686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
12x8E (12x8E.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 0.1070 0.0511 0.001 0.065 0.071 0.764 0.007 0.314 41.984 0.05 14797. 0.5458
|
|
0.32 0.0277 0.0566 0.1057 0.0518 0.001 0.065 0.070 0.773 0.007 0.311 40.999 0.05 14809. 0.5299
|
|
0.63 0.0555 0.1105 0.1044 0.0524 0.001 0.066 0.069 0.782 0.007 0.307 40.004 0.05 14822. 0.5137
|
|
0.95 0.0832 0.1616 0.1029 0.0530 0.001 0.067 0.068 0.791 0.008 0.302 39.002 0.05 14836. 0.4973
|
|
1.26 0.1109 0.2099 0.1013 0.0535 0.001 0.068 0.067 0.799 0.008 0.298 37.998 0.05 14852. 0.4806
|
|
1.58 0.1386 0.2555 0.0995 0.0540 0.001 0.068 0.066 0.806 0.008 0.292 36.996 0.05 14868. 0.4638
|
|
1.89 0.1664 0.2983 0.0975 0.0544 0.001 0.069 0.064 0.812 0.008 0.287 35.997 0.05 14887. 0.4468
|
|
2.21 0.1941 0.3385 0.0954 0.0547 0.001 0.069 0.063 0.817 0.008 0.280 35.005 0.05 14906. 0.4297
|
|
2.52 0.2218 0.3759 0.0930 0.0549 0.001 0.069 0.061 0.820 0.008 0.273 34.021 0.05 14927. 0.4125
|
|
2.84 0.2495 0.4108 0.0905 0.0550 0.001 0.069 0.060 0.821 0.008 0.266 33.045 0.05 14950. 0.3951
|
|
3.15 0.2773 0.4431 0.0877 0.0549 0.001 0.069 0.058 0.820 0.008 0.258 32.078 0.05 14974. 0.3777
|
|
3.47 0.3050 0.4728 0.0848 0.0547 0.001 0.069 0.056 0.816 0.008 0.249 31.117 0.05 15000. 0.3601
|
|
3.78 0.3327 0.4999 0.0816 0.0543 0.001 0.069 0.054 0.810 0.008 0.240 30.161 0.05 15028. 0.3424
|
|
4.10 0.3604 0.5244 0.0781 0.0537 0.001 0.068 0.052 0.802 0.008 0.230 29.205 0.05 15057. 0.3244
|
|
4.41 0.3882 0.5462 0.0744 0.0529 0.001 0.067 0.049 0.790 0.008 0.219 28.244 0.05 15088. 0.3063
|
|
4.73 0.4159 0.5650 0.0705 0.0519 0.001 0.066 0.047 0.775 0.007 0.207 27.271 0.05 15120. 0.2879
|
|
5.04 0.4436 0.5807 0.0664 0.0507 0.001 0.064 0.044 0.757 0.007 0.195 26.278 0.05 15154. 0.2691
|
|
5.36 0.4713 0.5930 0.0620 0.0493 0.001 0.062 0.041 0.736 0.007 0.182 25.254 0.05 15190. 0.2500
|
|
5.67 0.4991 0.6013 0.0574 0.0477 0.001 0.060 0.038 0.712 0.007 0.169 24.185 0.05 15227. 0.2304
|
|
5.99 0.5268 0.6051 0.0527 0.0458 0.001 0.058 0.035 0.685 0.007 0.155 23.058 0.05 15266. 0.2103
|
|
6.30 0.5545 0.6037 0.0477 0.0438 0.001 0.055 0.032 0.655 0.006 0.140 21.854 0.05 15306. 0.1898
|
|
6.62 0.5823 0.5961 0.0427 0.0417 0.001 0.053 0.028 0.622 0.006 0.125 20.551 0.05 15348. 0.1687
|
|
6.93 0.6100 0.5811 0.0375 0.0393 0.001 0.050 0.025 0.587 0.006 0.110 19.123 0.05 15392. 0.1472
|
|
