538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
14x14 (14x14.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 0.1247 0.0729 0.003 0.199 0.153 2.351 0.022 0.679 29.461 0.06 25197. 0.4825
|
|
0.53 0.0400 0.0668 0.1242 0.0744 0.003 0.203 0.152 2.400 0.023 0.676 28.735 0.06 25225. 0.4697
|
|
1.06 0.0800 0.1301 0.1236 0.0760 0.003 0.207 0.151 2.454 0.023 0.673 27.975 0.06 25256. 0.4561
|
|
1.59 0.1200 0.1896 0.1229 0.0778 0.003 0.212 0.150 2.510 0.024 0.669 27.190 0.06 25293. 0.4421
|
|
2.12 0.1600 0.2454 0.1221 0.0796 0.003 0.217 0.150 2.570 0.025 0.665 26.388 0.06 25334. 0.4276
|
|
2.65 0.2000 0.2972 0.1211 0.0815 0.004 0.222 0.148 2.630 0.025 0.660 25.576 0.06 25380. 0.4128
|
|
3.18 0.2400 0.3453 0.1200 0.0834 0.004 0.227 0.147 2.691 0.026 0.653 24.762 0.06 25432. 0.3978
|
|
3.71 0.2800 0.3897 0.1186 0.0852 0.004 0.232 0.145 2.750 0.026 0.646 23.953 0.06 25490. 0.3825
|
|
4.24 0.3200 0.4306 0.1169 0.0869 0.004 0.237 0.143 2.805 0.027 0.637 23.155 0.06 25553. 0.3672
|
|
4.77 0.3599 0.4680 0.1150 0.0884 0.004 0.241 0.141 2.854 0.027 0.626 22.372 0.06 25623. 0.3518
|
|
5.30 0.3999 0.5023 0.1127 0.0897 0.004 0.245 0.138 2.896 0.028 0.614 21.607 0.06 25698. 0.3363
|
|
5.83 0.4399 0.5334 0.1100 0.0907 0.004 0.247 0.135 2.927 0.028 0.599 20.862 0.06 25780. 0.3208
|
|
6.36 0.4799 0.5617 0.1069 0.0913 0.004 0.249 0.131 2.947 0.028 0.582 20.136 0.06 25868. 0.3052
|
|
6.89 0.5199 0.5871 0.1033 0.0915 0.004 0.250 0.126 2.953 0.028 0.563 19.427 0.06 25962. 0.2896
|
|
7.42 0.5599 0.6097 0.0992 0.0911 0.004 0.249 0.121 2.941 0.028 0.540 18.735 0.06 26062. 0.2737
|
|
7.95 0.5999 0.6295 0.0947 0.0902 0.004 0.246 0.116 2.912 0.028 0.516 18.055 0.06 26168. 0.2576
|
|
8.48 0.6399 0.6465 0.0896 0.0886 0.004 0.242 0.110 2.861 0.027 0.488 17.384 0.06 26280. 0.2413
|
|
9.01 0.6799 0.6606 0.0840 0.0864 0.004 0.236 0.103 2.789 0.027 0.457 16.718 0.06 26398. 0.2247
|
|
9.54 0.7199 0.6716 0.0780 0.0836 0.004 0.228 0.095 2.698 0.026 0.425 16.051 0.06 26522. 0.2079
|
|
10.07 0.7599 0.6789 0.0717 0.0802 0.003 0.219 0.088 2.588 0.025 0.390 15.373 0.06 26652. 0.1908
|
|
10.60 0.7999 0.6822 0.0651 0.0763 0.003 0.208 0.080 2.462 0.024 0.354 14.674 0.06 26787. 0.1736
|
|
11.13 0.8399 0.6805 0.0583 0.0719 0.003 0.196 0.071 2.321 0.022 0.317 13.941 0.06 26927. 0.1561
|
|
11.66 0.8799 0.6728 0.0513 0.0671 0.003 0.183 0.063 2.165 0.021 0.279 13.156 0.06 27073. 0.1382
|
|
12.20 0.9199 0.6573 0.0442 0.0618 0.003 0.169 0.054 1.995 0.019 0.241 12.295 0.06 27224. 0.1198
|
|
12.73 0.9599 0.6316 0.0370 0.0562 0.002 0.153 0.045 1.812 0.017 0.201 11.321 0.06 27380. 0.1009
|
|
13.26 0.9998 0.5915 0.0296 0.0501 0.002 0.137 0.036 1.617 0.015 0.161 10.178 0.06 27542. 0.0813
|
|
13.79 1.0398 0.5301 0.0223 0.0437 0.002 0.119 0.027 1.410 0.013 0.121 8.772 0.06 27709. 0.0607
|
|
14.32 1.0798 0.4351 0.0149 0.0370 0.002 0.101 0.018 1.193 0.011 0.081 6.933 0.06 27880. 0.0392
|
|
14.85 1.1198 0.2812 0.0075 0.0299 0.001 0.082 0.009 0.965 0.009 0.041 4.321 0.06 28057. 0.0174
|
|
15.38 1.1598 0.0090 0.0002 0.0226 0.001 0.062 0.000 0.729 0.007 0.001 0.133 0.06 28238. 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 0.1253 0.0661 0.023 0.722 0.613 17.079 0.082 2.728 16.289 0.11 50394. 0.5347
|
|
1.07 0.0403 0.0743 0.1248 0.0677 0.023 0.739 0.611 17.484 0.083 2.718 15.849 0.11 50450. 0.5192
|
|
2.14 0.0806 0.1443 0.1242 0.0694 0.024 0.758 0.608 17.925 0.086 2.705 15.390 0.11 50514. 0.5030
|
|
3.21 0.1210 0.2098 0.1235 0.0712 0.025 0.777 0.605 18.395 0.088 2.691 14.918 0.11 50587. 0.4863
|
|
4.28 0.1613 0.2707 0.1228 0.0732 0.025 0.798 0.601 18.888 0.090 2.674 14.437 0.11 50670. 0.4692
|
|
5.35 0.2016 0.3270 0.1218 0.0751 0.026 0.820 0.597 19.394 0.093 2.654 13.954 0.11 50764. 0.4517
|
|
6.41 0.2419 0.3789 0.1207 0.0771 0.027 0.841 0.591 19.901 0.095 2.629 13.472 0.11 50869. 0.4341
|
|
7.48 0.2822 0.4264 0.1193 0.0790 0.027 0.862 0.584 20.396 0.097 2.600 12.996 0.11 50986. 0.4164
|
|
8.55 0.3226 0.4699 0.1177 0.0808 0.028 0.882 0.576 20.863 0.100 2.564 12.531 0.11 51115. 0.3987
|
|
9.62 0.3629 0.5095 0.1157 0.0824 0.029 0.900 0.567 21.286 0.102 2.521 12.078 0.11 51255. 0.3811
|
|
10.69 0.4032 0.5455 0.1134 0.0838 0.029 0.915 0.555 21.646 0.103 2.471 11.639 0.11 51409. 0.3635
|
|
11.76 0.4435 0.5782 0.1107 0.0849 0.029 0.927 0.542 21.927 0.105 2.412 11.215 0.11 51575. 0.3461
|
|
12.83 0.4839 0.6078 0.1076 0.0856 0.030 0.934 0.527 22.110 0.106 2.343 10.806 0.11 51753. 0.3287
|
|
13.90 0.5242 0.6344 0.1040 0.0859 0.030 0.937 0.509 22.177 0.106 2.264 10.412 0.11 51944. 0.3113
|
|
14.97 0.5645 0.6582 0.0998 0.0856 0.030 0.934 0.489 22.107 0.106 2.175 10.030 0.11 52148. 0.2939
|
|
16.04 0.6048 0.6792 0.0952 0.0847 0.029 0.925 0.466 21.881 0.104 2.073 9.661 0.11 52363. 0.2764
|
|
17.11 0.6451 0.6976 0.0900 0.0832 0.029 0.908 0.441 21.484 0.103 1.960 9.303 0.11 52591. 0.2588
|
|
18.18 0.6855 0.7133 0.0843 0.0810 0.028 0.884 0.413 20.914 0.100 1.836 8.952 0.11 52830. 0.2411
|
|
19.24 0.7258 0.7262 0.0782 0.0782 0.027 0.853 0.383 20.180 0.096 1.703 8.608 0.11 53082. 0.2233
|
|
20.31 0.7661 0.7360 0.0718 0.0747 0.026 0.815 0.352 19.294 0.092 1.564 8.264 0.11 53344. 0.2054
|
|
21.38 0.8064 0.7422 0.0651 0.0708 0.024 0.772 0.319 18.267 0.087 1.418 7.917 0.11 53618. 0.1874
|
|
22.45 0.8467 0.7442 0.0582 0.0663 0.023 0.723 0.285 17.109 0.082 1.269 7.561 0.12 53903. 0.1692
|
|
23.52 0.8871 0.7409 0.0512 0.0613 0.021 0.669 0.251 15.827 0.076 1.115 7.185 0.12 54199. 0.1508
|
|
24.59 0.9274 0.7309 0.0440 0.0559 0.019 0.610 0.216 14.427 0.069 0.959 6.780 0.12 54506. 0.1320
