538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
16x10 (16x10.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 0.1071 0.0489 0.004 0.260 0.224 3.075 0.029 0.995 33.013 0.06 30442. 0.5727
|
|
0.41 0.0271 0.0580 0.1057 0.0495 0.004 0.263 0.221 3.115 0.030 0.982 32.151 0.06 30466. 0.5540
|
|
0.82 0.0543 0.1128 0.1042 0.0501 0.004 0.267 0.218 3.154 0.030 0.968 31.287 0.06 30492. 0.5352
|
|
1.23 0.0814 0.1646 0.1025 0.0507 0.004 0.270 0.214 3.190 0.030 0.952 30.426 0.06 30520. 0.5162
|
|
1.65 0.1086 0.2133 0.1006 0.0512 0.004 0.272 0.210 3.223 0.031 0.935 29.570 0.06 30551. 0.4971
|
|
2.06 0.1357 0.2589 0.0986 0.0517 0.004 0.275 0.206 3.251 0.031 0.916 28.721 0.06 30585. 0.4779
|
|
2.47 0.1629 0.3016 0.0964 0.0520 0.004 0.277 0.201 3.274 0.031 0.895 27.879 0.06 30621. 0.4587
|
|
2.88 0.1900 0.3414 0.0940 0.0523 0.004 0.278 0.196 3.291 0.031 0.873 27.047 0.06 30660. 0.4394
|
|
3.29 0.2172 0.3783 0.0914 0.0525 0.004 0.279 0.191 3.301 0.032 0.849 26.225 0.06 30702. 0.4202
|
|
3.70 0.2443 0.4124 0.0886 0.0525 0.004 0.279 0.185 3.302 0.032 0.823 25.412 0.06 30746. 0.4009
|
|
4.11 0.2715 0.4437 0.0856 0.0524 0.004 0.278 0.179 3.295 0.031 0.795 24.608 0.06 30794. 0.3815
|
|
4.52 0.2986 0.4723 0.0824 0.0521 0.004 0.277 0.172 3.277 0.031 0.765 23.811 0.06 30845. 0.3622
|
|
4.94 0.3258 0.4981 0.0789 0.0516 0.004 0.275 0.165 3.248 0.031 0.733 23.021 0.06 30899. 0.3428
|
|
5.35 0.3529 0.5212 0.0753 0.0510 0.004 0.271 0.157 3.208 0.031 0.699 22.234 0.06 30955. 0.3233
|
|
5.76 0.3800 0.5414 0.0714 0.0501 0.004 0.267 0.149 3.155 0.030 0.664 21.447 0.06 31015. 0.3038
|
|
6.17 0.4072 0.5587 0.0674 0.0491 0.004 0.261 0.141 3.091 0.030 0.626 20.658 0.06 31078. 0.2842
|
|
6.58 0.4343 0.5730 0.0632 0.0479 0.004 0.255 0.132 3.014 0.029 0.587 19.861 0.06 31144. 0.2646
|
|
6.99 0.4615 0.5840 0.0588 0.0465 0.004 0.247 0.123 2.926 0.028 0.547 19.051 0.06 31213. 0.2449
|
|
7.40 0.4886 0.5914 0.0544 0.0449 0.004 0.239 0.114 2.827 0.027 0.505 18.220 0.06 31286. 0.2252
|
|
7.81 0.5158 0.5948 0.0498 0.0432 0.004 0.230 0.104 2.716 0.026 0.462 17.361 0.06 31361. 0.2053
|
|
8.23 0.5429 0.5936 0.0451 0.0412 0.003 0.219 0.094 2.594 0.025 0.419 16.461 0.06 31439. 0.1852
|
|
8.64 0.5701 0.5872 0.0403 0.0391 0.003 0.208 0.084 2.460 0.023 0.374 15.507 0.06 31521. 0.1649
|
|
9.05 0.5972 0.5744 0.0354 0.0368 0.003 0.196 0.074 2.316 0.022 0.329 14.480 0.06 31606. 0.1444
|
|
9.46 0.6244 0.5537 0.0305 0.0343 0.003 0.183 0.064 2.160 0.021 0.283 13.352 0.06 31694. 0.1235
|
|
9.87 0.6515 0.5231 0.0254 0.0317 0.003 0.169 0.053 1.994 0.019 0.236 12.087 0.06 31785. 0.1022
|
|
10.28 0.6787 0.4791 0.0204 0.0289 0.002 0.154 0.043 1.817 0.017 0.189 10.629 0.06 31879. 0.0804
|
|
10.69 0.7058 0.4169 0.0153 0.0259 0.002 0.138 0.032 1.630 0.016 0.142 8.893 0.07 31976. 0.0583
|
|
11.11 0.7329 0.3283 0.0102 0.0228 0.002 0.121 0.021 1.433 0.014 0.095 6.743 0.07 32076. 0.0361
|
|
11.52 0.7601 0.1989 0.0051 0.0195 0.002 0.104 0.011 1.227 0.012 0.047 3.939 0.07 32180. 0.0149
|
|
11.93 0.7872 0.0011 0.0000 0.0161 0.001 0.086 0.000 1.012 0.010 0.000 0.022 0.07 32285. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 2000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1076 0.0439 0.030 0.934 0.899 22.097 0.106 3.999 18.457 0.13 60883. 0.6418
|
|
0.83 0.0273 0.0651 0.1062 0.0446 0.030 0.949 0.887 22.452 0.107 3.947 17.927 0.13 60931. 0.6193
|
|
1.66 0.0546 0.1263 0.1047 0.0453 0.031 0.963 0.874 22.793 0.109 3.890 17.401 0.13 60983. 0.5967
|
|
2.48 0.0820 0.1838 0.1030 0.0459 0.031 0.977 0.860 23.114 0.110 3.826 16.881 0.13 61041. 0.5742
|
|
3.31 0.1093 0.2376 0.1011 0.0465 0.031 0.989 0.845 23.408 0.112 3.757 16.367 0.13 61103. 0.5517
|
|
4.14 0.1366 0.2878 0.0991 0.0470 0.032 1.000 0.828 23.667 0.113 3.682 15.862 0.13 61171. 0.5292
|
|
4.97 0.1639 0.3346 0.0969 0.0474 0.032 1.009 0.809 23.885 0.114 3.599 15.367 0.13 61244. 0.5069
|
|
5.79 0.1912 0.3781 0.0945 0.0478 0.032 1.016 0.789 24.051 0.115 3.510 14.881 0.13 61323. 0.4848
|
|
6.62 0.2186 0.4183 0.0919 0.0480 0.032 1.021 0.767 24.160 0.115 3.413 14.406 0.13 61407. 0.4628
|
|
7.45 0.2459 0.4554 0.0890 0.0481 0.032 1.023 0.744 24.201 0.116 3.309 13.941 0.13 61498. 0.4410
|
|
8.28 0.2732 0.4895 0.0860 0.0480 0.032 1.021 0.719 24.167 0.115 3.196 13.487 0.13 61594. 0.4193
|
|
9.11 0.3005 0.5206 0.0828 0.0478 0.032 1.016 0.692 24.050 0.115 3.076 13.042 0.13 61697. 0.3977
|
|
9.93 0.3278 0.5490 0.0793 0.0474 0.032 1.008 0.663 23.841 0.114 2.947 12.605 0.13 61805. 0.3763
|
|
10.76 0.3551 0.5745 0.0756 0.0468 0.032 0.995 0.632 23.534 0.112 2.810 12.176 0.13 61920. 0.3549
|
|
11.59 0.3825 0.5972 0.0717 0.0459 0.031 0.977 0.599 23.126 0.110 2.666 11.753 0.13 62041. 0.3337
|
|
12.42 0.4098 0.6171 0.0677 0.0449 0.030 0.956 0.565 22.618 0.108 2.514 11.335 0.13 62168. 0.3125
|
|
13.25 0.4371 0.6340 0.0634 0.0437 0.030 0.930 0.530 22.008 0.105 2.357 10.918 0.13 62302. 0.2914
|
|
14.07 0.4644 0.6479 0.0590 0.0423 0.029 0.900 0.493 21.300 0.102 2.194 10.501 0.13 62442. 0.2704
|
|
14.90 0.4917 0.6584 0.0545 0.0407 0.027 0.866 0.455 20.494 0.098 2.026 10.079 0.13 62588. 0.2494
|
|
15.73 0.5191 0.6653 0.0499 0.0389 0.026 0.828 0.417 19.589 0.094 1.854 9.649 0.13 62741. 0.2284
|
|
16.56 0.5464 0.6681 0.0451 0.0369 0.025 0.786 0.377 18.587 0.089 1.678 9.204 0.13 62899. 0.2073
|
|
17.38 0.5737 0.6659 0.0403 0.0347 0.023 0.739 0.337 17.489 0.084 1.498 8.737 0.13 63064. 0.1860
|
|
18.21 0.6010 0.6577 0.0354 0.0324 0.022 0.689 0.296 16.293 0.078 1.316 8.238 0.13 63236. 0.1643
|
|
