1.991 347.903 0.415 8.858 2.596 0.51 194779. 0.1344 53.84 0.4442 0.5435 0.0119 0.0097 0.419 3.298 1.585 312.184 0.373 7.049 2.303 0.51 195042. 0.1063 55.99 0.4619 0.4779 0.0088 0.0085 0.369 2.903 1.179 274.798 0.328 5.246 1.947 0.51 195314. 0.0775 58.14 0.4797 0.3808 0.0058 0.0073 0.316 2.492 0.777 235.894 0.282 3.456 1.494 0.51 195594. 0.0483 60.30 0.4975 0.2325 0.0028 0.0061 0.262 2.067 0.379 195.630 0.234 1.688 0.880 0.51 195882. 0.0199 62.45 0.5152 -0.0158 -0.0001 0.0048 0.206 1.620 -0.019 153.334 0.183 -0.087 -0.058 0.51 196150. 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 0.0722 0.0205 1.260 8.823 12.211 939.445 0.997 54.317 5.896 0.57 214645. 0.7556 2.45 0.0180 0.0618 0.0707 0.0206 1.266 8.869 11.963 944.350 1.002 53.211 5.746 0.57 214746. 0.7288 4.90 0.0360 0.1203 0.0692 0.0207 1.271 8.904 11.700 948.140 1.006 52.042 5.597 0.57 214853. 0.7021 7.35 0.0539 0.1757 0.0675 0.0207 1.275 8.928 11.424 950.656 1.009 50.812 5.450 0.57 214967. 0.6756 9.81 0.0719 0.2281 0.0658 0.0207 1.276 8.938 11.133 951.750 1.010 49.518 5.305 0.57 215088. 0.6492 12.26 0.0899 0.2774 0.0640 0.0207 1.276 8.934 10.827 951.262 1.009 48.158 5.162 0.57 215216. 0.6229 14.71 0.1079 0.3238 0.0621 0.0207 1.273 8.913 10.506 949.039 1.007 46.732 5.021 0.57 215351. 0.5969 17.16 0.1259 0.3673 0.0601 0.0206 1.267 8.874 10.170 944.924 1.003 45.238 4.882 0.57 215493. 0.5710 19.61 0.1438 0.4079 0.0580 0.0205 1.259 8.816 9.819 938.766 0.996 43.676 4.744 0.57 215643. 0.5452 22.06 0.1618 0.4457 0.0559 0.0203 1.248 8.738 9.453 930.412 0.987 42.046 4.608 0.57 215801. 0.5196 24.52 0.1798 0.4808 0.0536 0.0201 1.233 8.637 9.071 919.714 0.976 40.346 4.473 0.57 215967. 0.4941 26.97 0.1978 0.5130 0.0513 0.0198 1.216 8.513 8.673 906.518 0.962 38.578 4.340 0.57 216141. 0.4687 29.42 0.2157 0.5425 0.0488 0.0194 1.194 8.365 8.260 890.658 0.945 36.740 4.206 0.57 216323. 0.4433 31.87 0.2337 0.5691 0.0463 0.0190 1.169 8.189 7.831 871.983 0.925 34.832 4.073 0.57 216514. 0.4180 34.32 0.2517 0.5929 0.0437 0.0185 1.140 7.987 7.388 850.437 0.902 32.860 3.940 0.57 216713. 0.3927 36.77 0.2697 0.6136 0.0410 0.0180 1.108 7.757 6.931 825.998 0.876 30.828 3.806 0.57 216921. 0.3674 39.23 0.2877 0.6311 0.0382 0.0174 1.071 7.500 6.462 798.641 0.847 28.741 3.670 0.57 217138. 0.3421 41.68 0.3056 0.6451 0.0354 0.0168 1.030 7.216 5.981 768.342 0.815 26.604 3.531 0.57 217365. 0.3167 44.13 0.3236 0.6554 0.0325 0.0160 0.986 6.903 5.490 735.076 0.780 24.420 3.388 0.57 217600. 0.2911 46.58 0.3416 0.6614 0.0295 0.0152 0.937 6.563 4.990 698.828 0.741 22.196 3.239 0.57 217844. 0.2653 49.03 0.3596 0.6625 0.0265 0.0144 0.885 6.195 4.482 659.599 0.700 19.935 3.082 0.57 218098. 0.2393 51.48 0.3776 0.6577 0.0234 0.0135 0.828 5.798 3.967 617.407 0.655 17.644 2.914 0.58 218362. 