|
|
25.66 0.9677 0.7115 0.0368 0.0500 0.017 0.546 0.180 12.914 0.062 0.801 6.325 0.12 54824. 0.1125
|
|
26.73 1.0080 0.6785 0.0294 0.0437 0.015 0.477 0.144 11.294 0.054 0.641 5.791 0.12 55151. 0.0922
|
|
27.80 1.0483 0.6241 0.0221 0.0371 0.013 0.405 0.108 9.572 0.046 0.481 5.121 0.12 55489. 0.0706
|
|
28.87 1.0887 0.5323 0.0147 0.0300 0.010 0.328 0.072 7.755 0.037 0.320 4.206 0.12 55838. 0.0473
|
|
29.94 1.1290 0.3650 0.0073 0.0227 0.008 0.247 0.036 5.854 0.028 0.160 2.781 0.12 56196. 0.0221
|
|
31.00 1.1693 0.0030 0.0000 0.0150 0.005 0.164 0.000 3.878 0.019 0.001 0.022 0.12 56562. 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 0.1255 0.0634 0.074 1.557 1.383 55.266 0.176 6.151 11.350 0.17 75591. 0.5594
|
|
1.61 0.0405 0.0778 0.1250 0.0650 0.076 1.596 1.378 56.652 0.180 6.128 11.031 0.17 75674. 0.5427
|
|
3.22 0.0809 0.1509 0.1245 0.0667 0.078 1.639 1.372 58.160 0.185 6.102 10.699 0.17 75770. 0.5252
|
|
4.83 0.1214 0.2192 0.1239 0.0686 0.080 1.684 1.365 59.774 0.190 6.071 10.357 0.17 75881. 0.5071
|
|
6.44 0.1618 0.2825 0.1231 0.0705 0.082 1.732 1.357 61.469 0.196 6.034 10.011 0.17 76006. 0.4887
|
|
8.05 0.2023 0.3408 0.1222 0.0725 0.085 1.781 1.347 63.212 0.201 5.990 9.663 0.17 76148. 0.4699
|
|
9.66 0.2428 0.3944 0.1211 0.0746 0.087 1.830 1.334 64.965 0.207 5.936 9.317 0.17 76306. 0.4511
|
|
11.26 0.2832 0.4433 0.1198 0.0765 0.089 1.879 1.320 66.679 0.212 5.870 8.977 0.17 76482. 0.4322
|
|
12.87 0.3237 0.4879 0.1181 0.0784 0.092 1.924 1.302 68.301 0.217 5.790 8.645 0.17 76676. 0.4134
|
|
14.48 0.3641 0.5284 0.1162 0.0801 0.094 1.966 1.280 69.775 0.222 5.695 8.323 0.17 76889. 0.3947
|
|
16.09 0.4046 0.5652 0.1139 0.0815 0.095 2.001 1.255 71.040 0.226 5.582 8.012 0.17 77120. 0.3762
|
|
17.70 0.4451 0.5986 0.1112 0.0827 0.097 2.029 1.225 72.034 0.229 5.449 7.714 0.17 77371. 0.3578
|
|
19.31 0.4855 0.6287 0.1080 0.0834 0.097 2.048 1.190 72.694 0.231 5.294 7.427 0.17 77640. 0.3396
|
|
20.92 0.5260 0.6559 0.1044 0.0837 0.098 2.055 1.150 72.956 0.232 5.116 7.151 0.17 77929. 0.3215
|
|
22.53 0.5664 0.6802 0.1003 0.0835 0.098 2.050 1.105 72.750 0.232 4.913 6.887 0.17 78236. 0.3034
|
|
24.14 0.6069 0.7018 0.0956 0.0826 0.097 2.029 1.053 72.007 0.229 4.683 6.632 0.17 78561. 0.2852
|
|
25.75 0.6474 0.7209 0.0903 0.0811 0.095 1.991 0.995 70.679 0.225 4.427 6.386 0.17 78905. 0.2670
|
|
27.36 0.6878 0.7374 0.0846 0.0789 0.092 1.937 0.932 68.757 0.219 4.146 6.149 0.17 79267. 0.2488
|
|
28.97 0.7283 0.7513 0.0785 0.0761 0.089 1.867 0.864 66.269 0.211 3.845 5.917 0.17 79646. 0.2306
|
|
30.57 0.7687 0.7624 0.0720 0.0726 0.085 1.782 0.793 63.256 0.201 3.528 5.688 0.17 80042. 0.2123
|
|
32.18 0.8092 0.7702 0.0653 0.0686 0.080 1.684 0.719 59.755 0.190 3.199 5.459 0.17 80456. 0.1940
|
|
33.79 0.8496 0.7743 0.0584 0.0640 0.075 1.572 0.643 55.798 0.178 2.860 5.227 0.17 80886. 0.1756
|
|
35.40 0.8901 0.7737 0.0513 0.0590 0.069 1.448 0.565 51.410 0.164 2.513 4.985 0.17 81333. 0.1570
|
|
37.01 0.9306 0.7669 0.0441 0.0535 0.063 1.313 0.486 46.608 0.148 2.160 4.727 0.17 81796. 0.1381
|
|
38.62 0.9710 0.7517 0.0368 0.0475 0.056 1.167 0.405 41.413 0.132 1.803 4.440 0.17 82275. 0.1185
|
|
40.23 1.0115 0.7238 0.0294 0.0411 0.048 1.010 0.324 35.841 0.114 1.442 4.104 0.18 82770. 0.0979
|
|
41.84 1.0519 0.6753 0.0220 0.0343 0.040 0.843 0.243 29.914 0.095 1.080 3.682 0.18 83280. 0.0760
|
|
43.45 1.0924 0.5891 0.0146 0.0271 0.032 0.667 0.161 23.657 0.075 0.718 3.093 0.18 83806. 0.0521
|
|
45.06 1.1329 0.4201 0.0073 0.0196 0.023 0.482 0.080 17.106 0.054 0.357 2.127 0.18 84346. 0.0252
|
|
46.67 1.1733 -0.0011 0.0000 0.0118 0.014 0.290 0.000 10.295 0.033 -0.001 -0.005 0.18 84897. 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 0.1257 0.0619 0.172 2.704 2.463 127.948 0.305 10.954 8.730 0.22 100786. 0.5742
|
|
2.15 0.0405 0.0799 0.1253 0.0635 0.176 2.774 2.454 131.260 0.313 10.915 8.479 0.22 100898. 0.5567
|
|
4.30 0.0811 0.1549 0.1248 0.0653 0.181 2.850 2.444 134.870 0.322 10.870 8.218 0.22 101026. 0.5385
|
|
6.45 0.1216 0.2248 0.1242 0.0672 0.186 2.932 2.432 138.738 0.331 10.817 7.951 0.22 101174. 0.5196
|
|
8.60 0.1621 0.2894 0.1234 0.0691 0.192 3.018 2.418 142.807 0.341 10.754 7.679 0.22 101342. 0.5004
|
|
10.75 0.2027 0.3490 0.1225 0.0712 0.197 3.106 2.400 147.003 0.351 10.677 7.406 0.22 101531. 0.4809
|
|
12.90 0.2432 0.4035 0.1215 0.0732 0.203 3.196 2.379 151.228 0.361 10.583 7.136 0.22 101743. 0.4613
|
|
15.05 0.2837 0.4532 0.1201 0.0752 0.208 3.283 2.353 155.369 0.371 10.468 6.871 0.22 101978. 0.4418
|
|
17.20 0.3243 0.4984 0.1185 0.0771 0.214 3.366 2.322 159.298 0.380 10.329 6.612 0.22 102238. 0.4223
|
|
19.35 0.3648 0.5395 0.1166 0.0789 0.218 3.442 2.284 162.878 0.389 10.161 6.362 0.22 102522. 0.4030
|
|
21.50 0.4053 0.5768 0.1143 0.0803 0.223 3.507 2.240 165.961 0.396 9.961 6.121 0.22 102831. 0.3839
|
|
23.64 0.4459 0.6105 0.1116 0.0815 0.226 3.558 2.187 168.400 0.402 9.726 5.889 0.22 103166. 0.3650
|
|
25.79 0.4864 0.6410 0.1085 0.0823 0.228 3.593 2.125 170.042 0.406 9.452 5.668 0.22 103527. 0.3463
|
|
27.94 0.5269 0.6684 0.1049 0.0827 0.229 3.608 2.054 170.729 0.408 9.135 5.456 0.23 103913. 0.3277
|
|
30.09 0.5675 0.6931 0.1007 0.0824 0.228 3.598 1.972 170.295 0.407 8.773 5.253 0.23 104324. 0.3092
|
|
32.24 0.6080 0.7151 0.0960 0.0816 0.226 3.562 1.880 168.573 0.402 8.363 5.059 0.23 104759. 0.2907
|
|
34.39 0.6485 0.7346 0.0907 0.0801 0.222 3.496 1.777 165.443 0.395 7.905 4.872 0.23 105219. 0.2722
|
|
36.54 0.6891 0.7517 0.0850 0.0779 0.216 3.400 1.664 160.887 0.384 7.403 4.692 0.23 105703. 0.2537
