723 lines
128 KiB
Plaintext
723 lines
128 KiB
Plaintext
12x9W (12x9W.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 0.1371 0.0764 0.002 0.096 0.091 1.140 0.011 0.403 36.038 0.05 22181. 0.5304
|
|
0.36 0.0315 0.0551 0.1355 0.0774 0.002 0.098 0.090 1.155 0.011 0.398 35.161 0.05 22204. 0.5145
|
|
0.72 0.0630 0.1075 0.1337 0.0783 0.002 0.099 0.088 1.169 0.011 0.393 34.278 0.05 22228. 0.4983
|
|
1.07 0.0945 0.1571 0.1318 0.0792 0.002 0.100 0.087 1.183 0.011 0.387 33.394 0.05 22255. 0.4819
|
|
1.43 0.1259 0.2040 0.1296 0.0800 0.002 0.101 0.086 1.195 0.011 0.381 32.512 0.05 22285. 0.4653
|
|
1.79 0.1574 0.2481 0.1273 0.0808 0.002 0.102 0.084 1.206 0.012 0.374 31.633 0.05 22317. 0.4486
|
|
2.15 0.1889 0.2895 0.1247 0.0814 0.002 0.103 0.082 1.215 0.012 0.366 30.760 0.05 22352. 0.4317
|
|
2.50 0.2204 0.3282 0.1219 0.0818 0.002 0.103 0.081 1.222 0.012 0.358 29.894 0.05 22390. 0.4148
|
|
2.86 0.2519 0.3643 0.1188 0.0821 0.002 0.104 0.078 1.226 0.012 0.349 29.036 0.05 22431. 0.3977
|
|
3.22 0.2834 0.3979 0.1154 0.0822 0.002 0.104 0.076 1.227 0.012 0.339 28.185 0.05 22475. 0.3806
|
|
3.58 0.3148 0.4288 0.1118 0.0821 0.002 0.104 0.074 1.226 0.012 0.329 27.341 0.05 22522. 0.3634
|
|
3.94 0.3463 0.4572 0.1079 0.0817 0.002 0.103 0.071 1.220 0.012 0.317 26.502 0.05 22571. 0.3460
|
|
4.29 0.3778 0.4831 0.1037 0.0811 0.002 0.102 0.069 1.211 0.012 0.305 25.667 0.05 22624. 0.3285
|
|
4.65 0.4093 0.5063 0.0991 0.0801 0.002 0.101 0.066 1.197 0.011 0.291 24.832 0.05 22680. 0.3108
|
|
5.01 0.4408 0.5269 0.0943 0.0789 0.002 0.100 0.062 1.178 0.011 0.277 23.995 0.05 22739. 0.2929
|
|
5.37 0.4723 0.5446 0.0892 0.0773 0.002 0.098 0.059 1.154 0.011 0.262 23.149 0.05 22801. 0.2748
|
|
5.72 0.5037 0.5594 0.0837 0.0754 0.002 0.095 0.055 1.126 0.011 0.246 22.292 0.05 22865. 0.2564
|
|
6.08 0.5352 0.5710 0.0781 0.0732 0.001 0.092 0.052 1.093 0.010 0.230 21.415 0.05 22933. 0.2379
|
|
6.44 0.5667 0.5791 0.0722 0.0707 0.001 0.089 0.048 1.056 0.010 0.212 20.511 0.05 23004. 0.2191
|
|
6.80 0.5982 0.5832 0.0662 0.0679 0.001 0.086 0.044 1.014 0.010 0.195 19.569 0.05 23078. 0.2002
|
|
7.16 0.6297 0.5828 0.0600 0.0649 0.001 0.082 0.040 0.968 0.009 0.176 18.577 0.05 23155. 0.1809
|
|
7.51 0.6612 0.5770 0.0537 0.0615 0.001 0.078 0.035 0.919 0.009 0.158 17.519 0.05 23234. 0.1614
|
|
7.87 0.6927 0.5649 0.0473 0.0579 0.001 0.073 0.031 0.865 0.008 0.139 16.372 0.05 23317. 0.1415
|
|
8.23 0.7241 0.5450 0.0407 0.0541 0.001 0.068 0.027 0.808 0.008 0.120 15.106 0.05 23402. 0.1212
|
|
8.59 0.7556 0.5150 0.0341 0.0500 0.001 0.063 0.023 0.747 0.007 0.100 13.680 0.05 23491. 0.1004
|
|
8.94 0.7871 0.4718 0.0274 0.0457 0.001 0.058 0.018 0.682 0.007 0.080 12.033 0.05 23582. 0.0791
|
|
9.30 0.8186 0.4107 0.0206 0.0411 0.001 0.052 0.014 0.614 0.006 0.061 10.071 0.05 23677. 0.0575
|
|
9.66 0.8501 0.3238 0.0138 0.0363 0.001 0.046 0.009 0.542 0.005 0.041 7.646 0.05 23774. 0.0357
|
|
10.02 0.8816 0.1980 0.0070 0.0313 0.001 0.040 0.005 0.467 0.004 0.021 4.509 0.05 23874. 0.0150
|
|
10.38 0.9130 0.0088 0.0003 0.0261 0.001 0.033 0.000 0.390 0.004 0.001 0.193 0.05 23976. 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 0.1378 0.0684 0.011 0.345 0.364 8.168 0.039 1.620 20.226 0.10 44363. 0.5969
|
|
0.72 0.0318 0.0623 0.1362 0.0695 0.011 0.351 0.360 8.297 0.040 1.601 19.681 0.10 44407. 0.5774
|
|
1.44 0.0635 0.1212 0.1345 0.0705 0.011 0.356 0.355 8.423 0.040 1.581 19.137 0.10 44457. 0.5579
|
|
2.17 0.0953 0.1766 0.1325 0.0715 0.011 0.361 0.350 8.543 0.041 1.558 18.597 0.10 44512. 0.5382
|
|
2.89 0.1271 0.2287 0.1304 0.0724 0.012 0.366 0.345 8.654 0.041 1.533 18.061 0.10 44572. 0.5184
|
|
3.61 0.1588 0.2775 0.1280 0.0733 0.012 0.370 0.338 8.753 0.042 1.505 17.532 0.10 44637. 0.4987
|
|
4.33 0.1906 0.3231 0.1254 0.0740 0.012 0.373 0.331 8.838 0.042 1.474 17.012 0.10 44708. 0.4789
|
|
5.05 0.2224 0.3656 0.1226 0.0745 0.012 0.376 0.324 8.905 0.043 1.441 16.501 0.10 44785. 0.4592
|
|
5.78 0.2542 0.4051 0.1195 0.0749 0.012 0.378 0.316 8.952 0.043 1.405 15.999 0.10 44868. 0.4396
|
|
6.50 0.2859 0.4418 0.1161 0.0751 0.012 0.379 0.307 8.975 0.043 1.365 15.506 0.10 44957. 0.4200
|
|
7.22 0.3177 0.4756 0.1124 0.0751 0.012 0.379 0.297 8.971 0.043 1.322 15.024 0.10 45052. 0.4005
|
|
7.94 0.3495 0.5066 0.1085 0.0748 0.012 0.378 0.287 8.938 0.043 1.275 14.550 0.10 45153. 0.3809
|
|
8.66 0.3812 0.5349 0.1042 0.0743 0.012 0.375 0.275 8.870 0.042 1.225 14.083 0.10 45260. 0.3614
|
|
9.39 0.4130 0.5606 0.0996 0.0734 0.012 0.370 0.263 8.766 0.042 1.171 13.623 0.10 45373. 0.3418
|
|
10.11 0.4448 0.5836 0.0947 0.0722 0.012 0.364 0.250 8.622 0.041 1.113 13.168 0.10 45493. 0.3222
|
|
10.83 0.4765 0.6038 0.0895 0.0706 0.011 0.357 0.237 8.437 0.040 1.052 12.716 0.10 45618. 0.3024
|
|
11.55 0.5083 0.6212 0.0840 0.0687 0.011 0.347 0.222 8.211 0.039 0.988 12.265 0.10 45750. 0.2826
|
|
12.27 0.5401 0.6355 0.0783 0.0665 0.011 0.336 0.207 7.946 0.038 0.920 11.810 0.10 45888. 0.2627
|
|
13.00 0.5719 0.6466 0.0724 0.0640 0.010 0.323 0.191 7.643 0.036 0.851 11.349 0.10 46032. 0.2427
|
|
13.72 0.6036 0.6541 0.0663 0.0611 0.010 0.309 0.175 7.304 0.035 0.779 10.876 0.10 46182. 0.2225
|
|
14.44 0.6354 0.6574 0.0600 0.0580 0.009 0.293 0.159 6.928 0.033 0.706 10.384 0.10 46338. 0.2022
|
|
15.16 0.6672 0.6557 0.0536 0.0546 0.009 0.275 0.142 6.518 0.031 0.631 9.865 0.10 46500. 0.1816
|
|
15.88 0.6989 0.6481 0.0471 0.0508 0.008 0.257 0.125 6.074 0.029 0.554 9.306 0.10 46667. 0.1606
|
|
16.61 0.7307 0.6327 0.0406 0.0468 0.008 0.236 0.107 5.595 0.027 0.477 8.691 0.10 46841. 0.1391
|
|
17.33 0.7625 0.6072 0.0339 0.0426 0.007 0.215 0.090 5.084 0.024 0.398 7.993 0.10 47021. 0.1170
|
|
18.05 0.7942 0.5677 0.0272 0.0380 0.006 0.192 0.072 4.540 0.022 0.319 7.174 0.10 47207. 0.0940
|
|
18.77 0.8260 0.5076 0.0204 0.0332 0.005 0.168 0.054 3.965 0.019 0.240 6.167 0.10 47399. 0.0700
|
|
19.50 0.8578 0.4148 0.0136 0.0281 0.005 0.142 0.036 3.361 0.016 0.160 4.854 0.10 47596. 0.0450
|
|
20.22 0.8896 0.2656 0.0068 0.0228 0.004 0.115 0.018 2.729 0.013 0.080 2.997 0.10 47799. 0.0197
|
|
20.94 0.9213 0.0036 0.0001 0.0173 0.003 0.088 0.000 2.072 0.010 0.001 0.040 0.10 48006. 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 0.1382 0.0651 0.035 0.740 0.822 26.251 0.084 3.656 14.200 0.14 66543. 0.6295
|
|
1.09 0.0319 0.0658 0.1366 0.0662 0.036 0.752 0.813 26.706 0.085 3.614 13.800 0.14 66610. 0.6082
|
|
2.17 0.0638 0.1278 0.1349 0.0673 0.036 0.765 0.802 27.148 0.086 3.568 13.401 0.14 66685. 0.5869
|
|
3.26 0.0957 0.1860 0.1329 0.0684 0.037 0.777 0.791 27.571 0.088 3.517 13.007 0.14 66768. 0.5655
|
|
4.35 0.1276 0.2406 0.1308 0.0694 0.038 0.788 0.778 27.964 0.089 3.460 12.617 0.14 66858. 0.5441
|
|
5.44 0.1595 0.2916 0.1284 0.0702 0.038 0.798 0.764 28.318 0.090 3.398 12.234 0.14 66957. 0.5228
|
|
6.52 0.1914 0.3391 0.1258 0.0710 0.038 0.806 0.748 28.624 0.091 3.329 11.859 0.14 67064. 0.5016
|
|
7.61 0.2232 0.3834 0.1230 0.0716 0.039 0.813 0.731 28.870 0.092 3.254 11.492 0.14 67180. 0.4806
|
|
8.70 0.2551 0.4245 0.1199 0.0720 0.039 0.818 0.713 29.047 0.092 3.171 11.133 0.14 67305. 0.4597
|
|
9.79 0.2870 0.4626 0.1165 0.0723 0.039 0.821 0.693 29.142 0.093 3.082 10.783 0.14 67439. 0.4389
|
|
10.87 0.3189 0.4977 0.1128 0.0723 0.039 0.821 0.671 29.146 0.093 2.984 10.441 0.14 67583. 0.4182
|
|
11.96 0.3508 0.5300 0.1088 0.0720 0.039 0.818 0.647 29.045 0.092 2.879 10.108 0.14 67735. 0.3976
|
|
13.05 0.3827 0.5595 0.1045 0.0715 0.039 0.812 0.622 28.829 0.092 2.765 9.782 0.14 67897. 0.3771
|
|