7.25 0.6377 0.5571 0.0322 0.0369 0.001 0.047 0.021 0.551 0.005 0.095 17.536 0.05 15437. 0.1251
|
|
7.56 0.6654 0.5219 0.0269 0.0343 0.001 0.043 0.018 0.512 0.005 0.079 15.742 0.05 15484. 0.1026
|
|
7.88 0.6932 0.4724 0.0215 0.0316 0.001 0.040 0.014 0.471 0.005 0.063 13.681 0.05 15533. 0.0798
|
|
8.19 0.7209 0.4046 0.0161 0.0287 0.001 0.036 0.011 0.429 0.004 0.047 11.265 0.05 15583. 0.0569
|
|
8.51 0.7486 0.3121 0.0108 0.0258 0.001 0.033 0.007 0.386 0.004 0.032 8.369 0.05 15635. 0.0345
|
|
8.82 0.7763 0.1858 0.0055 0.0229 0.000 0.029 0.004 0.341 0.003 0.016 4.804 0.05 15688. 0.0141
|
|
9.14 0.8041 0.0109 0.0003 0.0198 0.000 0.025 0.000 0.296 0.003 0.001 0.271 0.05 15743. 0.0002
|
|
|
|
|
|
|
|
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 0.1073 0.0465 0.007 0.235 0.284 5.559 0.027 1.262 23.151 0.10 29595. 0.6030
|
|
0.64 0.0280 0.0628 0.1061 0.0472 0.008 0.238 0.280 5.641 0.027 1.248 22.551 0.10 29618. 0.5840
|
|
1.27 0.0559 0.1223 0.1048 0.0479 0.008 0.242 0.277 5.722 0.027 1.232 21.948 0.10 29644. 0.5647
|
|
1.91 0.0839 0.1784 0.1033 0.0486 0.008 0.245 0.273 5.800 0.028 1.214 21.346 0.10 29673. 0.5453
|
|
2.54 0.1118 0.2312 0.1016 0.0492 0.008 0.248 0.269 5.874 0.028 1.195 20.747 0.10 29704. 0.5258
|
|
3.18 0.1398 0.2807 0.0998 0.0497 0.008 0.251 0.264 5.940 0.028 1.174 20.152 0.10 29738. 0.5062
|
|
3.81 0.1677 0.3270 0.0979 0.0502 0.008 0.253 0.259 5.998 0.029 1.151 19.565 0.10 29775. 0.4866
|
|
4.45 0.1957 0.3702 0.0957 0.0506 0.008 0.255 0.253 6.045 0.029 1.125 18.986 0.10 29815. 0.4670
|
|
5.08 0.2236 0.4104 0.0934 0.0509 0.008 0.257 0.247 6.078 0.029 1.098 18.417 0.10 29857. 0.4474
|
|
5.72 0.2516 0.4477 0.0908 0.0510 0.008 0.258 0.240 6.096 0.029 1.068 17.858 0.10 29903. 0.4278
|
|
6.35 0.2796 0.4821 0.0880 0.0510 0.008 0.258 0.233 6.096 0.029 1.035 17.309 0.10 29953. 0.4082
|
|
6.99 0.3075 0.5138 0.0850 0.0509 0.008 0.257 0.225 6.076 0.029 0.999 16.771 0.10 30005. 0.3887
|
|
7.62 0.3355 0.5428 0.0817 0.0505 0.008 0.255 0.216 6.034 0.029 0.961 16.240 0.10 30061. 0.3691
|
|
8.26 0.3634 0.5691 0.0782 0.0500 0.008 0.252 0.207 5.968 0.028 0.920 15.717 0.10 30120. 0.3495
|
|
8.89 0.3914 0.5927 0.0745 0.0492 0.008 0.248 0.197 5.878 0.028 0.876 15.198 0.10 30182. 0.3298
|
|
9.53 0.4193 0.6133 0.0706 0.0482 0.008 0.244 0.186 5.762 0.028 0.829 14.680 0.10 30248. 0.3100
|
|
10.17 0.4473 0.6310 0.0664 0.0470 0.008 0.237 0.175 5.619 0.027 0.780 14.158 0.10 30317. 0.2899
|
|