|
|
38.69 0.7296 0.7662 0.0788 0.0750 0.208 3.275 1.543 154.969 0.370 6.865 4.517 0.23 106211. 0.2352
|
|
40.84 0.7701 0.7782 0.0723 0.0715 0.198 3.123 1.416 147.783 0.353 6.299 4.346 0.23 106741. 0.2168
|
|
42.99 0.8107 0.7872 0.0655 0.0675 0.187 2.946 1.284 139.420 0.333 5.711 4.177 0.23 107295. 0.1983
|
|
45.14 0.8512 0.7927 0.0586 0.0629 0.174 2.746 1.148 129.952 0.310 5.105 4.006 0.23 107871. 0.1798
|
|
47.29 0.8917 0.7939 0.0515 0.0578 0.160 2.524 1.008 119.437 0.285 4.485 3.829 0.23 108468. 0.1612
|
|
49.44 0.9323 0.7894 0.0442 0.0523 0.145 2.280 0.867 107.923 0.258 3.855 3.642 0.23 109088. 0.1421
|
|
51.59 0.9728 0.7772 0.0369 0.0462 0.128 2.017 0.723 95.451 0.228 3.217 3.436 0.23 109729. 0.1225
|
|
53.74 1.0133 0.7532 0.0295 0.0397 0.110 1.734 0.578 82.066 0.196 2.573 3.197 0.23 110390. 0.1019
|
|
55.89 1.0539 0.7096 0.0221 0.0328 0.091 1.433 0.433 67.819 0.162 1.926 2.896 0.23 111073. 0.0799
|
|
58.04 1.0944 0.6290 0.0147 0.0256 0.071 1.115 0.288 52.775 0.126 1.279 2.472 0.24 111776. 0.0556
|
|
60.19 1.1349 0.4623 0.0073 0.0179 0.050 0.782 0.143 37.017 0.088 0.636 1.752 0.24 112499. 0.0278
|
|
62.34 1.1755 -0.0013 0.0000 0.0100 0.028 0.436 0.000 20.631 0.049 -0.001 -0.005 0.24 113235. 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 0.1259 0.0611 0.330 4.164 3.854 246.326 0.470 17.142 7.096 0.28 125981. 0.5839
|
|
2.69 0.0406 0.0813 0.1255 0.0627 0.339 4.274 3.841 252.834 0.483 17.084 6.890 0.28 126120. 0.5660
|
|
5.38 0.0812 0.1575 0.1250 0.0644 0.349 4.394 3.826 259.939 0.496 17.017 6.676 0.28 126281. 0.5472
|
|
8.07 0.1218 0.2285 0.1244 0.0663 0.359 4.523 3.808 267.567 0.511 16.938 6.455 0.28 126466. 0.5280
|
|
10.76 0.1624 0.2941 0.1237 0.0683 0.370 4.659 3.787 275.609 0.526 16.843 6.232 0.28 126676. 0.5082
|
|
13.46 0.2030 0.3544 0.1229 0.0704 0.381 4.799 3.761 283.916 0.542 16.727 6.008 0.28 126913. 0.4883
|
|
16.15 0.2436 0.4095 0.1218 0.0725 0.392 4.941 3.729 292.298 0.558 16.584 5.786 0.28 127178. 0.4682
|
|
18.84 0.2842 0.4598 0.1205 0.0745 0.403 5.080 3.689 300.530 0.574 16.409 5.568 0.28 127473. 0.4482
|
|
21.53 0.3248 0.5055 0.1190 0.0764 0.414 5.213 3.641 308.359 0.589 16.195 5.356 0.28 127798. 0.4283
|
|
24.22 0.3654 0.5469 0.1171 0.0782 0.423 5.334 3.583 315.508 0.603 15.937 5.151 0.28 128155. 0.4086
|
|
26.91 0.4060 0.5844 0.1148 0.0797 0.431 5.438 3.513 321.688 0.614 15.628 4.954 0.28 128543. 0.3892
|
|
29.60 0.4466 0.6184 0.1121 0.0810 0.438 5.521 3.431 326.598 0.624 15.262 4.765 0.28 128963. 0.3700
|
|
32.29 0.4872 0.6491 0.1090 0.0818 0.442 5.577 3.335 329.937 0.630 14.835 4.585 0.28 129415. 0.3509
|
|
34.98 0.5278 0.6768 0.1053 0.0821 0.444 5.602 3.224 331.389 0.633 14.341 4.413 0.28 129899. 0.3321
|
|
37.68 0.5684 0.7017 0.1012 0.0820 0.443 5.589 3.097 330.624 0.631 13.774 4.248 0.28 130414. 0.3133
|
|
40.37 0.6090 0.7240 0.0965 0.0811 0.439 5.533 2.952 327.309 0.625 13.131 4.091 0.28 130960. 0.2946
|
|
43.06 0.6496 0.7438 0.0912 0.0796 0.431 5.430 2.790 321.208 0.613 12.412 3.940 0.28 131537. 0.2759
|
|
45.75 0.6902 0.7613 0.0854 0.0774 0.419 5.279 2.613 312.279 0.596 11.624 3.796 0.28 132144. 0.2572
|
|
48.44 0.7308 0.7764 0.0792 0.0745 0.403 5.082 2.423 300.649 0.574 10.779 3.656 0.29 132780. 0.2385
|
|
51.13 0.7714 0.7890 0.0726 0.0710 0.384 4.843 2.223 286.502 0.547 9.889 3.520 0.29 133446. 0.2200
|
|
53.82 0.8120 0.7988 0.0658 0.0669 0.362 4.564 2.015 270.016 0.516 8.964 3.385 0.29 134140. 0.2014
|
|
56.51 0.8525 0.8053 0.0588 0.0623 0.337 4.249 1.801 251.333 0.480 8.012 3.250 0.29 134862. 0.1828
|
|
59.20 0.8931 0.8079 0.0517 0.0572 0.309 3.898 1.582 230.566 0.440 7.038 3.112 0.29 135611. 0.1641
|
|
61.90 0.9337 0.8052 0.0444 0.0515 0.279 3.513 1.359 207.809 0.397 6.047 2.967 0.29 136388. 0.1450
|
|
64.59 0.9743 0.7951 0.0370 0.0454 0.246 3.096 1.134 183.145 0.350 5.044 2.808 0.29 137191. 0.1253
|
|
67.28 1.0149 0.7740 0.0296 0.0388 0.210 2.648 0.906 156.663 0.299 4.032 2.624 0.29 138021. 0.1047
|
|
69.97 1.0555 0.7342 0.0222 0.0318 0.172 2.172 0.678 128.465 0.245 3.016 2.394 0.29 138877. 0.0826
|
|
72.66 1.0961 0.6581 0.0147 0.0245 0.132 1.668 0.449 98.681 0.188 1.999 2.066 0.29 139758. 0.0581
|
|
75.35 1.1367 0.4934 0.0073 0.0167 0.090 1.141 0.222 67.476 0.129 0.988 1.494 0.30 140664. 0.0295
|
|
78.04 1.1773 -0.0119 -0.0001 0.0087 0.047 0.592 -0.003 35.020 0.067 -0.012 -0.035 0.30 141584. 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 0.1261 0.0605 0.566 5.943 5.559 421.900 0.671 24.725 5.976 0.33 151175. 0.5905
|
|
3.23 0.0406 0.0822 0.1257 0.0621 0.581 6.102 5.541 433.189 0.689 24.645 5.801 0.33 151342. 0.5723
|
|
6.46 0.0812 0.1592 0.1252 0.0639 0.597 6.276 5.520 445.539 0.709 24.553 5.620 0.33 151535. 0.5534
|
|
9.69 0.1218 0.2309 0.1247 0.0658 0.615 6.464 5.496 458.826 0.730 24.446 5.433 0.33 151756. 0.5338
|
|
12.92 0.1625 0.2971 0.1240 0.0678 0.634 6.661 5.467 472.866 0.753 24.316 5.244 0.33 152008. 0.5138
|
|
16.15 0.2031 0.3579 0.1232 0.0699 0.654 6.866 5.431 487.401 0.776 24.156 5.054 0.33 152293. 0.4936
|
|
19.39 0.2437 0.4135 0.1222 0.0720 0.673 7.073 5.386 502.104 0.799 23.958 4.866 0.33 152611. 0.4733
|
|
22.62 0.2843 0.4641 0.1210 0.0741 0.693 7.277 5.331 516.578 0.822 23.714 4.681 0.33 152965. 0.4530
|
|
25.85 0.3249 0.5101 0.1194 0.0761 0.711 7.471 5.264 530.379 0.844 23.413 4.502 0.33 153355. 0.4329
|
|
29.08 0.3655 0.5517 0.1176 0.0779 0.728 7.650 5.182 543.019 0.864 23.048 4.328 0.34 153783. 0.4129
|
|
32.31 0.4062 0.5895 0.1153 0.0795 0.743 7.804 5.083 553.984 0.882 22.610 4.162 0.34 154249. 0.3933