14.13 0.4146 0.5863 0.0999 0.0707 0.038 0.803 0.594 28.487 0.091 2.643 9.462 0.14 68068. 0.3567
|
|
15.22 0.4465 0.6105 0.0950 0.0695 0.038 0.789 0.565 28.007 0.089 2.513 9.148 0.14 68249. 0.3362
|
|
16.31 0.4784 0.6319 0.0897 0.0679 0.037 0.772 0.534 27.386 0.087 2.374 8.839 0.14 68438. 0.3157
|
|
17.40 0.5103 0.6507 0.0842 0.0660 0.036 0.750 0.501 26.624 0.085 2.228 8.532 0.14 68637. 0.2952
|
|
18.48 0.5422 0.6666 0.0784 0.0638 0.034 0.725 0.467 25.725 0.082 2.075 8.226 0.14 68845. 0.2748
|
|
19.57 0.5741 0.6794 0.0725 0.0613 0.033 0.696 0.431 24.694 0.079 1.918 7.919 0.15 69063. 0.2542
|
|
20.66 0.6060 0.6888 0.0664 0.0584 0.032 0.663 0.395 23.535 0.075 1.755 7.606 0.15 69289. 0.2336
|
|
21.74 0.6378 0.6943 0.0601 0.0552 0.030 0.627 0.357 22.251 0.071 1.589 7.283 0.15 69525. 0.2129
|
|
22.83 0.6697 0.6952 0.0537 0.0517 0.028 0.587 0.319 20.844 0.066 1.420 6.946 0.15 69769. 0.1919
|
|
23.92 0.7016 0.6905 0.0472 0.0479 0.026 0.544 0.280 19.316 0.061 1.247 6.585 0.15 70023. 0.1705
|
|
25.01 0.7335 0.6786 0.0405 0.0438 0.024 0.498 0.241 17.669 0.056 1.073 6.190 0.15 70286. 0.1486
|
|
26.09 0.7654 0.6568 0.0339 0.0395 0.021 0.448 0.201 15.906 0.051 0.896 5.742 0.15 70557. 0.1260
|
|
27.18 0.7973 0.6212 0.0271 0.0348 0.019 0.395 0.161 14.029 0.045 0.717 5.213 0.15 70838. 0.1024
|
|
28.27 0.8292 0.5642 0.0203 0.0299 0.016 0.339 0.121 12.043 0.038 0.538 4.553 0.15 71127. 0.0774
|
|
29.36 0.8611 0.4718 0.0135 0.0247 0.013 0.280 0.080 9.953 0.032 0.358 3.666 0.15 71425. 0.0508
|
|
30.44 0.8930 0.3124 0.0067 0.0193 0.010 0.219 0.040 7.768 0.025 0.178 2.341 0.15 71732. 0.0229
|
|
31.53 0.9249 -0.0009 0.0000 0.0136 0.007 0.155 0.000 5.493 0.017 0.000 -0.006 0.15 72044. 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 0.1385 0.0633 0.081 1.279 1.465 60.521 0.144 6.516 10.978 0.19 88722. 0.6497
|
|
1.45 0.0320 0.0679 0.1370 0.0645 0.083 1.302 1.448 61.624 0.147 6.442 10.660 0.19 88812. 0.6273
|
|
2.91 0.0639 0.1318 0.1352 0.0656 0.084 1.325 1.430 62.701 0.150 6.361 10.344 0.19 88912. 0.6048
|
|
4.36 0.0959 0.1917 0.1333 0.0667 0.085 1.347 1.410 63.731 0.152 6.270 10.032 0.19 89022. 0.5824
|
|
5.81 0.1279 0.2478 0.1312 0.0677 0.087 1.367 1.387 64.692 0.154 6.169 9.725 0.19 89143. 0.5600
|
|
7.27 0.1598 0.3001 0.1288 0.0686 0.088 1.385 1.362 65.562 0.157 6.058 9.423 0.19 89275. 0.5377
|
|
8.72 0.1918 0.3489 0.1262 0.0694 0.089 1.401 1.335 66.315 0.158 5.936 9.128 0.19 89419. 0.5156
|
|
10.17 0.2238 0.3942 0.1234 0.0700 0.090 1.414 1.305 66.927 0.160 5.802 8.841 0.19 89574. 0.4937
|
|
11.62 0.2557 0.4363 0.1203 0.0705 0.090 1.424 1.272 67.372 0.161 5.656 8.561 0.19 89742. 0.4720
|
|
13.08 0.2877 0.4752 0.1169 0.0708 0.091 1.429 1.236 67.623 0.161 5.496 8.288 0.19 89922. 0.4505
|
|
14.53 0.3197 0.5111 0.1132 0.0708 0.091 1.430 1.197 67.653 0.162 5.323 8.023 0.19 90113. 0.4292
|
|
15.98 0.3517 0.5441 0.1092 0.0706 0.090 1.425 1.154 67.434 0.161 5.135 7.765 0.19 90318. 0.4080
|
|
17.44 0.3836 0.5744 0.1049 0.0700 0.090 1.414 1.109 66.937 0.160 4.932 7.514 0.19 90535. 0.3869
|
|
18.89 0.4156 0.6019 0.1002 0.0692 0.089 1.397 1.060 66.135 0.158 4.714 7.269 0.19 90764. 0.3659
|
|
20.34 0.4476 0.6269 0.0953 0.0680 0.087 1.374 1.007 65.004 0.155 4.481 7.029 0.19 91005. 0.3449
|
|
21.80 0.4795 0.6491 0.0900 0.0665 0.085 1.342 0.952 63.531 0.152 4.232 6.793 0.19 91259. 0.3240
|
|
23.25 0.5115 0.6688 0.0844 0.0646 0.083 1.304 0.893 61.718 0.147 3.971 6.561 0.19 91526. 0.3031
|
|
24.70 0.5435 0.6857 0.0787 0.0623 0.080 1.259 0.832 59.576 0.142 3.699 6.331 0.19 91805. 0.2823
|
|
26.16 0.5754 0.6996 0.0727 0.0598 0.077 1.207 0.768 57.114 0.136 3.417 6.101 0.19 92096. 0.2615
|
|
27.61 0.6074 0.7103 0.0665 0.0569 0.073 1.148 0.703 54.341 0.130 3.128 5.869 0.19 92399. 0.2406
|
|
29.06 0.6394 0.7174 0.0602 0.0536 0.069 1.083 0.636 51.265 0.122 2.831 5.631 0.19 92714. 0.2197
|
|
30.52 0.6713 0.7202 0.0538 0.0501 0.064 1.012 0.568 47.890 0.114 2.528 5.383 0.19 93042. 0.1984
|
|
31.97 0.7033 0.7176 0.0472 0.0463 0.059 0.934 0.499 44.221 0.106 2.220 5.120 0.20 93382. 0.1769
|
|
33.42 0.7353 0.7081 0.0406 0.0421 0.054 0.851 0.429 40.263 0.096 1.908 4.833 0.20 93733. 0.1548
|
|
34.87 0.7672 0.6893 0.0339 0.0377 0.048 0.761 0.358 36.021 0.086 1.593 4.509 0.20 94097. 0.1319
|
|
36.33 0.7992 0.6569 0.0271 0.0330 0.042 0.666 0.287 31.503 0.075 1.274 4.125 0.20 94473. 0.1080
|
|
37.78 0.8312 0.6033 0.0203 0.0280 0.036 0.565 0.215 26.720 0.064 0.954 3.642 0.20 94861. 0.0825
|
|
39.23 0.8631 0.5126 0.0135 0.0227 0.029 0.458 0.142 21.687 0.052 0.634 2.980 0.20 95260. 0.0550
|
|
40.69 0.8951 0.3478 0.0067 0.0172 0.022 0.347 0.071 16.421 0.039 0.314 1.950 0.20 95670. 0.0253
|
|
42.14 0.9271 -0.0074 -0.0001 0.0114 0.015 0.231 -0.001 10.935 0.026 -0.004 -0.040 0.20 96086. 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 0.1389 0.0622 0.156 1.964 2.295 116.174 0.222 10.208 8.960 0.24 110899. 0.6637
|
|
1.82 0.0320 0.0693 0.1374 0.0634 0.159 2.001 2.269 118.370 0.226 10.094 8.696 0.24 111012. 0.6405
|
|
3.64 0.0640 0.1345 0.1356 0.0646 0.162 2.037 2.241 120.517 0.230 9.967 8.433 0.24 111137. 0.6173
|
|
5.46 0.0960 0.1956 0.1337 0.0657 0.164 2.072 2.209 122.573 0.234 9.826 8.175 0.24 111275. 0.5941
|
|
7.28 0.1281 0.2527 0.1316 0.0667 0.167 2.105 2.174 124.495 0.238 9.670 7.920 0.24 111427. 0.5710
|
|
9.10 0.1601 0.3059 0.1292 0.0676 0.169 2.134 2.135 126.237 0.241 9.497 7.671 0.24 111593. 0.5481
|
|
10.91 0.1921 0.3555 0.1266 0.0684 0.171 2.160 2.092 127.751 0.244 9.307 7.428 0.24 111773. 0.5254
|
|
12.73 0.2241 0.4015 0.1238 0.0691 0.173 2.180 2.045 128.988 0.246 9.097 7.192 0.24 111968. 0.5029
|
|
14.55 0.2561 0.4442 0.1207 0.0696 0.174 2.196 1.994 129.894 0.248 8.868 6.962 0.24 112177. 0.4807
|
|
16.37 0.2881 0.4837 0.1173 0.0699 0.175 2.205 1.938 130.419 0.249 8.619 6.739 0.24 112403. 0.4587
|
|
18.19 0.3202 0.5201 0.1136 0.0699 0.175 2.206 1.877 130.508 0.249 8.347 6.522 0.24 112643. 0.4369
|
|
20.01 0.3522 0.5537 0.1096 0.0697 0.174 2.199 1.810 130.105 0.248 8.053 6.311 0.24 112900. 0.4152
|
|
21.83 0.3842 0.5844 0.1053 0.0692 0.173 2.183 1.739 129.152 0.247 7.735 6.107 0.24 113171. 0.3938
|
|
23.65 0.4162 0.6125 0.1006 0.0684 0.171 2.157 1.662 127.597 0.244 7.393 5.908 0.24 113459. 0.3724
|
|
25.47 0.4482 0.6380 0.0956 0.0672 0.168 2.120 1.580 125.392 0.239 7.027 5.714 0.24 113762. 0.3512
|
|
27.29 0.4802 0.6609 0.0903 0.0656 0.164 2.071 1.492 122.510 0.234 6.637 5.524 0.24 114080. 0.3300
|
|
29.11 0.5123 0.6811 0.0847 0.0637 0.160 2.011 1.400 118.955 0.227 6.227 5.338 0.24 114414. 0.3088
|
|
30.93 0.5443 0.6988 0.0789 0.0615 0.154 1.940 1.304 114.746 0.219 5.800 5.154 0.24 114764. 0.2878
|
|
32.74 0.5763 0.7136 0.0729 0.0589 0.147 1.858 1.205 109.904 0.210 5.358 4.971 0.24 115129. 0.2668
|
|
34.56 0.6083 0.7253 0.0667 0.0560 0.140 1.766 1.102 104.445 0.199 4.903 4.787 0.24 115509. 0.2457
|
|
36.38 0.6403 0.7336 0.0604 0.0527 0.132 1.663 0.998 98.382 0.188 4.437 4.599 0.24 115904. 0.2246
|
|
38.20 0.6723 0.7377 0.0539 0.0491 0.123 1.551 0.891 91.725 0.175 3.962 4.405 0.24 116315. 0.2033
|
|
40.02 0.7044 0.7368 0.0474 0.0453 0.113 1.428 0.782 84.483 0.161 3.479 4.200 0.24 116741. 0.1816
|
|
41.84 0.7364 0.7294 0.0407 0.0411 0.103 1.296 0.672 76.666 0.146 2.990 3.977 0.24 117182. 0.1594
|
|
43.66 0.7684 0.7130 0.0339 0.0366 0.092 1.154 0.561 68.284 0.130 2.495 3.725 0.25 117638. 0.1364
|
|
45.48 0.8004 0.6835 0.0272 0.0318 0.080 1.003 0.449 59.353 0.113 1.995 3.428 0.25 118109. 0.1123
|
|
47.30 0.8324 0.6329 0.0203 0.0267 0.067 0.843 0.336 49.895 0.095 1.494 3.052 0.25 118595. 0.0865