10.80 0.4752 0.6453 0.0619 0.0456 0.007 0.230 0.164 5.448 0.026 0.728 13.628 0.10 30389. 0.2696
|
|
11.44 0.5032 0.6560 0.0573 0.0439 0.007 0.222 0.151 5.249 0.025 0.673 13.083 0.10 30465. 0.2489
|
|
12.07 0.5312 0.6624 0.0524 0.0421 0.007 0.212 0.139 5.024 0.024 0.617 12.516 0.10 30544. 0.2279
|
|
12.71 0.5591 0.6639 0.0475 0.0400 0.006 0.202 0.125 4.775 0.023 0.558 11.917 0.10 30626. 0.2064
|
|
13.34 0.5871 0.6595 0.0424 0.0377 0.006 0.190 0.112 4.504 0.022 0.498 11.274 0.10 30712. 0.1844
|
|
13.98 0.6150 0.6479 0.0371 0.0353 0.006 0.178 0.098 4.211 0.020 0.437 10.572 0.10 30800. 0.1620
|
|
14.61 0.6430 0.6273 0.0318 0.0326 0.005 0.165 0.084 3.899 0.019 0.374 9.791 0.10 30892. 0.1389
|
|
15.25 0.6709 0.5951 0.0265 0.0299 0.005 0.151 0.070 3.570 0.017 0.312 8.901 0.10 30988. 0.1152
|
|
15.88 0.6989 0.5474 0.0211 0.0270 0.004 0.136 0.056 3.223 0.015 0.248 7.861 0.10 31086. 0.0908
|
|
16.52 0.7268 0.4783 0.0158 0.0240 0.004 0.121 0.042 2.862 0.014 0.185 6.604 0.10 31188. 0.0659
|
|
17.15 0.7548 0.3781 0.0104 0.0208 0.003 0.105 0.028 2.490 0.012 0.123 5.028 0.10 31293. 0.0408
|
|
17.79 0.7828 0.2302 0.0052 0.0176 0.003 0.089 0.014 2.107 0.010 0.061 2.951 0.10 31401. 0.0169
|
|
18.43 0.8107 0.0027 0.0000 0.0144 0.002 0.073 0.000 1.718 0.008 0.001 0.033 0.10 31512. 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 0.1076 0.0445 0.024 0.506 0.640 17.955 0.057 2.846 16.164 0.14 44391. 0.6323
|
|
0.96 0.0280 0.0659 0.1064 0.0453 0.024 0.514 0.633 18.246 0.058 2.814 15.726 0.14 44427. 0.6116
|
|
1.91 0.0561 0.1282 0.1050 0.0460 0.025 0.522 0.625 18.533 0.059 2.778 15.287 0.14 44466. 0.5907
|
|
2.87 0.0841 0.1867 0.1035 0.0467 0.025 0.530 0.616 18.810 0.060 2.739 14.849 0.14 44509. 0.5698
|
|
3.82 0.1122 0.2417 0.1019 0.0473 0.026 0.537 0.606 19.071 0.061 2.696 14.415 0.14 44556. 0.5487
|
|
4.78 0.1402 0.2931 0.1001 0.0479 0.026 0.544 0.595 19.309 0.061 2.648 13.986 0.14 44607. 0.5277
|
|
5.74 0.1683 0.3411 0.0981 0.0484 0.026 0.550 0.584 19.519 0.062 2.596 13.563 0.14 44663. 0.5067
|
|
6.69 0.1963 0.3858 0.0960 0.0488 0.026 0.555 0.571 19.690 0.063 2.539 13.149 0.14 44723. 0.4858
|
|
7.65 0.2244 0.4273 0.0936 0.0492 0.027 0.558 0.557 19.817 0.063 2.476 12.743 0.14 44788. 0.4649
|
|
8.61 0.2524 0.4658 0.0910 0.0493 0.027 0.560 0.541 19.891 0.063 2.408 12.346 0.14 44857. 0.4442
|
|
9.56 0.2805 0.5013 0.0882 0.0494 0.027 0.561 0.525 19.903 0.063 2.334 11.958 0.14 44931. 0.4236
|
|
