538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
15x13.5-3 (15x135-3.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 0.1539 0.0879 0.005 0.339 0.248 4.007 0.038 1.104 28.109 0.06 23168. 0.5479
|
|
0.53 0.0375 0.0639 0.1531 0.0898 0.005 0.346 0.247 4.090 0.039 1.099 27.395 0.06 23195. 0.5326
|
|
1.06 0.0749 0.1243 0.1522 0.0917 0.006 0.353 0.246 4.178 0.040 1.092 26.660 0.06 23226. 0.5168
|
|
1.60 0.1124 0.1813 0.1511 0.0937 0.006 0.361 0.244 4.268 0.041 1.085 25.911 0.06 23260. 0.5005
|
|
2.13 0.1498 0.2347 0.1498 0.0957 0.006 0.368 0.242 4.359 0.042 1.075 25.154 0.06 23298. 0.4838
|
|
2.66 0.1873 0.2845 0.1483 0.0976 0.006 0.376 0.239 4.449 0.042 1.064 24.394 0.06 23341. 0.4668
|
|
3.19 0.2247 0.3307 0.1465 0.0995 0.006 0.383 0.236 4.536 0.043 1.051 23.636 0.06 23387. 0.4495
|
|
3.72 0.2622 0.3736 0.1443 0.1013 0.006 0.390 0.233 4.616 0.044 1.036 22.884 0.06 23439. 0.4320
|
|
4.26 0.2996 0.4131 0.1418 0.1028 0.006 0.396 0.229 4.686 0.045 1.017 22.141 0.06 23494. 0.4142
|
|
4.79 0.3371 0.4494 0.1388 0.1041 0.006 0.401 0.224 4.742 0.045 0.996 21.411 0.06 23555. 0.3963
|
|
5.32 0.3745 0.4826 0.1352 0.1049 0.006 0.404 0.218 4.781 0.046 0.970 20.695 0.06 23620. 0.3781
|
|
5.85 0.4120 0.5129 0.1311 0.1053 0.006 0.405 0.211 4.796 0.046 0.940 19.995 0.06 23690. 0.3597
|
|
6.38 0.4494 0.5404 0.1263 0.1050 0.006 0.405 0.204 4.786 0.046 0.906 19.310 0.06 23765. 0.3410
|
|
6.92 0.4869 0.5651 0.1209 0.1042 0.006 0.401 0.195 4.747 0.045 0.868 18.639 0.06 23844. 0.3220
|
|
7.45 0.5243 0.5870 0.1150 0.1027 0.006 0.396 0.186 4.680 0.045 0.825 17.979 0.06 23929. 0.3029
|
|
7.98 0.5618 0.6061 0.1086 0.1006 0.006 0.388 0.175 4.586 0.044 0.779 17.325 0.06 24018. 0.2836
|
|
8.51 0.5992 0.6220 0.1017 0.0980 0.006 0.377 0.164 4.465 0.043 0.730 16.669 0.06 24112. 0.2641
|
|
9.04 0.6367 0.6346 0.0945 0.0948 0.006 0.365 0.152 4.320 0.041 0.678 16.006 0.06 24210. 0.2445
|
|
9.58 0.6741 0.6434 0.0870 0.0911 0.006 0.351 0.140 4.152 0.040 0.624 15.327 0.06 24313. 0.2246
|
|
10.11 0.7116 0.6479 0.0792 0.0869 0.005 0.335 0.128 3.961 0.038 0.568 14.622 0.06 24420. 0.2044
|
|
10.64 0.7490 0.6473 0.0711 0.0823 0.005 0.317 0.115 3.749 0.036 0.510 13.878 0.06 24532. 0.1839
|
|
11.17 0.7865 0.6406 0.0628 0.0771 0.005 0.297 0.101 3.515 0.034 0.451 13.080 0.06 24648. 0.1629
|
|
11.70 0.8239 0.6262 0.0544 0.0716 0.004 0.276 0.088 3.261 0.031 0.390 12.204 0.06 24768. 0.1414
|
|
12.24 0.8614 0.6017 0.0458 0.0656 0.004 0.252 0.074 2.987 0.029 0.329 11.218 0.06 24893. 0.1193
|
|
12.77 0.8988 0.5637 0.0371 0.0591 0.004 0.228 0.060 2.694 0.026 0.266 10.071 0.06 25022. 0.0963
|
|
13.30 0.9363 0.5062 0.0283 0.0523 0.003 0.201 0.046 2.382 0.023 0.203 8.683 0.06 25155. 0.0725
|
|
13.83 0.9737 0.4194 0.0194 0.0450 0.003 0.173 0.031 2.052 0.020 0.139 6.917 0.06 25292. 0.0479
|
|
14.36 1.0112 0.2843 0.0105 0.0375 0.002 0.144 0.017 1.707 0.016 0.076 4.515 0.06 25433. 0.0230
|
|
14.90 1.0486 0.0605 0.0017 0.0296 0.002 0.114 0.003 1.348 0.013 0.012 0.927 0.06 25578. 0.0019
|
|
15.43 1.0861
|
|
|
|
|
|
|
|
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 0.1547 0.0795 0.039 1.225 0.998 28.982 0.138 4.439 15.620 0.12 46336. 0.6104
|
|
1.04 0.0367 0.0695 0.1539 0.0814 0.040 1.253 0.993 29.657 0.142 4.419 15.193 0.12 46389. 0.5924
|
|
2.09 0.0734 0.1349 0.1531 0.0833 0.041 1.283 0.988 30.365 0.145 4.395 14.758 0.12 46449. 0.5738
|
|
3.13 0.1101 0.1963 0.1521 0.0853 0.042 1.314 0.982 31.098 0.148 4.366 14.316 0.12 46516. 0.5548
|
|
4.17 0.1468 0.2537 0.1509 0.0874 0.043 1.346 0.974 31.843 0.152 4.332 13.872 0.12 46590. 0.5355
|
|
5.21 0.1835 0.3069 0.1495 0.0894 0.044 1.377 0.965 32.585 0.156 4.291 13.428 0.12 46672. 0.5159
|
|
6.26 0.2202 0.3563 0.1478 0.0914 0.045 1.408 0.954 33.306 0.159 4.242 12.989 0.12 46763. 0.4962
|
|
7.30 0.2569 0.4018 0.1458 0.0932 0.046 1.436 0.941 33.984 0.162 4.184 12.555 0.12 46862. 0.4764
|
|
8.34 0.2936 0.4436 0.1434 0.0949 0.046 1.462 0.925 34.595 0.165 4.115 12.131 0.12 46970. 0.4564
|
|
9.38 0.3303 0.4820 0.1405 0.0963 0.047 1.484 0.907 35.110 0.168 4.034 11.716 0.12 47086. 0.4365
|
|
10.43 0.3671 0.5172 0.1372 0.0974 0.048 1.500 0.885 35.497 0.169 3.938 11.313 0.12 47212. 0.4164
|
|
11.47 0.4038 0.5493 0.1333 0.0980 0.048 1.510 0.860 35.719 0.171 3.826 10.923 0.12 47348. 0.3963
|
|
12.51 0.4405 0.5785 0.1288 0.0981 0.048 1.511 0.831 35.747 0.171 3.697 10.546 0.12 47492. 0.3761
|
|
13.56 0.4772 0.6051 0.1237 0.0975 0.048 1.503 0.798 35.559 0.170 3.550 10.181 0.12 47646. 0.3558
|
|
14.60 0.5139 0.6290 0.1180 0.0964 0.047 1.485 0.762 35.150 0.168 3.388 9.828 0.12 47809. 0.3355
|
|
15.64 0.5506 0.6504 0.1119 0.0947 0.046 1.459 0.722 34.525 0.165 3.211 9.485 0.12 47982. 0.3152
|
|
16.68 0.5873 0.6691 0.1053 0.0924 0.045 1.424 0.679 33.690 0.161 3.022 9.148 0.12 48163. 0.2950
|
|
17.73 0.6240 0.6850 0.0983 0.0896 0.044 1.380 0.635 32.656 0.156 2.823 8.814 0.12 48352. 0.2747
|
|
18.77 0.6607 0.6979 0.0911 0.0862 0.042 1.328 0.588 31.431 0.150 2.614 8.481 0.12 48551. 0.2543
|
|
19.81 0.6974 0.7074 0.0835 0.0823 0.040 1.269 0.539 30.020 0.143 2.397 8.144 0.12 48758. 0.2339
|
|
20.86 0.7341 0.7130 0.0757 0.0780 0.038 1.201 0.489 28.430 0.136 2.174 7.798 0.12 48974. 0.2133
|
|
21.90 0.7708 0.7140 0.0678 0.0731 0.036 1.127 0.437 26.663 0.127 1.945 7.437 0.12 49198. 0.1924
|
|
22.94 0.8075 0.7094 0.0596 0.0678 0.033 1.045 0.384 24.726 0.118 1.710 7.053 0.12 49430. 0.1711
|
|
23.98 0.8442 0.6974 0.0513 0.0621 0.030 0.956 0.331 22.621 0.108 1.471 6.633 0.12 49671. 0.1492
|
|