19.04 0.6283 0.6420 0.0305 0.0298 0.020 0.634 0.254 15.002 0.072 1.132 7.691 0.13 63414. 0.1423
|
|
19.87 0.6557 0.6162 0.0254 0.0271 0.018 0.575 0.212 13.617 0.065 0.945 7.075 0.13 63598. 0.1196
|
|
20.70 0.6830 0.5765 0.0204 0.0241 0.016 0.513 0.170 12.140 0.058 0.756 6.354 0.13 63788. 0.0961
|
|
21.52 0.7103 0.5161 0.0153 0.0210 0.014 0.447 0.127 10.573 0.050 0.567 5.469 0.13 63985. 0.0716
|
|
22.35 0.7376 0.4227 0.0102 0.0177 0.012 0.377 0.085 8.922 0.043 0.377 4.313 0.13 64188. 0.0461
|
|
23.18 0.7649 0.2711 0.0051 0.0143 0.010 0.304 0.042 7.191 0.034 0.188 2.667 0.13 64397. 0.0201
|
|
24.01 0.7922 -0.0006 0.0000 0.0107 0.007 0.228 0.000 5.385 0.026 0.000 -0.006 0.13 64608. 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 0.1080 0.0419 0.096 2.007 2.030 71.228 0.227 9.032 12.930 0.19 91323. 0.6757
|
|
1.25 0.0274 0.0685 0.1066 0.0427 0.097 2.042 2.004 72.472 0.231 8.914 12.543 0.19 91395. 0.6512
|
|
2.49 0.0548 0.1328 0.1051 0.0434 0.099 2.076 1.975 73.672 0.235 8.785 12.160 0.19 91474. 0.6267
|
|
3.74 0.0822 0.1930 0.1034 0.0440 0.100 2.108 1.943 74.806 0.238 8.643 11.782 0.19 91560. 0.6023
|
|
4.98 0.1096 0.2492 0.1015 0.0446 0.102 2.137 1.908 75.848 0.241 8.488 11.411 0.19 91654. 0.5781
|
|
6.23 0.1370 0.3016 0.0995 0.0452 0.103 2.163 1.870 76.774 0.244 8.318 11.048 0.19 91756. 0.5540
|
|
7.47 0.1644 0.3502 0.0973 0.0457 0.104 2.185 1.828 77.556 0.247 8.132 10.693 0.19 91866. 0.5302
|
|
8.72 0.1918 0.3954 0.0949 0.0460 0.105 2.202 1.783 78.168 0.249 7.931 10.346 0.19 91985. 0.5067
|
|
9.96 0.2192 0.4371 0.0922 0.0463 0.105 2.214 1.734 78.579 0.250 7.713 10.009 0.19 92112. 0.4833
|
|
11.21 0.2466 0.4756 0.0894 0.0464 0.106 2.219 1.681 78.761 0.251 7.477 9.680 0.19 92249. 0.4603
|
|
12.45 0.2740 0.5110 0.0864 0.0463 0.106 2.217 1.624 78.684 0.250 7.223 9.361 0.19 92394. 0.4374
|
|
13.70 0.3014 0.5434 0.0831 0.0461 0.105 2.207 1.563 78.320 0.249 6.950 9.049 0.19 92549. 0.4148
|
|
14.94 0.3288 0.5730 0.0796 0.0457 0.104 2.187 1.497 77.641 0.247 6.659 8.746 0.19 92713. 0.3924
|
|
16.19 0.3562 0.5997 0.0759 0.0451 0.103 2.159 1.427 76.625 0.244 6.349 8.449 0.19 92886. 0.3702
|
|
17.43 0.3836 0.6236 0.0720 0.0443 0.101 2.120 1.354 75.261 0.240 6.022 8.159 0.19 93068. 0.3481
|
|
18.68 0.4109 0.6448 0.0679 0.0433 0.099 2.072 1.277 73.547 0.234 5.679 7.874 0.19 93260. 0.3263
|
|
19.92 0.4383 0.6632 0.0637 0.0421 0.096 2.014 1.197 71.485 0.228 5.322 7.592 0.19 93462. 0.3046
|
|
21.17 0.4657 0.6786 0.0592 0.0407 0.093 1.946 1.114 69.078 0.220 4.953 7.312 0.19 93673. 0.2830
|
|
22.42 0.4931 0.6909 0.0547 0.0390 0.089 1.869 1.028 66.328 0.211 4.573 7.031 0.19 93893. 0.2615
|
|
23.66 0.5205 0.6999 0.0500 0.0372 0.085 1.782 0.941 63.236 0.201 4.184 6.747 0.19 94123. 0.2400
|
|
24.91 0.5479 0.7049 0.0453 0.0352 0.080 1.685 0.851 59.805 0.190 3.786 6.456 0.19 94362. 0.2184
|
|
26.15 0.5753 0.7053 0.0404 0.0330 0.075 1.579 0.760 56.034 0.178 3.381 6.152 0.19 94611. 0.1967
|
|
27.40 0.6027 0.7002 0.0355 0.0306 0.070 1.463 0.667 51.926 0.165 2.969 5.830 0.19 94870. 0.1747
|
|
28.64 0.6301 0.6879 0.0305 0.0279 0.064 1.338 0.574 47.483 0.151 2.551 5.479 0.19 95138. 0.1522
|
|
29.89 0.6575 0.6660 0.0255 0.0251 0.057 1.203 0.479 42.709 0.136 2.129 5.083 0.19 95416. 0.1290
|
|
31.13 0.6849 0.6304 0.0204 0.0221 0.050 1.060 0.383 37.613 0.120 1.704 4.619 0.19 95703. 0.1048
|
|
32.38 0.7123 0.5735 0.0153 0.0190 0.043 0.907 0.287 32.206 0.103 1.276 4.041 0.20 96000. 0.0794
|
|
33.62 0.7397 0.4810 0.0101 0.0156 0.036 0.747 0.191 26.503 0.084 0.848 3.263 0.20 96306. 0.0523
|
|
34.87 0.7671 0.3199 0.0050 0.0121 0.028 0.578 0.095 20.524 0.065 0.421 2.093 0.20 96620. 0.0236
|
|
36.11 0.7945 -0.0045 0.0000 0.0084 0.019 0.402 -0.001 14.275 0.045 -0.004 -0.028 0.20 96937. 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 0.1085 0.0409 0.221 3.481 3.624 164.747 0.393 16.121 9.978 0.25 121760. 0.6966
|
|
1.66 0.0274 0.0705 0.1071 0.0417 0.225 3.545 3.578 167.773 0.401 15.914 9.672 0.25 121856. 0.6709
|
|
3.32 0.0548 0.1365 0.1055 0.0424 0.229 3.607 3.526 170.697 0.408 15.685 9.370 0.25 121962. 0.6453
|
|
4.99 0.0823 0.1983 0.1038 0.0431 0.233 3.665 3.470 173.463 0.414 15.434 9.073 0.25 122077. 0.6198
|
|
6.65 0.1097 0.2559 0.1020 0.0437 0.236 3.719 3.408 176.014 0.420 15.159 8.782 0.25 122202. 0.5945
|
|
8.31 0.1371 0.3096 0.1000 0.0443 0.239 3.767 3.340 178.287 0.426 14.857 8.497 0.25 122339. 0.5695
|
|
9.97 0.1645 0.3594 0.0977 0.0448 0.242 3.808 3.266 180.218 0.430 14.528 8.220 0.25 122486. 0.5448
|
|
11.63 0.1920 0.4055 0.0953 0.0451 0.244 3.840 3.186 181.740 0.434 14.170 7.950 0.25 122645. 0.5204
|
|
13.30 0.2194 0.4481 0.0927 0.0454 0.245 3.862 3.098 182.783 0.436 13.781 7.688 0.25 122815. 0.4963
|
|
14.96 0.2468 0.4875 0.0899 0.0455 0.246 3.873 3.004 183.277 0.438 13.361 7.434 0.25 122997. 0.4725
|
|
16.62 0.2742 0.5237 0.0868 0.0455 0.246 3.870 2.902 183.150 0.437 12.908 7.187 0.25 123192. 0.4490
|
|
18.28 0.3017 0.5568 0.0836 0.0453 0.245 3.853 2.793 182.333 0.435 12.423 6.947 0.26 123398. 0.4258
|
|
19.94 0.3291 0.5871 0.0801 0.0449 0.242 3.820 2.676 180.760 0.432 11.903 6.715 0.26 123617. 0.4028
|
|
21.61 0.3565 0.6146 0.0764 0.0443 0.239 3.769 2.552 178.378 0.426 11.350 6.488 0.26 123849. 0.3801
|
|
23.27 0.3839 0.6393 0.0724 0.0435 0.235 3.701 2.420 175.157 0.418 10.766 6.267 0.26 124093. 0.3576
|
|
24.93 0.4114 0.6614 0.0683 0.0425 0.229 3.615 2.283 171.091 0.408 10.153 6.051 0.26 124350. 0.3353
|
|
26.59 0.4388 0.6807 0.0640 0.0413 0.223 3.512 2.139 166.186 0.397 9.516 5.839 0.26 124619. 0.3132
|
|