10.52 0.3085 0.5339 0.0852 0.0492 0.027 0.559 0.507 19.847 0.063 2.254 11.580 0.14 45010. 0.4030
|
|
11.47 0.3366 0.5638 0.0819 0.0489 0.026 0.555 0.487 19.715 0.063 2.167 11.209 0.14 45094. 0.3826
|
|
12.43 0.3646 0.5910 0.0784 0.0484 0.026 0.549 0.466 19.502 0.062 2.074 10.846 0.14 45184. 0.3622
|
|
13.39 0.3927 0.6155 0.0747 0.0476 0.026 0.541 0.444 19.202 0.061 1.975 10.488 0.14 45278. 0.3417
|
|
14.34 0.4207 0.6371 0.0707 0.0467 0.025 0.530 0.420 18.812 0.060 1.869 10.133 0.14 45377. 0.3212
|
|
15.30 0.4488 0.6559 0.0664 0.0455 0.025 0.516 0.395 18.329 0.058 1.758 9.779 0.14 45481. 0.3006
|
|
16.25 0.4768 0.6714 0.0620 0.0440 0.024 0.500 0.369 17.748 0.056 1.640 9.422 0.14 45590. 0.2797
|
|
17.21 0.5049 0.6834 0.0573 0.0423 0.023 0.481 0.341 17.069 0.054 1.516 9.057 0.14 45704. 0.2586
|
|
18.17 0.5329 0.6914 0.0525 0.0404 0.022 0.459 0.312 16.299 0.052 1.388 8.681 0.14 45823. 0.2371
|
|
19.12 0.5609 0.6948 0.0474 0.0383 0.021 0.435 0.282 15.442 0.049 1.255 8.287 0.15 45947. 0.2152
|
|
20.08 0.5890 0.6925 0.0423 0.0360 0.019 0.409 0.252 14.506 0.046 1.119 7.867 0.15 46076. 0.1930
|
|
21.04 0.6170 0.6834 0.0371 0.0335 0.018 0.380 0.221 13.496 0.043 0.981 7.411 0.15 46210. 0.1702
|
|
21.99 0.6451 0.6656 0.0318 0.0308 0.017 0.350 0.189 12.415 0.040 0.840 6.903 0.15 46349. 0.1467
|
|
22.95 0.6731 0.6362 0.0264 0.0280 0.015 0.317 0.157 11.269 0.036 0.699 6.324 0.15 46493. 0.1226
|
|
23.90 0.7012 0.5912 0.0210 0.0250 0.013 0.284 0.125 10.064 0.032 0.557 5.641 0.15 46641. 0.0976
|
|
24.86 0.7292 0.5236 0.0157 0.0218 0.012 0.248 0.093 8.807 0.028 0.415 4.804 0.15 46795. 0.0717
|
|
25.82 0.7573 0.4216 0.0104 0.0186 0.010 0.211 0.062 7.507 0.024 0.274 3.725 0.15 46953. 0.0452
|
|
26.77 0.7853 0.2632 0.0051 0.0153 0.008 0.174 0.031 6.172 0.020 0.136 2.243 0.15 47117. 0.0192
|
|
27.73 0.8134 0.0011 0.0000 0.0119 0.006 0.136 0.000 4.814 0.015 0.000 0.009 0.15 47284. 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 0.1078 0.0434 0.056 0.876 1.140 41.471 0.099 5.071 12.470 0.19 59188. 0.6511
|
|
1.30 0.0285 0.0688 0.1066 0.0441 0.057 0.891 1.127 42.190 0.101 5.013 12.117 0.19 59236. 0.6290
|
|
2.59 0.0570 0.1336 0.1052 0.0449 0.058 0.906 1.113 42.899 0.102 4.949 11.764 0.19 59289. 0.6068
|
|
3.89 0.0855 0.1945 0.1037 0.0456 0.058 0.921 1.097 43.585 0.104 4.878 11.413 0.19 59348. 0.5845
|
|
5.18 0.1140 0.2514 0.1021 0.0463 0.059 0.935 1.079 44.232 0.106 4.800 11.066 0.19 59412. 0.5621
|
|