0.2128 53.94 0.3955 0.6458 0.0204 0.0125 0.767 5.375 3.446 572.292 0.607 15.328 2.731 0.58 218635. 0.1859 56.39 0.4135 0.6247 0.0173 0.0114 0.703 4.924 2.921 524.324 0.556 12.994 2.527 0.58 218918. 0.1584 58.84 0.4315 0.5915 0.0142 0.0103 0.635 4.448 2.394 473.608 0.503 10.650 2.293 0.58 219210. 0.1301 61.29 0.4495 0.5415 0.0110 0.0092 0.564 3.947 1.867 420.290 0.446 8.306 2.015 0.58 219513. 0.1010 63.74 0.4674 0.4668 0.0079 0.0079 0.489 3.424 1.343 364.565 0.387 5.972 1.670 0.58 219825. 0.0710 66.19 0.4854 0.3530 0.0049 0.0067 0.411 2.880 0.822 306.671 0.325 3.658 1.216 0.58 220147. 0.0405 68.65 0.5034 0.1709 0.0018 0.0054 0.331 2.318 0.309 246.801 0.262 1.374 0.568 0.58 220476. 0.0116 71.10 0.5214 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 0.0731 0.0207 1.745 11.000 15.272 1301.440 1.243 67.929 5.322 0.63 238478. 0.7628 2.69 0.0177 0.0611 0.0717 0.0208 1.754 11.056 14.966 1308.006 1.249 66.568 5.190 0.63 238589. 0.7362 5.37 0.0355 0.1192 0.0701 0.0209 1.761 11.098 14.643 1313.040 1.254 65.130 5.058 0.63 238708. 0.7098 8.06 0.0532 0.1742 0.0685 0.0209 1.765 11.126 14.302 1316.329 1.257 63.617 4.928 0.63 238833. 0.6835 10.75 0.0709 0.2262 0.0668 0.0209 1.767 11.137 13.945 1317.671 1.258 62.026 4.800 0.63 238966. 0.6573 13.44 0.0887 0.2753 0.0650 0.0209 1.766 11.130 13.569 1316.858 1.258 60.355 4.674 0.63 239107. 0.6314 16.12 0.1064 0.3215 0.0631 0.0209 1.762 11.104 13.175 1313.681 1.254 58.603 4.549 0.64 239255. 0.6055 18.81 0.1242 0.3650 0.0611 0.0208 1.754 11.055 12.763 1307.934 1.249 56.768 4.426 0.64 239411. 0.5798 21.50 0.1419 0.4057 0.0590 0.0207 1.743 10.983 12.331 1299.412 1.241 54.850 4.304 0.64 239576. 0.5543 24.19 0.1596 0.4436 0.0569 0.0205 1.727 10.886 11.881 1287.912 1.230 52.848 4.184 0.64 239748. 0.5289 26.87 0.1774 0.4789 0.0546 0.0202 1.707 10.762 11.412 1273.240 1.216 50.762 4.065 0.64 239930. 0.5037 29.56 0.1951 0.5116 0.0523 0.0199 1.683 10.609 10.924 1255.190 1.199 48.591 3.948 0.64 240120. 0.4785 32.25 0.2128 0.5415 0.0499 0.0196 1.654 10.426 10.417 1233.548 1.178 46.336 3.830 0.64 240319. 0.4534 34.93 0.2306 0.5687 0.0474 0.0192 1.620 10.211 9.891 1208.099 1.154 43.995 3.713 0.64 240527. 0.4283 37.62 0.2483 0.5932 0.0448 0.0187 1.581 9.963 9.347 1178.746 1.126 41.574 3.597 0.64 240745. 0.4032 40.31 0.2660 0.6148 0.0421 0.0182 1.536 9.682 8.786 1145.457 1.094 39.079 3.479 0.64 240972. 0.3782 43.00 0.2838 0.6333 0.0393 0.0176 1.486 9.367 8.209 1108.205 1.058 36.515 3.360 0.64 241208. 0.3530 45.68 0.3015 0.6486 0.0365 0.0170 1.431 9.018 7.619 1066.954 1.019 33.888 3.239 0.64 241455. 0.3278 48.37 0.3192 0.6604 0.0336 0.0162 1.370 8.635 7.015 1021.673 0.976 31.204 3.114 0.64 241711. 