|
|
35.54 0.4468 0.6236 0.1127 0.0807 0.755 7.927 4.966 562.748 0.896 22.089 4.003 0.34 154754. 0.3738
|
|
38.77 0.4874 0.6545 0.1096 0.0816 0.763 8.012 4.829 568.774 0.905 21.478 3.851 0.34 155297. 0.3546
|
|
42.00 0.5280 0.6824 0.1059 0.0820 0.766 8.051 4.670 571.510 0.910 20.770 3.706 0.34 155878. 0.3356
|
|
45.23 0.5686 0.7075 0.1018 0.0818 0.765 8.035 4.486 570.376 0.908 19.956 3.568 0.34 156497. 0.3167
|
|
48.46 0.6092 0.7300 0.0971 0.0810 0.757 7.956 4.278 564.789 0.899 19.030 3.436 0.34 157153. 0.2979
|
|
51.69 0.6499 0.7501 0.0918 0.0795 0.743 7.809 4.045 554.327 0.882 17.992 3.310 0.34 157847. 0.2790
|
|
54.92 0.6905 0.7679 0.0860 0.0773 0.723 7.592 3.789 538.911 0.858 16.854 3.189 0.34 158576. 0.2602
|
|
58.16 0.7311 0.7835 0.0797 0.0744 0.696 7.308 3.515 518.751 0.826 15.633 3.073 0.34 159341. 0.2415
|
|
61.39 0.7717 0.7966 0.0732 0.0709 0.663 6.961 3.225 494.173 0.787 14.345 2.960 0.34 160140. 0.2228
|
|
64.62 0.8123 0.8071 0.0663 0.0668 0.624 6.557 2.924 465.483 0.741 13.006 2.849 0.34 160974. 0.2042
|
|
67.85 0.8529 0.8146 0.0593 0.0621 0.581 6.099 2.614 432.934 0.689 11.627 2.739 0.35 161841. 0.1856
|
|
71.08 0.8936 0.8182 0.0521 0.0569 0.532 5.589 2.297 396.721 0.631 10.216 2.626 0.35 162742. 0.1668
|
|
74.31 0.9342 0.8170 0.0448 0.0512 0.479 5.029 1.974 357.010 0.568 8.781 2.508 0.35 163675. 0.1477
|
|
77.54 0.9748 0.8090 0.0374 0.0450 0.421 4.423 1.647 313.946 0.500 7.327 2.380 0.35 164640. 0.1280
|
|
80.77 1.0154 0.7905 0.0299 0.0384 0.359 3.771 1.318 267.683 0.426 5.861 2.233 0.35 165636. 0.1074
|
|
84.00 1.0560 0.7544 0.0224 0.0313 0.293 3.077 0.986 218.404 0.348 4.388 2.049 0.35 166664. 0.0853
|
|
87.23 1.0966 0.6833 0.0149 0.0239 0.223 2.343 0.655 166.334 0.265 2.915 1.787 0.35 167723. 0.0606
|
|
90.46 1.1373 0.5244 0.0074 0.0160 0.150 1.574 0.326 111.767 0.178 1.449 1.322 0.35 168811. 0.0316
|
|
93.69 1.1779 -0.0007 0.0000 0.0079 0.074 0.775 0.000 54.994 0.088 -0.001 -0.002 0.36 169914. 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 0.1263 0.0602 0.894 8.049 7.579 666.594 0.909 33.710 5.157 0.39 176367. 0.5950
|
|
3.77 0.0406 0.0828 0.1260 0.0618 0.918 8.266 7.556 684.582 0.934 33.608 5.006 0.39 176561. 0.5767
|
|
7.54 0.0813 0.1604 0.1255 0.0636 0.944 8.504 7.529 704.307 0.961 33.491 4.849 0.39 176787. 0.5577
|
|
11.32 0.1219 0.2325 0.1250 0.0655 0.973 8.761 7.499 725.582 0.990 33.353 4.687 0.39 177045. 0.5380
|
|
15.09 0.1626 0.2992 0.1244 0.0676 1.003 9.033 7.461 748.120 1.021 33.187 4.523 0.39 177339. 0.5179
|
|
18.86 0.2032 0.3604 0.1236 0.0697 1.035 9.316 7.415 771.517 1.052 32.980 4.359 0.39 177671. 0.4975
|
|
22.63 0.2439 0.4163 0.1226 0.0718 1.066 9.602 7.357 795.247 1.085 32.723 4.196 0.39 178042. 0.4770
|
|
26.41 0.2845 0.4672 0.1214 0.0740 1.098 9.885 7.285 818.673 1.117 32.403 4.036 0.39 178455. 0.4566
|
|
30.18 0.3252 0.5134 0.1200 0.0760 1.128 10.156 7.196 841.069 1.147 32.007 3.881 0.39 178911. 0.4363
|
|
33.95 0.3658 0.5552 0.1181 0.0778 1.155 10.404 7.087 861.641 1.175 31.522 3.730 0.39 179411. 0.4162
|
|
37.72 0.4065 0.5931 0.1159 0.0795 1.179 10.620 6.955 879.553 1.200 30.935 3.586 0.39 179956. 0.3964
|
|
41.49 0.4471 0.6274 0.1133 0.0808 1.199 10.794 6.797 893.942 1.220 30.235 3.449 0.39 180545. 0.3769
|
|
45.27 0.4878 0.6584 0.1102 0.0817 1.212 10.915 6.612 903.938 1.233 29.411 3.318 0.39 181180. 0.3576
|
|
49.04 0.5284 0.6864 0.1066 0.0821 1.219 10.972 6.396 908.644 1.240 28.451 3.193 0.39 181859. 0.3384
|
|
52.81 0.5691 0.7117 0.1025 0.0819 1.216 10.953 6.148 907.122 1.237 27.345 3.074 0.40 182583. 0.3194
|
|
56.58 0.6097 0.7344 0.0978 0.0812 1.205 10.848 5.864 898.428 1.226 26.084 2.961 0.40 183350. 0.3005
|
|
60.36 0.6504 0.7547 0.0925 0.0797 1.183 10.648 5.546 881.878 1.203 24.669 2.852 0.40 184160. 0.2815
|
|
64.13 0.6910 0.7729 0.0866 0.0774 1.150 10.352 5.196 857.327 1.170 23.113 2.749 0.40 185013. 0.2626
|
|
67.90 0.7317 0.7888 0.0804 0.0745 1.106 9.963 4.821 825.111 1.126 21.442 2.650 0.40 185907. 0.2438
|
|
71.67 0.7723 0.8024 0.0737 0.0710 1.054 9.488 4.424 785.750 1.072 19.678 2.554 0.40 186841. 0.2251
|
|
75.44 0.8129 0.8135 0.0669 0.0668 0.992 8.932 4.011 739.744 1.009 17.843 2.460 0.40 187816. 0.2065
|
|
79.22 0.8536 0.8217 0.0598 0.0621 0.922 8.301 3.586 687.497 0.938 15.952 2.366 0.40 188830. 0.1878
|
|
82.99 0.8942 0.8263 0.0525 0.0569 0.844 7.599 3.151 629.330 0.859 14.017 2.271 0.40 189882. 0.1690
|
|
86.76 0.9349 0.8263 0.0452 0.0511 0.758 6.828 2.709 565.505 0.771 12.048 2.172 0.41 190972. 0.1498
|
|
90.53 0.9755 0.8198 0.0377 0.0448 0.665 5.992 2.260 496.261 0.677 10.053 2.066 0.41 192100. 0.1302
|
|
94.30 1.0162 0.8035 0.0301 0.0381 0.566 5.094 1.808 421.845 0.575 8.040 1.944 0.41 193265. 0.1095
|
|
98.08 1.0568 0.7703 0.0226 0.0309 0.459 4.136 1.353 342.551 0.467 6.018 1.791 0.41 194465. 0.0873
|
|
101.85 1.0975 0.7031 0.0150 0.0234 0.347 3.124 0.898 258.745 0.353 3.995 1.575 0.41 195702. 0.0625
|
|
105.62 1.1381 0.5480 0.0074 0.0154 0.229 2.064 0.446 170.904 0.233 1.983 1.183 0.41 196973. 0.0331
|
|
109.39 1.1788 -0.0053 0.0000 0.0072 0.107 0.960 -0.002 79.480 0.108 -0.009 -0.011 0.42 198260. 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 0.1266 0.0601 1.332 10.490 9.916 992.903 1.185 44.108 4.530 0.44 201558. 0.5979
|
|
4.31 0.0407 0.0832 0.1262 0.0617 1.368 10.775 9.888 1019.814 1.217 43.984 4.398 0.44 201780. 0.5796
|
|
8.63 0.0813 0.1611 0.1258 0.0635 1.407 11.087 9.857 1049.404 1.253 43.842 4.260 0.44 202037. 0.5606
|
|
12.94 0.1220 0.2336 0.1253 0.0654 1.450 11.425 9.819 1081.413 1.291 43.676 4.118 0.44 202332. 0.5409