25.03 0.8809 0.6757 0.0428 0.0558 0.027 0.860 0.276 20.353 0.097 1.229 6.158 0.12 49919. 0.1266
|
|
26.07 0.9176 0.6398 0.0343 0.0492 0.024 0.758 0.221 17.928 0.086 0.984 5.598 0.12 50176. 0.1030
|
|
27.11 0.9543 0.5823 0.0257 0.0421 0.021 0.649 0.166 15.354 0.073 0.738 4.899 0.12 50441. 0.0780
|
|
28.15 0.9910 0.4884 0.0171 0.0347 0.017 0.534 0.110 12.643 0.060 0.491 3.957 0.12 50714. 0.0514
|
|
29.20 1.0278 0.3251 0.0085 0.0269 0.013 0.414 0.055 9.806 0.047 0.244 2.540 0.13 50994. 0.0233
|
|
30.24 1.0645 -0.0012 0.0000 0.0188 0.009 0.290 0.000 6.851 0.033 -0.001 -0.009 0.13 51278. 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 0.1551 0.0761 0.126 2.637 2.252 93.611 0.298 10.016 10.910 0.18 69503. 0.6404
|
|
1.57 0.0368 0.0729 0.1544 0.0780 0.129 2.703 2.242 95.928 0.305 9.971 10.599 0.18 69583. 0.6208
|
|
3.14 0.0737 0.1415 0.1536 0.0800 0.132 2.771 2.230 98.367 0.313 9.918 10.282 0.18 69673. 0.6006
|
|
4.71 0.1105 0.2056 0.1526 0.0820 0.135 2.843 2.216 100.895 0.321 9.856 9.961 0.18 69774. 0.5800
|
|
6.28 0.1473 0.2653 0.1514 0.0841 0.139 2.915 2.199 103.472 0.329 9.781 9.639 0.18 69886. 0.5591
|
|
7.85 0.1842 0.3206 0.1501 0.0862 0.142 2.988 2.179 106.045 0.338 9.691 9.319 0.18 70010. 0.5381
|
|
9.42 0.2210 0.3716 0.1484 0.0882 0.146 3.058 2.155 108.551 0.346 9.583 9.002 0.18 70146. 0.5169
|
|
10.99 0.2578 0.4186 0.1464 0.0902 0.149 3.125 2.125 110.918 0.353 9.454 8.692 0.18 70295. 0.4957
|
|
12.56 0.2946 0.4617 0.1440 0.0919 0.152 3.185 2.091 113.061 0.360 9.300 8.388 0.18 70458. 0.4745
|
|
14.13 0.3315 0.5012 0.1412 0.0934 0.154 3.237 2.050 114.881 0.366 9.117 8.093 0.18 70634. 0.4532
|
|
15.69 0.3683 0.5372 0.1378 0.0945 0.156 3.276 2.001 116.266 0.370 8.902 7.807 0.18 70824. 0.4320
|
|
17.26 0.4051 0.5701 0.1339 0.0952 0.157 3.299 1.944 117.094 0.373 8.649 7.532 0.18 71028. 0.4108
|
|
18.83 0.4420 0.6000 0.1294 0.0953 0.157 3.304 1.879 117.254 0.373 8.356 7.267 0.18 71247. 0.3897
|
|
20.40 0.4788 0.6273 0.1243 0.0948 0.156 3.287 1.804 116.678 0.371 8.025 7.013 0.18 71479. 0.3685
|
|
21.97 0.5156 0.6520 0.1186 0.0938 0.155 3.250 1.721 115.345 0.367 7.657 6.769 0.18 71725. 0.3474
|
|
23.54 0.5525 0.6742 0.1124 0.0921 0.152 3.191 1.631 113.267 0.361 7.256 6.533 0.18 71985. 0.3264
|
|
25.11 0.5893 0.6939 0.1057 0.0898 0.148 3.112 1.535 110.468 0.352 6.828 6.303 0.18 72258. 0.3055
|
|
26.68 0.6261 0.7109 0.0987 0.0870 0.143 3.014 1.433 106.979 0.341 6.376 6.078 0.18 72545. 0.2846
|
|
28.25 0.6629 0.7251 0.0914 0.0836 0.138 2.897 1.327 102.823 0.327 5.903 5.855 0.18 72844. 0.2638
|
|
29.82 0.6998 0.7362 0.0838 0.0797 0.131 2.762 1.217 98.023 0.312 5.413 5.631 0.18 73157. 0.2430
|
|
31.39 0.7366 0.7437 0.0760 0.0753 0.124 2.609 1.103 92.595 0.295 4.907 5.404 0.18 73482. 0.2221
|
|
32.96 0.7734 0.7471 0.0679 0.0703 0.116 2.439 0.987 86.554 0.276 4.389 5.170 0.18 73820. 0.2009
|
|
34.53 0.8103 0.7453 0.0597 0.0650 0.107 2.251 0.867 79.911 0.254 3.858 4.923 0.18 74171. 0.1794
|
|
36.10 0.8471 0.7368 0.0514 0.0591 0.097 2.048 0.746 72.682 0.231 3.319 4.656 0.18 74534. 0.1573
|
|
37.67 0.8839 0.7192 0.0429 0.0527 0.087 1.828 0.623 64.883 0.207 2.771 4.355 0.19 74910. 0.1345
|
|
39.24 0.9208 0.6883 0.0343 0.0460 0.076 1.593 0.499 56.535 0.180 2.218 4.001 0.19 75298. 0.1105
|
|
40.81 0.9576 0.6361 0.0257 0.0387 0.064 1.343 0.374 47.666 0.152 1.662 3.556 0.19 75698. 0.0850
|
|
42.38 0.9944 0.5465 0.0171 0.0311 0.051 1.080 0.248 38.316 0.122 1.105 2.942 0.19 76109. 0.0574
|
|
43.95 1.0313 0.3791 0.0085 0.0232 0.038 0.804 0.124 28.528 0.091 0.551 1.968 0.19 76532. 0.0271
|
|
45.51 1.0681 -0.0011 0.0000 0.0149 0.025 0.516 0.000 18.321 0.058 -0.001 -0.006 0.19 76957. 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 0.1554 0.0742 0.290 4.575 4.012 216.513 0.517 17.846 8.405 0.24 92669. 0.6586
|
|
2.10 0.0369 0.0750 0.1548 0.0761 0.298 4.693 3.995 222.072 0.530 17.770 8.160 0.24 92776. 0.6380
|
|
4.19 0.0738 0.1454 0.1540 0.0782 0.306 4.816 3.975 227.936 0.544 17.680 7.909 0.24 92896. 0.6168
|
|
6.29 0.1107 0.2111 0.1530 0.0802 0.314 4.945 3.951 234.026 0.559 17.572 7.657 0.24 93031. 0.5953
|
|
8.39 0.1476 0.2722 0.1519 0.0824 0.322 5.076 3.922 240.243 0.574 17.443 7.404 0.24 93181. 0.5735
|
|
10.48 0.1845 0.3287 0.1506 0.0845 0.331 5.208 3.887 246.465 0.588 17.287 7.152 0.24 93346. 0.5516
|
|
12.58 0.2214 0.3808 0.1489 0.0866 0.339 5.336 3.844 252.541 0.603 17.099 6.904 0.24 93528. 0.5295
|
|
14.68 0.2583 0.4286 0.1470 0.0886 0.346 5.458 3.793 258.295 0.617 16.873 6.661 0.24 93728. 0.5075
|
|
16.77 0.2952 0.4724 0.1446 0.0904 0.353 5.568 3.732 263.523 0.629 16.602 6.424 0.24 93945. 0.4855
|
|
18.87 0.3321 0.5124 0.1418 0.0919 0.359 5.663 3.660 267.987 0.640 16.279 6.194 0.24 94181. 0.4636
|
|
20.97 0.3690 0.5490 0.1385 0.0931 0.364 5.735 3.574 271.415 0.648 15.897 5.973 0.24 94435. 0.4417
|
|
23.06 0.4059 0.5823 0.1345 0.0938 0.367 5.779 3.473 273.512 0.653 15.448 5.759 0.24 94709. 0.4199
|
|
25.16 0.4428 0.6127 0.1300 0.0940 0.367 5.790 3.356 274.012 0.654 14.928 5.555 0.24 95001. 0.3981
|
|
27.26 0.4797 0.6404 0.1249 0.0935 0.366 5.763 3.223 272.746 0.651 14.336 5.360 0.24 95311. 0.3764
|
|
29.35 0.5166 0.6656 0.1191 0.0925 0.362 5.698 3.075 269.659 0.644 13.679 5.173 0.24 95641. 0.3549
|
|
31.45 0.5535 0.6884 0.1129 0.0908 0.355 5.595 2.915 264.777 0.632 12.964 4.993 0.24 95989. 0.3334
|
|
33.55 0.5904 0.7086 0.1062 0.0885 0.346 5.455 2.743 258.158 0.616 12.199 4.819 0.24 96354. 0.3122
|
|
35.64 0.6273 0.7264 0.0992 0.0857 0.335 5.280 2.561 249.868 0.597 11.391 4.649 0.24 96738. 0.2910
|
|