0.3025 51.06 0.3370 0.6683 0.0306 0.0155 1.304 8.218 6.400 972.341 0.929 28.468 2.986 0.64 241976. 0.2770 53.75 0.3547 0.6716 0.0276 0.0146 1.232 7.767 5.775 918.954 0.878 25.686 2.850 0.64 242253. 0.2512 56.43 0.3725 0.6695 0.0246 0.0137 1.155 7.282 5.140 861.528 0.823 22.864 2.706 0.64 242539. 0.2250 59.12 0.3902 0.6609 0.0215 0.0127 1.073 6.763 4.499 800.110 0.764 20.010 2.550 0.64 242835. 0.1984 61.81 0.4079 0.6442 0.0184 0.0117 0.985 6.211 3.851 734.783 0.702 17.131 2.377 0.64 243142. 0.1711 64.49 0.4257 0.6166 0.0153 0.0106 0.893 5.626 3.201 665.673 0.636 14.237 2.181 0.64 243460. 0.1431 67.18 0.4434 0.5742 0.0122 0.0094 0.795 5.012 2.549 592.959 0.566 11.338 1.950 0.64 243788. 0.1142 69.87 0.4611 0.5104 0.0091 0.0082 0.693 4.369 1.899 516.883 0.494 8.446 1.666 0.64 244127. 0.0842 72.56 0.4789 0.4131 0.0060 0.0070 0.587 3.700 1.253 437.751 0.418 5.575 1.299 0.64 244476. 0.0533 75.24 0.4966 0.2587 0.0029 0.0057 0.477 3.008 0.615 355.887 0.340 2.737 0.784 0.64 244835. 0.0226 77.93 0.5143 -0.0146 -0.0001 0.0043 0.362 2.281 -0.025 269.840 0.258 -0.113 -0.043 0.64 245166. 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 0.0742 0.0210 2.357 13.505 18.761 1757.572 1.526 83.450 4.842 0.70 262304. 0.7691 2.97 0.0178 0.0614 0.0728 0.0211 2.368 13.571 18.385 1766.170 1.533 81.776 4.721 0.70 262428. 0.7424 5.93 0.0356 0.1197 0.0712 0.0212 2.377 13.621 17.987 1772.635 1.539 80.008 4.602 0.70 262560. 0.7158 8.90 0.0534 0.1750 0.0695 0.0212 2.383 13.652 17.568 1776.680 1.542 78.145 4.485 0.70 262700. 0.6894 11.87 0.0712 0.2273 0.0678 0.0212 2.384 13.662 17.128 1778.022 1.544 76.184 4.369 0.70 262848. 0.6631 14.83 0.0890 0.2767 0.0659 0.0212 2.382 13.649 16.665 1776.383 1.542 74.125 4.255 0.70 263004. 0.6370 17.80 0.1068 0.3233 0.0640 0.0212 2.376 13.612 16.179 1771.474 1.538 71.964 4.142 0.70 263169. 0.6111 20.77 0.1246 0.3671 0.0620 0.0211 2.364 13.547 15.670 1763.013 1.531 69.700 4.031 0.70 263343. 0.5852 23.74 0.1424 0.4081 0.0599 0.0209 2.348 13.452 15.138 1750.722 1.520 67.333 3.922 0.70 263526. 0.5596 26.70 0.1602 0.4464 0.0577 0.0207 2.326 13.326 14.582 1734.322 1.506 64.860 3.814 0.70 263718. 0.5340 29.67 0.1780 0.4821 0.0554 0.0205 2.298 13.167 14.003 1713.553 1.488 62.284 3.706 0.70 263920. 0.5086 32.64 0.1958 0.5151 0.0530 0.0202 2.264 12.971 13.400 1688.138 1.466 59.602 3.600 0.70 264131. 0.4833 35.60 0.2136 0.5455 0.0505 0.0198 2.223 12.738 12.773 1657.787 1.439 56.815 3.495 0.70 264352. 0.4580 38.57 0.2314 0.5731 0.0480 0.0194 2.175 12.465 12.123 1622.205 1.408 53.922 3.390 0.70 264584. 0.4328 41.54 0.2492 0.5981 0.0453 0.0189 2.121 12.150 11.450 1581.267 1.373 50.929 3.284 0.70 264826. 0.4075 44.50 0.2670 0.6201 0.0426 0.0183 2.058 11.794 10.756 1534.934 1.333 47.843 3.178 0.70 265078. 