28.25 0.4662 0.6973 0.0596 0.0398 0.215 3.390 1.991 160.446 0.383 8.857 5.629 0.26 124901. 0.2913
|
|
29.92 0.4936 0.7108 0.0550 0.0382 0.206 3.252 1.839 153.878 0.367 8.179 5.420 0.26 125195. 0.2695
|
|
31.58 0.5210 0.7211 0.0503 0.0364 0.196 3.095 1.682 146.483 0.350 7.483 5.209 0.26 125502. 0.2478
|
|
33.24 0.5485 0.7278 0.0456 0.0343 0.185 2.922 1.523 138.264 0.330 6.772 4.995 0.26 125822. 0.2260
|
|
34.90 0.5759 0.7302 0.0407 0.0321 0.173 2.731 1.360 129.223 0.308 6.048 4.772 0.26 126155. 0.2041
|
|
36.56 0.6033 0.7274 0.0357 0.0296 0.160 2.522 1.194 119.364 0.285 5.312 4.538 0.26 126501. 0.1819
|
|
38.23 0.6307 0.7179 0.0307 0.0270 0.146 2.297 1.027 108.693 0.259 4.566 4.284 0.26 126859. 0.1592
|
|
39.89 0.6582 0.6992 0.0256 0.0241 0.130 2.054 0.857 97.223 0.232 3.812 3.999 0.26 127230. 0.1358
|
|
41.55 0.6856 0.6673 0.0205 0.0211 0.114 1.795 0.686 84.970 0.203 3.053 3.664 0.26 127613. 0.1113
|
|
43.21 0.7130 0.6146 0.0154 0.0179 0.097 1.521 0.515 71.963 0.172 2.290 3.244 0.26 128010. 0.0854
|
|
44.87 0.7404 0.5254 0.0103 0.0145 0.078 1.231 0.343 58.238 0.139 1.525 2.671 0.26 128418. 0.0574
|
|
46.54 0.7679 0.3622 0.0051 0.0109 0.059 0.927 0.172 43.847 0.105 0.763 1.776 0.26 128839. 0.0270
|
|
48.20 0.7953 0.0033 0.0000 0.0071 0.039 0.608 0.001 28.793 0.069 0.004 0.016 0.26 129260. 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 0.1090 0.0404 0.426 5.367 5.690 317.468 0.606 25.308 8.129 0.32 152195. 0.7111
|
|
2.10 0.0277 0.0724 0.1076 0.0411 0.434 5.470 5.617 323.564 0.618 24.984 7.874 0.32 152316. 0.6844
|
|
4.20 0.0554 0.1402 0.1060 0.0419 0.442 5.569 5.536 329.459 0.629 24.626 7.622 0.32 152449. 0.6577
|
|
6.29 0.0831 0.2035 0.1043 0.0426 0.449 5.664 5.448 335.036 0.640 24.231 7.375 0.32 152595. 0.6313
|
|
8.39 0.1108 0.2624 0.1025 0.0433 0.456 5.751 5.350 340.179 0.650 23.797 7.133 0.32 152754. 0.6051
|
|
10.49 0.1385 0.3172 0.1004 0.0438 0.462 5.828 5.243 344.762 0.658 23.321 6.898 0.32 152927. 0.5792
|
|
12.59 0.1661 0.3680 0.0982 0.0443 0.468 5.894 5.126 348.651 0.666 22.801 6.669 0.32 153114. 0.5537
|
|
14.68 0.1938 0.4150 0.0957 0.0447 0.472 5.945 4.998 351.710 0.672 22.233 6.446 0.32 153315. 0.5285
|
|
16.78 0.2215 0.4584 0.0931 0.0450 0.474 5.981 4.860 353.796 0.676 21.617 6.230 0.32 153531. 0.5037
|
|
18.88 0.2492 0.4984 0.0902 0.0451 0.476 5.997 4.710 354.765 0.678 20.949 6.022 0.32 153763. 0.4792
|
|
20.98 0.2769 0.5352 0.0871 0.0451 0.475 5.992 4.548 354.474 0.677 20.229 5.819 0.32 154010. 0.4551
|
|
23.08 0.3046 0.5689 0.0838 0.0449 0.473 5.964 4.374 352.779 0.674 19.456 5.624 0.32 154273. 0.4313
|
|
25.17 0.3323 0.5997 0.0802 0.0444 0.469 5.909 4.188 349.550 0.668 18.627 5.434 0.32 154552. 0.4078
|
|
27.27 0.3600 0.6277 0.0764 0.0438 0.462 5.827 3.990 344.679 0.658 17.746 5.250 0.32 154846. 0.3846
|
|
29.37 0.3877 0.6529 0.0724 0.0430 0.453 5.716 3.780 338.111 0.646 16.814 5.071 0.32 155156. 0.3616
|
|
31.47 0.4154 0.6755 0.0682 0.0419 0.442 5.576 3.561 329.838 0.630 15.839 4.897 0.32 155483. 0.3389
|
|
33.56 0.4430 0.6953 0.0638 0.0407 0.429 5.407 3.333 319.868 0.611 14.823 4.726 0.32 155825. 0.3164
|
|
35.66 0.4707 0.7124 0.0593 0.0392 0.413 5.210 3.097 308.214 0.589 13.773 4.557 0.32 156184. 0.2941
|
|
37.76 0.4984 0.7266 0.0547 0.0375 0.395 4.985 2.854 294.884 0.563 12.693 4.389 0.32 156559. 0.2719
|
|
39.86 0.5261 0.7375 0.0499 0.0356 0.375 4.731 2.605 279.882 0.535 11.585 4.221 0.32 156950. 0.2498
|
|
41.96 0.5538 0.7449 0.0450 0.0335 0.353 4.449 2.350 263.214 0.503 10.454 4.050 0.32 157357. 0.2277
|
|
44.05 0.5815 0.7480 0.0400 0.0311 0.328 4.140 2.091 244.882 0.468 9.301 3.873 0.32 157780. 0.2054
|
|
46.15 0.6092 0.7458 0.0350 0.0286 0.302 3.802 1.828 224.896 0.430 8.130 3.686 0.32 158220. 0.1828
|
|
48.25 0.6369 0.7369 0.0299 0.0258 0.273 3.436 1.561 203.270 0.388 6.944 3.484 0.32 158675. 0.1596
|
|
50.35 0.6646 0.7184 0.0247 0.0229 0.241 3.043 1.292 180.031 0.344 5.746 3.255 0.32 159147. 0.1357
|
|
52.44 0.6923 0.6856 0.0195 0.0197 0.208 2.624 1.021 155.219 0.296 4.539 2.982 0.32 159636. 0.1105
|
|
54.54 0.7199 0.6295 0.0143 0.0164 0.173 2.179 0.748 128.894 0.246 3.328 2.633 0.33 160140. 0.0835
|
|
56.64 0.7476 0.5298 0.0091 0.0129 0.136 1.710 0.476 101.141 0.193 2.116 2.133 0.33 160660. 0.0540
|
|
58.74 0.7753 0.3313 0.0039 0.0092 0.097 1.218 0.204 72.063 0.138 0.909 1.286 0.33 161194. 0.0213
|
|
60.83 0.8030
|
|
|
|
|
|
|
|
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 0.1096 0.0401 0.731 7.678 8.239 545.072 0.868 36.649 6.856 0.38 182625. 0.7217
|
|
2.50 0.0275 0.0727 0.1082 0.0409 0.745 7.829 8.137 555.751 0.885 36.191 6.641 0.38 182769. 0.6947
|
|
5.00 0.0550 0.1408 0.1067 0.0417 0.759 7.975 8.023 566.090 0.901 35.685 6.428 0.38 182928. 0.6677
|
|
7.50 0.0824 0.2044 0.1050 0.0424 0.772 8.113 7.897 575.890 0.917 35.126 6.220 0.38 183101. 0.6410
|
|
9.99 0.1099 0.2636 0.1032 0.0430 0.784 8.240 7.759 584.948 0.931 34.510 6.016 0.38 183290. 0.6145
|
|
12.49 0.1374 0.3186 0.1012 0.0436 0.795 8.354 7.607 593.047 0.944 33.834 5.818 0.38 183496. 0.5884
|
|
14.99 0.1649 0.3697 0.0990 0.0441 0.805 8.452 7.440 599.963 0.955 33.095 5.625 0.38 183718. 0.5627
|
|
17.49 0.1924 0.4169 0.0965 0.0445 0.812 8.529 7.259 605.457 0.964 32.288 5.438 0.38 183958. 0.5373
|
|
19.99 0.2199 0.4606 0.0939 0.0448 0.817 8.583 7.062 609.287 0.970 31.411 5.257 0.38 184215. 0.5123
|
|
22.49 0.2473 0.5010 0.0911 0.0450 0.820 8.610 6.848 611.208 0.973 30.461 5.082 0.38 184490. 0.4877
|
|
24.98 0.2748 0.5381 0.0880 0.0450 0.819 8.607 6.618 610.970 0.972 29.435 4.913 0.38 184784. 0.4635