37.74 0.6642 0.7415 0.0919 0.0823 0.322 5.071 2.371 239.968 0.573 10.547 4.482 0.24 97139. 0.2699
|
|
39.84 0.7011 0.7536 0.0842 0.0784 0.306 4.828 2.174 228.506 0.546 9.670 4.315 0.24 97557. 0.2489
|
|
41.93 0.7380 0.7625 0.0763 0.0739 0.289 4.554 1.971 215.520 0.515 8.766 4.148 0.24 97993. 0.2278
|
|
44.03 0.7749 0.7674 0.0683 0.0689 0.270 4.248 1.762 201.045 0.480 7.839 3.976 0.25 98445. 0.2065
|
|
46.12 0.8118 0.7676 0.0600 0.0635 0.248 3.912 1.549 185.112 0.442 6.891 3.796 0.25 98914. 0.1848
|
|
48.22 0.8487 0.7617 0.0516 0.0575 0.225 3.545 1.333 167.753 0.400 5.927 3.603 0.25 99400. 0.1627
|
|
50.32 0.8856 0.7472 0.0431 0.0511 0.200 3.149 1.113 149.009 0.356 4.950 3.387 0.25 99903. 0.1398
|
|
52.41 0.9225 0.7201 0.0345 0.0442 0.173 2.724 0.891 128.931 0.308 3.962 3.134 0.25 100422. 0.1157
|
|
54.51 0.9594 0.6725 0.0259 0.0369 0.144 2.273 0.668 107.592 0.257 2.969 2.814 0.25 100957. 0.0899
|
|
56.61 0.9963 0.5876 0.0172 0.0292 0.114 1.798 0.444 85.081 0.203 1.975 2.368 0.25 101508. 0.0617
|
|
58.70 1.0332 0.4206 0.0086 0.0211 0.082 1.300 0.222 61.513 0.147 0.986 1.634 0.25 102073. 0.0301
|
|
60.80 1.0701 0.0010 0.0000 0.0127 0.049 0.780 0.000 36.904 0.088 0.001 0.004 0.25 102639. 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 0.1558 0.0731 0.559 7.043 6.283 416.623 0.796 27.947 6.840 0.30 115834. 0.6707
|
|
2.63 0.0370 0.0764 0.1551 0.0751 0.573 7.228 6.258 427.603 0.817 27.834 6.638 0.30 115968. 0.6495
|
|
5.25 0.0740 0.1481 0.1544 0.0771 0.589 7.425 6.227 439.206 0.839 27.699 6.431 0.30 116118. 0.6278
|
|
7.88 0.1109 0.2149 0.1535 0.0792 0.605 7.629 6.191 451.280 0.862 27.538 6.223 0.30 116287. 0.6057
|
|
10.50 0.1479 0.2769 0.1524 0.0814 0.622 7.837 6.147 463.633 0.885 27.343 6.014 0.30 116474. 0.5833
|
|
13.13 0.1849 0.3342 0.1511 0.0836 0.638 8.047 6.094 476.020 0.909 27.106 5.807 0.30 116682. 0.5607
|
|
15.76 0.2219 0.3870 0.1495 0.0857 0.655 8.252 6.029 488.145 0.932 26.818 5.602 0.30 116910. 0.5381
|
|
18.38 0.2588 0.4354 0.1475 0.0877 0.670 8.446 5.951 499.654 0.954 26.471 5.402 0.30 117160. 0.5155
|
|
21.01 0.2958 0.4796 0.1452 0.0896 0.684 8.624 5.857 510.140 0.974 26.053 5.208 0.30 117433. 0.4930
|
|
23.64 0.3328 0.5201 0.1424 0.0911 0.696 8.776 5.745 519.130 0.991 25.553 5.019 0.30 117729. 0.4706
|
|
26.26 0.3698 0.5570 0.1391 0.0924 0.705 8.893 5.611 526.079 1.005 24.959 4.838 0.30 118048. 0.4483
|
|
28.89 0.4067 0.5906 0.1352 0.0931 0.711 8.966 5.454 530.398 1.013 24.258 4.664 0.30 118390. 0.4261
|
|
31.51 0.4437 0.6213 0.1307 0.0933 0.713 8.986 5.271 531.556 1.015 23.444 4.497 0.30 118757. 0.4039
|
|
34.14 0.4807 0.6494 0.1255 0.0929 0.710 8.946 5.062 529.211 1.011 22.517 4.339 0.30 119147. 0.3819
|
|
36.77 0.5177 0.6749 0.1198 0.0919 0.702 8.845 4.831 523.253 0.999 21.486 4.187 0.30 119561. 0.3600
|
|
39.39 0.5546 0.6980 0.1135 0.0902 0.689 8.684 4.578 513.725 0.981 20.363 4.042 0.30 119997. 0.3383
|
|
42.02 0.5916 0.7187 0.1068 0.0879 0.672 8.465 4.308 500.743 0.956 19.160 3.902 0.30 120456. 0.3168
|
|
44.64 0.6286 0.7370 0.0997 0.0850 0.650 8.189 4.022 484.435 0.925 17.890 3.766 0.30 120938. 0.2954
|
|
47.27 0.6656 0.7527 0.0923 0.0816 0.623 7.859 3.723 464.918 0.888 16.561 3.632 0.30 121441. 0.2742
|
|
49.90 0.7025 0.7657 0.0846 0.0776 0.593 7.477 3.413 442.287 0.845 15.182 3.500 0.30 121966. 0.2530
|
|
52.52 0.7395 0.7754 0.0767 0.0731 0.559 7.043 3.093 416.621 0.796 13.759 3.368 0.31 122512. 0.2317
|
|
55.15 0.7765 0.7816 0.0686 0.0681 0.520 6.559 2.765 387.983 0.741 12.300 3.233 0.31 123080. 0.2103
|
|
57.78 0.8135 0.7832 0.0603 0.0626 0.478 6.025 2.430 356.435 0.681 10.809 3.092 0.31 123669. 0.1886
|
|
60.40 0.8504 0.7791 0.0518 0.0565 0.432 5.444 2.089 322.044 0.615 9.292 2.942 0.31 124279. 0.1663
|
|
63.03 0.8874 0.7668 0.0432 0.0500 0.382 4.816 1.743 284.890 0.544 7.754 2.775 0.31 124910. 0.1433
|
|
65.65 0.9244 0.7425 0.0346 0.0430 0.329 4.143 1.394 245.078 0.468 6.200 2.580 0.31 125561. 0.1191
|
|
68.28 0.9614 0.6983 0.0259 0.0356 0.272 3.427 1.043 202.749 0.387 4.638 2.333 0.31 126232. 0.0932
|
|
70.91 0.9984 0.6166 0.0171 0.0278 0.212 2.672 0.691 158.091 0.302 3.075 1.984 0.31 126923. 0.0645
|
|
73.53 1.0353 0.4486 0.0085 0.0195 0.149 1.882 0.342 111.330 0.213 1.519 1.392 0.31 127632. 0.0318
|
|
76.16 1.0723 -0.0165 -0.0002 0.0110 0.084 1.055 -0.007 62.421 0.119 -0.030 -0.050 0.31 128335. 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 0.1561 0.0725 0.957 10.050 9.069 713.437 1.135 40.339 5.766 0.36 138997. 0.6792
|
|
3.15 0.0370 0.0773 0.1556 0.0744 0.982 10.320 9.034 732.577 1.166 40.185 5.594 0.36 139158. 0.6577
|
|
6.30 0.0740 0.1497 0.1548 0.0765 1.010 10.605 8.993 752.848 1.198 40.003 5.418 0.36 139338. 0.6356
|
|
9.46 0.1109 0.2173 0.1540 0.0786 1.038 10.903 8.944 773.989 1.232 39.782 5.241 0.36 139540. 0.6132
|
|
12.61 0.1479 0.2799 0.1530 0.0808 1.067 11.209 8.883 795.668 1.266 39.514 5.064 0.36 139765. 0.5904
|
|
15.76 0.1849 0.3377 0.1517 0.0831 1.096 11.516 8.810 817.462 1.301 39.186 4.888 0.36 140014. 0.5675
|
|
18.91 0.2219 0.3909 0.1501 0.0852 1.125 11.817 8.720 838.848 1.335 38.785 4.715 0.36 140288. 0.5446
|
|
22.06 0.2589 0.4396 0.1482 0.0873 1.152 12.104 8.610 859.211 1.367 38.298 4.545 0.36 140588. 0.5217
|
|
25.21 0.2959 0.4842 0.1460 0.0892 1.177 12.366 8.478 877.830 1.397 37.708 4.380 0.36 140915. 0.4989
|
|
28.37 0.3328 0.5249 0.1432 0.0908 1.199 12.592 8.318 893.872 1.423 37.000 4.221 0.36 141270. 0.4762
|
|
31.52 0.3698 0.5620 0.1400 0.0921 1.215 12.768 8.128 906.383 1.443 36.155 4.068 0.36 141653. 0.4536
|
|
34.67 0.4068 0.5959 0.1361 0.0929 1.226 12.880 7.903 914.322 1.455 35.154 3.921 0.36 142065. 0.4312