0.3823 47.47 0.2848 0.6392 0.0397 0.0177 1.989 11.396 10.043 1483.166 1.288 44.673 3.071 0.70 265340. 0.3570 50.44 0.3026 0.6550 0.0369 0.0170 1.912 10.957 9.313 1425.920 1.238 41.425 2.962 0.70 265613. 0.3315 53.41 0.3204 0.6674 0.0339 0.0163 1.828 10.474 8.567 1363.158 1.183 38.105 2.850 0.70 265897. 0.3060 56.37 0.3382 0.6757 0.0309 0.0155 1.736 9.949 7.806 1294.853 1.124 34.721 2.734 0.70 266192. 0.2802 59.34 0.3560 0.6796 0.0278 0.0146 1.637 9.382 7.032 1221.005 1.060 31.280 2.612 0.70 266498. 0.2540 62.31 0.3738 0.6780 0.0247 0.0136 1.531 8.772 6.248 1141.646 0.991 27.789 2.482 0.70 266816. 0.2275 65.27 0.3916 0.6698 0.0216 0.0126 1.417 8.121 5.454 1056.860 0.917 24.259 2.341 0.70 267145. 0.2005 68.24 0.4094 0.6531 0.0184 0.0115 1.296 7.429 4.653 966.780 0.839 20.698 2.183 0.70 267485. 0.1727 71.21 0.4272 0.6252 0.0152 0.0104 1.169 6.697 3.849 871.606 0.757 17.120 2.003 0.70 267837. 0.1441 74.17 0.4450 0.5817 0.0120 0.0092 1.035 5.929 3.043 771.622 0.670 13.536 1.789 0.71 268201. 0.1144 77.14 0.4628 0.5149 0.0089 0.0080 0.895 5.127 2.240 667.205 0.579 9.962 1.522 0.71 268576. 0.0836 80.11 0.4806 0.4111 0.0057 0.0067 0.749 4.294 1.442 558.835 0.485 6.415 1.171 0.71 268963. 0.0516 83.07 0.4984 0.2418 0.0026 0.0053 0.599 3.435 0.654 446.997 0.388 2.910 0.664 0.71 269359. 0.0197 86.04 0.5163 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 0.0756 0.0214 3.126 16.419 22.731 2331.113 1.855 101.107 4.423 0.76 286120. 0.7733 3.24 0.0178 0.0612 0.0741 0.0215 3.139 16.489 22.277 2341.040 1.863 99.087 4.316 0.76 286258. 0.7471 6.47 0.0356 0.1195 0.0725 0.0216 3.149 16.540 21.797 2348.276 1.869 96.951 4.210 0.76 286403. 0.7208 9.71 0.0534 0.1748 0.0708 0.0216 3.155 16.569 21.290 2352.412 1.872 94.700 4.105 0.76 286557. 0.6946 12.95 0.0712 0.2271 0.0690 0.0216 3.156 16.574 20.758 2353.059 1.873 92.330 4.001 0.76 286720. 0.6685 16.19 0.0890 0.2766 0.0672 0.0216 3.151 16.551 20.197 2349.818 1.870 89.838 3.899 0.76 286892. 0.6425 19.42 0.1068 0.3233 0.0652 0.0215 3.141 16.498 19.609 2342.279 1.864 87.223 3.797 0.76 287074. 0.6167 22.66 0.1246 0.3673 0.0632 0.0214 3.125 16.412 18.993 2330.039 1.854 84.482 3.697 0.76 287265. 0.5909 25.90 0.1424 0.4085 0.0610 0.0213 3.101 16.290 18.349 2312.702 1.840 81.614 3.599 0.76 287466. 0.5653 29.13 0.1602 0.4471 0.0588 0.0211 3.071 16.129 17.675 2289.889 1.822 78.619 3.501 0.76 287677. 0.5398 32.37 0.1780 0.4831 0.0564 0.0208 3.032 15.927 16.973 2261.235 1.799 75.496 3.405 0.76 287898. 0.5144 35.61 0.1958 0.5165 0.0540 0.0205 2.986 15.682 16.242 2226.401 1.772 72.245 3.309 0.76 288131. 0.4890 38.84 0.2136 0.5473 0.0515 0.0201 2.930 15.390 15.482 2185.011 1.739 68.865 3.214 0.76 288373. 