|
|
49.12 0.8644 0.5448 0.0135 0.0214 0.054 0.675 0.223 39.939 0.076 0.991 2.530 0.25 119095. 0.0584
|
|
50.94 0.8965 0.3776 0.0067 0.0158 0.040 0.499 0.110 29.522 0.056 0.490 1.691 0.25 119610. 0.0274
|
|
52.75 0.9285 -0.0119 -0.0001 0.0100 0.025 0.315 -0.002 18.663 0.036 -0.009 -0.051 0.25 120129. 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 0.1393 0.0616 0.266 2.797 3.314 198.544 0.316 14.742 7.572 0.29 133075. 0.6740
|
|
2.18 0.0320 0.0703 0.1378 0.0628 0.271 2.851 3.278 202.402 0.322 14.580 7.345 0.29 133210. 0.6503
|
|
4.37 0.0641 0.1364 0.1361 0.0639 0.276 2.904 3.237 206.177 0.328 14.399 7.121 0.29 133360. 0.6265
|
|
6.55 0.0961 0.1982 0.1342 0.0650 0.281 2.955 3.192 209.797 0.334 14.197 6.901 0.29 133526. 0.6028
|
|
8.74 0.1281 0.2560 0.1321 0.0661 0.286 3.003 3.141 213.185 0.339 13.973 6.684 0.29 133708. 0.5793
|
|
10.92 0.1602 0.3098 0.1297 0.0671 0.290 3.046 3.086 216.261 0.344 13.725 6.472 0.29 133907. 0.5559
|
|
13.10 0.1922 0.3599 0.1271 0.0679 0.294 3.084 3.024 218.940 0.348 13.452 6.265 0.29 134124. 0.5328
|
|
15.29 0.2242 0.4065 0.1243 0.0686 0.297 3.115 2.957 221.137 0.352 13.151 6.064 0.29 134358. 0.5099
|
|
17.47 0.2563 0.4496 0.1212 0.0691 0.299 3.138 2.883 222.759 0.355 12.822 5.869 0.29 134610. 0.4873
|
|
19.66 0.2883 0.4895 0.1178 0.0694 0.300 3.152 2.802 223.717 0.356 12.462 5.680 0.29 134881. 0.4649
|
|
21.84 0.3203 0.5264 0.1141 0.0694 0.300 3.154 2.714 223.914 0.356 12.071 5.497 0.29 135170. 0.4428
|
|
24.03 0.3524 0.5603 0.1101 0.0692 0.299 3.145 2.618 223.253 0.355 11.647 5.320 0.29 135478. 0.4209
|
|
26.21 0.3844 0.5915 0.1057 0.0687 0.297 3.122 2.515 221.636 0.353 11.189 5.148 0.29 135805. 0.3992
|
|
28.39 0.4164 0.6200 0.1011 0.0679 0.294 3.085 2.404 218.967 0.348 10.695 4.981 0.29 136150. 0.3776
|
|
30.58 0.4485 0.6458 0.0961 0.0667 0.289 3.031 2.285 215.164 0.342 10.166 4.818 0.29 136515. 0.3561
|
|
32.76 0.4805 0.6692 0.0908 0.0652 0.282 2.961 2.159 210.179 0.335 9.603 4.659 0.29 136897. 0.3348
|
|
34.95 0.5125 0.6900 0.0852 0.0633 0.274 2.874 2.026 204.017 0.325 9.011 4.504 0.29 137299. 0.3135
|
|
37.13 0.5446 0.7082 0.0793 0.0610 0.264 2.771 1.887 196.712 0.313 8.393 4.351 0.29 137719. 0.2923
|
|
39.31 0.5766 0.7238 0.0733 0.0584 0.253 2.653 1.743 188.297 0.300 7.754 4.199 0.29 138157. 0.2711
|
|
41.50 0.6086 0.7363 0.0671 0.0554 0.240 2.519 1.596 178.802 0.285 7.097 4.047 0.29 138614. 0.2500
|
|
43.68 0.6407 0.7456 0.0607 0.0522 0.226 2.370 1.444 168.249 0.268 6.424 3.893 0.29 139089. 0.2288
|
|
45.87 0.6727 0.7509 0.0542 0.0486 0.210 2.207 1.290 156.656 0.249 5.737 3.734 0.29 139583. 0.2074
|
|
48.05 0.7047 0.7515 0.0476 0.0447 0.193 2.029 1.133 144.037 0.229 5.039 3.567 0.29 140095. 0.1857
|
|
50.23 0.7368 0.7458 0.0409 0.0404 0.175 1.837 0.974 130.409 0.208 4.331 3.387 0.29 140624. 0.1634
|
|
52.42 0.7688 0.7316 0.0342 0.0359 0.155 1.631 0.813 115.792 0.184 3.615 3.184 0.29 141172. 0.1403
|
|
54.60 0.8008 0.7047 0.0273 0.0311 0.134 1.412 0.650 100.213 0.159 2.893 2.944 0.29 141738. 0.1161
|
|
56.79 0.8329 0.6574 0.0205 0.0260 0.112 1.179 0.487 83.710 0.133 2.168 2.641 0.30 142322. 0.0901
|
|
58.97 0.8649 0.5728 0.0136 0.0206 0.089 0.934 0.324 66.332 0.106 1.441 2.216 0.30 142923. 0.0617
|
|
61.15 0.8969 0.4069 0.0068 0.0149 0.065 0.678 0.161 48.148 0.077 0.717 1.518 0.30 143541. 0.0298
|
|
63.34 0.9290 -0.0045 0.0000 0.0090 0.039 0.411 -0.001 29.185 0.046 -0.005 -0.016 0.30 144163. 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 0.1398 0.0611 0.420 3.781 4.526 313.156 0.427 20.131 6.555 0.33 155247. 0.6819
|
|
2.55 0.0320 0.0711 0.1383 0.0624 0.428 3.856 4.477 319.382 0.436 19.913 6.358 0.33 155405. 0.6578
|
|
5.10 0.0641 0.1377 0.1366 0.0636 0.436 3.930 4.422 325.480 0.444 19.669 6.162 0.33 155581. 0.6336
|
|
7.65 0.0961 0.2002 0.1347 0.0647 0.444 4.001 4.361 331.331 0.452 19.397 5.970 0.33 155775. 0.6095
|
|
10.20 0.1282 0.2584 0.1326 0.0658 0.452 4.067 4.293 336.813 0.459 19.094 5.781 0.33 155987. 0.5856
|
|
12.75 0.1602 0.3127 0.1302 0.0667 0.458 4.127 4.217 341.798 0.466 18.758 5.596 0.33 156220. 0.5619
|
|
15.30 0.1923 0.3632 0.1277 0.0676 0.464 4.180 4.134 346.147 0.472 18.387 5.417 0.33 156472. 0.5385
|
|
17.85 0.2243 0.4101 0.1248 0.0683 0.469 4.223 4.042 349.723 0.477 17.979 5.242 0.33 156746. 0.5154
|
|
20.39 0.2564 0.4536 0.1217 0.0688 0.473 4.255 3.941 352.378 0.481 17.531 5.073 0.33 157041. 0.4925
|
|
22.94 0.2884 0.4938 0.1183 0.0691 0.475 4.274 3.831 353.967 0.483 17.042 4.909 0.33 157357. 0.4699
|
|
25.49 0.3205 0.5310 0.1146 0.0692 0.475 4.278 3.712 354.337 0.483 16.509 4.751 0.33 157695. 0.4476
|
|
28.04 0.3525 0.5652 0.1106 0.0690 0.474 4.266 3.582 353.332 0.482 15.931 4.598 0.34 158055. 0.4255
|
|
30.59 0.3846 0.5967 0.1063 0.0685 0.470 4.236 3.441 350.792 0.479 15.306 4.449 0.34 158437. 0.4036
|
|
33.14 0.4166 0.6255 0.1016 0.0677 0.465 4.185 3.290 346.566 0.473 14.632 4.305 0.34 158841. 0.3818
|
|
35.69 0.4487 0.6517 0.0966 0.0665 0.457 4.112 3.127 340.520 0.465 13.910 4.165 0.34 159267. 0.3602
|
|
38.24 0.4807 0.6755 0.0912 0.0649 0.446 4.016 2.954 332.577 0.454 13.141 4.029 0.34 159714. 0.3386
|
|
40.79 0.5128 0.6967 0.0856 0.0630 0.433 3.897 2.772 322.744 0.440 12.332 3.896 0.34 160183. 0.3172
|
|
43.34 0.5448 0.7155 0.0798 0.0607 0.417 3.756 2.583 311.071 0.424 11.488 3.766 0.34 160674. 0.2959
|
|
45.89 0.5769 0.7316 0.0737 0.0581 0.399 3.594 2.386 297.615 0.406 10.614 3.637 0.34 161186. 0.2747
|
|
48.44 0.6089 0.7448 0.0675 0.0551 0.379 3.410 2.184 282.423 0.385 9.715 3.508 0.34 161720. 0.2535
|
|
50.99 0.6410 0.7549 0.0611 0.0518 0.356 3.206 1.977 265.528 0.362 8.794 3.377 0.34 162275. 0.2322
|
|
53.54 0.6730 0.7612 0.0545 0.0482 0.331 2.982 1.766 246.960 0.337 7.855 3.243 0.34 162852. 0.2108
|
|
56.09 0.7051 0.7630 0.0479 0.0443 0.304 2.738 1.551 226.742 0.309 6.900 3.103 0.34 163449. 0.1890
|
|
58.64 0.7371 0.7588 0.0412 0.0400 0.275 2.474 1.334 204.901 0.280 5.932 2.952 0.34 164068. 0.1667
|
|
61.18 0.7692 0.7465 0.0344 0.0354 0.243 2.191 1.113 181.468 0.248 4.952 2.783 0.34 164708. 0.1436
|
|
63.73 0.8012 0.7219 0.0275 0.0306 0.210 1.890 0.891 156.487 0.213 3.965 2.584 0.34 165369. 0.1193
|
|
66.28 0.8333 0.6775 0.0206 0.0254 0.174 1.570 0.668 130.019 0.177 2.973 2.331 0.34 166051. 0.0932
|
|
68.83 0.8653 0.5961 0.0137 0.0199 0.137 1.233 0.445 102.146 0.139 1.979 1.975 0.35 166753. 0.0644
|
|
71.38 0.8974 0.4317 0.0069 0.0142 0.098 0.881 0.222 72.974 0.100 0.987 1.380 0.35 167474. 0.0318
|
|
73.93 0.9294 0.0002 0.0000 0.0083 0.057 0.514 0.000 42.543 0.058 0.000 0.001 0.35 168200. 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 0.1403 0.0609 0.625 4.921 5.933 465.786 0.556 26.389 5.777 0.38 177417. 0.6881
|
|
2.92 0.0321 0.0716 0.1388 0.0622 0.637 5.021 5.870 475.240 0.567 26.108 5.602 0.38 177598. 0.6636
|
|
5.83 0.0642 0.1388 0.1371 0.0634 0.650 5.119 5.799 484.506 0.578 25.793 5.428 0.38 177798. 0.6392
|
|
8.75 0.0962 0.2016 0.1352 0.0645 0.662 5.213 5.720 493.404 0.589 25.441 5.258 0.38 178020. 0.6148
|
|
11.66 0.1283 0.2603 0.1332 0.0656 0.673 5.301 5.631 501.747 0.599 25.048 5.091 0.38 178264. 0.5907
|
|
14.58 0.1604 0.3150 0.1308 0.0666 0.683 5.381 5.533 509.339 0.608 24.612 4.927 0.38 178530. 0.5668
|
|
17.50 0.1925 0.3658 0.1283 0.0675 0.692 5.451 5.425 515.974 0.616 24.129 4.769 0.38 178819. 0.5431
|
|
20.41 0.2245 0.4129 0.1254 0.0682 0.699 5.509 5.305 521.438 0.622 23.597 4.615 0.38 179133. 0.5197
|
|