|
|
37.82 0.4438 0.6268 0.1316 0.0931 1.229 12.914 7.641 916.748 1.459 33.987 3.780 0.36 142505. 0.4088
|
|
40.97 0.4808 0.6551 0.1264 0.0928 1.224 12.862 7.342 913.046 1.453 32.655 3.647 0.36 142973. 0.3866
|
|
44.13 0.5177 0.6809 0.1207 0.0917 1.211 12.721 7.008 903.004 1.437 31.170 3.520 0.36 143470. 0.3645
|
|
47.28 0.5547 0.7044 0.1144 0.0901 1.189 12.491 6.643 886.692 1.411 29.550 3.398 0.36 143994. 0.3426
|
|
50.43 0.5917 0.7255 0.1077 0.0878 1.159 12.176 6.253 864.307 1.376 27.813 3.281 0.36 144546. 0.3210
|
|
53.58 0.6287 0.7442 0.1006 0.0849 1.121 11.778 5.840 836.073 1.331 25.976 3.168 0.36 145124. 0.2995
|
|
56.73 0.6657 0.7605 0.0931 0.0815 1.076 11.301 5.408 802.195 1.277 24.054 3.058 0.36 145728. 0.2781
|
|
59.89 0.7027 0.7741 0.0854 0.0775 1.023 10.746 4.959 762.843 1.214 22.058 2.949 0.37 146359. 0.2568
|
|
63.04 0.7396 0.7847 0.0774 0.0730 0.963 10.117 4.496 718.153 1.143 19.999 2.840 0.37 147015. 0.2355
|
|
66.19 0.7766 0.7919 0.0692 0.0679 0.896 9.414 4.021 668.239 1.064 17.885 2.729 0.37 147697. 0.2141
|
|
69.34 0.8136 0.7949 0.0609 0.0623 0.822 8.638 3.535 613.209 0.976 15.725 2.615 0.37 148404. 0.1923
|
|
72.49 0.8506 0.7925 0.0524 0.0562 0.742 7.793 3.041 553.178 0.880 13.527 2.494 0.37 149137. 0.1701
|
|
75.64 0.8876 0.7824 0.0437 0.0496 0.655 6.879 2.540 488.287 0.777 11.298 2.359 0.37 149894. 0.1471
|
|
78.80 0.9245 0.7610 0.0350 0.0425 0.562 5.899 2.034 418.720 0.666 9.046 2.203 0.37 150676. 0.1229
|
|
81.95 0.9615 0.7207 0.0263 0.0350 0.462 4.856 1.525 344.725 0.549 6.782 2.006 0.37 151482. 0.0969
|
|
85.10 0.9985 0.6443 0.0175 0.0271 0.358 3.756 1.015 266.629 0.424 4.516 1.727 0.37 152311. 0.0681
|
|
88.25 1.0355 0.4823 0.0087 0.0188 0.248 2.604 0.508 184.830 0.294 2.260 1.247 0.38 153162. 0.0348
|
|
91.40 1.0725 0.0050 0.0000 0.0101 0.133 1.398 0.003 99.248 0.158 0.012 0.012 0.38 154006. 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 0.1565 0.0721 1.512 13.611 12.375 1127.234 1.538 55.045 4.980 0.42 162158. 0.6852
|
|
3.68 0.0370 0.0780 0.1560 0.0741 1.553 13.982 12.332 1157.932 1.580 54.851 4.830 0.42 162346. 0.6635
|
|
7.36 0.0741 0.1510 0.1553 0.0762 1.597 14.375 12.279 1190.525 1.624 54.619 4.678 0.42 162557. 0.6413
|
|
11.05 0.1111 0.2191 0.1545 0.0784 1.642 14.787 12.216 1224.606 1.671 54.337 4.525 0.42 162792. 0.6186
|
|
14.73 0.1481 0.2822 0.1535 0.0806 1.689 15.210 12.138 1259.649 1.718 53.991 4.371 0.42 163055. 0.5957
|
|
18.41 0.1852 0.3404 0.1523 0.0829 1.737 15.636 12.042 1294.975 1.767 53.565 4.218 0.42 163345. 0.5726
|
|
22.09 0.2222 0.3939 0.1508 0.0851 1.783 16.056 11.924 1329.737 1.814 53.040 4.067 0.42 163665. 0.5494
|
|
25.77 0.2592 0.4430 0.1490 0.0872 1.828 16.457 11.780 1362.932 1.859 52.397 3.920 0.42 164016. 0.5263
|
|
29.46 0.2962 0.4878 0.1468 0.0891 1.869 16.825 11.604 1393.388 1.901 51.614 3.777 0.42 164398. 0.5033
|
|
33.14 0.3333 0.5287 0.1441 0.0908 1.904 17.143 11.391 1419.745 1.937 50.667 3.639 0.42 164813. 0.4804
|
|
36.82 0.3703 0.5660 0.1409 0.0922 1.932 17.393 11.135 1440.444 1.965 49.530 3.506 0.42 165261. 0.4577
|
|
40.50 0.4073 0.6000 0.1370 0.0930 1.950 17.554 10.831 1453.793 1.983 48.177 3.379 0.42 165742. 0.4350
|
|
44.18 0.4444 0.6311 0.1325 0.0933 1.956 17.608 10.475 1458.244 1.989 46.594 3.258 0.42 166257. 0.4125
|
|
47.87 0.4814 0.6596 0.1274 0.0929 1.948 17.542 10.068 1452.784 1.982 44.781 3.143 0.42 166806. 0.3901
|
|
51.55 0.5184 0.6856 0.1216 0.0919 1.927 17.352 9.612 1437.052 1.960 42.754 3.034 0.42 167387. 0.3679
|
|
55.23 0.5555 0.7093 0.1153 0.0903 1.892 17.039 9.114 1411.148 1.925 40.539 2.929 0.42 168001. 0.3459
|
|
58.91 0.5925 0.7307 0.1085 0.0880 1.844 16.607 8.579 1375.392 1.876 38.161 2.829 0.42 168646. 0.3242
|
|
62.59 0.6295 0.7498 0.1014 0.0851 1.784 16.061 8.013 1330.150 1.815 35.643 2.732 0.42 169323. 0.3026
|
|
66.28 0.6665 0.7665 0.0939 0.0816 1.711 15.404 7.421 1275.760 1.740 33.007 2.638 0.43 170030. 0.2811
|
|
69.96 0.7036 0.7807 0.0861 0.0776 1.626 14.640 6.805 1212.497 1.654 30.268 2.546 0.43 170768. 0.2598
|
|
73.64 0.7406 0.7920 0.0780 0.0730 1.530 13.772 6.169 1140.586 1.556 27.442 2.453 0.43 171536. 0.2384
|
|
77.32 0.7776 0.8000 0.0698 0.0678 1.422 12.802 5.517 1060.215 1.446 24.539 2.360 0.43 172334. 0.2169
|
|
81.00 0.8147 0.8040 0.0614 0.0622 1.303 11.731 4.850 971.559 1.325 21.572 2.264 0.43 173161. 0.1951
|
|
84.69 0.8517 0.8028 0.0528 0.0560 1.173 10.563 4.171 874.803 1.193 18.552 2.163 0.43 174018. 0.1728
|
|
88.37 0.8887 0.7944 0.0440 0.0493 1.033 9.300 3.482 770.179 1.051 15.488 2.051 0.43 174903. 0.1497
|
|
92.05 0.9258 0.7751 0.0352 0.0421 0.882 7.945 2.786 657.983 0.898 12.394 1.921 0.43 175818. 0.1254
|
|
95.73 0.9628 0.7374 0.0264 0.0345 0.722 6.504 2.087 538.620 0.735 9.281 1.757 0.44 176760. 0.0993
|
|
99.41 0.9998 0.6641 0.0175 0.0264 0.553 4.982 1.386 412.624 0.563 6.165 1.524 0.44 177731. 0.0702
|
|
103.10 1.0368 0.5031 0.0087 0.0180 0.376 3.389 0.689 280.640 0.383 3.064 1.113 0.44 178726. 0.0361
|
|
106.78 1.0739 -0.0104 -0.0001 0.0091 0.191 1.719 -0.007 142.333 0.194 -0.031 -0.022 0.44 179703. 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 0.1570 0.0720 2.252 17.743 16.208 1679.331 2.005 72.092 4.378 0.48 185318. 0.6894
|
|
4.21 0.0371 0.0784 0.1565 0.0740 2.314 18.231 16.156 1725.584 2.060 71.860 4.247 0.48 185532. 0.6677
|
|
8.42 0.0741 0.1519 0.1559 0.0761 2.380 18.752 16.093 1774.837 2.119 71.582 4.113 0.48 185772. 0.6454
|
|
12.63 0.1112 0.2203 0.1551 0.0783 2.449 19.298 16.017 1826.502 2.180 71.241 3.977 0.48 186042. 0.6227