|
|
27.48 0.3023 0.5722 0.0847 0.0448 0.816 8.570 6.370 608.332 0.968 28.332 4.749 0.38 185096. 0.4396
|
|
29.98 0.3298 0.6034 0.0812 0.0444 0.809 8.495 6.104 603.066 0.960 27.151 4.591 0.38 185426. 0.4160
|
|
32.48 0.3573 0.6319 0.0774 0.0438 0.798 8.382 5.821 594.981 0.947 25.893 4.438 0.38 185776. 0.3927
|
|
34.98 0.3848 0.6577 0.0734 0.0430 0.783 8.226 5.522 583.970 0.929 24.562 4.289 0.38 186144. 0.3696
|
|
37.48 0.4122 0.6809 0.0693 0.0419 0.764 8.030 5.208 570.012 0.907 23.167 4.144 0.38 186531. 0.3469
|
|
39.97 0.4397 0.7015 0.0649 0.0407 0.742 7.792 4.882 553.119 0.880 21.714 4.003 0.38 186937. 0.3244
|
|
42.47 0.4672 0.7195 0.0604 0.0392 0.715 7.513 4.544 533.312 0.849 20.210 3.864 0.38 187362. 0.3021
|
|
44.97 0.4947 0.7347 0.0558 0.0376 0.685 7.193 4.195 510.608 0.813 18.661 3.727 0.39 187806. 0.2799
|
|
47.47 0.5222 0.7470 0.0511 0.0357 0.650 6.832 3.838 485.014 0.772 17.073 3.589 0.39 188270. 0.2579
|
|
49.97 0.5497 0.7559 0.0462 0.0336 0.612 6.431 3.473 456.537 0.727 15.449 3.451 0.39 188752. 0.2358
|
|
52.47 0.5771 0.7610 0.0412 0.0313 0.570 5.990 3.101 425.185 0.677 13.795 3.308 0.39 189254. 0.2137
|
|
54.97 0.6046 0.7613 0.0362 0.0288 0.524 5.508 2.723 390.970 0.622 12.114 3.160 0.39 189774. 0.1912
|
|
57.46 0.6321 0.7556 0.0311 0.0260 0.475 4.986 2.340 353.915 0.563 10.410 2.999 0.39 190314. 0.1683
|
|
59.96 0.6596 0.7416 0.0260 0.0231 0.421 4.424 1.953 314.060 0.500 8.688 2.821 0.39 190873. 0.1446
|
|
62.46 0.6871 0.7151 0.0208 0.0200 0.364 3.824 1.563 271.471 0.432 6.953 2.612 0.39 191451. 0.1197
|
|
64.96 0.7146 0.6686 0.0156 0.0166 0.303 3.187 1.171 226.243 0.360 5.209 2.348 0.39 192048. 0.0932
|
|
67.46 0.7420 0.5850 0.0104 0.0131 0.239 2.515 0.779 178.512 0.284 3.463 1.978 0.39 192664. 0.0640
|
|
69.96 0.7695 0.4194 0.0052 0.0095 0.172 1.810 0.387 128.453 0.204 1.723 1.368 0.39 193297. 0.0312
|
|
72.45 0.7970 -0.0060 0.0000 0.0056 0.102 1.070 -0.003 75.981 0.121 -0.014 -0.019 0.39 193921. 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 0.1103 0.0401 1.159 10.438 11.289 864.453 1.179 50.212 5.923 0.44 213049. 0.7298
|
|
2.93 0.0276 0.0737 0.1090 0.0409 1.183 10.649 11.150 881.896 1.203 49.594 5.734 0.44 213219. 0.7022
|
|
5.86 0.0553 0.1426 0.1074 0.0416 1.205 10.853 10.996 898.790 1.226 48.908 5.549 0.44 213405. 0.6748
|
|
8.79 0.0829 0.2069 0.1058 0.0424 1.227 11.046 10.825 914.807 1.248 48.149 5.367 0.44 213609. 0.6476
|
|
11.73 0.1106 0.2668 0.1039 0.0431 1.247 11.225 10.636 929.610 1.268 47.311 5.190 0.44 213832. 0.6207
|
|
14.66 0.1382 0.3224 0.1019 0.0437 1.264 11.384 10.429 942.844 1.286 46.388 5.017 0.44 214074. 0.5942
|
|
17.59 0.1658 0.3739 0.0997 0.0442 1.280 11.521 10.201 954.133 1.302 45.376 4.850 0.44 214336. 0.5680
|
|
20.52 0.1935 0.4217 0.0973 0.0446 1.292 11.629 9.953 963.089 1.314 44.270 4.687 0.45 214619. 0.5423
|
|
23.45 0.2211 0.4658 0.0946 0.0449 1.300 11.704 9.682 969.314 1.322 43.065 4.530 0.45 214922. 0.5170
|
|
26.38 0.2488 0.5065 0.0917 0.0451 1.304 11.741 9.388 972.401 1.327 41.758 4.379 0.45 215246. 0.4920
|
|
29.32 0.2764 0.5440 0.0886 0.0450 1.303 11.736 9.070 971.949 1.326 40.345 4.233 0.45 215593. 0.4675
|
|
32.25 0.3040 0.5784 0.0853 0.0448 1.298 11.683 8.728 967.560 1.320 38.823 4.092 0.45 215961. 0.4433
|
|
35.18 0.3317 0.6100 0.0817 0.0444 1.286 11.578 8.362 958.865 1.308 37.192 3.955 0.45 216351. 0.4194
|
|
38.11 0.3593 0.6388 0.0779 0.0438 1.268 11.417 7.971 945.554 1.290 35.453 3.823 0.45 216763. 0.3959
|
|
41.04 0.3870 0.6649 0.0738 0.0430 1.244 11.199 7.557 927.463 1.265 33.614 3.696 0.45 217198. 0.3726
|
|
43.97 0.4146 0.6885 0.0696 0.0419 1.213 10.922 7.123 904.558 1.234 31.683 3.572 0.45 217654. 0.3496
|
|
46.90 0.4422 0.7096 0.0652 0.0406 1.176 10.588 6.671 876.864 1.196 29.673 3.451 0.45 218133. 0.3269
|
|
49.84 0.4699 0.7280 0.0606 0.0391 1.132 10.196 6.203 844.417 1.152 27.593 3.332 0.45 218635. 0.3044
|
|
52.77 0.4975 0.7437 0.0559 0.0374 1.083 9.747 5.722 807.242 1.101 25.450 3.215 0.45 219159. 0.2820
|
|
55.70 0.5252 0.7565 0.0511 0.0355 1.026 9.241 5.228 765.355 1.044 23.253 3.098 0.45 219705. 0.2598
|
|
58.63 0.5528 0.7660 0.0461 0.0333 0.964 8.679 4.723 718.767 0.981 21.006 2.980 0.45 220274. 0.2375
|
|
61.56 0.5804 0.7717 0.0411 0.0309 0.895 8.060 4.208 667.488 0.911 18.718 2.859 0.45 220866. 0.2151
|
|
64.49 0.6081 0.7728 0.0360 0.0283 0.820 7.384 3.685 611.544 0.834 16.392 2.733 0.45 221480. 0.1924
|
|
67.43 0.6357 0.7678 0.0308 0.0255 0.739 6.653 3.155 550.973 0.752 14.035 2.598 0.45 222117. 0.1692
|
|
70.36 0.6634 0.7544 0.0256 0.0225 0.652 5.866 2.620 485.846 0.663 11.653 2.446 0.45 222776. 0.1452
|
|
73.29 0.6910 0.7282 0.0203 0.0193 0.558 5.026 2.080 416.274 0.568 9.252 2.266 0.45 223457. 0.1199
|
|
76.22 0.7186 0.6808 0.0150 0.0159 0.459 4.135 1.538 342.423 0.467 6.841 2.037 0.46 224161. 0.0927
|
|
79.15 0.7463 0.5924 0.0097 0.0123 0.355 3.194 0.996 264.524 0.361 4.429 1.707 0.46 224887. 0.0625
|
|
82.08 0.7739 0.4063 0.0044 0.0085 0.245 2.208 0.455 182.876 0.249 2.025 1.129 0.46 225633. 0.0279
|
|
85.01 0.8016
|
|
|
|
|
|
|
|
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 0.1112 0.0402 1.735 13.673 14.857 1294.140 1.545 66.084 5.207 0.51 243467. 0.7360
|
|
3.33 0.0275 0.0737 0.1098 0.0410 1.771 13.954 14.680 1320.714 1.576 65.296 5.041 0.51 243660. 0.7084
|
|
6.67 0.0550 0.1426 0.1083 0.0418 1.806 14.226 14.483 1346.482 1.607 64.418 4.879 0.51 243872. 0.6809
|
|
10.00 0.0825 0.2069 0.1067 0.0426 1.838 14.484 14.264 1370.939 1.636 63.445 4.719 0.51 244105. 0.6536
|
|