6.48 0.1425 0.3046 0.1002 0.0469 0.060 0.947 1.060 44.824 0.107 4.714 10.724 0.19 59482. 0.5398
|
|
7.77 0.1710 0.3540 0.0982 0.0474 0.061 0.958 1.039 45.342 0.108 4.619 10.389 0.19 59557. 0.5177
|
|
9.07 0.1995 0.4000 0.0960 0.0479 0.061 0.967 1.015 45.768 0.109 4.515 10.060 0.19 59639. 0.4956
|
|
10.36 0.2280 0.4425 0.0936 0.0482 0.062 0.974 0.989 46.081 0.110 4.401 9.739 0.19 59728. 0.4737
|
|
11.66 0.2565 0.4819 0.0909 0.0484 0.062 0.978 0.961 46.260 0.110 4.277 9.427 0.19 59823. 0.4520
|
|
12.96 0.2850 0.5181 0.0880 0.0484 0.062 0.978 0.931 46.287 0.111 4.141 9.123 0.19 59924. 0.4304
|
|
14.25 0.3135 0.5515 0.0849 0.0483 0.062 0.975 0.898 46.141 0.110 3.994 8.827 0.19 60033. 0.4090
|
|
15.55 0.3420 0.5819 0.0816 0.0479 0.061 0.968 0.862 45.805 0.109 3.835 8.538 0.19 60148. 0.3877
|
|
16.84 0.3705 0.6096 0.0779 0.0474 0.061 0.956 0.824 45.266 0.108 3.665 8.256 0.19 60270. 0.3664
|
|
18.14 0.3990 0.6345 0.0741 0.0466 0.060 0.941 0.783 44.509 0.106 3.483 7.979 0.19 60399. 0.3453
|
|
19.43 0.4275 0.6565 0.0699 0.0455 0.058 0.920 0.739 43.526 0.104 3.289 7.706 0.19 60535. 0.3240
|
|
20.73 0.4560 0.6755 0.0656 0.0443 0.057 0.894 0.693 42.308 0.101 3.084 7.434 0.19 60678. 0.3027
|
|
22.02 0.4845 0.6914 0.0610 0.0427 0.055 0.863 0.645 40.845 0.098 2.868 7.160 0.19 60828. 0.2811
|
|
23.32 0.5130 0.7036 0.0562 0.0410 0.052 0.827 0.594 39.140 0.093 2.642 6.882 0.19 60984. 0.2593
|
|
24.62 0.5415 0.7118 0.0512 0.0389 0.050 0.786 0.541 37.209 0.089 2.407 6.596 0.19 61148. 0.2372
|
|
25.91 0.5700 0.7151 0.0460 0.0367 0.047 0.741 0.487 35.067 0.084 2.165 6.295 0.19 61318. 0.2148
|
|
27.21 0.5986 0.7127 0.0408 0.0342 0.044 0.692 0.431 32.727 0.078 1.918 5.975 0.19 61495. 0.1918
|
|
28.50 0.6271 0.7029 0.0354 0.0316 0.041 0.638 0.375 30.202 0.072 1.666 5.625 0.19 61679. 0.1683
|
|
29.80 0.6556 0.6837 0.0300 0.0288 0.037 0.581 0.317 27.502 0.066 1.411 5.233 0.19 61869. 0.1442
|
|
31.09 0.6841 0.6516 0.0246 0.0258 0.033 0.521 0.260 24.643 0.059 1.155 4.780 0.19 62067. 0.1191
|
|
32.39 0.7126 0.6012 0.0191 0.0226 0.029 0.457 0.202 21.641 0.052 0.899 4.234 0.20 62271. 0.0930
|
|
33.68 0.7411 0.5231 0.0137 0.0194 0.025 0.391 0.145 18.513 0.044 0.643 3.542 0.20 62482. 0.0659
|
|
34.98 0.7696 0.3998 0.0083 0.0160 0.020 0.323 0.088 15.283 0.036 0.391 2.607 0.20 62699. 0.0378
|
|
36.28 0.7981 0.1940 0.0030 0.0125 0.016 0.253 0.032 11.978 0.029 0.143 1.220 0.20 62923. 0.0107
|
|
37.57 0.8266
|
|
|
|
|
|
|
|