|
|
17.25 0.1627 0.3006 0.1247 0.0675 1.496 11.785 9.774 1115.430 1.331 43.474 3.974 0.44 202668. 0.5208
|
|
21.57 0.2033 0.3621 0.1240 0.0696 1.543 12.159 9.717 1150.856 1.374 43.222 3.830 0.45 203047. 0.5003
|
|
25.88 0.2440 0.4182 0.1231 0.0718 1.592 12.540 9.646 1186.903 1.417 42.905 3.686 0.45 203471. 0.4798
|
|
30.19 0.2847 0.4693 0.1220 0.0740 1.640 12.917 9.556 1222.603 1.459 42.506 3.545 0.45 203943. 0.4593
|
|
34.51 0.3253 0.5156 0.1205 0.0761 1.685 13.279 9.444 1256.844 1.500 42.008 3.408 0.45 204464. 0.4390
|
|
38.82 0.3660 0.5575 0.1188 0.0780 1.728 13.612 9.306 1288.405 1.538 41.393 3.276 0.45 205036. 0.4189
|
|
43.13 0.4067 0.5955 0.1166 0.0796 1.765 13.904 9.138 1315.995 1.571 40.644 3.149 0.45 205659. 0.3990
|
|
47.45 0.4474 0.6299 0.1140 0.0810 1.795 14.139 8.936 1338.290 1.597 39.745 3.028 0.45 206333. 0.3794
|
|
51.76 0.4880 0.6611 0.1110 0.0819 1.816 14.305 8.696 1353.948 1.616 38.681 2.913 0.45 207059. 0.3601
|
|
56.07 0.5287 0.6892 0.1074 0.0824 1.826 14.386 8.416 1361.600 1.625 37.436 2.804 0.45 207837. 0.3409
|
|
60.39 0.5694 0.7146 0.1033 0.0823 1.824 14.367 8.093 1359.817 1.623 35.997 2.699 0.45 208665. 0.3218
|
|
64.70 0.6100 0.7375 0.0986 0.0815 1.807 14.233 7.723 1347.167 1.608 34.351 2.600 0.45 209544. 0.3028
|
|
69.01 0.6507 0.7581 0.0932 0.0800 1.774 13.974 7.306 1322.590 1.579 32.498 2.506 0.45 210471. 0.2839
|
|
73.33 0.6914 0.7765 0.0874 0.0778 1.724 13.585 6.848 1285.848 1.535 30.459 2.415 0.45 211447. 0.2649
|
|
77.64 0.7320 0.7928 0.0811 0.0749 1.659 13.074 6.354 1237.435 1.477 28.264 2.329 0.46 212470. 0.2461
|
|
81.95 0.7727 0.8068 0.0744 0.0713 1.580 12.447 5.833 1178.145 1.406 25.945 2.246 0.46 213540. 0.2273
|
|
86.27 0.8134 0.8184 0.0675 0.0671 1.487 11.714 5.290 1108.740 1.323 23.530 2.164 0.46 214656. 0.2086
|
|
90.58 0.8540 0.8273 0.0604 0.0623 1.381 10.881 4.730 1029.840 1.229 21.039 2.083 0.46 215816. 0.1899
|
|
94.89 0.8947 0.8327 0.0531 0.0570 1.263 9.952 4.157 941.935 1.124 18.490 2.002 0.46 217020. 0.1710
|
|
99.21 0.9354 0.8338 0.0456 0.0512 1.134 8.932 3.573 845.425 1.009 15.894 1.917 0.46 218268. 0.1519
|
|
103.52 0.9760 0.8288 0.0381 0.0448 0.993 7.825 2.982 740.672 0.884 13.264 1.826 0.47 219558. 0.1322
|
|
107.83 1.0167 0.8143 0.0304 0.0380 0.842 6.636 2.385 628.051 0.750 10.609 1.723 0.47 220891. 0.1115
|
|
112.15 1.0574 0.7837 0.0228 0.0307 0.681 5.367 1.785 508.005 0.606 7.941 1.594 0.47 222265. 0.0893
|
|
116.46 1.0981 0.7202 0.0151 0.0231 0.511 4.026 1.185 381.094 0.455 5.272 1.411 0.47 223680. 0.0644
|
|
120.77 1.1387 0.5693 0.0075 0.0150 0.333 2.621 0.588 248.044 0.296 2.616 1.075 0.47 225133. 0.0346
|
|
125.09 1.1794 -0.0077 0.0000 0.0066 0.147 1.157 -0.003 109.521 0.131 -0.015 -0.014 0.47 226603. 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 0.1268 0.0601 1.896 13.280 12.574 1414.045 1.500 55.930 4.033 0.50 226746. 0.5994
|
|
4.85 0.0407 0.0834 0.1265 0.0617 1.948 13.640 12.542 1452.402 1.541 55.785 3.917 0.50 226996. 0.5813
|
|
9.71 0.0814 0.1615 0.1261 0.0635 2.004 14.037 12.505 1494.707 1.586 55.622 3.795 0.50 227285. 0.5624
|
|
14.56 0.1221 0.2342 0.1257 0.0655 2.066 14.469 12.462 1540.629 1.635 55.430 3.669 0.50 227616. 0.5428
|
|
19.42 0.1627 0.3014 0.1251 0.0676 2.132 14.929 12.409 1589.610 1.687 55.196 3.541 0.50 227994. 0.5228
|
|
24.27 0.2034 0.3631 0.1245 0.0697 2.200 15.410 12.343 1640.819 1.741 54.902 3.412 0.50 228420. 0.5024
|
|
29.13 0.2441 0.4194 0.1236 0.0720 2.271 15.901 12.259 1693.130 1.796 54.529 3.284 0.50 228897. 0.4819
|
|
33.98 0.2848 0.4705 0.1225 0.0742 2.340 16.389 12.153 1745.141 1.852 54.054 3.158 0.50 229428. 0.4615
|
|
38.84 0.3255 0.5170 0.1212 0.0763 2.407 16.860 12.018 1795.220 1.905 53.454 3.036 0.50 230014. 0.4412
|
|
43.69 0.3662 0.5590 0.1195 0.0783 2.470 17.295 11.849 1841.563 1.954 52.705 2.918 0.50 230657. 0.4210
|
|
48.55 0.4069 0.5971 0.1174 0.0800 2.524 17.677 11.642 1882.267 1.997 51.785 2.805 0.50 231358. 0.4012
|
|
53.40 0.4475 0.6315 0.1149 0.0814 2.569 17.988 11.392 1915.372 2.032 50.671 2.698 0.50 232118. 0.3816
|
|
58.25 0.4882 0.6627 0.1119 0.0824 2.600 18.209 11.093 1938.902 2.057 49.343 2.595 0.51 232935. 0.3623
|
|
63.11 0.5289 0.6910 0.1083 0.0829 2.616 18.321 10.743 1950.851 2.070 47.783 2.498 0.51 233811. 0.3431
|
|
67.96 0.5696 0.7166 0.1042 0.0828 2.614 18.305 10.335 1949.141 2.068 45.970 2.405 0.51 234745. 0.3240
|
|
72.82 0.6103 0.7396 0.0995 0.0821 2.590 18.141 9.867 1931.688 2.050 43.891 2.317 0.51 235734. 0.3050
|
|
77.67 0.6510 0.7604 0.0942 0.0806 2.544 17.815 9.340 1896.928 2.013 41.543 2.233 0.51 236779. 0.2860
|
|
82.53 0.6917 0.7791 0.0883 0.0784 2.473 17.322 8.757 1844.475 1.957 38.951 2.153 0.51 237879. 0.2671
|
|
87.38 0.7323 0.7957 0.0820 0.0754 2.380 16.670 8.129 1775.030 1.883 36.156 2.077 0.51 239032. 0.2482
|
|
92.24 0.7730 0.8101 0.0753 0.0718 2.266 15.869 7.464 1689.747 1.793 33.200 2.004 0.51 240237. 0.2294
|
|
97.09 0.8137 0.8223 0.0683 0.0676 2.132 14.930 6.771 1589.747 1.687 30.117 1.932 0.52 241494. 0.2107
|
|
101.95 0.8544 0.8317 0.0611 0.0627 1.979 13.861 6.056 1475.944 1.566 26.936 1.861 0.52 242801. 0.1919
|
|
106.80 0.8951 0.8379 0.0537 0.0573 1.809 12.669 5.323 1349.053 1.431 23.677 1.790 0.52 244158. 0.1731
|
|
111.65 0.9358 0.8400 0.0462 0.0514 1.622 11.360 4.577 1209.656 1.283 20.357 1.716 0.52 245563. 0.1539
|
|
116.51 0.9765 0.8362 0.0385 0.0450 1.419 9.939 3.820 1058.282 1.123 16.991 1.637 0.52 247016. 0.1341
|
|
121.36 1.0171 0.8235 0.0308 0.0381 1.201 8.410 3.056 895.471 0.950 13.592 1.548 0.53 248517. 0.1134