0.4638 42.08 0.2314 0.5754 0.0489 0.0197 2.865 15.050 14.693 2136.689 1.700 65.355 3.119 0.76 288627. 0.4385 45.32 0.2493 0.6008 0.0461 0.0191 2.791 14.660 13.877 2081.280 1.656 61.723 3.024 0.76 288892. 0.4131 48.56 0.2671 0.6234 0.0433 0.0186 2.707 14.219 13.035 2018.757 1.606 57.979 2.929 0.76 289168. 0.3878 51.79 0.2849 0.6430 0.0405 0.0179 2.614 13.729 12.170 1949.098 1.551 54.131 2.832 0.76 289456. 0.3623 55.03 0.3027 0.6594 0.0375 0.0172 2.511 13.188 11.283 1872.287 1.490 50.187 2.733 0.77 289755. 0.3367 58.27 0.3205 0.6723 0.0345 0.0164 2.398 12.596 10.377 1788.312 1.423 46.155 2.632 0.77 290066. 0.3109 61.50 0.3383 0.6811 0.0314 0.0156 2.276 11.954 9.452 1697.202 1.351 42.044 2.526 0.77 290388. 0.2848 64.74 0.3561 0.6853 0.0283 0.0147 2.144 11.263 8.512 1599.024 1.272 37.863 2.415 0.77 290723. 0.2584 67.98 0.3739 0.6839 0.0251 0.0137 2.003 10.522 7.559 1493.906 1.189 33.621 2.295 0.77 291070. 0.2314 71.21 0.3917 0.6756 0.0219 0.0127 1.853 9.735 6.594 1382.048 1.100 29.330 2.164 0.77 291430. 0.2038 74.45 0.4095 0.6584 0.0187 0.0116 1.695 8.901 5.621 1263.738 1.006 25.000 2.017 0.77 291801. 0.1754 77.69 0.4273 0.6294 0.0154 0.0105 1.528 8.025 4.642 1139.370 0.907 20.648 1.848 0.77 292186. 0.1460 80.93 0.4451 0.5837 0.0122 0.0093 1.354 7.110 3.662 1009.459 0.803 16.288 1.645 0.77 292583. 0.1155 84.16 0.4629 0.5135 0.0089 0.0080 1.173 6.161 2.684 874.655 0.696 11.938 1.392 0.77 292993. 0.0836 87.40 0.4807 0.4047 0.0057 0.0068 0.987 5.182 1.713 735.741 0.585 7.620 1.056 0.77 293415. 0.0507 90.64 0.4985 0.2289 0.0025 0.0055 0.796 4.180 0.754 593.482 0.472 3.353 0.576 0.77 293848. 0.0183 93.87 0.5163 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 0.0772 0.0225 4.180 20.265 27.250 3116.789 2.289 121.208 3.966 0.83 309925. 0.7592 3.50 0.0178 0.0596 0.0757 0.0226 4.183 20.282 26.711 3119.488 2.291 118.809 3.884 0.83 310075. 0.7361 7.00 0.0355 0.1166 0.0741 0.0226 4.183 20.280 26.140 3119.101 2.291 116.271 3.801 0.83 310234. 0.7127 10.49 0.0533 0.1711 0.0724 0.0225 4.178 20.254 25.538 3115.199 2.288 113.593 3.718 0.83 310402. 0.6891 13.99 0.0710 0.2230 0.0706 0.0225 4.167 20.203 24.904 3107.328 2.283 110.772 3.635 0.83 310580. 0.6653 17.49 0.0888 0.2723 0.0687 0.0224 4.151 20.123 24.237 3095.033 2.273 107.805 3.552 0.83 310768. 0.6413 20.99 0.1065 0.3191 0.0667 0.0223 4.127 20.011 23.536 3077.824 2.261 104.688 3.468 0.83 310966. 0.6171 24.48 0.1243 0.3633 0.0646 0.0221 4.097 19.864 22.801 3055.212 2.244 101.421 3.385 0.83 311174. 0.5928 27.98 0.1421 0.4050 0.0624 0.0219 4.059 19.679 22.032 3026.707 2.223 98.000 3.302 0.83 311393. 0.5683 31.48 0.1598 0.4442 0.0601 0.0216 4.012 19.452 21.229 2991.787 2.198 94.426 3.218 0.83 311623. 