23.33 0.2566 0.4567 0.1223 0.0687 0.705 5.552 5.174 525.513 0.627 23.013 4.465 0.38 179470. 0.4967
|
|
26.24 0.2887 0.4972 0.1189 0.0691 0.708 5.578 5.030 527.975 0.630 22.374 4.321 0.38 179833. 0.4739
|
|
29.16 0.3208 0.5346 0.1152 0.0691 0.709 5.585 4.873 528.595 0.631 21.677 4.182 0.38 180220. 0.4514
|
|
32.08 0.3528 0.5691 0.1112 0.0690 0.707 5.569 4.703 527.137 0.629 20.920 4.047 0.38 180633. 0.4291
|
|
34.99 0.3849 0.6008 0.1069 0.0685 0.702 5.529 4.519 523.361 0.625 20.101 3.916 0.38 181070. 0.4071
|
|
37.91 0.4170 0.6299 0.1022 0.0676 0.693 5.463 4.321 517.036 0.617 19.218 3.790 0.38 181533. 0.3852
|
|
40.82 0.4491 0.6564 0.0971 0.0664 0.681 5.367 4.108 507.962 0.606 18.270 3.668 0.38 182020. 0.3635
|
|
43.74 0.4811 0.6805 0.0918 0.0649 0.665 5.241 3.881 496.022 0.592 17.262 3.549 0.39 182533. 0.3418
|
|
46.66 0.5132 0.7021 0.0861 0.0629 0.645 5.084 3.642 481.222 0.574 16.199 3.433 0.39 183070. 0.3203
|
|
49.57 0.5453 0.7213 0.0802 0.0606 0.622 4.899 3.393 463.641 0.553 15.090 3.319 0.39 183633. 0.2989
|
|
52.49 0.5774 0.7379 0.0741 0.0580 0.595 4.684 3.135 443.363 0.529 13.942 3.207 0.39 184219. 0.2776
|
|
55.40 0.6094 0.7517 0.0678 0.0550 0.564 4.442 2.869 420.458 0.502 12.761 3.095 0.39 184831. 0.2563
|
|
58.32 0.6415 0.7625 0.0614 0.0517 0.530 4.173 2.597 394.979 0.471 11.551 2.982 0.39 185467. 0.2350
|
|
61.24 0.6736 0.7696 0.0548 0.0480 0.492 3.877 2.319 366.967 0.438 10.317 2.867 0.39 186127. 0.2135
|
|
64.15 0.7057 0.7724 0.0482 0.0440 0.451 3.555 2.037 336.461 0.402 9.062 2.746 0.39 186811. 0.1917
|
|
67.07 0.7378 0.7694 0.0414 0.0397 0.407 3.207 1.751 303.500 0.362 7.789 2.617 0.39 187520. 0.1693
|
|
69.98 0.7698 0.7586 0.0346 0.0351 0.360 2.833 1.462 268.131 0.320 6.501 2.473 0.39 188252. 0.1462
|
|
72.90 0.8019 0.7359 0.0277 0.0301 0.309 2.434 1.170 230.421 0.275 5.203 2.303 0.39 189009. 0.1218
|
|
75.82 0.8340 0.6937 0.0207 0.0249 0.255 2.012 0.876 190.462 0.227 3.898 2.087 0.39 189789. 0.0955
|
|
78.73 0.8661 0.6148 0.0138 0.0194 0.199 1.568 0.583 148.378 0.177 2.592 1.781 0.40 190593. 0.0665
|
|
81.65 0.8981 0.4507 0.0068 0.0136 0.140 1.102 0.290 104.334 0.125 1.288 1.259 0.40 191419. 0.0331
|
|
84.56 0.9302 -0.0066 -0.0001 0.0076 0.078 0.617 -0.002 58.361 0.070 -0.010 -0.018 0.40 192246. 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 0.1408 0.0609 0.888 6.222 7.539 662.526 0.703 33.534 5.161 0.43 199583. 0.6930
|
|
3.31 0.0323 0.0725 0.1394 0.0621 0.907 6.352 7.460 676.327 0.718 33.182 5.003 0.43 199788. 0.6681
|
|
6.61 0.0646 0.1405 0.1377 0.0634 0.925 6.479 7.371 689.861 0.732 32.785 4.846 0.43 200016. 0.6433
|
|
9.92 0.0970 0.2040 0.1358 0.0646 0.943 6.601 7.271 702.858 0.746 32.340 4.692 0.43 200267. 0.6186
|
|
13.22 0.1293 0.2633 0.1337 0.0657 0.959 6.715 7.159 715.042 0.759 31.843 4.541 0.43 200544. 0.5941
|
|
16.53 0.1616 0.3184 0.1314 0.0667 0.974 6.819 7.034 726.122 0.770 31.289 4.394 0.43 200847. 0.5699
|
|
19.84 0.1939 0.3697 0.1288 0.0676 0.987 6.910 6.896 735.789 0.781 30.675 4.251 0.43 201177. 0.5459
|
|
23.14 0.2263 0.4172 0.1260 0.0683 0.997 6.985 6.744 743.729 0.789 29.996 4.113 0.43 201534. 0.5222
|
|
26.45 0.2586 0.4613 0.1228 0.0689 1.005 7.040 6.576 749.619 0.795 29.248 3.979 0.43 201919. 0.4989
|
|
29.75 0.2909 0.5021 0.1194 0.0692 1.010 7.073 6.391 753.128 0.799 28.429 3.849 0.43 202332. 0.4758
|
|
33.06 0.3232 0.5398 0.1157 0.0693 1.011 7.080 6.190 753.918 0.800 27.535 3.724 0.43 202774. 0.4531
|
|
36.37 0.3556 0.5745 0.1116 0.0691 1.008 7.059 5.972 751.643 0.798 26.563 3.604 0.43 203245. 0.4306
|
|
39.67 0.3879 0.6065 0.1071 0.0685 1.000 7.006 5.735 745.950 0.791 25.509 3.487 0.43 203744. 0.4083
|
|
42.98 0.4202 0.6358 0.1024 0.0677 0.988 6.917 5.479 736.505 0.781 24.372 3.374 0.43 204272. 0.3862
|
|
46.28 0.4525 0.6625 0.0972 0.0664 0.970 6.790 5.205 723.016 0.767 23.151 3.265 0.43 204828. 0.3642
|
|
49.59 0.4849 0.6868 0.0918 0.0648 0.946 6.624 4.913 705.327 0.748 21.851 3.159 0.43 205413. 0.3424
|
|
52.89 0.5172 0.7086 0.0860 0.0628 0.917 6.419 4.605 683.462 0.725 20.482 3.056 0.43 206026. 0.3207
|
|
56.20 0.5495 0.7280 0.0800 0.0604 0.882 6.175 4.284 657.539 0.698 19.054 2.955 0.43 206668. 0.2991
|
|
59.51 0.5818 0.7449 0.0738 0.0577 0.842 5.895 3.951 627.683 0.666 17.576 2.855 0.44 207338. 0.2775
|
|
62.81 0.6142 0.7590 0.0674 0.0546 0.797 5.578 3.610 593.992 0.630 16.056 2.756 0.44 208035. 0.2561
|
|
66.12 0.6465 0.7700 0.0609 0.0511 0.746 5.227 3.260 556.546 0.591 14.498 2.656 0.44 208761. 0.2345
|
|
69.42 0.6788 0.7774 0.0542 0.0473 0.691 4.840 2.902 515.403 0.547 12.910 2.554 0.44 209514. 0.2128
|
|
72.73 0.7111 0.7803 0.0474 0.0432 0.631 4.420 2.539 470.619 0.499 11.295 2.447 0.44 210295. 0.1907
|
|
76.04 0.7435 0.7774 0.0406 0.0388 0.566 3.966 2.171 422.251 0.448 9.658 2.332 0.44 211103. 0.1680
|
|
79.34 0.7758 0.7663 0.0336 0.0340 0.497 3.478 1.799 370.376 0.393 8.002 2.203 0.44 211939. 0.1445
|
|
82.65 0.8081 0.7426 0.0266 0.0289 0.423 2.959 1.424 315.095 0.334 6.333 2.050 0.44 212802. 0.1196
|
|
85.95 0.8404 0.6974 0.0196 0.0236 0.344 2.409 1.047 256.553 0.272 4.657 1.851 0.44 213692. 0.0926
|
|
89.26 0.8728 0.6096 0.0125 0.0179 0.261 1.831 0.670 194.944 0.207 2.978 1.558 0.44 214609. 0.0623
|
|
92.57 0.9051 0.4140 0.0055 0.0120 0.175 1.226 0.294 130.520 0.138 1.306 1.020 0.45 215550. 0.0270
|
|
95.87 0.9374
|
|
|
|
|
|
|
|
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 0.1415 0.0609 1.220 7.690 9.349 909.845 0.869 41.586 4.661 0.48 221745. 0.6968
|
|
3.65 0.0321 0.0723 0.1400 0.0622 1.246 7.852 9.254 929.013 0.887 41.163 4.518 0.48 221971. 0.6721
|
|
7.30 0.0642 0.1400 0.1384 0.0635 1.271 8.011 9.147 947.829 0.905 40.685 4.377 0.48 222222. 0.6473
|
|
10.95 0.0963 0.2034 0.1366 0.0647 1.295 8.164 9.026 965.923 0.922 40.149 4.238 0.48 222499. 0.6227
|
|
14.59 0.1284 0.2625 0.1345 0.0658 1.318 8.308 8.891 982.917 0.939 39.548 4.103 0.48 222804. 0.5982
|
|
18.24 0.1605 0.3176 0.1323 0.0669 1.339 8.439 8.740 998.408 0.953 38.878 3.971 0.48 223138. 0.5740
|
|
21.89 0.1926 0.3688 0.1297 0.0678 1.357 8.553 8.573 1011.977 0.966 38.132 3.842 0.48 223501. 0.5501
|
|
25.54 0.2248 0.4163 0.1269 0.0685 1.372 8.648 8.387 1023.193 0.977 37.307 3.718 0.48 223894. 0.5265
|
|
29.19 0.2569 0.4604 0.1238 0.0691 1.383 8.719 8.183 1031.615 0.985 36.398 3.598 0.48 224318. 0.5032
|
|
32.84 0.2890 0.5012 0.1204 0.0694 1.390 8.763 7.959 1036.794 0.990 35.401 3.482 0.48 224773. 0.4803
|
|
36.49 0.3211 0.5390 0.1167 0.0695 1.392 8.776 7.714 1038.272 0.991 34.310 3.370 0.48 225260. 0.4576
|
|
40.14 0.3532 0.5739 0.1127 0.0694 1.389 8.753 7.447 1035.579 0.989 33.124 3.262 0.48 225777. 0.4352
|
|
43.78 0.3853 0.6060 0.1083 0.0689 1.379 8.691 7.158 1028.239 0.982 31.837 3.157 0.48 226327. 0.4130
|
|
47.43 0.4174 0.6356 0.1036 0.0680 1.362 8.586 6.845 1015.794 0.970 30.447 3.056 0.48 226908. 0.3910
|
|
51.08 0.4495 0.6626 0.0985 0.0668 1.338 8.434 6.509 997.840 0.953 28.954 2.959 0.48 227520. 0.3691
|
|
54.73 0.4816 0.6872 0.0931 0.0652 1.306 8.234 6.152 974.135 0.930 27.362 2.864 0.48 228163. 0.3474
|
|
58.38 0.5137 0.7095 0.0874 0.0633 1.267 7.985 5.774 944.691 0.902 25.683 2.772 0.48 228838. 0.3257
|
|
62.03 0.5458 0.7294 0.0814 0.0609 1.220 7.689 5.380 909.659 0.869 23.929 2.682 0.48 229543. 0.3042
|
|
65.68 0.5779 0.7469 0.0752 0.0582 1.166 7.347 4.971 869.212 0.830 22.112 2.594 0.48 230279. 0.2828
|
|
69.32 0.6101 0.7618 0.0689 0.0552 1.104 6.960 4.551 823.495 0.786 20.242 2.506 0.48 231046. 0.2614
|
|
72.97 0.6422 0.7737 0.0623 0.0517 1.036 6.530 4.120 772.618 0.738 18.325 2.419 0.49 231843. 0.2400