13.34 0.1100 0.2668 0.1049 0.0433 1.869 14.724 14.021 1393.578 1.663 62.367 4.564 0.51 244358. 0.6267
|
|
16.67 0.1375 0.3225 0.1029 0.0439 1.896 14.938 13.754 1413.864 1.688 61.178 4.412 0.51 244634. 0.6001
|
|
20.01 0.1650 0.3741 0.1007 0.0444 1.919 15.121 13.460 1431.230 1.708 59.872 4.266 0.51 244932. 0.5739
|
|
23.34 0.1926 0.4220 0.0983 0.0449 1.938 15.268 13.139 1445.093 1.725 58.441 4.124 0.51 245253. 0.5482
|
|
26.67 0.2201 0.4662 0.0957 0.0452 1.951 15.371 12.788 1454.858 1.737 56.880 3.987 0.51 245598. 0.5228
|
|
30.01 0.2476 0.5071 0.0928 0.0453 1.958 15.424 12.406 1459.917 1.743 55.184 3.854 0.51 245967. 0.4979
|
|
33.34 0.2751 0.5448 0.0897 0.0453 1.957 15.422 11.994 1459.669 1.742 53.348 3.727 0.51 246360. 0.4733
|
|
36.68 0.3026 0.5795 0.0864 0.0451 1.949 15.357 11.549 1453.522 1.735 51.369 3.604 0.51 246779. 0.4491
|
|
40.01 0.3301 0.6113 0.0828 0.0447 1.932 15.224 11.072 1440.923 1.720 49.246 3.485 0.51 247222. 0.4253
|
|
43.35 0.3576 0.6405 0.0790 0.0441 1.906 15.018 10.562 1421.401 1.697 46.980 3.370 0.51 247690. 0.4017
|
|
46.68 0.3851 0.6670 0.0750 0.0433 1.870 14.735 10.023 1394.689 1.665 44.580 3.259 0.51 248184. 0.3784
|
|
50.01 0.4126 0.6911 0.0707 0.0422 1.825 14.376 9.456 1360.724 1.624 42.059 3.152 0.51 248702. 0.3554
|
|
53.35 0.4401 0.7127 0.0663 0.0410 1.770 13.941 8.865 1319.546 1.575 39.431 3.047 0.51 249246. 0.3327
|
|
56.68 0.4676 0.7317 0.0617 0.0395 1.705 13.431 8.253 1271.209 1.517 36.709 2.945 0.51 249816. 0.3102
|
|
60.02 0.4951 0.7482 0.0570 0.0377 1.630 12.845 7.622 1215.758 1.451 33.904 2.844 0.51 250410. 0.2879
|
|
63.35 0.5226 0.7619 0.0522 0.0358 1.546 12.184 6.975 1153.219 1.377 31.025 2.743 0.51 251030. 0.2657
|
|
66.68 0.5502 0.7725 0.0472 0.0336 1.453 11.449 6.313 1083.614 1.293 28.081 2.643 0.52 251676. 0.2435
|
|
70.02 0.5777 0.7796 0.0422 0.0313 1.350 10.639 5.639 1006.958 1.202 25.080 2.540 0.52 252346. 0.2212
|
|
73.35 0.6052 0.7824 0.0371 0.0287 1.238 9.755 4.953 923.286 1.102 22.029 2.433 0.52 253043. 0.1986
|
|
76.69 0.6327 0.7796 0.0318 0.0258 1.117 8.797 4.257 832.652 0.994 18.936 2.319 0.52 253764. 0.1755
|
|
80.02 0.6602 0.7692 0.0266 0.0228 0.986 7.767 3.554 735.156 0.878 15.808 2.193 0.52 254512. 0.1516
|
|
83.36 0.6877 0.7473 0.0213 0.0196 0.846 6.666 2.845 630.955 0.753 12.654 2.045 0.52 255284. 0.1265
|
|
86.69 0.7152 0.7064 0.0160 0.0161 0.698 5.497 2.132 520.284 0.621 9.484 1.859 0.52 256082. 0.0995
|
|
90.02 0.7427 0.6294 0.0106 0.0125 0.541 4.263 1.419 403.480 0.482 6.310 1.595 0.52 256904. 0.0697
|
|
93.36 0.7702 0.4671 0.0053 0.0087 0.377 2.969 0.707 280.977 0.335 3.145 1.141 0.52 257750. 0.0352
|
|
96.69 0.7977 -0.0054 0.0000 0.0047 0.204 1.610 -0.004 152.381 0.182 -0.019 -0.013 0.52 258574. 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 0.1121 0.0404 2.487 17.419 18.968 1854.783 1.968 84.369 4.638 0.57 273878. 0.7408
|
|
3.75 0.0275 0.0739 0.1108 0.0413 2.540 17.785 18.749 1893.774 2.009 83.395 4.490 0.57 274095. 0.7131
|
|
7.51 0.0550 0.1430 0.1094 0.0421 2.590 18.140 18.504 1931.603 2.049 82.307 4.345 0.57 274334. 0.6855
|
|
11.26 0.0826 0.2075 0.1078 0.0429 2.639 18.478 18.231 1967.542 2.088 81.093 4.203 0.57 274596. 0.6581
|
|
15.01 0.1101 0.2675 0.1060 0.0436 2.683 18.791 17.928 2000.830 2.123 79.746 4.064 0.57 274882. 0.6311
|
|
18.77 0.1376 0.3233 0.1040 0.0443 2.723 19.071 17.593 2030.678 2.155 78.254 3.930 0.57 275192. 0.6044
|
|
22.52 0.1651 0.3751 0.1018 0.0448 2.757 19.311 17.223 2056.259 2.182 76.609 3.799 0.57 275529. 0.5782
|
|
26.27 0.1927 0.4231 0.0994 0.0453 2.785 19.503 16.817 2076.716 2.203 74.802 3.673 0.57 275891. 0.5524
|
|
30.03 0.2202 0.4675 0.0968 0.0456 2.804 19.639 16.373 2091.181 2.219 72.826 3.551 0.57 276281. 0.5270
|
|
33.78 0.2477 0.5085 0.0939 0.0458 2.815 19.710 15.889 2098.775 2.227 70.675 3.434 0.57 276698. 0.5020
|
|
37.53 0.2752 0.5464 0.0908 0.0458 2.814 19.709 15.365 2098.617 2.227 68.342 3.321 0.57 277142. 0.4774
|
|
41.29 0.3028 0.5813 0.0875 0.0456 2.803 19.627 14.798 2089.863 2.217 65.824 3.212 0.57 277614. 0.4531
|
|
45.04 0.3303 0.6134 0.0839 0.0452 2.778 19.456 14.190 2071.708 2.198 63.118 3.107 0.57 278115. 0.4292
|
|
48.79 0.3578 0.6429 0.0800 0.0445 2.740 19.191 13.540 2043.475 2.168 60.226 3.005 0.57 278644. 0.4056
|
|
52.55 0.3853 0.6698 0.0760 0.0437 2.688 18.828 12.851 2004.768 2.127 57.160 2.907 0.58 279201. 0.3822
|
|
56.30 0.4129 0.6942 0.0717 0.0426 2.622 18.365 12.126 1955.499 2.075 53.936 2.813 0.58 279786. 0.3592
|
|
60.05 0.4404 0.7162 0.0672 0.0413 2.542 17.804 11.370 1895.730 2.011 50.573 2.720 0.58 280400. 0.3364
|
|
63.81 0.4679 0.7357 0.0626 0.0398 2.448 17.144 10.586 1825.547 1.937 47.087 2.630 0.58 281042. 0.3138
|
|
67.56 0.4954 0.7528 0.0578 0.0380 2.340 16.388 9.778 1745.024 1.852 43.494 2.542 0.58 281713. 0.2915
|
|
71.31 0.5230 0.7671 0.0529 0.0361 2.218 15.535 8.949 1654.208 1.755 39.804 2.454 0.58 282412. 0.2692
|
|
75.07 0.5505 0.7785 0.0479 0.0339 2.083 14.586 8.100 1553.132 1.648 36.029 2.366 0.58 283140. 0.2469
|
|
78.82 0.5780 0.7864 0.0428 0.0314 1.934 13.541 7.235 1441.824 1.530 32.180 2.276 0.58 283896. 0.2245
|
|
82.57 0.6055 0.7903 0.0376 0.0288 1.771 12.400 6.355 1320.334 1.401 28.266 2.183 0.58 284681. 0.2018
|
|
86.33 0.6331 0.7887 0.0323 0.0259 1.594 11.164 5.462 1188.742 1.261 24.296 2.084 0.58 285495. 0.1786
|
|
90.08 0.6606 0.7799 0.0270 0.0228 1.404 9.835 4.559 1047.194 1.111 20.280 1.975 0.58 286337. 0.1546
|
|
93.83 0.6881 0.7599 0.0216 0.0195 1.201 8.414 3.649 895.916 0.951 16.230 1.847 0.58 287207. 0.1294
|
|