|
|
16.85 0.1482 0.2837 0.1542 0.0806 2.521 19.861 15.922 1879.798 2.244 70.820 3.842 0.48 186341. 0.5996
|
|
21.06 0.1853 0.3422 0.1531 0.0829 2.593 20.430 15.804 1933.704 2.308 70.296 3.707 0.48 186673. 0.5765
|
|
25.27 0.2224 0.3960 0.1516 0.0852 2.665 20.993 15.657 1986.932 2.372 69.645 3.574 0.48 187039. 0.5532
|
|
29.48 0.2594 0.4452 0.1499 0.0873 2.733 21.531 15.476 2037.943 2.433 68.838 3.444 0.48 187440. 0.5301
|
|
33.69 0.2965 0.4901 0.1477 0.0894 2.796 22.028 15.253 2084.931 2.489 67.847 3.318 0.48 187877. 0.5070
|
|
37.90 0.3336 0.5312 0.1451 0.0911 2.851 22.460 14.982 2125.810 2.537 66.640 3.197 0.48 188352. 0.4840
|
|
42.12 0.3706 0.5686 0.1419 0.0925 2.894 22.802 14.654 2158.178 2.576 65.179 3.080 0.48 188865. 0.4612
|
|
46.33 0.4077 0.6028 0.1381 0.0934 2.923 23.026 14.261 2179.434 2.602 63.433 2.968 0.48 189416. 0.4384
|
|
50.54 0.4447 0.6340 0.1336 0.0937 2.933 23.108 13.799 2187.184 2.611 61.377 2.862 0.48 190006. 0.4158
|
|
54.75 0.4818 0.6626 0.1285 0.0934 2.923 23.031 13.267 2179.835 2.602 59.013 2.761 0.48 190634. 0.3933
|
|
58.96 0.5189 0.6888 0.1227 0.0924 2.892 22.787 12.672 2156.802 2.574 56.363 2.665 0.48 191300. 0.3711
|
|
63.17 0.5559 0.7127 0.1164 0.0908 2.841 22.380 12.019 2118.220 2.528 53.459 2.574 0.48 192003. 0.3490
|
|
67.39 0.5930 0.7344 0.1096 0.0885 2.769 21.813 11.317 2064.577 2.464 50.336 2.486 0.48 192742. 0.3272
|
|
71.60 0.6301 0.7539 0.1024 0.0856 2.677 21.093 10.572 1996.443 2.383 47.026 2.402 0.49 193517. 0.3055
|
|
75.81 0.6671 0.7711 0.0948 0.0821 2.567 20.226 9.792 1914.340 2.285 43.555 2.320 0.49 194328. 0.2840
|
|
80.02 0.7042 0.7857 0.0870 0.0780 2.439 19.215 8.981 1818.708 2.171 39.947 2.240 0.49 195173. 0.2626
|
|
84.23 0.7412 0.7977 0.0789 0.0733 2.293 18.066 8.143 1709.892 2.041 36.221 2.160 0.49 196053. 0.2411
|
|
88.44 0.7783 0.8064 0.0705 0.0681 2.130 16.780 7.283 1588.186 1.896 32.393 2.080 0.49 196967. 0.2196
|
|
92.66 0.8154 0.8114 0.0620 0.0623 1.950 15.360 6.403 1453.856 1.735 28.479 1.997 0.49 197914. 0.1977
|
|
96.87 0.8524 0.8113 0.0533 0.0560 1.753 13.811 5.506 1307.193 1.560 24.492 1.911 0.49 198895. 0.1754
|
|
101.08 0.8895 0.8044 0.0445 0.0492 1.540 12.135 4.597 1148.542 1.371 20.447 1.815 0.49 199909. 0.1523
|
|
105.29 0.9266 0.7870 0.0356 0.0419 1.312 10.337 3.678 978.358 1.168 16.359 1.705 0.50 200956. 0.1279
|
|
109.50 0.9636 0.7519 0.0267 0.0342 1.069 8.423 2.753 797.257 0.952 12.247 1.566 0.50 202036. 0.1017
|
|
113.71 1.0007 0.6819 0.0177 0.0260 0.813 6.403 1.828 606.051 0.723 8.129 1.368 0.50 203146. 0.0723
|
|
117.92 1.0377 0.5235 0.0088 0.0174 0.544 4.287 0.906 405.731 0.484 4.029 1.013 0.50 204286. 0.0377
|
|
122.14 1.0748 -0.0187 -0.0001 0.0084 0.262 2.066 -0.015 195.520 0.233 -0.067 -0.035 0.50 205395. 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 0.1574 0.0720 3.208 22.468 20.573 2392.360 2.538 91.507 3.900 0.54 208475. 0.6920
|
|
4.74 0.0371 0.0787 0.1570 0.0740 3.297 23.092 20.513 2458.803 2.609 91.243 3.784 0.54 208715. 0.6704
|
|
9.48 0.0742 0.1524 0.1564 0.0762 3.393 23.758 20.442 2529.801 2.684 90.927 3.665 0.54 208986. 0.6482
|
|
14.23 0.1113 0.2211 0.1558 0.0784 3.493 24.460 20.354 2604.555 2.764 90.537 3.545 0.54 209288. 0.6256
|
|
18.97 0.1484 0.2847 0.1549 0.0807 3.597 25.187 20.245 2681.979 2.846 90.049 3.424 0.54 209625. 0.6026
|
|
23.71 0.1855 0.3434 0.1539 0.0831 3.702 25.926 20.107 2760.608 2.929 89.435 3.304 0.54 209998. 0.5795
|
|
28.45 0.2225 0.3973 0.1525 0.0854 3.807 26.658 19.933 2838.574 3.012 88.662 3.185 0.54 210409. 0.5563
|
|
33.19 0.2596 0.4466 0.1509 0.0877 3.907 27.363 19.715 2913.618 3.091 87.694 3.069 0.54 210860. 0.5331
|
|
37.93 0.2967 0.4917 0.1488 0.0898 4.000 28.015 19.445 2983.082 3.165 86.490 2.957 0.54 211353. 0.5100
|
|
42.68 0.3338 0.5328 0.1462 0.0916 4.082 28.586 19.112 3043.878 3.230 85.009 2.848 0.54 211887. 0.4870
|
|
47.42 0.3709 0.5703 0.1431 0.0931 4.147 29.043 18.706 3092.466 3.281 83.202 2.744 0.54 212465. 0.4642
|
|
52.16 0.4080 0.6046 0.1394 0.0941 4.191 29.348 18.216 3125.007 3.316 81.025 2.644 0.54 213086. 0.4414
|
|
56.90 0.4451 0.6359 0.1350 0.0945 4.208 29.470 17.636 3137.941 3.329 78.446 2.549 0.54 213751. 0.4188
|
|
61.64 0.4822 0.6646 0.1298 0.0942 4.196 29.384 16.966 3128.865 3.320 75.465 2.459 0.54 214459. 0.3963
|
|
66.38 0.5193 0.6910 0.1241 0.0932 4.153 29.084 16.212 3096.863 3.286 72.110 2.374 0.54 215210. 0.3740
|
|
71.13 0.5564 0.7151 0.1177 0.0916 4.080 28.570 15.383 3042.106 3.228 68.421 2.293 0.54 216003. 0.3519
|
|
75.87 0.5935 0.7371 0.1109 0.0893 3.977 27.848 14.489 2965.302 3.146 64.446 2.216 0.54 216837. 0.3300
|
|
80.61 0.6305 0.7569 0.1036 0.0863 3.845 26.928 13.540 2867.306 3.042 60.224 2.142 0.55 217711. 0.3083
|
|
85.35 0.6676 0.7744 0.0960 0.0828 3.686 25.816 12.543 2748.918 2.917 55.793 2.070 0.55 218625. 0.2867
|
|
90.09 0.7047 0.7896 0.0881 0.0786 3.501 24.519 11.507 2610.789 2.770 51.182 1.999 0.55 219579. 0.2653
|
|
94.84 0.7418 0.8021 0.0799 0.0739 3.290 23.041 10.435 2453.452 2.603 46.417 1.929 0.55 220570. 0.2438
|
|
99.58 0.7789 0.8115 0.0714 0.0686 3.054 21.387 9.334 2277.340 2.416 41.518 1.859 0.55 221601. 0.2222
|
|
104.32 0.8160 0.8173 0.0628 0.0627 2.793 19.561 8.207 2082.853 2.210 36.505 1.787 0.55 222669. 0.2003
|
|
109.06 0.8531 0.8184 0.0540 0.0563 2.508 17.566 7.059 1870.411 1.985 31.397 1.712 0.55 223775. 0.1779
|
|
113.80 0.8902 0.8128 0.0451 0.0494 2.200 15.407 5.893 1640.519 1.741 26.212 1.629 0.56 224918. 0.1547
|
|
118.54 0.9273 0.7973 0.0361 0.0420 1.869 13.090 4.714 1393.839 1.479 20.970 1.534 0.56 226098. 0.1303