|
|
76.62 0.6743 0.7823 0.0557 0.0480 0.961 6.057 3.680 716.665 0.684 16.368 2.329 0.49 232671. 0.2185
|
|
80.27 0.7064 0.7868 0.0489 0.0439 0.879 5.542 3.232 655.712 0.626 14.378 2.236 0.49 233529. 0.1966
|
|
83.92 0.7385 0.7861 0.0420 0.0395 0.791 4.985 2.779 589.836 0.563 12.359 2.137 0.49 234417. 0.1741
|
|
87.57 0.7706 0.7779 0.0351 0.0348 0.696 4.388 2.319 519.135 0.496 10.316 2.026 0.49 235336. 0.1509
|
|
91.22 0.8027 0.7587 0.0281 0.0297 0.595 3.751 1.856 443.740 0.424 8.256 1.897 0.49 236284. 0.1264
|
|
94.86 0.8348 0.7208 0.0210 0.0244 0.488 3.075 1.390 363.836 0.347 6.184 1.733 0.49 237261. 0.0999
|
|
98.51 0.8669 0.6471 0.0140 0.0187 0.375 2.364 0.924 279.675 0.267 4.109 1.498 0.49 238268. 0.0704
|
|
102.16 0.8990 0.4860 0.0069 0.0128 0.257 1.619 0.458 191.588 0.183 2.039 1.085 0.50 239302. 0.0359
|
|
105.81 0.9311 -0.0122 -0.0001 0.0067 0.133 0.841 -0.006 99.550 0.095 -0.026 -0.026 0.50 240331. 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 0.1422 0.0611 1.629 9.333 11.369 1214.675 1.054 50.567 4.245 0.52 243902. 0.6999
|
|
4.01 0.0321 0.0724 0.1408 0.0624 1.664 9.534 11.256 1240.737 1.077 50.068 4.115 0.52 244150. 0.6751
|
|
8.03 0.0642 0.1403 0.1392 0.0637 1.698 9.730 11.129 1266.345 1.099 49.502 3.986 0.52 244426. 0.6502
|
|
12.04 0.0963 0.2038 0.1374 0.0650 1.731 9.920 10.986 1290.992 1.121 48.865 3.860 0.52 244731. 0.6255
|
|
16.06 0.1285 0.2630 0.1354 0.0661 1.762 10.098 10.825 1314.160 1.141 48.148 3.736 0.52 245067. 0.6010
|
|
20.07 0.1606 0.3181 0.1331 0.0672 1.791 10.260 10.644 1335.297 1.159 47.346 3.616 0.52 245434. 0.5768
|
|
24.09 0.1927 0.3694 0.1306 0.0681 1.816 10.403 10.443 1353.836 1.175 46.452 3.499 0.52 245834. 0.5529
|
|
28.10 0.2248 0.4171 0.1278 0.0689 1.836 10.521 10.220 1369.186 1.189 45.459 3.386 0.52 246267. 0.5292
|
|
32.11 0.2569 0.4613 0.1247 0.0695 1.852 10.610 9.974 1380.754 1.199 44.364 3.276 0.53 246735. 0.5059
|
|
36.13 0.2890 0.5022 0.1213 0.0698 1.861 10.665 9.703 1387.931 1.205 43.159 3.171 0.53 247236. 0.4830
|
|
40.14 0.3211 0.5401 0.1176 0.0699 1.864 10.681 9.406 1390.102 1.207 41.840 3.069 0.53 247772. 0.4603
|
|
44.16 0.3532 0.5752 0.1136 0.0698 1.860 10.655 9.083 1386.636 1.204 40.402 2.971 0.53 248343. 0.4379
|
|
48.17 0.3854 0.6075 0.1092 0.0693 1.846 10.580 8.732 1376.893 1.195 38.842 2.877 0.53 248949. 0.4156
|
|
52.18 0.4175 0.6372 0.1045 0.0684 1.824 10.452 8.353 1360.258 1.181 37.154 2.785 0.53 249589. 0.3936
|
|
56.20 0.4496 0.6645 0.0994 0.0672 1.792 10.267 7.945 1336.186 1.160 35.340 2.697 0.53 250264. 0.3717
|
|
60.21 0.4817 0.6893 0.0939 0.0656 1.749 10.022 7.510 1304.348 1.132 33.404 2.611 0.53 250973. 0.3499
|
|
64.23 0.5138 0.7119 0.0882 0.0636 1.696 9.718 7.050 1264.750 1.098 31.359 2.528 0.53 251716. 0.3283
|
|
68.24 0.5459 0.7322 0.0822 0.0613 1.633 9.356 6.570 1217.602 1.057 29.223 2.447 0.53 252493. 0.3067
|
|
72.26 0.5780 0.7500 0.0759 0.0585 1.560 8.937 6.072 1163.139 1.010 27.009 2.368 0.53 253304. 0.2853
|
|
76.27 0.6102 0.7654 0.0695 0.0554 1.477 8.464 5.559 1101.561 0.956 24.728 2.289 0.53 254149. 0.2639
|
|
80.28 0.6423 0.7779 0.0630 0.0520 1.385 7.938 5.034 1033.019 0.897 22.390 2.210 0.53 255027. 0.2425
|
|
84.30 0.6744 0.7872 0.0562 0.0482 1.284 7.358 4.497 957.630 0.831 20.003 2.130 0.54 255938. 0.2209
|
|
88.31 0.7065 0.7925 0.0494 0.0441 1.174 6.727 3.951 875.495 0.760 17.574 2.047 0.54 256883. 0.1990
|
|
92.33 0.7386 0.7927 0.0425 0.0396 1.055 6.045 3.397 786.721 0.683 15.110 1.958 0.54 257861. 0.1765
|
|
96.34 0.7707 0.7858 0.0355 0.0348 0.927 5.313 2.836 691.437 0.600 12.616 1.861 0.54 258872. 0.1532
|
|
100.35 0.8028 0.7682 0.0284 0.0297 0.791 4.532 2.271 589.821 0.512 10.100 1.746 0.54 259915. 0.1287
|
|
104.37 0.8349 0.7325 0.0213 0.0243 0.647 3.705 1.702 482.118 0.419 7.569 1.601 0.54 260991. 0.1021
|
|
108.38 0.8671 0.6616 0.0142 0.0186 0.494 2.833 1.132 368.671 0.320 5.034 1.392 0.54 262099. 0.0724
|
|
112.40 0.8992 0.5034 0.0070 0.0126 0.335 1.920 0.563 249.927 0.217 2.504 1.022 0.54 263238. 0.0375
|
|
116.41 0.9313 -0.0083 -0.0001 0.0063 0.169 0.967 -0.005 125.823 0.109 -0.020 -0.016 0.55 264367. 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 0.1429 0.0614 2.125 11.160 13.602 1584.486 1.261 60.503 3.894 0.57 266054. 0.7022
|
|
4.38 0.0321 0.0725 0.1416 0.0628 2.171 11.405 13.473 1619.149 1.288 59.927 3.774 0.57 266324. 0.6774
|
|
8.76 0.0642 0.1404 0.1400 0.0641 2.217 11.645 13.325 1653.244 1.316 59.272 3.656 0.57 266625. 0.6525
|
|
13.14 0.0964 0.2039 0.1383 0.0653 2.261 11.876 13.159 1686.093 1.342 58.529 3.540 0.57 266957. 0.6279
|
|
17.52 0.1285 0.2632 0.1363 0.0665 2.303 12.094 12.970 1717.000 1.366 57.691 3.426 0.57 267324. 0.6034
|
|
21.90 0.1606 0.3184 0.1341 0.0676 2.340 12.293 12.758 1745.227 1.389 56.749 3.316 0.57 267725. 0.5791
|
|
26.28 0.1927 0.3697 0.1316 0.0686 2.374 12.467 12.522 1770.011 1.409 55.696 3.209 0.57 268162. 0.5552
|
|
30.66 0.2249 0.4174 0.1288 0.0694 2.401 12.612 12.258 1790.570 1.425 54.523 3.105 0.57 268636. 0.5316
|
|
35.05 0.2570 0.4617 0.1257 0.0700 2.422 12.721 11.966 1806.114 1.437 53.225 3.005 0.57 269146. 0.5083
|
|
39.43 0.2891 0.5027 0.1224 0.0704 2.435 12.790 11.644 1815.843 1.445 51.795 2.909 0.57 269695. 0.4853
|
|
43.81 0.3212 0.5407 0.1187 0.0705 2.439 12.812 11.292 1818.944 1.447 50.226 2.816 0.57 270281. 0.4626
|
|
48.19 0.3534 0.5759 0.1146 0.0703 2.433 12.781 10.907 1814.589 1.444 48.512 2.726 0.57 270906. 0.4402
|
|
52.57 0.3855 0.6084 0.1102 0.0698 2.416 12.692 10.488 1801.944 1.434 46.650 2.640 0.58 271568. 0.4180
|
|
56.95 0.4176 0.6383 0.1055 0.0690 2.387 12.539 10.034 1780.199 1.417 44.633 2.557 0.58 272268. 0.3960
|
|
61.33 0.4498 0.6658 0.1003 0.0678 2.345 12.317 9.546 1748.640 1.392 42.462 2.476 0.58 273006. 0.3741
|
|
65.71 0.4819 0.6909 0.0948 0.0662 2.289 12.022 9.025 1706.827 1.358 40.144 2.398 0.58 273782. 0.3523
|
|
70.09 0.5140 0.7137 0.0891 0.0641 2.219 11.655 8.474 1654.763 1.317 37.694 2.323 0.58 274594. 0.3306
|
|
74.47 0.5461 0.7343 0.0830 0.0617 2.136 11.218 7.898 1592.725 1.267 35.131 2.249 0.58 275444. 0.3091
|
|
78.85 0.5782 0.7526 0.0767 0.0589 2.040 10.713 7.301 1521.033 1.210 32.474 2.177 0.58 276330. 0.2876
|
|
83.23 0.6104 0.7684 0.0703 0.0558 1.931 10.142 6.685 1439.956 1.146 29.735 2.106 0.58 277253. 0.2662
|
|
87.61 0.6425 0.7814 0.0636 0.0523 1.810 9.507 6.054 1349.700 1.074 26.927 2.034 0.58 278213. 0.2448
|
|
91.99 0.6746 0.7913 0.0568 0.0485 1.677 8.807 5.409 1250.421 0.995 24.059 1.962 0.58 279209. 0.2231
|
|
96.38 0.7067 0.7974 0.0499 0.0443 1.532 8.046 4.753 1142.256 0.909 21.140 1.887 0.59 280241. 0.2012
|
|
100.76 0.7389 0.7985 0.0429 0.0397 1.375 7.222 4.087 1025.342 0.816 18.177 1.808 0.59 281309. 0.1787
|
|
105.14 0.7710 0.7928 0.0359 0.0349 1.207 6.338 3.412 899.852 0.716 15.178 1.720 0.59 282413. 0.1554
|
|
109.52 0.8031 0.7766 0.0287 0.0297 1.027 5.395 2.732 766.019 0.610 12.151 1.618 0.59 283553. 0.1307
|
|
113.90 0.8352 0.7429 0.0215 0.0242 0.837 4.396 2.047 624.164 0.497 9.106 1.488 0.59 284728. 0.1041
|
|
118.28 0.8674 0.6743 0.0143 0.0184 0.637 3.344 1.361 474.738 0.378 6.055 1.300 0.59 285938. 0.0742
|
|
122.66 0.8995 0.5183 0.0071 0.0123 0.427 2.242 0.676 318.334 0.253 3.009 0.964 0.59 287181. 0.0388
|
|
127.04 0.9316 -0.0118 -0.0001 0.0060 0.208 1.090 -0.007 154.785 0.123 -0.032 -0.021 0.60 288409. 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 0.1438 0.0618 2.719 13.184 16.057 2027.719 1.489 71.422 3.592 0.62 288200. 0.7037
|
|