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 0.1081 0.0427 0.107 1.347 1.786 79.654 0.152 7.943 10.169 0.24 73984. 0.6645
|
|
1.62 0.0286 0.0703 0.1069 0.0434 0.109 1.371 1.766 81.088 0.155 7.853 9.876 0.24 74044. 0.6416
|
|
3.25 0.0571 0.1364 0.1055 0.0442 0.111 1.395 1.743 82.505 0.158 7.753 9.582 0.24 74111. 0.6186
|
|
4.87 0.0857 0.1984 0.1040 0.0449 0.112 1.418 1.718 83.876 0.160 7.643 9.292 0.24 74184. 0.5955
|
|
6.49 0.1143 0.2563 0.1023 0.0456 0.114 1.440 1.691 85.173 0.163 7.521 9.004 0.24 74264. 0.5725
|
|
8.12 0.1428 0.3103 0.1005 0.0463 0.116 1.460 1.661 86.362 0.165 7.386 8.721 0.24 74352. 0.5495
|
|
9.74 0.1714 0.3605 0.0985 0.0468 0.117 1.478 1.627 87.407 0.167 7.238 8.444 0.24 74447. 0.5267
|
|
11.36 0.2000 0.4071 0.0963 0.0473 0.118 1.492 1.591 88.269 0.169 7.075 8.173 0.24 74550. 0.5040
|
|
12.99 0.2286 0.4503 0.0938 0.0476 0.119 1.503 1.550 88.909 0.170 6.896 7.909 0.24 74661. 0.4815
|
|
14.61 0.2571 0.4901 0.0912 0.0478 0.120 1.509 1.506 89.285 0.171 6.701 7.653 0.24 74780. 0.4593
|
|
16.23 0.2857 0.5269 0.0883 0.0479 0.120 1.511 1.459 89.358 0.171 6.488 7.404 0.24 74908. 0.4372
|
|
17.86 0.3143 0.5606 0.0852 0.0477 0.119 1.506 1.407 89.090 0.170 6.257 7.162 0.24 75044. 0.4154
|
|
19.48 0.3428 0.5915 0.0818 0.0474 0.119 1.495 1.351 88.445 0.169 6.008 6.927 0.24 75189. 0.3936
|
|
21.10 0.3714 0.6196 0.0781 0.0468 0.117 1.477 1.291 87.395 0.167 5.740 6.698 0.24 75342. 0.3720
|
|
22.73 0.4000 0.6449 0.0742 0.0460 0.115 1.452 1.226 85.913 0.164 5.454 6.474 0.24 75504. 0.3505
|
|
24.35 0.4285 0.6675 0.0701 0.0450 0.113 1.420 1.158 83.981 0.160 5.150 6.253 0.24 75675. 0.3290
|
|
25.97 0.4571 0.6870 0.0657 0.0437 0.109 1.379 1.085 81.579 0.156 4.827 6.034 0.24 75854. 0.3074
|
|
27.60 0.4857 0.7035 0.0611 0.0422 0.106 1.330 1.009 78.690 0.150 4.487 5.815 0.24 76042. 0.2856
|
|
29.22 0.5142 0.7164 0.0562 0.0404 0.101 1.273 0.929 75.319 0.144 4.131 5.593 0.24 76239. 0.2636
|
|
30.84 0.5428 0.7254 0.0512 0.0383 0.096 1.209 0.846 71.497 0.137 3.762 5.365 0.24 76444. 0.2413
|
|
32.47 0.5714 0.7298 0.0460 0.0360 0.090 1.137 0.760 67.252 0.128 3.382 5.128 0.24 76657. 0.2186
|
|
34.09 0.6000 0.7286 0.0407 0.0335 0.084 1.058 0.673 62.610 0.120 2.993 4.875 0.24 76880. 0.1956
|
|
35.71 0.6285 0.7202 0.0354 0.0309 0.077 0.974 0.584 57.595 0.110 2.598 4.600 0.24 77110. 0.1719
|
|
37.33 0.6571 0.7026 0.0299 0.0280 0.070 0.883 0.494 52.232 0.100 2.199 4.292 0.24 77350. 0.1476
|
|