97.59 0.7156 0.7214 0.0162 0.0160 0.986 6.905 2.734 735.250 0.780 12.159 1.686 0.59 288106. 0.1022
|
|
101.34 0.7432 0.6472 0.0107 0.0123 0.759 5.313 1.817 565.685 0.600 8.081 1.457 0.59 289033. 0.0720
|
|
105.09 0.7707 0.4862 0.0053 0.0085 0.520 3.643 0.902 387.860 0.412 4.014 1.055 0.59 289985. 0.0368
|
|
108.85 0.7982 -0.0141 -0.0001 0.0044 0.269 1.887 -0.013 200.934 0.213 -0.058 -0.030 0.59 290902. 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 0.1132 0.0408 3.447 21.723 23.649 2570.075 2.454 105.192 4.174 0.63 304279. 0.7443
|
|
4.17 0.0275 0.0739 0.1120 0.0417 3.521 22.190 23.388 2625.377 2.507 104.029 4.041 0.63 304520. 0.7166
|
|
8.35 0.0551 0.1430 0.1106 0.0426 3.593 22.645 23.094 2679.135 2.558 102.721 3.910 0.63 304786. 0.6890
|
|
12.52 0.0826 0.2075 0.1090 0.0434 3.661 23.077 22.764 2730.274 2.607 101.256 3.782 0.63 305077. 0.6617
|
|
16.69 0.1102 0.2676 0.1072 0.0441 3.725 23.478 22.397 2777.701 2.653 99.620 3.657 0.64 305396. 0.6347
|
|
20.86 0.1377 0.3234 0.1053 0.0448 3.782 23.838 21.988 2820.273 2.693 97.800 3.536 0.64 305742. 0.6081
|
|
25.04 0.1652 0.3753 0.1031 0.0454 3.831 24.146 21.535 2856.796 2.728 95.786 3.419 0.64 306117. 0.5819
|
|
29.21 0.1928 0.4233 0.1007 0.0459 3.870 24.394 21.035 2886.062 2.756 93.566 3.306 0.64 306521. 0.5560
|
|
33.38 0.2203 0.4678 0.0981 0.0462 3.898 24.569 20.488 2906.844 2.776 91.130 3.197 0.64 306956. 0.5307
|
|
37.55 0.2479 0.5090 0.0952 0.0464 3.913 24.663 19.890 2917.902 2.786 88.470 3.092 0.64 307421. 0.5057
|
|
41.73 0.2754 0.5471 0.0921 0.0464 3.913 24.664 19.240 2918.019 2.787 85.579 2.991 0.64 307917. 0.4811
|
|
45.90 0.3029 0.5822 0.0888 0.0462 3.897 24.562 18.537 2906.006 2.775 82.451 2.893 0.64 308444. 0.4568
|
|
50.07 0.3305 0.6145 0.0851 0.0458 3.863 24.349 17.780 2880.745 2.751 79.084 2.799 0.64 309002. 0.4329
|
|
54.24 0.3580 0.6442 0.0813 0.0452 3.810 24.015 16.970 2841.297 2.713 75.482 2.709 0.64 309592. 0.4092
|
|
58.42 0.3856 0.6714 0.0771 0.0443 3.738 23.557 16.110 2787.098 2.661 71.656 2.622 0.64 310213. 0.3859
|
|
62.59 0.4131 0.6962 0.0728 0.0432 3.645 22.973 15.204 2718.029 2.596 67.629 2.537 0.64 310866. 0.3628
|
|
66.76 0.4406 0.7186 0.0683 0.0419 3.533 22.265 14.259 2634.187 2.515 63.425 2.455 0.64 311550. 0.3400
|
|
70.93 0.4682 0.7386 0.0636 0.0403 3.400 21.432 13.279 2535.713 2.421 59.063 2.375 0.64 312266. 0.3174
|
|
75.11 0.4957 0.7562 0.0587 0.0385 3.249 20.477 12.267 2422.722 2.314 54.564 2.297 0.64 313013. 0.2950
|
|
79.28 0.5232 0.7711 0.0538 0.0365 3.078 19.400 11.228 2295.298 2.192 49.942 2.219 0.64 313792. 0.2726
|
|
83.45 0.5508 0.7832 0.0487 0.0342 2.888 18.202 10.164 2153.493 2.056 45.211 2.141 0.64 314603. 0.2503
|
|
87.63 0.5783 0.7920 0.0435 0.0317 2.678 16.882 9.079 1997.352 1.907 40.385 2.062 0.65 315445. 0.2278
|
|
91.80 0.6059 0.7969 0.0382 0.0290 2.450 15.442 7.976 1826.948 1.745 35.475 1.980 0.65 316319. 0.2051
|
|
95.97 0.6334 0.7966 0.0328 0.0261 2.202 13.882 6.856 1642.398 1.568 30.493 1.893 0.65 317225. 0.1818
|
|
100.14 0.6609 0.7892 0.0274 0.0229 1.936 12.204 5.722 1443.899 1.379 25.453 1.798 0.65 318162. 0.1577
|
|
104.32 0.6885 0.7711 0.0219 0.0196 1.652 10.411 4.579 1231.770 1.176 20.367 1.686 0.65 319131. 0.1323
|
|
108.49 0.7160 0.7350 0.0164 0.0160 1.350 8.507 3.429 1006.492 0.961 15.253 1.545 0.65 320131. 0.1049
|
|
112.66 0.7436 0.6635 0.0109 0.0122 1.031 6.498 2.277 768.750 0.734 10.128 1.343 0.65 321162. 0.0743
|
|
116.83 0.7711 0.5043 0.0054 0.0083 0.697 4.391 1.128 519.451 0.496 5.016 0.985 0.65 322222. 0.0383
|
|
121.01 0.7986 -0.0237 -0.0001 0.0041 0.345 2.172 -0.025 256.985 0.245 -0.112 -0.045 0.65 323227. 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 0.1145 0.0416 4.675 26.787 28.932 3486.122 3.026 128.690 3.764 0.70 334668. 0.7425
|
|
4.60 0.0276 0.0736 0.1133 0.0425 4.774 27.353 28.630 3559.842 3.090 127.344 3.648 0.70 334934. 0.7158
|
|
9.21 0.0552 0.1426 0.1119 0.0434 4.870 27.905 28.287 3631.645 3.153 125.818 3.533 0.70 335227. 0.6891
|
|
13.81 0.0829 0.2070 0.1104 0.0442 4.962 28.431 27.899 3700.108 3.212 124.096 3.420 0.70 335549. 0.6625
|
|
18.41 0.1105 0.2671 0.1087 0.0449 5.047 28.920 27.464 3763.767 3.267 122.159 3.310 0.70 335901. 0.6361
|
|
23.02 0.1381 0.3231 0.1067 0.0456 5.124 29.360 26.976 3821.060 3.317 119.991 3.202 0.70 336284. 0.6099
|
|
27.62 0.1657 0.3751 0.1046 0.0462 5.190 29.739 26.434 3870.353 3.360 117.576 3.098 0.70 336700. 0.5841
|
|
32.22 0.1933 0.4233 0.1022 0.0467 5.243 30.044 25.832 3909.954 3.394 114.901 2.997 0.70 337148. 0.5585
|
|
36.82 0.2209 0.4680 0.0996 0.0470 5.281 30.260 25.169 3938.129 3.419 111.953 2.899 0.70 337630. 0.5333
|
|
41.43 0.2486 0.5093 0.0967 0.0472 5.301 30.375 24.443 3953.131 3.432 108.721 2.804 0.70 338145. 0.5085
|
|
46.03 0.2762 0.5476 0.0936 0.0472 5.301 30.376 23.650 3953.200 3.432 105.196 2.713 0.70 338695. 0.4839
|
|
50.63 0.3038 0.5829 0.0902 0.0470 5.279 30.249 22.791 3936.633 3.417 101.372 2.626 0.70 339280. 0.4597
|
|
55.24 0.3314 0.6154 0.0865 0.0466 5.232 29.981 21.863 3901.836 3.387 97.247 2.541 0.70 339899. 0.4358
|
|
59.84 0.3590 0.6454 0.0826 0.0459 5.160 29.563 20.869 3847.456 3.340 92.824 2.460 0.70 340553. 0.4122
|
|
64.44 0.3867 0.6729 0.0784 0.0450 5.059 28.989 19.811 3772.734 3.275 88.121 2.382 0.70 341242. 0.3888
|
|
69.05 0.4143 0.6980 0.0740 0.0439 4.932 28.258 18.697 3677.517 3.193 83.163 2.306 0.70 341966. 0.3657
|
|
73.65 0.4419 0.7208 0.0694 0.0425 4.777 27.370 17.532 3561.971 3.092 77.981 2.232 0.71 342724. 0.3428
|
|