|
|
123.29 0.9644 0.7646 0.0270 0.0341 1.517 10.624 3.528 1131.262 1.200 15.693 1.415 0.56 227314. 0.1039
|
|
128.03 1.0015 0.6976 0.0179 0.0257 1.145 8.020 2.340 853.976 0.906 10.409 1.243 0.56 228566. 0.0744
|
|
132.77 1.0386 0.5420 0.0089 0.0170 0.756 5.291 1.157 563.424 0.598 5.145 0.931 0.56 229850. 0.0392
|
|
137.51 1.0756 -0.0293 -0.0002 0.0078 0.346 2.423 -0.028 258.037 0.274 -0.123 -0.049 0.57 231087. 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 0.1579 0.0722 4.413 27.816 25.476 3290.929 3.143 113.315 3.511 0.59 231630. 0.6932
|
|
5.28 0.0371 0.0788 0.1575 0.0742 4.536 28.592 25.412 3382.799 3.230 113.031 3.407 0.60 231897. 0.6719
|
|
10.55 0.0743 0.1527 0.1570 0.0764 4.669 29.425 25.335 3481.375 3.324 112.688 3.301 0.60 232197. 0.6499
|
|
15.83 0.1114 0.2215 0.1564 0.0787 4.808 30.307 25.239 3585.633 3.424 112.264 3.193 0.60 232532. 0.6274
|
|
21.10 0.1485 0.2853 0.1557 0.0811 4.954 31.224 25.118 3694.146 3.528 111.726 3.084 0.60 232906. 0.6046
|
|
26.38 0.1857 0.3441 0.1547 0.0835 5.102 32.160 24.964 3804.902 3.633 111.039 2.976 0.60 233320. 0.5816
|
|
31.65 0.2228 0.3981 0.1535 0.0859 5.251 33.093 24.766 3915.307 3.739 110.161 2.869 0.60 233777. 0.5585
|
|
36.93 0.2600 0.4475 0.1520 0.0883 5.394 33.996 24.515 4022.153 3.841 109.043 2.765 0.60 234279. 0.5354
|
|
42.20 0.2971 0.4927 0.1500 0.0904 5.527 34.837 24.198 4121.621 3.936 107.634 2.663 0.60 234826. 0.5124
|
|
47.48 0.3342 0.5338 0.1475 0.0924 5.645 35.578 23.803 4209.277 4.020 105.876 2.565 0.60 235421. 0.4895
|
|
52.75 0.3714 0.5714 0.1445 0.0939 5.740 36.176 23.316 4280.046 4.087 103.709 2.471 0.60 236064. 0.4667
|
|
58.03 0.4085 0.6057 0.1408 0.0950 5.804 36.585 22.723 4328.410 4.133 101.071 2.381 0.60 236756. 0.4440
|
|
63.30 0.4456 0.6371 0.1365 0.0954 5.832 36.761 22.015 4349.234 4.153 97.923 2.296 0.60 237497. 0.4214
|
|
68.58 0.4828 0.6660 0.1314 0.0952 5.819 36.674 21.191 4338.985 4.143 94.259 2.215 0.60 238286. 0.3989
|
|
73.85 0.5199 0.6925 0.1256 0.0943 5.761 36.313 20.260 4296.267 4.103 90.115 2.139 0.60 239123. 0.3766
|
|
79.13 0.5571 0.7168 0.1192 0.0926 5.661 35.679 19.232 4221.285 4.031 85.542 2.066 0.60 240007. 0.3545
|
|
84.40 0.5942 0.7390 0.1123 0.0903 5.518 34.781 18.120 4115.055 3.930 80.600 1.997 0.61 240937. 0.3326
|
|
89.68 0.6313 0.7591 0.1050 0.0873 5.336 33.630 16.938 3978.823 3.799 75.340 1.931 0.61 241912. 0.3109
|
|
94.95 0.6685 0.7770 0.0973 0.0837 5.114 32.235 15.695 3813.764 3.642 69.811 1.867 0.61 242931. 0.2893
|
|
100.23 0.7056 0.7926 0.0893 0.0795 4.856 30.604 14.400 3620.849 3.458 64.051 1.804 0.61 243994. 0.2678
|
|
105.50 0.7427 0.8056 0.0810 0.0746 4.561 28.745 13.060 3400.867 3.248 58.092 1.742 0.61 245100. 0.2462
|
|
110.78 0.7799 0.8157 0.0724 0.0692 4.230 26.662 11.682 3154.451 3.012 51.961 1.680 0.61 246248. 0.2246
|
|
116.05 0.8170 0.8223 0.0637 0.0632 3.865 24.361 10.271 2882.175 2.752 45.684 1.616 0.61 247439. 0.2026
|
|
121.33 0.8541 0.8243 0.0547 0.0567 3.466 21.846 8.831 2584.636 2.468 39.282 1.550 0.62 248671. 0.1802
|
|
126.60 0.8913 0.8200 0.0457 0.0497 3.034 19.124 7.370 2262.548 2.161 32.781 1.477 0.62 249945. 0.1569
|
|
131.88 0.9284 0.8059 0.0365 0.0421 2.571 16.202 5.891 1916.839 1.830 26.204 1.394 0.62 251259. 0.1324
|
|
137.15 0.9656 0.7752 0.0273 0.0340 2.077 13.091 4.402 1548.767 1.479 19.582 1.289 0.62 252614. 0.1058
|
|
142.43 1.0027 0.7106 0.0180 0.0255 1.556 9.805 2.911 1160.007 1.108 12.947 1.138 0.62 254008. 0.0760
|
|
147.70 1.0398 0.5558 0.0088 0.0165 1.009 6.361 1.424 752.596 0.719 6.334 0.858 0.63 255438. 0.0401
|
|
152.98 1.0770 -0.0653 -0.0004 0.0071 0.433 2.729 -0.069 322.842 0.308 -0.308 -0.097 0.63 256783. 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 0.1584 0.0728 5.919 33.916 30.921 4413.993 3.832 137.538 3.177 0.65 254782. 0.6911
|
|
5.84 0.0374 0.0789 0.1581 0.0748 6.084 34.862 30.855 4536.982 3.939 137.244 3.085 0.65 255077. 0.6703
|
|
11.68 0.0747 0.1530 0.1577 0.0770 6.262 35.880 30.776 4669.555 4.054 136.891 2.989 0.65 255408. 0.6487
|
|
17.51 0.1121 0.2221 0.1571 0.0793 6.451 36.963 30.677 4810.479 4.176 136.450 2.892 0.65 255779. 0.6267
|
|
23.35 0.1495 0.2861 0.1565 0.0817 6.649 38.096 30.549 4957.885 4.304 135.883 2.795 0.66 256192. 0.6043
|
|
29.19 0.1868 0.3452 0.1556 0.0842 6.851 39.258 30.383 5109.141 4.435 135.145 2.697 0.66 256651. 0.5816
|
|
35.03 0.2242 0.3994 0.1545 0.0867 7.055 40.422 30.167 5260.699 4.567 134.181 2.601 0.66 257156. 0.5588
|
|
40.87 0.2615 0.4490 0.1531 0.0892 7.252 41.555 29.885 5408.116 4.695 132.929 2.506 0.66 257712. 0.5360
|
|
46.70 0.2989 0.4944 0.1512 0.0914 7.437 42.615 29.523 5546.047 4.815 131.319 2.414 0.66 258319. 0.5132
|
|
52.54 0.3363 0.5357 0.1489 0.0935 7.601 43.554 29.063 5668.241 4.921 129.274 2.326 0.66 258979. 0.4904
|
|
58.38 0.3736 0.5734 0.1459 0.0951 7.734 44.317 28.488 5767.509 5.007 126.714 2.240 0.66 259694. 0.4678
|
|
64.22 0.4110 0.6078 0.1423 0.0962 7.826 44.843 27.779 5836.026 5.066 123.560 2.159 0.66 260463. 0.4451
|
|
70.06 0.4484 0.6393 0.1379 0.0967 7.867 45.077 26.924 5866.462 5.093 119.756 2.082 0.66 261287. 0.4225
|
|
75.89 0.4857 0.6683 0.1328 0.0965 7.850 44.979 25.921 5853.748 5.082 115.298 2.008 0.66 262166. 0.4000
|
|
81.73 0.5231 0.6949 0.1269 0.0956 7.772 44.534 24.781 5795.816 5.031 110.228 1.939 0.66 263098. 0.3777
|
|
87.57 0.5604 0.7194 0.1205 0.0939 7.634 43.743 23.519 5692.907 4.942 104.612 1.874 0.66 264082. 0.3555
|
|
93.41 0.5978 0.7418 0.1135 0.0914 7.438 42.618 22.151 5546.487 4.815 98.526 1.811 0.67 265118. 0.3335