0.5438 34.98 0.1776 0.4807 0.0578 0.0213 3.957 19.183 20.391 2950.482 2.167 90.697 3.135 0.83 311864. 0.5191 38.48 0.1953 0.5145 0.0553 0.0210 3.892 18.869 19.518 2902.079 2.132 86.814 3.050 0.83 312116. 0.4942 41.97 0.2131 0.5457 0.0527 0.0206 3.817 18.505 18.610 2846.202 2.091 82.776 2.966 0.83 312380. 0.4692 45.47 0.2309 0.5741 0.0501 0.0201 3.731 18.089 17.667 2782.217 2.044 78.581 2.880 0.83 312656. 0.4439 48.97 0.2486 0.5997 0.0473 0.0196 3.634 17.620 16.690 2709.983 1.991 74.238 2.793 0.83 312943. 0.4185 52.47 0.2664 0.6223 0.0444 0.0190 3.526 17.096 15.683 2629.407 1.931 69.759 2.705 0.83 313242. 0.3929 55.96 0.2841 0.6417 0.0415 0.0184 3.407 16.516 14.648 2540.312 1.866 65.153 2.615 0.83 313554. 0.3671 59.46 0.3019 0.6576 0.0385 0.0177 3.276 15.883 13.586 2442.844 1.794 60.431 2.523 0.83 313878. 0.3410 62.96 0.3196 0.6697 0.0354 0.0169 3.134 15.195 12.501 2337.016 1.717 55.603 2.426 0.83 314215. 0.3146 66.46 0.3374 0.6773 0.0323 0.0161 2.981 14.454 11.394 2223.041 1.633 50.678 2.325 0.83 314564. 0.2878 69.96 0.3552 0.6797 0.0291 0.0152 2.818 13.661 10.267 2101.208 1.543 45.667 2.216 0.83 314926. 0.2604 73.45 0.3729 0.6758 0.0258 0.0143 2.644 12.821 9.124 1971.944 1.449 40.581 2.099 0.83 315301. 0.2325 76.95 0.3907 0.6640 0.0226 0.0133 2.462 11.935 7.966 1835.714 1.348 35.433 1.968 0.83 315690. 0.2037 80.45 0.4084 0.6423 0.0193 0.0122 2.270 11.008 6.798 1693.095 1.244 30.238 1.821 0.83 316092. 0.1741 83.95 0.4262 0.6076 0.0159 0.0112 2.072 10.044 5.623 1544.826 1.135 25.011 1.651 0.83 316507. 0.1436 87.44 0.4439 0.5553 0.0126 0.0101 1.866 9.049 4.445 1391.818 1.022 19.773 1.449 0.83 316935. 0.1120 90.94 0.4617 0.4787 0.0093 0.0089 1.656 8.030 3.270 1235.098 0.907 14.544 1.201 0.83 317378. 0.0796 94.44 0.4795 0.3669 0.0060 0.0078 1.443 6.995 2.102 1075.827 0.790 9.350 0.886 0.83 317834. 0.0471 97.94 0.4972 0.2016 0.0027 0.0066 1.227 5.950 0.947 915.070 0.672 4.213 0.469 0.84 318301. 0.0168 101.44 0.5150 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 0.0790 0.0253 5.865 26.405 32.334 4373.674 2.983 143.822 3.353 0.89 333716. 0.6992 3.76 0.0177 0.0544 0.0775 0.0252 5.834 26.266 31.708 4350.529 2.967 141.036 3.306 0.89 333879. 0.6826 7.51 0.0354 0.1073 0.0758 0.0250 5.798 26.102 31.044 4323.437 2.949 138.083 3.257 0.89 334052. 0.6655 11.27 0.0531 0.1584 0.0741 0.0249 5.756 25.912 30.342 4292.041 2.928 134.963 3.206 0.89 334235. 0.6477 15.03 0.0708 0.2078 0.0723 0.0246 5.707 25.694 29.602 4255.910 2.903 131.670 3.155 0.89 334428. 0.6295 18.78 0.0885 0.2554 0.0704 0.0244 5.652 25.445 28.822 4214.611 2.875 128.201 3.102 0.89 334631. 0.6107 22.54 0.1063 0.3011 0.0684 0.0241 5.589 25.162 28.002 4167.704 2.843 124.552 3.047 0.89 334846. 