4.75 0.0321 0.0725 0.1425 0.0632 2.780 13.477 15.911 2072.895 1.523 70.771 3.481 0.62 288491. 0.6790
|
|
9.50 0.0643 0.1404 0.1410 0.0645 2.840 13.767 15.743 2117.416 1.555 70.026 3.372 0.62 288817. 0.6543
|
|
14.24 0.0964 0.2039 0.1393 0.0659 2.897 14.046 15.553 2160.384 1.587 69.178 3.265 0.62 289177. 0.6297
|
|
18.99 0.1285 0.2631 0.1373 0.0671 2.951 14.310 15.336 2200.879 1.617 68.216 3.161 0.62 289574. 0.6052
|
|
23.74 0.1607 0.3183 0.1351 0.0682 3.001 14.550 15.092 2237.923 1.644 67.130 3.059 0.62 290009. 0.5810
|
|
28.49 0.1928 0.3697 0.1327 0.0692 3.045 14.762 14.818 2270.500 1.668 65.910 2.960 0.62 290483. 0.5572
|
|
33.23 0.2250 0.4174 0.1299 0.0700 3.081 14.938 14.511 2297.583 1.688 64.546 2.865 0.62 290997. 0.5336
|
|
37.98 0.2571 0.4617 0.1269 0.0707 3.109 15.072 14.171 2318.135 1.703 63.032 2.773 0.62 291552. 0.5104
|
|
42.73 0.2892 0.5028 0.1235 0.0711 3.126 15.156 13.795 2331.113 1.712 61.358 2.684 0.62 292148. 0.4874
|
|
47.48 0.3214 0.5409 0.1198 0.0712 3.132 15.185 13.381 2335.476 1.716 59.518 2.599 0.62 292785. 0.4648
|
|
52.22 0.3535 0.5761 0.1158 0.0710 3.125 15.150 12.928 2330.156 1.712 57.505 2.517 0.62 293463. 0.4424
|
|
56.97 0.3856 0.6088 0.1113 0.0705 3.103 15.046 12.435 2314.079 1.700 55.312 2.437 0.62 294183. 0.4203
|
|
61.72 0.4178 0.6388 0.1066 0.0697 3.066 14.864 11.901 2286.210 1.679 52.936 2.361 0.62 294944. 0.3983
|
|
66.47 0.4499 0.6665 0.1014 0.0685 3.011 14.600 11.325 2245.631 1.650 50.374 2.287 0.63 295745. 0.3764
|
|
71.21 0.4821 0.6919 0.0959 0.0668 2.939 14.250 10.709 2191.763 1.610 47.634 2.216 0.63 296588. 0.3546
|
|
75.96 0.5142 0.7150 0.0901 0.0648 2.849 13.814 10.057 2124.606 1.561 44.735 2.147 0.63 297470. 0.3329
|
|
80.71 0.5463 0.7359 0.0839 0.0623 2.742 13.293 9.375 2044.522 1.502 41.701 2.080 0.63 298393. 0.3114
|
|
85.46 0.5785 0.7545 0.0776 0.0595 2.618 12.691 8.667 1951.938 1.434 38.553 2.014 0.63 299355. 0.2899
|
|
90.20 0.6106 0.7707 0.0711 0.0563 2.477 12.010 7.938 1847.214 1.357 35.307 1.949 0.63 300357. 0.2685
|
|
94.95 0.6427 0.7843 0.0644 0.0528 2.321 11.252 7.189 1730.622 1.271 31.976 1.884 0.63 301399. 0.2470
|
|
99.70 0.6749 0.7948 0.0575 0.0488 2.149 10.418 6.424 1602.371 1.177 28.574 1.818 0.63 302480. 0.2254
|
|
104.45 0.7070 0.8016 0.0505 0.0446 1.961 9.510 5.645 1462.637 1.074 25.109 1.751 0.63 303600. 0.2034
|
|
109.19 0.7392 0.8036 0.0435 0.0400 1.759 8.528 4.854 1311.605 0.963 21.592 1.679 0.64 304759. 0.1808
|
|
113.94 0.7713 0.7989 0.0363 0.0350 1.541 7.474 4.053 1149.493 0.844 18.030 1.599 0.64 305957. 0.1575
|
|
118.69 0.8034 0.7842 0.0291 0.0298 1.310 6.350 3.245 976.598 0.717 14.434 1.507 0.64 307193. 0.1328
|
|
123.44 0.8356 0.7523 0.0218 0.0242 1.064 5.158 2.432 793.339 0.583 10.815 1.390 0.64 308467. 0.1060
|
|
128.18 0.8677 0.6861 0.0145 0.0183 0.805 3.903 1.616 600.296 0.441 7.187 1.221 0.64 309779. 0.0759
|
|
132.93 0.8998 0.5321 0.0072 0.0121 0.534 2.589 0.802 398.236 0.293 3.566 0.913 0.64 311126. 0.0400
|
|
137.68 0.9320 -0.0178 -0.0001 0.0057 0.251 1.215 -0.012 186.802 0.137 -0.054 -0.030 0.65 312452. 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 0.1447 0.0625 3.432 15.452 18.738 2559.422 1.746 83.347 3.321 0.67 310339. 0.7029
|
|
5.14 0.0323 0.0725 0.1434 0.0639 3.509 15.799 18.576 2616.898 1.785 82.625 3.220 0.67 310653. 0.6785
|
|
10.28 0.0646 0.1405 0.1420 0.0653 3.585 16.141 18.389 2673.613 1.824 81.793 3.120 0.67 311005. 0.6541
|
|
15.41 0.0969 0.2042 0.1403 0.0666 3.659 16.472 18.174 2728.408 1.861 80.838 3.021 0.67 311394. 0.6298
|
|
20.55 0.1292 0.2636 0.1384 0.0679 3.728 16.784 17.929 2780.096 1.896 79.746 2.925 0.67 311824. 0.6056
|
|
25.69 0.1615 0.3189 0.1363 0.0690 3.792 17.070 17.650 2827.419 1.929 78.505 2.831 0.67 312296. 0.5816
|
|
30.83 0.1938 0.3704 0.1338 0.0700 3.847 17.321 17.334 2869.063 1.957 77.103 2.740 0.67 312811. 0.5579
|
|
35.97 0.2261 0.4182 0.1311 0.0709 3.894 17.531 16.980 2903.705 1.981 75.529 2.652 0.67 313370. 0.5344
|
|
41.11 0.2584 0.4627 0.1281 0.0715 3.929 17.689 16.585 2929.988 1.999 73.772 2.567 0.67 313973. 0.5113
|
|
46.24 0.2907 0.5039 0.1247 0.0719 3.951 17.789 16.147 2946.548 2.010 71.824 2.486 0.67 314621. 0.4884
|
|
51.38 0.3230 0.5422 0.1209 0.0720 3.959 17.822 15.664 2952.007 2.014 69.675 2.407 0.67 315315. 0.4658
|
|
56.52 0.3553 0.5776 0.1168 0.0719 3.949 17.780 15.134 2944.971 2.009 67.317 2.331 0.67 316053. 0.4434
|
|
61.66 0.3876 0.6103 0.1124 0.0714 3.921 17.653 14.556 2924.032 1.994 64.744 2.258 0.67 316837. 0.4212
|
|
66.80 0.4199 0.6406 0.1075 0.0705 3.873 17.435 13.927 2887.843 1.970 61.949 2.187 0.67 317665. 0.3992
|
|
71.94 0.4522 0.6684 0.1023 0.0692 3.802 17.117 13.249 2835.233 1.934 58.932 2.120 0.67 318537. 0.3772
|
|
77.07 0.4845 0.6940 0.0967 0.0675 3.709 16.696 12.523 2765.487 1.886 55.702 2.054 0.67 319454. 0.3554
|
|
82.21 0.5168 0.7173 0.0908 0.0654 3.592 16.172 11.754 2678.641 1.827 52.283 1.990 0.68 320415. 0.3337
|
|
87.35 0.5491 0.7385 0.0845 0.0629 3.453 15.547 10.949 2575.189 1.757 48.702 1.928 0.68 321419. 0.3120
|
|
92.49 0.5814 0.7574 0.0781 0.0599 3.293 14.826 10.113 2455.698 1.675 44.984 1.868 0.68 322466. 0.2905
|
|
97.63 0.6137 0.7739 0.0714 0.0566 3.112 14.010 9.251 2320.641 1.583 41.150 1.808 0.68 323557. 0.2689
|
|
102.77 0.6460 0.7878 0.0646 0.0530 2.911 13.103 8.367 2170.370 1.480 37.216 1.749 0.68 324690. 0.2473
|
|
107.90 0.6783 0.7986 0.0576 0.0489 2.689 12.106 7.463 2005.162 1.368 33.196 1.688 0.68 325866. 0.2255
|
|
113.04 0.7106 0.8057 0.0505 0.0445 2.448 11.020 6.543 1825.249 1.245 29.101 1.626 0.68 327084. 0.2033
|
|
118.18 0.7428 0.8080 0.0433 0.0398 2.187 9.846 5.608 1630.866 1.112 24.943 1.560 0.68 328344. 0.1806
|
|
123.32 0.7751 0.8036 0.0360 0.0347 1.907 8.587 4.661 1422.303 0.970 20.732 1.486 0.69 329646. 0.1569
|
|
128.46 0.8074 0.7887 0.0286 0.0293 1.609 7.245 3.705 1199.957 0.818 16.480 1.400 0.69 330990. 0.1318
|
|
133.60 0.8397 0.7556 0.0212 0.0235 1.293 5.822 2.743 964.382 0.658 12.201 1.290 0.69 332375. 0.1045
|
|
138.73 0.8720 0.6850 0.0137 0.0175 0.961 4.325 1.779 716.362 0.489 7.912 1.126 0.69 333801. 0.0734
|
|
143.87 0.9043 0.5110 0.0063 0.0112 0.613 2.759 0.816 456.961 0.312 3.630 0.810 0.69 335264. 0.0358
|
|
149.01 0.9366
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1456 0.0638 4.309 18.104 21.649 3212.858 2.045 96.296 3.056 0.71 332471. 0.6953
|
|
5.48 0.0322 0.0713 0.1444 0.0651 4.402 18.499 21.475 3282.908 2.090 95.522 2.967 0.71 332804. 0.6723
|
|
10.96 0.0643 0.1383 0.1431 0.0665 4.495 18.887 21.273 3351.917 2.134 94.623 2.879 0.71 333177. 0.6492
|
|
16.44 0.0965 0.2012 0.1415 0.0678 4.584 19.262 21.039 3418.448 2.176 93.583 2.792 0.71 333591. 0.6261
|
|
21.92 0.1286 0.2601 0.1397 0.0691 4.668 19.615 20.770 3481.051 2.216 92.385 2.706 0.71 334048. 0.6031
|
|
27.40 0.1608 0.3151 0.1376 0.0702 4.745 19.937 20.462 3538.227 2.253 91.014 2.623 0.71 334551. 0.5802
|
|
32.88 0.1929 0.3665 0.1353 0.0712 4.812 20.220 20.111 3588.416 2.284 89.454 2.542 0.72 335099. 0.5574
|
|
38.36 0.2251 0.4143 0.1326 0.0720 4.868 20.455 19.715 3630.034 2.311 87.693 2.463 0.72 335694. 0.5348
|
|
43.85 0.2572 0.4589 0.1296 0.0727 4.910 20.632 19.271 3661.492 2.331 85.718 2.387 0.72 336337. 0.5124
|
|
49.33 0.2894 0.5003 0.1263 0.0730 4.937 20.743 18.776 3681.164 2.344 83.517 2.314 0.72 337029. 0.4902
|
|
54.81 0.3215 0.5387 0.1226 0.0732 4.945 20.778 18.229 3687.397 2.347 81.082 2.242 0.72 337768. 0.4681
|
|
60.29 0.3537 0.5744 0.1185 0.0730 4.933 20.728 17.626 3678.496 2.342 78.402 2.173 0.72 338556. 0.4462