|
|
126.22 1.0578 0.7953 0.0231 0.0307 0.968 6.779 2.287 721.863 0.766 10.175 1.437 0.53 250064. 0.0911
|
|
131.07 1.0985 0.7352 0.0153 0.0229 0.722 5.055 1.518 538.273 0.571 6.754 1.280 0.53 251657. 0.0661
|
|
135.93 1.1392 0.5887 0.0076 0.0147 0.464 3.247 0.753 345.754 0.367 3.349 0.988 0.53 253294. 0.0359
|
|
140.78 1.1799 -0.0105 -0.0001 0.0062 0.195 1.364 -0.005 145.238 0.154 -0.024 -0.017 0.53 254945. 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 0.1271 0.0602 2.607 16.433 15.555 1944.188 1.857 69.187 3.629 0.56 251933. 0.5998
|
|
5.43 0.0410 0.0839 0.1268 0.0619 2.678 16.880 15.518 1997.146 1.907 69.023 3.524 0.56 252212. 0.5819
|
|
10.86 0.0819 0.1626 0.1264 0.0637 2.757 17.376 15.477 2055.797 1.963 68.840 3.415 0.56 252535. 0.5630
|
|
16.30 0.1229 0.2358 0.1260 0.0657 2.843 17.916 15.429 2119.730 2.024 68.627 3.301 0.56 252906. 0.5435
|
|
21.73 0.1639 0.3035 0.1255 0.0678 2.934 18.495 15.370 2188.231 2.090 68.366 3.186 0.56 253329. 0.5235
|
|
27.16 0.2049 0.3655 0.1249 0.0700 3.031 19.103 15.295 2260.160 2.158 68.034 3.069 0.56 253806. 0.5031
|
|
32.59 0.2458 0.4220 0.1242 0.0723 3.130 19.727 15.199 2333.939 2.229 67.607 2.954 0.56 254341. 0.4826
|
|
38.02 0.2868 0.4734 0.1231 0.0746 3.229 20.349 15.075 2407.560 2.299 67.054 2.840 0.56 254937. 0.4622
|
|
43.46 0.3278 0.5200 0.1218 0.0768 3.324 20.950 14.916 2478.646 2.367 66.345 2.729 0.56 255596. 0.4418
|
|
48.89 0.3687 0.5621 0.1202 0.0788 3.412 21.507 14.714 2544.561 2.430 65.447 2.623 0.56 256319. 0.4217
|
|
54.32 0.4097 0.6002 0.1181 0.0806 3.490 21.997 14.463 2602.504 2.485 64.330 2.521 0.56 257108. 0.4018
|
|
59.75 0.4507 0.6347 0.1156 0.0821 3.553 22.395 14.156 2649.608 2.530 62.964 2.423 0.56 257962. 0.3821
|
|
65.18 0.4917 0.6660 0.1126 0.0831 3.598 22.677 13.787 2682.994 2.562 61.324 2.331 0.56 258883. 0.3627
|
|
70.61 0.5326 0.6943 0.1090 0.0837 3.620 22.819 13.350 2699.752 2.578 59.382 2.243 0.56 259869. 0.3435
|
|
76.05 0.5736 0.7200 0.1049 0.0836 3.617 22.795 12.841 2696.887 2.575 57.116 2.160 0.56 260920. 0.3243
|
|
81.48 0.6146 0.7431 0.1001 0.0828 3.582 22.580 12.254 2671.438 2.551 54.504 2.080 0.57 262035. 0.3052
|
|
86.91 0.6556 0.7641 0.0947 0.0812 3.515 22.155 11.589 2621.252 2.503 51.549 2.005 0.57 263213. 0.2861
|
|
92.34 0.6965 0.7829 0.0887 0.0789 3.414 21.519 10.855 2545.909 2.431 48.283 1.934 0.57 264451. 0.2670
|
|
97.77 0.7375 0.7997 0.0822 0.0758 3.281 20.678 10.063 2446.505 2.336 44.760 1.866 0.57 265750. 0.2480
|
|
103.21 0.7785 0.8143 0.0754 0.0720 3.118 19.649 9.225 2324.721 2.220 41.033 1.800 0.57 267107. 0.2291
|
|
108.64 0.8194 0.8267 0.0682 0.0676 2.926 18.444 8.351 2182.161 2.084 37.146 1.736 0.57 268522. 0.2102
|
|
114.07 0.8604 0.8364 0.0608 0.0626 2.709 17.074 7.449 2020.108 1.929 33.135 1.673 0.58 269994. 0.1913
|
|
119.50 0.9014 0.8429 0.0533 0.0570 2.467 15.548 6.525 1839.568 1.757 29.025 1.609 0.58 271521. 0.1723
|
|
124.93 0.9424 0.8452 0.0456 0.0509 2.201 13.873 5.584 1641.361 1.567 24.839 1.543 0.58 273103. 0.1528
|
|
130.37 0.9833 0.8415 0.0378 0.0442 1.913 12.055 4.630 1426.233 1.362 20.594 1.472 0.58 274739. 0.1328
|
|
135.80 1.0243 0.8284 0.0299 0.0370 1.602 10.100 3.666 1194.974 1.141 16.307 1.392 0.58 276428. 0.1117
|
|
141.23 1.0653 0.7986 0.0220 0.0294 1.272 8.017 2.697 948.525 0.906 11.997 1.290 0.59 278169. 0.0888
|
|
146.66 1.1062 0.7323 0.0141 0.0213 0.923 5.816 1.728 688.096 0.657 7.686 1.139 0.59 279961. 0.0627
|
|
152.09 1.1472 0.5561 0.0062 0.0129 0.557 3.510 0.764 415.267 0.397 3.397 0.834 0.59 281801. 0.0305
|
|
157.52 1.1882
|
|
|
|
|
|
|
|
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 0.1273 0.0605 3.486 19.976 18.860 2599.745 2.257 83.891 3.291 0.61 277118. 0.5989
|
|
5.94 0.0407 0.0832 0.1270 0.0621 3.580 20.512 18.820 2669.458 2.317 83.713 3.198 0.61 277422. 0.5814
|
|
11.87 0.0814 0.1614 0.1268 0.0639 3.684 21.107 18.777 2746.918 2.385 83.520 3.100 0.61 277774. 0.5631
|
|
17.81 0.1221 0.2342 0.1264 0.0659 3.797 21.758 18.727 2831.709 2.458 83.297 3.000 0.61 278178. 0.5440
|
|
23.75 0.1628 0.3015 0.1260 0.0680 3.920 22.460 18.666 2923.003 2.538 83.025 2.896 0.61 278637. 0.5245
|
|
29.68 0.2035 0.3633 0.1255 0.0703 4.049 23.201 18.588 3019.426 2.621 82.678 2.792 0.61 279156. 0.5045
|
|
35.62 0.2442 0.4198 0.1248 0.0726 4.183 23.966 18.486 3118.976 2.708 82.225 2.688 0.61 279737. 0.4844
|
|
41.56 0.2850 0.4711 0.1239 0.0749 4.317 24.735 18.352 3219.041 2.795 81.631 2.586 0.61 280384. 0.4643
|
|
47.49 0.3257 0.5176 0.1227 0.0772 4.447 25.483 18.178 3316.447 2.879 80.854 2.486 0.61 281099. 0.4442
|
|
53.43 0.3664 0.5597 0.1212 0.0793 4.570 26.183 17.953 3407.598 2.958 79.854 2.390 0.62 281885. 0.4244
|
|
59.36 0.4071 0.5978 0.1193 0.0812 4.678 26.806 17.669 3488.649 3.029 78.591 2.297 0.62 282742. 0.4047
|
|
65.30 0.4478 0.6324 0.1169 0.0828 4.768 27.321 17.317 3555.643 3.087 77.027 2.209 0.62 283671. 0.3853
|
|
71.24 0.4885 0.6638 0.1140 0.0839 4.834 27.697 16.891 3604.617 3.129 75.130 2.125 0.62 284672. 0.3661
|
|
77.17 0.5292 0.6922 0.1106 0.0845 4.870 27.905 16.382 3631.615 3.153 72.866 2.046 0.62 285745. 0.3471
|
|
83.11 0.5699 0.7180 0.1065 0.0846 4.871 27.912 15.783 3632.612 3.154 70.205 1.971 0.62 286889. 0.3281
|
|
89.05 0.6106 0.7415 0.1019 0.0839 4.833 27.690 15.090 3603.604 3.128 67.121 1.899 0.62 288102. 0.3092
|
|
94.98 0.6513 0.7627 0.0965 0.0824 4.749 27.212 14.301 3541.486 3.074 63.610 1.832 0.62 289383. 0.2903
|
|
100.92 0.6920 0.7819 0.0906 0.0802 4.620 26.473 13.424 3445.338 2.991 59.709 1.767 0.63 290731. 0.2714