78.25 0.4695 0.7412 0.0646 0.0409 4.595 26.327 16.322 3426.308 2.974 72.602 2.161 0.71 343518. 0.3201
|
|
82.85 0.4971 0.7593 0.0596 0.0391 4.386 25.132 15.074 3270.714 2.839 67.048 2.090 0.71 344346. 0.2976
|
|
87.46 0.5247 0.7748 0.0546 0.0370 4.151 23.784 13.791 3095.332 2.687 61.340 2.021 0.71 345209. 0.2752
|
|
92.06 0.5524 0.7875 0.0494 0.0346 3.889 22.285 12.477 2900.243 2.518 55.496 1.951 0.71 346107. 0.2528
|
|
96.66 0.5800 0.7970 0.0441 0.0321 3.601 20.635 11.135 2685.530 2.331 49.530 1.881 0.71 347040. 0.2302
|
|
101.27 0.6076 0.8026 0.0387 0.0293 3.287 18.835 9.770 2451.295 2.128 43.458 1.808 0.71 348008. 0.2072
|
|
105.87 0.6352 0.8032 0.0332 0.0262 2.947 16.887 8.385 2197.706 1.908 37.296 1.730 0.71 349010. 0.1838
|
|
110.47 0.6628 0.7967 0.0276 0.0230 2.582 14.792 6.982 1925.076 1.671 31.058 1.645 0.71 350047. 0.1594
|
|
115.08 0.6905 0.7796 0.0220 0.0195 2.191 12.555 5.567 1633.919 1.418 24.762 1.545 0.71 351119. 0.1337
|
|
119.68 0.7181 0.7441 0.0164 0.0158 1.777 10.181 4.143 1325.031 1.150 18.428 1.418 0.72 352226. 0.1059
|
|
124.28 0.7457 0.6715 0.0107 0.0119 1.340 7.681 2.716 999.580 0.868 12.081 1.232 0.72 353366. 0.0745
|
|
128.88 0.7733 0.5023 0.0051 0.0079 0.884 5.065 1.292 659.123 0.572 5.747 0.889 0.72 354538. 0.0371
|
|
133.49 0.8009
|
|
|
|
|
|
|
|
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 0.1158 0.0437 6.367 33.444 34.840 4748.243 3.779 154.970 3.328 0.76 365045. 0.7204
|
|
5.01 0.0275 0.0710 0.1147 0.0445 6.487 34.071 34.506 4837.166 3.849 153.481 3.236 0.76 365332. 0.6970
|
|
10.01 0.0551 0.1380 0.1135 0.0453 6.602 34.675 34.122 4922.947 3.918 151.776 3.144 0.76 365650. 0.6735
|
|
15.02 0.0826 0.2010 0.1120 0.0460 6.710 35.245 33.685 5003.837 3.982 149.832 3.053 0.76 366000. 0.6499
|
|
20.02 0.1101 0.2602 0.1104 0.0467 6.810 35.767 33.190 5078.040 4.041 147.628 2.964 0.76 366383. 0.6263
|
|
25.03 0.1376 0.3157 0.1085 0.0473 6.898 36.230 32.630 5143.681 4.093 145.139 2.877 0.76 366800. 0.6028
|
|
30.03 0.1652 0.3676 0.1064 0.0478 6.972 36.618 32.002 5198.824 4.137 142.346 2.792 0.76 367252. 0.5792
|
|
35.04 0.1927 0.4160 0.1041 0.0482 7.029 36.919 31.302 5241.479 4.171 139.230 2.709 0.76 367740. 0.5558
|
|
40.04 0.2202 0.4612 0.1015 0.0485 7.067 37.117 30.525 5269.636 4.193 135.776 2.627 0.76 368265. 0.5323
|
|
45.05 0.2478 0.5032 0.0987 0.0486 7.082 37.198 29.669 5281.220 4.203 131.970 2.548 0.76 368827. 0.5090
|
|
50.05 0.2753 0.5422 0.0955 0.0485 7.073 37.149 28.732 5274.142 4.197 127.800 2.471 0.76 369426. 0.4857
|
|
55.06 0.3028 0.5783 0.0921 0.0483 7.035 36.952 27.711 5246.296 4.175 123.260 2.396 0.77 370063. 0.4625
|
|
60.06 0.3303 0.6116 0.0885 0.0478 6.967 36.596 26.607 5195.658 4.135 118.347 2.323 0.77 370738. 0.4394
|
|
65.07 0.3579 0.6423 0.0845 0.0471 6.867 36.066 25.419 5120.395 4.075 113.064 2.252 0.77 371451. 0.4163
|
|
70.07 0.3854 0.6705 0.0803 0.0462 6.731 35.354 24.152 5019.295 3.994 107.430 2.183 0.77 372202. 0.3934
|
|
75.08 0.4129 0.6962 0.0759 0.0450 6.560 34.456 22.815 4891.920 3.893 101.479 2.115 0.77 372990. 0.3705
|
|
80.08 0.4405 0.7197 0.0712 0.0436 6.354 33.374 21.414 4738.249 3.771 95.248 2.050 0.77 373816. 0.3479
|
|
85.09 0.4680 0.7407 0.0664 0.0419 6.113 32.107 19.957 4558.353 3.627 88.769 1.986 0.77 374679. 0.3253
|
|
90.09 0.4955 0.7595 0.0614 0.0400 5.837 30.655 18.451 4352.287 3.463 82.072 1.923 0.77 375580. 0.3029
|
|
95.10 0.5230 0.7758 0.0562 0.0379 5.525 29.020 16.902 4120.112 3.279 75.181 1.861 0.77 376519. 0.2805
|
|
100.10 0.5506 0.7893 0.0509 0.0355 5.179 27.202 15.315 3861.932 3.073 68.119 1.799 0.77 377495. 0.2581
|
|
105.11 0.5781 0.7998 0.0455 0.0329 4.798 25.202 13.693 3577.962 2.847 60.905 1.736 0.77 378509. 0.2355
|
|
110.11 0.6056 0.8066 0.0400 0.0301 4.383 23.022 12.040 3268.523 2.601 53.556 1.671 0.78 379561. 0.2126
|
|
115.12 0.6332 0.8084 0.0345 0.0270 3.935 20.667 10.362 2934.136 2.335 46.090 1.602 0.78 380650. 0.1891
|
|
120.12 0.6607 0.8033 0.0288 0.0237 3.454 18.141 8.662 2575.577 2.050 38.527 1.525 0.78 381776. 0.1646
|
|
125.13 0.6882 0.7874 0.0231 0.0202 2.942 15.454 6.944 2194.015 1.746 30.885 1.435 0.78 382940. 0.1387
|
|
130.13 0.7157 0.7531 0.0173 0.0165 2.402 12.616 5.213 1791.112 1.425 23.188 1.320 0.78 384141. 0.1105
|
|
135.14 0.7433 0.6823 0.0116 0.0126 1.836 9.643 3.476 1369.112 1.090 15.463 1.152 0.78 385379. 0.0787
|
|
140.15 0.7708 0.5211 0.0058 0.0086 1.248 6.557 1.741 930.894 0.741 7.742 0.848 0.78 386651. 0.0410
|
|
145.15 0.7983 -0.0008 0.0000 0.0044 0.638 3.350 -0.001 475.551 0.378 -0.006 -0.001 0.79 387869. 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 0.1172 0.0484 8.970 43.488 41.377 6688.700 4.913 184.044 2.806 0.83 395406. 0.6619
|
|
5.43 0.0275 0.0652 0.1162 0.0491 9.103 44.132 41.022 6787.813 4.986 182.464 2.741 0.83 395715. 0.6438
|
|
10.85 0.0551 0.1274 0.1151 0.0498 9.226 44.732 40.609 6879.982 5.054 180.630 2.677 0.83 396058. 0.6257
|
|
16.28 0.0826 0.1866 0.1137 0.0504 9.337 45.270 40.133 6962.754 5.115 178.511 2.614 0.83 396436. 0.6074
|
|
21.70 0.1102 0.2429 0.1122 0.0509 9.433 45.732 39.586 7033.899 5.167 176.077 2.553 0.83 396850. 0.5890
|
|
27.13 0.1377 0.2964 0.1104 0.0513 9.509 46.105 38.960 7091.223 5.209 173.295 2.492 0.83 397302. 0.5704
|
|
32.55 0.1653 0.3471 0.1084 0.0516 9.565 46.374 38.251 7132.626 5.239 170.139 2.432 0.83 397794. 0.5517
|
|
37.98 0.1928 0.3952 0.1061 0.0518 9.596 46.527 37.452 7156.029 5.257 166.584 2.374 0.83 398325. 0.5327
|
|
43.41 0.2204 0.4407 0.1036 0.0518 9.601 46.548 36.558 7159.404 5.259 162.608 2.316 0.83 398896. 0.5135
|
|