|
|
99.25 0.6352 0.7621 0.1060 0.0883 7.186 41.173 20.692 5358.365 4.652 92.039 1.752 0.67 266203. 0.3117
|
|
105.08 0.6725 0.7802 0.0981 0.0846 6.880 39.420 19.157 5130.257 4.454 85.209 1.694 0.67 267338. 0.2900
|
|
110.92 0.7099 0.7961 0.0899 0.0802 6.522 37.371 17.556 4863.583 4.222 78.087 1.637 0.67 268521. 0.2683
|
|
116.76 0.7473 0.8095 0.0814 0.0752 6.114 35.034 15.898 4559.481 3.958 70.713 1.581 0.67 269752. 0.2467
|
|
122.60 0.7846 0.8200 0.0727 0.0696 5.658 32.417 14.191 4218.863 3.662 63.123 1.526 0.67 271031. 0.2248
|
|
128.44 0.8220 0.8270 0.0637 0.0634 5.153 29.526 12.443 3842.541 3.336 55.346 1.469 0.68 272356. 0.2027
|
|
134.27 0.8594 0.8294 0.0546 0.0566 4.602 26.366 10.659 3431.374 2.979 47.412 1.409 0.68 273727. 0.1799
|
|
140.11 0.8967 0.8253 0.0453 0.0492 4.005 22.947 8.847 2986.383 2.593 39.351 1.344 0.68 275145. 0.1563
|
|
145.95 0.9341 0.8112 0.0359 0.0414 3.364 19.278 7.013 2508.898 2.178 31.195 1.268 0.68 276607. 0.1313
|
|
151.79 0.9714 0.7794 0.0265 0.0330 2.683 15.373 5.167 2000.742 1.737 22.981 1.171 0.69 278114. 0.1041
|
|
157.63 1.0088 0.7098 0.0170 0.0241 1.964 11.252 3.316 1464.424 1.271 14.751 1.027 0.69 279664. 0.0732
|
|
163.46 1.0462 0.5301 0.0075 0.0149 1.211 6.939 1.473 903.005 0.784 6.550 0.740 0.69 281252. 0.0351
|
|
169.30 1.0835
|
|
|
|
|
|
|
|
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 0.1589 0.0744 7.856 41.263 36.907 5858.300 4.662 164.164 2.857 0.71 277932. 0.6791
|
|
6.38 0.0374 0.0777 0.1586 0.0764 8.069 42.380 36.842 6016.803 4.788 163.874 2.777 0.71 278253. 0.6594
|
|
12.76 0.0749 0.1508 0.1583 0.0786 8.299 43.588 36.765 6188.374 4.925 163.531 2.695 0.71 278614. 0.6391
|
|
19.14 0.1123 0.2191 0.1578 0.0809 8.544 44.878 36.668 6371.515 5.070 163.101 2.610 0.71 279018. 0.6183
|
|
25.53 0.1498 0.2826 0.1573 0.0834 8.802 46.233 36.543 6563.930 5.223 162.543 2.525 0.71 279469. 0.5971
|
|
31.91 0.1872 0.3413 0.1566 0.0859 9.068 47.630 36.376 6762.178 5.381 161.801 2.440 0.72 279969. 0.5756
|
|
38.29 0.2246 0.3954 0.1556 0.0884 9.336 49.034 36.153 6961.524 5.540 160.808 2.356 0.72 280520. 0.5540
|
|
44.67 0.2621 0.4451 0.1543 0.0909 9.596 50.403 35.856 7155.946 5.695 159.486 2.273 0.72 281126. 0.5323
|
|
51.05 0.2995 0.4906 0.1527 0.0932 9.841 51.686 35.464 7338.138 5.840 157.743 2.192 0.72 281789. 0.5106
|
|
57.43 0.3369 0.5323 0.1505 0.0952 10.057 52.824 34.955 7499.603 5.968 155.480 2.114 0.72 282510. 0.4889
|
|
63.81 0.3744 0.5705 0.1477 0.0969 10.233 53.747 34.305 7630.714 6.072 152.590 2.039 0.72 283292. 0.4672
|
|
70.20 0.4118 0.6054 0.1442 0.0981 10.354 54.384 33.491 7721.081 6.144 148.968 1.967 0.72 284134. 0.4454
|
|
76.58 0.4493 0.6376 0.1399 0.0986 10.408 54.665 32.496 7760.982 6.176 144.541 1.899 0.72 285036. 0.4235
|
|
82.96 0.4867 0.6671 0.1348 0.0983 10.384 54.543 31.316 7743.677 6.162 139.294 1.834 0.72 285999. 0.4015
|
|
89.34 0.5241 0.6943 0.1290 0.0974 10.281 53.999 29.963 7666.419 6.101 133.274 1.773 0.72 287021. 0.3796
|
|
95.72 0.5616 0.7193 0.1225 0.0956 10.097 53.035 28.454 7529.565 5.992 126.566 1.714 0.73 288100. 0.3577
|
|
102.10 0.5990 0.7421 0.1154 0.0932 9.836 51.664 26.812 7334.984 5.837 119.260 1.658 0.73 289236. 0.3358
|
|
108.48 0.6364 0.7629 0.1078 0.0900 9.501 49.903 25.055 7084.910 5.638 111.446 1.604 0.73 290427. 0.3141
|
|
114.87 0.6739 0.7814 0.0999 0.0861 9.094 47.765 23.201 6781.373 5.396 103.199 1.552 0.73 291671. 0.2924
|
|
121.25 0.7113 0.7978 0.0915 0.0816 8.617 45.262 21.264 6426.065 5.114 94.583 1.501 0.73 292969. 0.2707
|
|
127.63 0.7488 0.8117 0.0829 0.0765 8.073 42.405 19.256 6020.407 4.791 85.649 1.451 0.73 294319. 0.2490
|
|
134.01 0.7862 0.8228 0.0740 0.0707 7.464 39.202 17.186 5565.646 4.429 76.441 1.401 0.74 295720. 0.2271
|
|
140.39 0.8236 0.8305 0.0648 0.0643 6.789 35.661 15.062 5062.905 4.029 66.998 1.349 0.74 297173. 0.2049
|
|
146.77 0.8611 0.8338 0.0555 0.0573 6.053 31.790 12.894 4513.419 3.592 57.354 1.296 0.74 298676. 0.1820
|
|
153.15 0.8985 0.8307 0.0460 0.0498 5.255 27.602 10.690 3918.754 3.118 47.547 1.237 0.74 300229. 0.1582
|
|
159.54 0.9359 0.8176 0.0364 0.0417 4.400 23.110 8.457 3281.018 2.611 37.616 1.169 0.75 301831. 0.1330
|
|
165.92 0.9734 0.7865 0.0267 0.0331 3.491 18.336 6.206 2603.262 2.072 27.604 1.081 0.75 303482. 0.1054
|
|
172.30 1.0108 0.7159 0.0170 0.0240 2.534 13.311 3.949 1889.795 1.504 17.564 0.948 0.75 305180. 0.0737
|
|
178.68 1.0483 0.5259 0.0073 0.0146 1.537 8.072 1.696 1146.082 0.912 7.546 0.671 0.75 306917. 0.0342
|
|
185.06 1.0857
|
|
|
|
|
|
|
|
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 0.1593 0.0782 10.497 50.894 43.421 7827.708 5.750 193.135 2.516 0.77 301078. 0.6485
|
|
6.91 0.0374 0.0742 0.1590 0.0802 10.763 52.183 43.358 8026.063 5.896 192.856 2.450 0.77 301424. 0.6311
|
|
13.81 0.0748 0.1442 0.1588 0.0823 11.052 53.585 43.286 8241.723 6.054 192.535 2.382 0.77 301814. 0.6131
|
|
20.72 0.1122 0.2100 0.1584 0.0846 11.362 55.089 43.197 8472.980 6.224 192.139 2.312 0.77 302250. 0.5945
|
|
27.62 0.1496 0.2715 0.1580 0.0871 11.690 56.676 43.081 8717.057 6.403 191.623 2.242 0.77 302736. 0.5755
|
|
34.53 0.1870 0.3286 0.1574 0.0896 12.028 58.318 42.924 8969.545 6.589 190.927 2.171 0.77 303274. 0.5563
|
|
41.44 0.2244 0.3815 0.1566 0.0921 12.370 59.973 42.710 9224.168 6.776 189.972 2.100 0.78 303868. 0.5369
|
|
48.34 0.2618 0.4304 0.1556 0.0946 12.703 61.588 42.416 9472.623 6.958 188.665 2.031 0.78 304521. 0.5174
|
|
55.25 0.2992 0.4756 0.1541 0.0969 13.014 63.097 42.017 9704.649 7.129 186.891 1.964 0.78 305235. 0.4979