|
|
106.86 0.7327 0.7991 0.0842 0.0772 4.447 25.483 12.472 3316.414 2.879 55.477 1.706 0.63 292145. 0.2525
|
|
112.79 0.7734 0.8143 0.0774 0.0735 4.234 24.258 11.462 3156.954 2.741 50.984 1.647 0.63 293622. 0.2337
|
|
118.73 0.8141 0.8274 0.0702 0.0691 3.982 22.815 10.406 2969.185 2.578 46.285 1.590 0.63 295163. 0.2149
|
|
124.67 0.8549 0.8380 0.0629 0.0641 3.694 21.168 9.313 2754.927 2.392 41.425 1.533 0.63 296764. 0.1961
|
|
130.60 0.8956 0.8457 0.0553 0.0586 3.373 19.329 8.192 2515.586 2.184 36.436 1.477 0.64 298426. 0.1772
|
|
136.54 0.9363 0.8495 0.0476 0.0524 3.020 17.306 7.047 2252.298 1.955 31.347 1.419 0.64 300148. 0.1579
|
|
142.48 0.9770 0.8481 0.0397 0.0458 2.637 15.107 5.886 1966.065 1.707 26.179 1.358 0.64 301927. 0.1381
|
|
148.41 1.0177 0.8385 0.0318 0.0386 2.223 12.739 4.711 1657.916 1.439 20.954 1.289 0.64 303765. 0.1172
|
|
154.35 1.0584 0.8147 0.0238 0.0309 1.782 10.212 3.528 1329.051 1.154 15.693 1.204 0.64 305659. 0.0948
|
|
160.29 1.0991 0.7612 0.0158 0.0228 1.316 7.538 2.343 981.008 0.852 10.421 1.083 0.65 307609. 0.0695
|
|
166.22 1.1398 0.6235 0.0078 0.0143 0.826 4.732 1.162 615.838 0.535 5.167 0.856 0.65 309611. 0.0387
|
|
172.16 1.1805 -0.0150 -0.0001 0.0055 0.316 1.808 -0.010 235.274 0.204 -0.046 -0.020 0.65 311621. 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 0.1276 0.0612 4.576 24.035 22.492 3412.385 2.715 100.046 2.990 0.67 302301. 0.5943
|
|
6.47 0.0407 0.0825 0.1273 0.0628 4.696 24.665 22.450 3501.790 2.787 99.857 2.908 0.67 302632. 0.5774
|
|
12.95 0.0814 0.1602 0.1271 0.0646 4.830 25.368 22.405 3601.532 2.866 99.657 2.822 0.67 303014. 0.5598
|
|
19.42 0.1221 0.2327 0.1268 0.0665 4.977 26.140 22.354 3711.189 2.953 99.432 2.732 0.67 303454. 0.5414
|
|
25.90 0.1628 0.2998 0.1265 0.0687 5.136 26.976 22.293 3829.840 3.048 99.159 2.640 0.67 303953. 0.5225
|
|
32.37 0.2035 0.3615 0.1260 0.0709 5.305 27.863 22.215 3955.830 3.148 98.811 2.547 0.67 304517. 0.5032
|
|
38.85 0.2442 0.4179 0.1254 0.0733 5.480 28.785 22.111 4086.664 3.252 98.349 2.454 0.67 305150. 0.4836
|
|
45.32 0.2849 0.4693 0.1246 0.0757 5.658 29.716 21.971 4218.955 3.357 97.728 2.362 0.67 305854. 0.4640
|
|
51.80 0.3256 0.5160 0.1236 0.0780 5.831 30.629 21.785 4348.516 3.460 96.898 2.272 0.67 306632. 0.4445
|
|
58.27 0.3663 0.5583 0.1222 0.0802 5.995 31.488 21.539 4470.542 3.558 95.806 2.185 0.67 307487. 0.4251
|
|
64.75 0.4070 0.5966 0.1204 0.0821 6.142 32.258 21.223 4579.870 3.645 94.398 2.102 0.67 308420. 0.4058
|
|
71.22 0.4477 0.6313 0.1181 0.0838 6.264 32.901 20.824 4671.162 3.717 92.626 2.022 0.67 309433. 0.3867
|
|
77.70 0.4884 0.6629 0.1153 0.0850 6.355 33.380 20.334 4739.075 3.771 90.444 1.946 0.67 310525. 0.3678
|
|
84.17 0.5291 0.6915 0.1120 0.0857 6.408 33.656 19.742 4778.226 3.802 87.813 1.874 0.68 311696. 0.3490
|
|
90.65 0.5698 0.7175 0.1080 0.0858 6.414 33.690 19.041 4783.122 3.806 84.693 1.806 0.68 312944. 0.3302
|
|
97.12 0.6105 0.7411 0.1034 0.0851 6.368 33.444 18.222 4748.251 3.779 81.052 1.741 0.68 314269. 0.3114
|
|
103.60 0.6512 0.7626 0.0980 0.0837 6.262 32.888 17.285 4669.258 3.716 76.884 1.679 0.68 315668. 0.2926
|
|
110.07 0.6919 0.7820 0.0921 0.0815 6.095 32.011 16.238 4544.676 3.617 72.228 1.621 0.68 317140. 0.2737
|
|
116.55 0.7326 0.7996 0.0856 0.0785 5.868 30.823 15.099 4376.086 3.482 67.161 1.565 0.68 318684. 0.2549
|
|
123.02 0.7733 0.8152 0.0788 0.0747 5.587 29.347 13.886 4166.515 3.316 61.763 1.512 0.69 320297. 0.2361
|
|
129.50 0.8140 0.8288 0.0716 0.0703 5.255 27.604 12.614 3919.006 3.119 56.107 1.460 0.69 321978. 0.2173
|
|
135.97 0.8547 0.8400 0.0641 0.0652 4.876 25.611 11.297 3636.067 2.893 50.248 1.409 0.69 323727. 0.1985
|
|
142.44 0.8954 0.8484 0.0564 0.0595 4.452 23.382 9.943 3319.611 2.642 44.227 1.359 0.69 325541. 0.1795
|
|
148.92 0.9361 0.8532 0.0486 0.0533 3.984 20.927 8.560 2971.162 2.364 38.077 1.307 0.70 327419. 0.1602
|
|
155.39 0.9768 0.8529 0.0406 0.0465 3.476 18.257 7.155 2592.075 2.063 31.825 1.252 0.70 329362. 0.1404
|
|
161.87 1.0175 0.8449 0.0325 0.0392 2.928 15.381 5.732 2183.740 1.738 25.498 1.191 0.70 331367. 0.1195
|
|
168.34 1.0582 0.8233 0.0244 0.0313 2.344 12.311 4.299 1747.866 1.391 19.121 1.116 0.70 333433. 0.0969
|
|
174.82 1.0989 0.7728 0.0162 0.0231 1.726 9.063 2.861 1286.745 1.024 12.724 1.008 0.71 335560. 0.0715
|
|
181.29 1.1396 0.6397 0.0081 0.0144 1.078 5.660 1.426 803.570 0.639 6.343 0.805 0.71 337744. 0.0403
|
|
187.77 1.1803 0.0005 0.0000 0.0054 0.404 2.123 0.000 301.405 0.240 0.002 0.001 0.71 339936. 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 0.1278 0.0628 5.973 28.958 26.447 4453.917 3.272 117.638 2.693 0.72 327480. 0.5805
|
|
7.01 0.0407 0.0807 0.1276 0.0644 6.122 29.683 26.402 4565.374 3.354 117.438 2.623 0.72 327838. 0.5649
|
|
14.03 0.0814 0.1567 0.1274 0.0661 6.290 30.495 26.357 4690.238 3.445 117.235 2.549 0.72 328252. 0.5484
|
|
21.04 0.1221 0.2280 0.1272 0.0681 6.475 31.391 26.307 4828.131 3.547 117.015 2.471 0.72 328727. 0.5313
|
|
28.05 0.1628 0.2941 0.1269 0.0702 6.676 32.366 26.249 4978.017 3.657 116.754 2.392 0.72 329266. 0.5136
|
|
35.07 0.2035 0.3552 0.1265 0.0725 6.890 33.405 26.174 5137.932 3.774 116.423 2.311 0.72 329875. 0.4955
|
|
42.08 0.2442 0.4113 0.1260 0.0748 7.114 34.490 26.074 5304.747 3.897 115.978 2.229 0.72 330558. 0.4771
|
|
49.09 0.2849 0.4625 0.1254 0.0772 7.341 35.591 25.937 5474.068 4.021 115.366 2.149 0.72 331318. 0.4587
|
|
56.11 0.3255 0.5093 0.1244 0.0795 7.564 36.672 25.747 5640.301 4.143 114.524 2.070 0.73 332159. 0.4403
|
|