0.5914 26.30 0.1240 0.3449 0.0663 0.0238 5.518 24.842 27.141 4114.730 2.807 120.721 2.992 0.89 335072. 0.5716 30.05 0.1417 0.3866 0.0641 0.0235 5.438 24.483 26.238 4055.243 2.766 116.707 2.935 0.89 335309. 0.5513 33.81 0.1594 0.4263 0.0618 0.0231 5.349 24.081 25.294 3988.768 2.721 112.508 2.876 0.89 335558. 0.5305 37.57 0.1771 0.4638 0.0594 0.0227 5.250 23.635 24.309 3914.819 2.670 108.125 2.816 0.89 335819. 0.5092 41.32 0.1948 0.4989 0.0569 0.0222 5.142 23.150 23.282 3834.426 2.615 103.557 2.754 0.89 336091. 0.4873 45.08 0.2125 0.5312 0.0543 0.0217 5.027 22.631 22.213 3748.488 2.557 98.803 2.688 0.89 336377. 0.4646 48.83 0.2302 0.5606 0.0516 0.0212 4.901 22.067 21.102 3655.044 2.493 93.863 2.619 0.89 336674. 0.4412 52.59 0.2479 0.5869 0.0487 0.0206 4.767 21.463 19.952 3555.067 2.425 88.745 2.546 0.89 336984. 0.4170 56.35 0.2656 0.6097 0.0458 0.0200 4.624 20.818 18.764 3448.175 2.352 83.461 2.468 0.89 337307. 0.3921 60.10 0.2833 0.6281 0.0429 0.0193 4.476 20.150 17.541 3337.594 2.277 78.024 2.384 0.89 337643. 0.3661 63.86 0.3011 0.6414 0.0398 0.0187 4.324 19.468 16.287 3224.680 2.200 72.445 2.291 0.89 337992. 0.3391 67.62 0.3188 0.6499 0.0367 0.0180 4.163 18.741 15.004 3104.188 2.117 66.738 2.192 0.89 338355. 0.3114 71.37 0.3365 0.6531 0.0335 0.0172 3.991 17.967 13.695 2976.012 2.030 60.916 2.087 0.89 338731. 0.2833 75.13 0.3542 0.6502 0.0302 0.0165 3.810 17.151 12.363 2840.794 1.938 54.991 1.974 0.89 339120. 0.2545 78.89 0.3719 0.6399 0.0269 0.0156 3.620 16.297 11.011 2699.322 1.841 48.977 1.850 0.89 339524. 0.2252 82.64 0.3896 0.6208 0.0236 0.0148 3.423 15.411 9.643 2552.580 1.741 42.891 1.713 0.90 339941. 0.1951 86.40 0.4073 0.5910 0.0202 0.0139 3.221 14.500 8.262 2401.716 1.638 36.748 1.560 0.90 340372. 0.1645 90.16 0.4250 0.5482 0.0168 0.0130 3.014 13.570 6.873 2247.631 1.533 30.571 1.387 0.90 340818. 0.1333 93.91 0.4427 0.4894 0.0134 0.0121 2.805 12.627 5.481 2091.567 1.427 24.381 1.189 0.90 341278. 0.1021 97.67 0.4604 0.4108 0.0100 0.0112 2.595 11.681 4.093 1934.874 1.320 18.206 0.959 0.90 341753. 0.0712 101.43 0.4782 0.3078 0.0066 0.0103 2.386 10.740 2.715 1778.980 1.213 12.075 0.692 0.90 342242. 0.0418 105.18 0.4959 0.1741 0.0033 0.0094 2.179 9.810 1.353 1624.814 1.108 6.016 0.378 0.90 342744. 0.0161 108.94 0.5136 -0.0016 0.0000 0.0085 1.963 8.836 -0.011 1463.606 0.998 -0.049 -0.003 0.90 343233. 0.0000 PROP RPM = 15000 V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM (mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - - 0.00 0.0000 0.0000 0.0803 0.0303 8.637 36.292 37.715 6440.733 4.100 167.756 2.656 0.95 357513. 0.5982 4.22 0.0185 0.0486 0.0787 0.0300 8.553 35.939 36.993 6378.019 4.060 164.545 2.631 0.95 357695. 0.5868 8.43 0.0371 0.0963 0.0771 0.0297 8.457 35.537 36.220 6306.613 4.015 161.107 2.605 0.95 357890. 