|
|
65.77 0.3858 0.6075 0.1141 0.0725 4.898 20.582 16.967 3652.727 2.325 75.470 2.107 0.72 339391. 0.4243
|
|
71.25 0.4180 0.6380 0.1093 0.0716 4.839 20.333 16.250 3608.390 2.297 72.278 2.043 0.72 340275. 0.4026
|
|
76.73 0.4501 0.6662 0.1041 0.0703 4.753 19.970 15.473 3543.960 2.256 68.826 1.980 0.72 341205. 0.3809
|
|
82.21 0.4823 0.6920 0.0985 0.0686 4.638 19.488 14.641 3458.409 2.202 65.123 1.920 0.72 342183. 0.3593
|
|
87.69 0.5145 0.7157 0.0925 0.0665 4.495 18.886 13.758 3351.621 2.134 61.194 1.862 0.72 343207. 0.3377
|
|
93.17 0.5466 0.7373 0.0863 0.0640 4.324 18.167 12.831 3224.138 2.053 57.072 1.805 0.72 344277. 0.3162
|
|
98.65 0.5788 0.7567 0.0798 0.0611 4.126 17.336 11.868 3076.648 1.959 52.788 1.750 0.73 345393. 0.2947
|
|
104.13 0.6109 0.7738 0.0731 0.0577 3.902 16.396 10.873 2909.742 1.852 48.364 1.695 0.73 346554. 0.2733
|
|
109.61 0.6431 0.7883 0.0663 0.0541 3.653 15.349 9.852 2723.888 1.734 43.821 1.640 0.73 347761. 0.2518
|
|
115.09 0.6752 0.8000 0.0592 0.0500 3.379 14.197 8.807 2519.444 1.604 39.174 1.586 0.73 349013. 0.2301
|
|
120.58 0.7074 0.8082 0.0521 0.0456 3.080 12.942 7.742 2296.708 1.462 34.438 1.529 0.73 350310. 0.2080
|
|
126.06 0.7395 0.8120 0.0448 0.0408 2.757 11.585 6.660 2055.971 1.309 29.625 1.469 0.73 351651. 0.1854
|
|
131.54 0.7717 0.8095 0.0374 0.0357 2.411 10.129 5.564 1797.584 1.144 24.747 1.404 0.74 353037. 0.1619
|
|
137.02 0.8038 0.7975 0.0300 0.0302 2.041 8.577 4.456 1522.081 0.969 19.818 1.328 0.74 354466. 0.1370
|
|
142.50 0.8360 0.7690 0.0225 0.0244 1.650 6.933 3.339 1230.330 0.783 14.853 1.231 0.74 355940. 0.1100
|
|
147.98 0.8681 0.7069 0.0149 0.0183 1.239 5.205 2.219 923.634 0.588 9.870 1.090 0.74 357456. 0.0794
|
|
153.46 0.9003 0.5555 0.0074 0.0120 0.810 3.402 1.099 603.767 0.384 4.889 0.826 0.74 359013. 0.0423
|
|
158.94 0.9324 -0.0266 -0.0002 0.0054 0.363 1.523 -0.023 270.365 0.172 -0.101 -0.038 0.74 360530. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1465 0.0663 5.434 21.408 24.790 4052.440 2.419 110.265 2.775 0.76 354595. 0.6755
|
|
5.84 0.0321 0.0691 0.1455 0.0676 5.546 21.847 24.607 4135.614 2.468 109.454 2.699 0.76 354948. 0.6546
|
|
11.69 0.0643 0.1344 0.1442 0.0689 5.655 22.277 24.394 4216.951 2.517 108.503 2.624 0.76 355343. 0.6336
|
|
17.53 0.0964 0.1959 0.1427 0.0702 5.759 22.687 24.144 4294.602 2.563 107.391 2.550 0.76 355782. 0.6126
|
|
23.37 0.1285 0.2538 0.1410 0.0714 5.856 23.068 23.853 4366.746 2.606 106.099 2.478 0.76 356268. 0.5917
|
|
29.21 0.1607 0.3083 0.1390 0.0725 5.943 23.410 23.517 4431.557 2.645 104.604 2.407 0.76 356803. 0.5708
|
|
35.06 0.1928 0.3593 0.1367 0.0734 6.017 23.705 23.132 4487.237 2.678 102.890 2.338 0.76 357387. 0.5499
|
|
40.90 0.2249 0.4072 0.1341 0.0741 6.078 23.941 22.693 4532.003 2.705 100.938 2.271 0.76 358022. 0.5290
|
|
46.74 0.2571 0.4520 0.1312 0.0746 6.121 24.111 22.198 4564.091 2.724 98.735 2.206 0.76 358709. 0.5082
|
|
52.58 0.2892 0.4939 0.1279 0.0749 6.144 24.204 21.643 4581.726 2.735 96.266 2.143 0.76 359447. 0.4874
|
|
58.43 0.3213 0.5330 0.1243 0.0749 6.146 24.211 21.025 4583.084 2.735 93.520 2.081 0.77 360237. 0.4665
|
|
64.27 0.3535 0.5693 0.1203 0.0747 6.123 24.122 20.343 4566.271 2.725 90.486 2.021 0.77 361079. 0.4456
|
|
70.11 0.3856 0.6031 0.1158 0.0741 6.074 23.927 19.594 4529.288 2.703 87.154 1.962 0.77 361973. 0.4247
|
|
75.95 0.4177 0.6344 0.1110 0.0731 5.995 23.614 18.776 4470.128 2.668 83.518 1.905 0.77 362917. 0.4037
|
|
81.80 0.4499 0.6633 0.1058 0.0717 5.883 23.175 17.890 4386.932 2.618 79.574 1.850 0.77 363912. 0.3825
|
|
87.64 0.4820 0.6898 0.1001 0.0700 5.737 22.601 16.937 4278.378 2.553 75.334 1.796 0.77 364957. 0.3613
|
|
93.48 0.5141 0.7142 0.0941 0.0678 5.557 21.892 15.923 4144.217 2.473 70.827 1.743 0.77 366051. 0.3400
|
|
99.32 0.5463 0.7364 0.0878 0.0652 5.344 21.051 14.858 3985.021 2.378 66.091 1.691 0.77 367195. 0.3188
|
|
105.17 0.5784 0.7564 0.0813 0.0622 5.098 20.082 13.750 3801.537 2.269 61.160 1.641 0.77 368387. 0.2975
|
|
111.01 0.6105 0.7740 0.0745 0.0588 4.820 18.988 12.604 3594.399 2.145 56.064 1.591 0.78 369627. 0.2761
|
|
116.85 0.6427 0.7892 0.0675 0.0550 4.511 17.771 11.427 3364.064 2.008 50.826 1.541 0.78 370916. 0.2547
|
|
122.69 0.6748 0.8016 0.0604 0.0509 4.172 16.434 10.222 3110.888 1.857 45.465 1.490 0.78 372252. 0.2330
|
|
128.54 0.7069 0.8106 0.0532 0.0464 3.802 14.978 8.992 2835.238 1.692 39.997 1.439 0.78 373636. 0.2109
|
|
134.38 0.7391 0.8152 0.0458 0.0415 3.403 13.406 7.742 2537.664 1.515 34.436 1.384 0.78 375067. 0.1883
|
|
140.22 0.7712 0.8135 0.0383 0.0363 2.976 11.722 6.474 2218.983 1.324 28.797 1.323 0.78 376546. 0.1646
|
|
146.06 0.8033 0.8019 0.0307 0.0307 2.522 9.934 5.192 1880.430 1.122 23.092 1.252 0.79 378070. 0.1395
|
|
151.91 0.8355 0.7728 0.0230 0.0249 2.043 8.049 3.898 1523.724 0.909 17.340 1.160 0.79 379641. 0.1120
|
|
157.75 0.8676 0.7081 0.0154 0.0188 1.544 6.081 2.599 1151.132 0.687 11.559 1.024 0.79 381258. 0.0807
|
|
163.59 0.8997 0.5514 0.0077 0.0125 1.027 4.044 1.298 765.535 0.457 5.773 0.769 0.79 382918. 0.0428
|
|
169.43 0.9319 -0.0058 0.0000 0.0060 0.493 1.941 -0.006 367.518 0.219 -0.028 -0.008 0.79 384549. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1474 0.0707 6.957 25.792 28.152 5187.527 2.914 125.220 2.461 0.81 376712. 0.6386
|
|
6.21 0.0321 0.0653 0.1464 0.0720 7.087 26.275 27.966 5284.784 2.969 124.394 2.400 0.81 377083. 0.6207
|
|
12.41 0.0643 0.1273 0.1453 0.0733 7.213 26.742 27.747 5378.696 3.021 123.417 2.340 0.81 377499. 0.6026
|
|
18.62 0.0964 0.1862 0.1439 0.0745 7.331 27.180 27.487 5466.624 3.071 122.262 2.281 0.81 377963. 0.5847
|
|
24.83 0.1285 0.2420 0.1423 0.0756 7.437 27.574 27.181 5546.057 3.115 120.901 2.223 0.81 378477. 0.5667
|
|
31.04 0.1607 0.2948 0.1405 0.0765 7.529 27.915 26.823 5614.613 3.154 119.310 2.167 0.81 379043. 0.5487
|
|
37.24 0.1928 0.3449 0.1383 0.0773 7.604 28.191 26.408 5670.131 3.185 117.462 2.112 0.81 379663. 0.5308
|
|
43.45 0.2249 0.3923 0.1358 0.0778 7.658 28.393 25.930 5710.663 3.208 115.338 2.060 0.81 380338. 0.5128
|
|
49.66 0.2571 0.4371 0.1329 0.0782 7.690 28.511 25.386 5734.427 3.221 112.918 2.008 0.81 381068. 0.4947
|
|
55.87 0.2892 0.4794 0.1297 0.0782 7.697 28.537 24.772 5739.719 3.224 110.186 1.958 0.81 381854. 0.4764
|
|
62.07 0.3213 0.5193 0.1261 0.0780 7.677 28.463 24.084 5724.831 3.216 107.127 1.908 0.81 382697. 0.4579
|
|
68.28 0.3535 0.5567 0.1221 0.0775 7.628 28.280 23.320 5687.925 3.195 103.729 1.860 0.81 383594. 0.4391
|
|
74.49 0.3856 0.5917 0.1177 0.0767 7.546 27.977 22.478 5627.012 3.161 99.981 1.812 0.82 384547. 0.4200
|
|
80.70 0.4177 0.6243 0.1129 0.0755 7.429 27.544 21.554 5540.000 3.112 95.874 1.765 0.82 385554. 0.4006
|
|
86.90 0.4499 0.6546 0.1076 0.0739 7.275 26.972 20.550 5424.877 3.047 91.406 1.718 0.82 386615. 0.3808
|
|
93.11 0.4820 0.6826 0.1019 0.0720 7.081 26.252 19.467 5280.150 2.966 86.588 1.672 0.82 387730. 0.3608
|
|
99.32 0.5141 0.7083 0.0959 0.0696 6.847 25.384 18.312 5105.548 2.868 81.454 1.627 0.82 388896. 0.3404
|
|
105.53 0.5462 0.7319 0.0895 0.0668 6.573 24.371 17.097 4901.777 2.753 76.047 1.582 0.82 390115. 0.3199
|
|
111.73 0.5784 0.7531 0.0829 0.0637 6.262 23.217 15.829 4669.727 2.623 70.409 1.538 0.82 391385. 0.2991
|
|
117.94 0.6105 0.7720 0.0760 0.0601 5.914 21.927 14.518 4410.093 2.477 64.575 1.493 0.82 392707. 0.2782
|
|
124.15 0.6426 0.7884 0.0690 0.0562 5.529 20.501 13.168 4123.309 2.316 58.571 1.448 0.83 394079. 0.2570
|
|