63.12 0.3662 0.5519 0.1232 0.0818 7.774 37.690 25.491 5796.983 4.258 113.384 1.994 0.73 333083. 0.4220
|
|
70.13 0.4069 0.5908 0.1216 0.0837 7.962 38.602 25.152 5937.213 4.361 111.874 1.921 0.73 334092. 0.4039
|
|
77.15 0.4476 0.6262 0.1195 0.0854 8.119 39.362 24.715 6054.032 4.447 109.930 1.852 0.73 335188. 0.3858
|
|
84.16 0.4883 0.6586 0.1168 0.0866 8.235 39.925 24.166 6140.647 4.511 107.491 1.785 0.73 336371. 0.3678
|
|
91.17 0.5290 0.6881 0.1136 0.0873 8.301 40.248 23.495 6190.386 4.547 104.505 1.721 0.73 337639. 0.3497
|
|
98.19 0.5697 0.7149 0.1097 0.0874 8.310 40.288 22.689 6196.460 4.552 100.922 1.661 0.73 338993. 0.3316
|
|
105.20 0.6104 0.7392 0.1051 0.0868 8.250 39.998 21.740 6151.881 4.519 96.701 1.603 0.74 340429. 0.3132
|
|
112.21 0.6511 0.7613 0.0998 0.0853 8.114 39.341 20.646 6050.844 4.445 91.831 1.548 0.74 341947. 0.2947
|
|
119.23 0.6918 0.7813 0.0938 0.0831 7.900 38.302 19.415 5891.027 4.327 86.357 1.495 0.74 343544. 0.2761
|
|
126.24 0.7325 0.7994 0.0873 0.0800 7.609 36.891 18.069 5674.022 4.168 80.369 1.444 0.74 345218. 0.2573
|
|
133.25 0.7732 0.8155 0.0804 0.0762 7.246 35.132 16.630 5403.414 3.969 73.968 1.396 0.74 346968. 0.2386
|
|
140.27 0.8139 0.8295 0.0731 0.0717 6.816 33.048 15.118 5082.986 3.734 67.243 1.349 0.75 348792. 0.2198
|
|
147.28 0.8546 0.8413 0.0655 0.0665 6.324 30.662 13.548 4715.968 3.464 60.263 1.303 0.75 350688. 0.2010
|
|
154.29 0.8952 0.8505 0.0577 0.0607 5.773 27.990 11.933 4304.960 3.162 53.079 1.257 0.75 352655. 0.1820
|
|
161.31 0.9359 0.8561 0.0497 0.0543 5.166 25.045 10.281 3852.096 2.830 45.731 1.211 0.75 354692. 0.1627
|
|
168.32 0.9766 0.8568 0.0416 0.0474 4.505 21.842 8.600 3359.408 2.468 38.252 1.161 0.76 356797. 0.1427
|
|
175.33 1.0173 0.8497 0.0333 0.0399 3.794 18.395 6.896 2829.226 2.078 30.672 1.105 0.76 358970. 0.1217
|
|
182.35 1.0580 0.8286 0.0250 0.0319 3.037 14.724 5.175 2264.588 1.663 23.020 1.037 0.76 361209. 0.0988
|
|
189.36 1.0987 0.7773 0.0167 0.0235 2.239 10.856 3.447 1669.644 1.226 15.331 0.936 0.76 363513. 0.0729
|
|
196.37 1.1394 0.6391 0.0083 0.0148 1.408 6.827 1.718 1049.994 0.771 7.644 0.742 0.77 365880. 0.0408
|
|
203.39 1.1801 -0.0033 0.0000 0.0058 0.552 2.675 -0.003 411.403 0.302 -0.015 -0.004 0.77 368251. 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 0.1280 0.0662 7.861 35.391 30.717 5862.110 3.999 136.630 2.377 0.78 352657. 0.5521
|
|
7.55 0.0407 0.0768 0.1278 0.0677 8.043 36.211 30.669 5997.843 4.091 136.414 2.319 0.78 353042. 0.5383
|
|
15.10 0.0814 0.1495 0.1276 0.0695 8.248 37.134 30.621 6150.690 4.195 136.204 2.258 0.78 353487. 0.5237
|
|
22.65 0.1220 0.2179 0.1274 0.0714 8.476 38.158 30.573 6320.376 4.311 135.988 2.194 0.78 353996. 0.5084
|
|
30.20 0.1627 0.2817 0.1272 0.0735 8.724 39.278 30.518 6505.829 4.438 135.746 2.128 0.78 354576. 0.4926
|
|
37.75 0.2034 0.3409 0.1269 0.0757 8.991 40.479 30.451 6704.764 4.573 135.445 2.060 0.78 355229. 0.4764
|
|
45.30 0.2441 0.3956 0.1265 0.0781 9.271 41.738 30.360 6913.304 4.716 135.041 1.992 0.78 355961. 0.4600
|
|
52.85 0.2848 0.4459 0.1260 0.0805 9.556 43.020 30.233 7125.717 4.860 134.476 1.924 0.78 356776. 0.4435
|
|
60.40 0.3254 0.4921 0.1252 0.0828 9.836 44.280 30.053 7334.337 5.003 133.674 1.859 0.78 357677. 0.4270
|
|
67.95 0.3661 0.5347 0.1242 0.0850 10.098 45.461 29.799 7529.978 5.136 132.547 1.795 0.78 358668. 0.4107
|
|
75.50 0.4068 0.5740 0.1227 0.0870 10.330 46.504 29.453 7702.812 5.254 131.006 1.734 0.78 359752. 0.3945
|
|
83.05 0.4475 0.6105 0.1208 0.0886 10.518 47.352 28.992 7843.283 5.350 128.958 1.677 0.79 360929. 0.3784
|
|
90.60 0.4881 0.6442 0.1184 0.0897 10.651 47.953 28.400 7942.720 5.418 126.324 1.622 0.79 362201. 0.3622
|
|
98.15 0.5288 0.6754 0.1153 0.0903 10.719 48.258 27.660 7993.264 5.452 123.030 1.570 0.79 363567. 0.3460
|
|
105.70 0.5695 0.7041 0.1115 0.0902 10.711 48.222 26.757 7987.391 5.448 119.015 1.519 0.79 365025. 0.3294
|
|
113.25 0.6102 0.7304 0.1070 0.0894 10.617 47.800 25.680 7917.363 5.400 114.226 1.471 0.79 366573. 0.3125
|
|
120.80 0.6509 0.7545 0.1018 0.0878 10.428 46.949 24.425 7776.453 5.304 108.641 1.425 0.79 368209. 0.2951
|
|
128.35 0.6915 0.7763 0.0959 0.0854 10.141 45.654 23.001 7562.032 5.158 102.308 1.380 0.80 369931. 0.2773
|
|
135.90 0.7322 0.7960 0.0893 0.0822 9.758 43.930 21.433 7276.375 4.963 95.332 1.336 0.80 371737. 0.2592
|
|
143.45 0.7729 0.8135 0.0823 0.0782 9.286 41.804 19.748 6924.250 4.723 87.837 1.294 0.80 373624. 0.2409
|
|
151.00 0.8136 0.8288 0.0749 0.0735 8.731 39.305 17.971 6510.421 4.441 79.933 1.252 0.80 375590. 0.2224
|
|
158.56 0.8543 0.8416 0.0672 0.0682 8.099 36.460 16.121 6039.148 4.119 71.705 1.211 0.81 377634. 0.2037
|
|
166.11 0.8949 0.8514 0.0592 0.0623 7.394 33.286 14.213 5513.399 3.761 63.218 1.169 0.81 379754. 0.1847
|
|
173.66 0.9356 0.8575 0.0511 0.0557 6.619 29.800 12.257 4935.938 3.367 54.521 1.126 0.81 381949. 0.1653
|
|
181.21 0.9763 0.8580 0.0428 0.0487 5.780 26.020 10.263 4309.861 2.940 45.651 1.080 0.81 384217. 0.1450
|
|
188.76 1.0170 0.8495 0.0343 0.0411 4.881 21.975 8.238 3639.845 2.483 36.643 1.027 0.82 386558. 0.1235
|
|
196.31 1.0577 0.8241 0.0258 0.0331 3.932 17.701 6.190 2931.934 2.000 27.532 0.958 0.82 388970. 0.0998
|
|
203.86 1.0983 0.7623 0.0172 0.0248 2.942 13.246 4.126 2193.943 1.496 18.353 0.853 0.82 391451. 0.0726
|
|
211.41 1.1390 0.6026 0.0086 0.0162 1.926 8.669 2.058 1435.853 0.979 9.155 0.650 0.83 393999. 0.0391
|
|
218.96 1.1797 -0.0032 0.0000 0.0075 0.896 4.033 -0.005 668.089 0.456 -0.022 -0.003 0.83 396564. 0.0000
|
|
|
|
|
|
|