0.5749 12.65 0.0556 0.1430 0.0753 0.0293 8.350 35.084 35.396 6226.326 3.964 157.440 2.578 0.95 358096. 0.5626 16.86 0.0742 0.1886 0.0735 0.0289 8.230 34.580 34.518 6136.920 3.907 153.538 2.551 0.95 358316. 0.5497 21.08 0.0927 0.2331 0.0715 0.0284 8.097 34.024 33.587 6038.218 3.844 149.396 2.523 0.95 358548. 0.5362 25.29 0.1113 0.2765 0.0694 0.0279 7.952 33.415 32.601 5930.105 3.775 145.010 2.494 0.95 358793. 0.5221 29.51 0.1298 0.3186 0.0672 0.0274 7.795 32.752 31.560 5812.445 3.700 140.377 2.463 0.95 359052. 0.5074 33.72 0.1484 0.3593 0.0648 0.0268 7.624 32.035 30.462 5685.090 3.619 135.496 2.430 0.95 359324. 0.4919 37.94 0.1669 0.3986 0.0624 0.0261 7.440 31.261 29.309 5547.906 3.532 130.368 2.396 0.95 359610. 0.4757 42.16 0.1855 0.4362 0.0598 0.0254 7.242 30.432 28.101 5400.677 3.438 124.993 2.360 0.95 359911. 0.4588 46.37 0.2040 0.4720 0.0571 0.0247 7.031 29.544 26.838 5243.094 3.338 119.373 2.322 0.95 360226. 0.4411 50.59 0.2226 0.5051 0.0543 0.0239 6.815 28.635 25.518 5081.797 3.235 113.504 2.278 0.95 360555. 0.4219 54.80 0.2411 0.5353 0.0514 0.0231 6.591 27.696 24.143 4915.155 3.129 107.389 2.228 0.95 360899. 0.4015 59.02 0.2597 0.5617 0.0483 0.0223 6.364 26.743 22.717 4745.949 3.021 101.047 2.171 0.96 361259. 0.3795 63.23 0.2782 0.5842 0.0452 0.0215 6.132 25.764 21.245 4572.317 2.911 94.497 2.107 0.96 361633. 0.3562 67.45 0.2968 0.6007 0.0420 0.0207 5.907 24.819 19.729 4404.562 2.804 87.754 2.032 0.96 362023. 0.3309 71.67 0.3153 0.6055 0.0387 0.0201 5.734 24.094 18.170 4275.927 2.722 80.820 1.927 0.96 362428. 0.3013 75.88 0.3339 0.6029 0.0353 0.0195 5.563 23.375 16.576 4148.326 2.641 73.731 1.812 0.96 362849. 0.2706 80.10 0.3524 0.5928 0.0318 0.0189 5.387 22.637 14.953 4017.338 2.558 66.512 1.688 0.96 363285. 0.2394 84.31 0.3710 0.5745 0.0283 0.0183 5.207 21.879 13.306 3882.796 2.472 59.185 1.554 0.96 363738. 0.2079 88.53 0.3895 0.5470 0.0248 0.0176 5.024 21.109 11.640 3746.079 2.385 51.773 1.409 0.96 364207. 0.1763 92.74 0.4081 0.5091 0.0212 0.0170 4.839 20.333 9.961 3608.495 2.297 44.306 1.252 0.96 364692. 0.1449 96.96 0.4266 0.4597 0.0176 0.0163 4.655 19.561 8.277 3471.468 2.210 36.816 1.081 0.96 365194. 0.1141 101.17 0.4452 0.3977 0.0140 0.0157 4.474 18.801 6.596 3336.612 2.124 29.340 0.897 0.96 365713. 0.0845 105.39 0.4637 0.3223 0.0105 0.0151 4.297 18.056 4.928 3204.394 2.040 21.920 0.698 0.96 366249. 0.0568 109.61 0.4823 0.2326 0.0070 0.0145 4.124 17.330 3.283 3075.485 1.958 14.601 0.484 0.96 366803. 0.0322 113.82 0.5008 0.1279 0.0035 0.0139 3.955 16.617 1.666 2949.049 1.877 7.412 0.256 0.96 367376. 0.0121 118.04 0.5194 0.0034 0.0001 0.0132 3.761 15.802 0.040 2804.322 1.785 0.180 0.007 0.96 367976. 0.0000 122.25 0.5379