130.36 0.6748 0.8019 0.0617 0.0519 5.109 18.941 11.785 3809.644 2.140 52.421 1.403 0.83 395502. 0.2355
|
|
136.56 0.7069 0.8115 0.0543 0.0473 4.655 17.258 10.374 3471.029 1.950 46.142 1.356 0.83 396975. 0.2135
|
|
142.77 0.7390 0.8157 0.0468 0.0424 4.171 15.463 8.936 3110.060 1.747 39.747 1.303 0.83 398498. 0.1905
|
|
148.98 0.7712 0.8124 0.0391 0.0372 3.656 13.554 7.476 2726.171 1.531 33.255 1.244 0.83 400071. 0.1663
|
|
155.18 0.8033 0.7973 0.0314 0.0316 3.114 11.543 5.999 2321.744 1.304 26.682 1.172 0.84 401693. 0.1403
|
|
161.39 0.8354 0.7612 0.0236 0.0259 2.548 9.446 4.506 1899.799 1.067 20.044 1.076 0.84 403363. 0.1117
|
|
167.60 0.8676 0.6839 0.0157 0.0200 1.963 7.279 3.005 1464.125 0.822 13.365 0.931 0.84 405082. 0.0789
|
|
173.81 0.8997 0.5085 0.0079 0.0139 1.367 5.067 1.500 1019.164 0.572 6.670 0.667 0.84 406846. 0.0400
|
|
180.01 0.9318 -0.0064 -0.0001 0.0077 0.759 2.816 -0.010 566.329 0.318 -0.045 -0.008 0.84 408589. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 18000
|
|
|
|
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 0.1479 0.0773 9.024 31.597 31.668 6728.979 3.570 140.859 2.135 0.86 398842. 0.5874
|
|
6.57 0.0321 0.0601 0.1470 0.0786 9.177 32.134 31.484 6843.345 3.631 140.041 2.087 0.86 399230. 0.5725
|
|
13.15 0.0643 0.1175 0.1460 0.0798 9.324 32.650 31.265 6953.121 3.689 139.067 2.040 0.86 399665. 0.5576
|
|
19.72 0.0964 0.1723 0.1448 0.0810 9.460 33.126 31.004 7054.509 3.743 137.907 1.993 0.86 400150. 0.5427
|
|
26.29 0.1285 0.2246 0.1434 0.0820 9.580 33.545 30.694 7143.691 3.790 136.526 1.949 0.86 400689. 0.5279
|
|
32.87 0.1607 0.2746 0.1416 0.0829 9.678 33.888 30.326 7216.918 3.829 134.889 1.906 0.86 401283. 0.5132
|
|
39.44 0.1928 0.3224 0.1396 0.0835 9.750 34.142 29.893 7270.826 3.857 132.963 1.865 0.86 401936. 0.4985
|
|
46.01 0.2249 0.3682 0.1373 0.0839 9.793 34.291 29.388 7302.641 3.874 130.719 1.825 0.86 402648. 0.4838
|
|
52.58 0.2571 0.4120 0.1345 0.0839 9.803 34.327 28.806 7310.227 3.878 128.131 1.787 0.86 403420. 0.4691
|
|
59.16 0.2892 0.4540 0.1314 0.0837 9.779 34.241 28.142 7291.954 3.869 125.175 1.750 0.86 404253. 0.4541
|
|
65.73 0.3214 0.4940 0.1279 0.0832 9.718 34.027 27.391 7246.438 3.844 121.835 1.714 0.86 405146. 0.4387
|
|
72.30 0.3535 0.5322 0.1240 0.0824 9.618 33.679 26.550 7172.267 3.805 118.093 1.679 0.86 406099. 0.4230
|
|
78.88 0.3856 0.5684 0.1196 0.0812 9.479 33.190 25.616 7068.285 3.750 113.938 1.644 0.86 407111. 0.4068
|
|
85.45 0.4178 0.6026 0.1148 0.0796 9.297 32.555 24.586 6932.859 3.678 109.360 1.609 0.86 408182. 0.3900
|
|
92.02 0.4499 0.6347 0.1096 0.0777 9.071 31.763 23.462 6764.275 3.589 104.357 1.573 0.87 409309. 0.3726
|
|
98.60 0.4820 0.6647 0.1039 0.0753 8.799 30.810 22.244 6561.306 3.481 98.941 1.538 0.87 410494. 0.3546
|
|
105.17 0.5142 0.6925 0.0978 0.0726 8.481 29.696 20.942 6324.006 3.355 93.148 1.502 0.87 411734. 0.3361
|
|
111.74 0.5463 0.7182 0.0914 0.0695 8.118 28.426 19.566 6053.550 3.212 87.031 1.466 0.87 413029. 0.3171
|
|
118.32 0.5784 0.7416 0.0847 0.0660 7.712 27.006 18.129 5751.183 3.051 80.637 1.430 0.87 414379. 0.2977
|
|
124.89 0.6106 0.7626 0.0777 0.0622 7.266 25.441 16.639 5417.998 2.874 74.009 1.393 0.87 415782. 0.2778
|
|
131.46 0.6427 0.7811 0.0705 0.0580 6.778 23.735 15.103 5054.548 2.682 67.179 1.355 0.87 417240. 0.2575
|
|
138.04 0.6748 0.7966 0.0632 0.0535 6.251 21.887 13.528 4661.076 2.473 60.174 1.316 0.88 418751. 0.2368
|
|
144.61 0.7070 0.8074 0.0557 0.0487 5.692 19.930 11.918 4244.268 2.252 53.010 1.274 0.88 420314. 0.2150
|
|
151.18 0.7391 0.8090 0.0480 0.0438 5.119 17.925 10.273 3817.371 2.025 45.694 1.221 0.88 421930. 0.1913
|
|
157.75 0.7712 0.8002 0.0402 0.0387 4.521 15.832 8.601 3371.555 1.789 38.255 1.157 0.88 423598. 0.1659
|
|
164.33 0.8034 0.7759 0.0323 0.0334 3.900 13.656 6.905 2908.186 1.543 30.715 1.077 0.88 425318. 0.1384
|
|
170.90 0.8355 0.7255 0.0243 0.0279 3.262 11.421 5.192 2432.136 1.290 23.095 0.968 0.89 427089. 0.1079
|
|
177.47 0.8676 0.6277 0.0162 0.0224 2.614 9.152 3.467 1949.078 1.034 15.422 0.807 0.89 428910. 0.0735
|
|
184.05 0.8998 0.4340 0.0081 0.0168 1.965 6.881 1.738 1465.363 0.777 7.730 0.538 0.89 430780. 0.0347
|
|
190.62 0.9319 0.0028 0.0000 0.0113 1.319 4.618 0.007 983.455 0.522 0.032 0.003 0.89 432650. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 19000
|
|
|
|
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 0.1469 0.0838 11.515 38.200 35.046 8587.007 4.316 155.884 1.851 0.90 421045. 0.5358
|
|
6.95 0.0322 0.0553 0.1461 0.0851 11.686 38.766 34.861 8714.291 4.380 155.064 1.814 0.90 421451. 0.5239
|
|
13.91 0.0644 0.1084 0.1452 0.0863 11.852 39.315 34.644 8837.801 4.442 154.096 1.778 0.90 421905. 0.5117
|
|
20.86 0.0966 0.1593 0.1441 0.0874 12.006 39.827 34.385 8952.854 4.500 152.944 1.742 0.90 422413. 0.4995
|
|
27.81 0.1288 0.2081 0.1428 0.0884 12.144 40.286 34.078 9055.930 4.551 151.577 1.707 0.91 422975. 0.4872
|
|
34.77 0.1610 0.2549 0.1413 0.0893 12.261 40.673 33.713 9143.035 4.595 149.957 1.672 0.91 423596. 0.4748
|
|
41.72 0.1932 0.2998 0.1395 0.0899 12.351 40.970 33.284 9209.841 4.629 148.046 1.639 0.91 424278. 0.4624
|
|
48.67 0.2254 0.3429 0.1374 0.0903 12.407 41.158 32.780 9252.076 4.650 145.805 1.607 0.91 425021. 0.4499
|
|
55.63 0.2576 0.3843 0.1350 0.0905 12.425 41.218 32.193 9265.476 4.657 143.196 1.576 0.91 425829. 0.4372
|
|
62.58 0.2898 0.4242 0.1321 0.0903 12.399 41.131 31.516 9245.830 4.647 140.183 1.546 0.91 426702. 0.4244
|
|
69.53 0.3220 0.4625 0.1289 0.0897 12.323 40.878 30.739 9189.020 4.618 136.729 1.517 0.91 427639. 0.4113
|
|
76.49 0.3542 0.4995 0.1252 0.0888 12.192 40.443 29.857 9091.272 4.569 132.804 1.490 0.91 428642. 0.3980
|
|
83.44 0.3865 0.5351 0.1210 0.0874 12.002 39.813 28.862 8949.593 4.498 128.380 1.463 0.91 429710. 0.3843
|
|
90.39 0.4187 0.5693 0.1163 0.0856 11.750 38.979 27.752 8762.072 4.404 123.439 1.437 0.91 430842. 0.3700
|
|
97.34 0.4509 0.6020 0.1112 0.0833 11.436 37.937 26.524 8527.905 4.286 117.977 1.411 0.91 432036. 0.3553
|
|
104.30 0.4831 0.6332 0.1056 0.0805 11.060 36.689 25.181 8247.359 4.145 112.006 1.385 0.92 433292. 0.3398
|
|
111.25 0.5153 0.6627 0.0995 0.0774 10.624 35.244 23.735 7922.475 3.982 105.572 1.359 0.92 434609. 0.3237
|
|
118.20 0.5475 0.6904 0.0931 0.0738 10.134 33.616 22.198 7556.710 3.798 98.737 1.332 0.92 435984. 0.3069
|
|
125.16 0.5797 0.7162 0.0863 0.0698 9.593 31.821 20.585 7153.198 3.595 91.562 1.305 0.92 437418. 0.2896
|
|
132.11 0.6119 0.7397 0.0793 0.0656 9.004 29.869 18.907 6714.329 3.375 84.098 1.277 0.92 438910. 0.2716
|
|
139.06 0.6441 0.7608 0.0720 0.0609 8.370 27.766 17.173 6241.683 3.137 76.387 1.248 0.92 440458. 0.2529
|
|
146.02 0.6763
|
|
152.97 0.7085 0.7921 0.0569 0.0509 6.986 23.175 13.566 5209.608 2.618 60.342 1.181 0.93 443723. 0.2127
|
|
159.92 0.7407 0.7897 0.0490 0.0460 6.314 20.946 11.692 4708.433 2.366 52.007 1.126 0.93 445439. 0.1883
|
|
166.88 0.7729 0.7701 0.0410 0.0411 5.651 18.746 9.780 4214.005 2.118 43.503 1.053 0.93 447209. 0.1610
|
|
173.83 0.8051 0.7305 0.0329 0.0362 4.975 16.505 7.841 3710.225 1.865 34.878 0.959 0.93 449034. 0.1313
|
|
180.78 0.8373 0.6599 0.0247 0.0313 4.297 14.255 5.882 3204.347 1.610 26.165 0.833 0.94 450912. 0.0987
|
|
187.74 0.8695 0.5403 0.0164 0.0264 3.626 12.029 3.914 2704.091 1.359 17.409 0.656 0.94 452844. 0.0635
|
|
194.69 0.9017 0.3405 0.0082 0.0216 2.973 9.863 1.950 2217.126 1.114 8.674 0.399 0.94 454826. 0.0272
|
|
201.64 0.9339 0.0002 0.0000 0.0170 2.338 7.757 0.001 1743.613 0.876 0.004 0.000 0.94 456830. 0.0000
|
|
|
|
|
|
|