|
|
62.16 0.3366 0.5174 0.1521 0.0990 13.287 64.421 41.484 9908.336 7.278 184.520 1.899 0.78 306013. 0.4784
|
|
69.06 0.3740 0.5562 0.1496 0.1006 13.505 65.476 40.785 10070.502 7.397 181.413 1.837 0.78 306857. 0.4589
|
|
75.97 0.4114 0.5921 0.1463 0.1017 13.648 66.171 39.890 10177.429 7.476 177.431 1.778 0.78 307766. 0.4392
|
|
82.87 0.4488 0.6254 0.1422 0.1021 13.701 66.426 38.775 10216.664 7.505 172.470 1.721 0.78 308742. 0.4193
|
|
89.78 0.4862 0.6564 0.1373 0.1017 13.651 66.186 37.432 10179.836 7.478 166.498 1.668 0.78 309784. 0.3992
|
|
96.69 0.5236 0.6853 0.1316 0.1005 13.496 65.434 35.873 10064.021 7.393 159.562 1.617 0.78 310891. 0.3788
|
|
103.59 0.5610 0.7120 0.1251 0.0986 13.237 64.176 34.118 9870.672 7.251 151.755 1.568 0.79 312060. 0.3582
|
|
110.50 0.5984 0.7365 0.1181 0.0959 12.878 62.438 32.193 9603.341 7.054 143.192 1.520 0.79 313291. 0.3375
|
|
117.40 0.6358 0.7589 0.1105 0.0926 12.426 60.244 30.122 9265.892 6.806 133.982 1.474 0.79 314582. 0.3166
|
|
124.31 0.6732 0.7790 0.1024 0.0885 11.884 57.616 27.927 8861.588 6.509 124.220 1.429 0.79 315930. 0.2955
|
|
131.22 0.7106 0.7967 0.0940 0.0838 11.255 54.568 25.626 8392.775 6.165 113.986 1.385 0.79 317337. 0.2742
|
|
138.12 0.7480 0.8118 0.0852 0.0785 10.542 51.110 23.235 7860.982 5.774 103.348 1.341 0.80 318799. 0.2528
|
|
145.03 0.7854 0.8239 0.0762 0.0726 9.746 47.252 20.764 7267.632 5.339 92.360 1.296 0.80 320318. 0.2310
|
|
151.94 0.8228 0.8326 0.0668 0.0661 8.869 43.000 18.227 6613.587 4.858 81.071 1.250 0.80 321891. 0.2088
|
|
158.84 0.8602 0.8367 0.0573 0.0589 7.912 38.361 15.630 5900.087 4.334 69.524 1.202 0.80 323519. 0.1858
|
|
165.75 0.8976 0.8344 0.0476 0.0512 6.879 33.351 12.986 5129.588 3.768 57.762 1.148 0.80 325200. 0.1619
|
|
172.65 0.9350 0.8214 0.0378 0.0430 5.775 27.998 10.304 4306.309 3.163 45.831 1.085 0.81 326935. 0.1363
|
|
179.56 0.9724 0.7890 0.0279 0.0343 4.608 22.343 7.594 3436.487 2.524 33.780 1.002 0.81 328721. 0.1081
|
|
186.47 1.0098 0.7143 0.0179 0.0253 3.391 16.440 4.871 2528.512 1.857 21.668 0.874 0.81 330558. 0.0754
|
|
193.37 1.0472 0.5185 0.0079 0.0159 2.136 10.356 2.148 1592.760 1.170 9.554 0.612 0.82 332439. 0.0351
|
|
200.28 1.0846
|
|
|
|
|
|
|
|
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 0.1595 0.0855 14.329 64.511 50.427 10685.313 7.288 224.300 2.141 0.83 324221. 0.5946
|
|
7.39 0.0371 0.0677 0.1593 0.0874 14.653 65.970 50.365 10927.046 7.453 224.024 2.091 0.83 324591. 0.5804
|
|
14.77 0.0743 0.1320 0.1591 0.0895 15.008 67.566 50.297 11191.393 7.634 223.723 2.038 0.83 325006. 0.5655
|
|
22.16 0.1114 0.1928 0.1588 0.0918 15.391 69.289 50.217 11476.716 7.828 223.367 1.985 0.83 325470. 0.5501
|
|
29.54 0.1486 0.2499 0.1585 0.0942 15.797 71.119 50.115 11779.977 8.035 222.913 1.930 0.83 325986. 0.5344
|
|
36.93 0.1857 0.3034 0.1581 0.0967 16.221 73.028 49.978 12096.024 8.251 222.302 1.874 0.83 326558. 0.5183
|
|
44.32 0.2228 0.3533 0.1574 0.0993 16.652 74.966 49.787 12417.028 8.470 221.454 1.819 0.84 327188. 0.5020
|
|
51.70 0.2600 0.3998 0.1566 0.1018 17.074 76.866 49.519 12731.887 8.684 220.261 1.764 0.84 327879. 0.4856
|
|
59.09 0.2971 0.4433 0.1554 0.1042 17.468 78.643 49.144 13026.142 8.885 218.594 1.711 0.84 328636. 0.4693
|
|
66.47 0.3343 0.4839 0.1538 0.1062 17.812 80.191 48.627 13282.525 9.060 216.294 1.661 0.84 329460. 0.4530
|
|
73.86 0.3714 0.5221 0.1516 0.1078 18.079 81.392 47.928 13481.507 9.196 213.183 1.612 0.84 330355. 0.4367
|
|
81.24 0.4085 0.5582 0.1486 0.1088 18.242 82.127 47.004 13603.224 9.279 209.075 1.567 0.84 331320. 0.4203
|
|
88.63 0.4457 0.5925 0.1449 0.1090 18.279 82.291 45.823 13630.436 9.297 203.819 1.525 0.84 332357. 0.4038
|
|
96.02 0.4828 0.6251 0.1403 0.1084 18.173 81.817 44.367 13551.911 9.244 197.345 1.485 0.84 333465. 0.3869
|
|
103.40 0.5200 0.6560 0.1349 0.1069 17.924 80.693 42.645 13365.644 9.117 189.686 1.447 0.84 334644. 0.3697
|
|
110.79 0.5571 0.6853 0.1286 0.1046 17.535 78.943 40.679 13075.880 8.919 180.941 1.411 0.85 335890. 0.3520
|
|
118.17 0.5942 0.7129 0.1217 0.1015 17.017 76.612 38.498 12689.721 8.656 171.237 1.376 0.85 337202. 0.3340
|
|
125.56 0.6314 0.7385 0.1143 0.0977 16.380 73.744 36.130 12214.648 8.332 160.704 1.342 0.85 338579. 0.3154
|
|
132.95 0.6685 0.7620 0.1063 0.0932 15.633 70.380 33.602 11657.520 7.952 149.460 1.307 0.85 340018. 0.2964
|
|
140.33 0.7057 0.7831 0.0978 0.0882 14.783 66.554 30.937 11023.758 7.519 137.608 1.273 0.85 341518. 0.2770
|
|
147.72 0.7428 0.8016 0.0890 0.0825 13.835 62.285 28.155 10316.650 7.037 125.235 1.238 0.86 343078. 0.2569
|
|
155.10 0.7799 0.8171 0.0799 0.0763 12.793 57.592 25.272 9539.383 6.507 112.410 1.202 0.86 344697. 0.2363
|
|
162.49 0.8171 0.8285 0.0705 0.0695 11.662 52.502 22.300 8696.194 5.932 99.191 1.163 0.86 346375. 0.2149
|
|
169.87 0.8542 0.8350 0.0609 0.0623 10.444 47.021 19.252 7788.426 5.312 85.634 1.121 0.86 348110. 0.1924
|
|
177.26 0.8914 0.8328 0.0510 0.0546 9.158 41.231 16.136 6829.436 4.658 71.775 1.072 0.87 349901. 0.1684
|
|
184.65 0.9285 0.8178 0.0410 0.0466 7.806 35.143 12.966 5820.935 3.970 57.672 1.010 0.87 351749. 0.1423
|
|
192.03 0.9656 0.7812 0.0308 0.0381 6.394 28.787 9.755 4768.255 3.252 43.391 0.928 0.87 353652. 0.1134
|
|
199.42 1.0028 0.7014 0.0206 0.0295 4.943 22.255 6.520 3686.242 2.514 29.001 0.802 0.87 355609. 0.0801
|
|
206.80 1.0399 0.5202 0.0104 0.0207 3.476 15.648 3.279 2591.897 1.768 14.584 0.574 0.88 357615. 0.0406
|
|
214.19 1.0771 0.0087 0.0001 0.0119 2.000 9.005 0.031 1491.557 1.017 0.136 0.009 0.88 359586. 0.0001
|
|
|
|
|
|
|