48.83 0.2479 0.4836 0.1008 0.0517 9.576 46.427 35.565 7140.770 5.245 158.193 2.259 0.83 399508. 0.4941
|
|
54.26 0.2755 0.5239 0.0977 0.0513 9.519 46.150 34.470 7098.139 5.214 153.325 2.203 0.83 400162. 0.4743
|
|
59.68 0.3030 0.5617 0.0943 0.0508 9.427 45.704 33.272 7029.528 5.164 147.994 2.147 0.83 400856. 0.4541
|
|
65.11 0.3305 0.5970 0.0906 0.0502 9.297 45.076 31.969 6932.949 5.093 142.199 2.091 0.83 401592. 0.4337
|
|
70.53 0.3581 0.6298 0.0866 0.0492 9.128 44.254 30.563 6806.559 5.000 135.942 2.037 0.83 402369. 0.4129
|
|
75.96 0.3856 0.6601 0.0823 0.0481 8.917 43.231 29.058 6649.117 4.884 129.248 1.982 0.83 403187. 0.3918
|
|
81.39 0.4132 0.6880 0.0778 0.0467 8.663 42.003 27.463 6460.279 4.745 122.157 1.928 0.83 404046. 0.3706
|
|
86.81 0.4407 0.7134 0.0731 0.0451 8.368 40.572 25.790 6240.176 4.584 114.714 1.875 0.83 404946. 0.3491
|
|
92.24 0.4683 0.7364 0.0681 0.0433 8.031 38.938 24.047 5988.938 4.399 106.962 1.821 0.83 405886. 0.3275
|
|
97.66 0.4958 0.7569 0.0630 0.0413 7.653 37.102 22.243 5706.510 4.192 98.937 1.768 0.84 406867. 0.3058
|
|
103.09 0.5234 0.7748 0.0578 0.0390 7.232 35.063 20.384 5392.835 3.961 90.669 1.714 0.84 407888. 0.2839
|
|
108.51 0.5509 0.7895 0.0523 0.0365 6.772 32.831 18.477 5049.619 3.709 82.184 1.660 0.84 408950. 0.2616
|
|
113.94 0.5785 0.8003 0.0468 0.0338 6.273 30.415 16.525 4678.005 3.436 73.504 1.602 0.84 410053. 0.2389
|
|
119.37 0.6060 0.8064 0.0412 0.0309 5.737 27.815 14.535 4278.085 3.143 64.652 1.541 0.84 411196. 0.2155
|
|
124.79 0.6336 0.8065 0.0354 0.0278 5.162 25.027 12.512 3849.312 2.828 55.652 1.474 0.84 412379. 0.1912
|
|
130.22 0.6611 0.7980 0.0296 0.0246 4.551 22.066 10.460 3393.815 2.493 46.525 1.398 0.84 413603. 0.1658
|
|
135.64 0.6886 0.7760 0.0238 0.0211 3.908 18.948 8.385 2914.333 2.141 37.295 1.305 0.84 414867. 0.1386
|
|
141.07 0.7162 0.7311 0.0178 0.0175 3.238 15.698 6.293 2414.429 1.774 27.989 1.182 0.85 416171. 0.1087
|
|
146.49 0.7437 0.6431 0.0119 0.0137 2.546 12.343 4.191 1898.394 1.394 18.641 1.001 0.85 417515. 0.0752
|
|
151.92 0.7713 0.4601 0.0059 0.0099 1.839 8.916 2.089 1371.299 1.007 9.290 0.691 0.85 418895. 0.0366
|
|
157.34 0.7988 -0.0077 -0.0001 0.0060 1.117 5.415 -0.020 832.835 0.612 -0.091 -0.011 0.85 420229. 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 0.1178 0.0557 12.903 58.091 48.211 9621.995 6.563 214.441 2.273 0.89 425791. 0.5787
|
|
5.86 0.0276 0.0572 0.1169 0.0565 13.074 58.857 47.867 9748.946 6.650 212.912 2.227 0.89 426118. 0.5650
|
|
11.71 0.0552 0.1121 0.1159 0.0571 13.228 59.552 47.462 9864.009 6.728 211.109 2.182 0.89 426482. 0.5514
|
|
17.57 0.0828 0.1648 0.1148 0.0577 13.359 60.143 46.984 9961.940 6.795 208.985 2.139 0.89 426883. 0.5377
|
|
23.43 0.1105 0.2154 0.1134 0.0581 13.462 60.606 46.424 10038.602 6.847 206.496 2.098 0.89 427325. 0.5241
|
|
29.29 0.1381 0.2642 0.1118 0.0584 13.530 60.914 45.772 10089.564 6.882 203.595 2.058 0.89 427809. 0.5105
|
|
35.14 0.1657 0.3111 0.1100 0.0586 13.559 61.044 45.018 10111.057 6.897 200.239 2.019 0.89 428337. 0.4969
|
|
41.00 0.1933 0.3564 0.1079 0.0585 13.545 60.978 44.152 10100.160 6.889 196.388 1.983 0.89 428909. 0.4832
|
|
46.86 0.2209 0.4000 0.1055 0.0582 13.484 60.704 43.168 10054.852 6.858 192.012 1.947 0.89 429525. 0.4692
|
|
52.71 0.2485 0.4420 0.1027 0.0578 13.375 60.215 42.060 9973.791 6.803 187.084 1.913 0.89 430188. 0.4549
|
|
58.57 0.2761 0.4824 0.0997 0.0571 13.217 59.504 40.824 9856.060 6.723 181.585 1.879 0.89 430896. 0.4402
|
|
64.43 0.3037 0.5211 0.0964 0.0562 13.009 58.568 39.457 9700.936 6.617 175.504 1.845 0.89 431649. 0.4250
|
|
70.29 0.3314 0.5580 0.0927 0.0551 12.750 57.401 37.957 9507.741 6.485 168.834 1.811 0.89 432448. 0.4091
|
|
76.14 0.3590 0.5930 0.0887 0.0537 12.439 56.001 36.327 9275.777 6.327 161.583 1.776 0.89 433292. 0.3926
|
|
82.00 0.3866 0.6260 0.0845 0.0522 12.076 54.365 34.572 9004.807 6.142 153.776 1.741 0.90 434181. 0.3755
|
|
87.86 0.4142 0.6570 0.0799 0.0504 11.661 52.498 32.703 8695.530 5.931 145.462 1.706 0.90 435115. 0.3577
|
|
93.72 0.4418 0.6859 0.0751 0.0484 11.197 50.408 30.733 8349.363 5.695 136.699 1.670 0.90 436092. 0.3394
|
|
99.57 0.4694 0.7125 0.0700 0.0461 10.685 48.103 28.674 7967.530 5.435 127.540 1.632 0.90 437114. 0.3205
|
|
105.43 0.4970 0.7368 0.0648 0.0437 10.126 45.587 26.537 7550.846 5.150 118.035 1.594 0.90 438179. 0.3011
|
|
111.29 0.5246 0.7584 0.0594 0.0411 9.521 42.863 24.331 7099.612 4.843 108.223 1.554 0.90 439288. 0.2812
|
|
117.14 0.5523 0.7767 0.0539 0.0383 8.873 39.945 22.063 6616.430 4.513 98.138 1.512 0.90 440441. 0.2605
|
|
123.00 0.5799 0.7901 0.0482 0.0354 8.195 36.894 19.740 6111.054 4.168 87.805 1.465 0.90 441637. 0.2387
|
|
128.86 0.6075 0.7939 0.0424 0.0325 7.515 33.833 17.363 5603.955 3.822 77.232 1.405 0.90 442877. 0.2148
|
|
134.72 0.6351 0.7869 0.0365 0.0295 6.820 30.706 14.940 5085.954 3.469 66.455 1.332 0.91 444160. 0.1889
|
|
140.57 0.6627 0.7675 0.0305 0.0263 6.096 27.445 12.482 4545.831 3.101 55.518 1.245 0.91 445486. 0.1614
|
|
146.43 0.6903 0.7296 0.0244 0.0231 5.349 24.081 9.994 3988.621 2.721 44.454 1.137 0.91 446856. 0.1318
|
|
152.29 0.7179 0.6629 0.0183 0.0198 4.587 20.651 7.488 3420.530 2.333 33.305 0.993 0.91 448268. 0.0996
|
|
158.14 0.7455 0.5491 0.0121 0.0165 3.820 17.197 4.973 2848.463 1.943 22.122 0.792 0.91 449722. 0.0648
|
|
164.00 0.7732 0.3529 0.0060 0.0132 3.057 13.761 2.466 2279.244 1.555 10.969 0.491 0.92 451217. 0.0283
|
|
169.86 0.8008 -0.0065 -0.0001 0.0099 2.294 10.329 -0.033 1710.916 1.167 -0.147 -0.009 0.92 452695. 0.0000
|
|
|
|
|
|
|