38.96 0.6857 0.6721 0.0244 0.0249 0.062 0.787 0.404 46.548 0.089 1.796 3.935 0.24 77597. 0.1223
|
|
40.58 0.7142 0.6233 0.0190 0.0217 0.054 0.686 0.313 40.575 0.077 1.394 3.503 0.24 77854. 0.0959
|
|
42.20 0.7428 0.5458 0.0135 0.0184 0.046 0.581 0.223 34.352 0.066 0.994 2.950 0.24 78118. 0.0682
|
|
43.83 0.7714 0.4199 0.0081 0.0150 0.037 0.472 0.135 27.926 0.053 0.598 2.185 0.25 78391. 0.0392
|
|
45.45 0.7999 0.2011 0.0029 0.0114 0.029 0.361 0.047 21.351 0.041 0.211 1.009 0.25 78672. 0.0108
|
|
47.07 0.8285
|
|
|
|
|
|
|
|
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 0.1084 0.0422 0.183 1.918 2.579 136.126 0.217 11.470 8.592 0.29 88778. 0.6747
|
|
1.94 0.0284 0.0709 0.1072 0.0430 0.186 1.953 2.550 138.633 0.221 11.341 8.342 0.29 88851. 0.6514
|
|
3.88 0.0569 0.1376 0.1058 0.0438 0.189 1.988 2.518 141.113 0.225 11.199 8.093 0.29 88930. 0.6279
|
|
5.82 0.0853 0.2001 0.1043 0.0445 0.192 2.022 2.482 143.517 0.228 11.042 7.845 0.29 89018. 0.6044
|
|
7.76 0.1138 0.2585 0.1027 0.0452 0.196 2.054 2.443 145.795 0.232 10.868 7.601 0.29 89114. 0.5810
|
|
9.70 0.1422 0.3130 0.1009 0.0459 0.198 2.083 2.400 147.890 0.235 10.676 7.361 0.29 89218. 0.5576
|
|
11.64 0.1707 0.3636 0.0989 0.0464 0.201 2.109 2.353 149.740 0.238 10.464 7.126 0.29 89332. 0.5344
|
|
13.58 0.1991 0.4105 0.0967 0.0469 0.203 2.131 2.300 151.279 0.241 10.232 6.897 0.29 89455. 0.5115
|
|
15.52 0.2276 0.4540 0.0943 0.0473 0.204 2.147 2.243 152.436 0.243 9.976 6.674 0.29 89587. 0.4887
|
|
17.46 0.2560 0.4942 0.0916 0.0475 0.205 2.157 2.180 153.142 0.244 9.697 6.457 0.29 89729. 0.4662
|
|
19.40 0.2845 0.5312 0.0888 0.0475 0.206 2.160 2.112 153.327 0.244 9.393 6.247 0.29 89881. 0.4439
|
|
21.34 0.3129 0.5653 0.0856 0.0474 0.205 2.154 2.038 152.925 0.243 9.063 6.043 0.29 90044. 0.4218
|
|
23.28 0.3414 0.5965 0.0823 0.0471 0.204 2.139 1.957 151.876 0.242 8.706 5.846 0.29 90216. 0.3999
|
|
25.22 0.3698 0.6250 0.0787 0.0465 0.201 2.115 1.871 150.126 0.239 8.323 5.654 0.29 90399. 0.3782
|
|
27.16 0.3983 0.6507 0.0748 0.0458 0.198 2.080 1.779 147.632 0.235 7.914 5.466 0.29 90592. 0.3565
|
|
29.10 0.4267 0.6737 0.0707 0.0448 0.194 2.034 1.681 144.359 0.230 7.478 5.282 0.29 90796. 0.3349
|
|
31.03 0.4552 0.6939 0.0663 0.0435 0.188 1.976 1.577 140.272 0.223 7.016 5.100 0.29 91009. 0.3132
|
|
32.97 0.4836 0.7110 0.0617 0.0420 0.181 1.907 1.468 135.341 0.215 6.528 4.919 0.29 91233. 0.2914
|
|
34.91 0.5121 0.7249 0.0569 0.0402 0.174 1.825 1.353 129.570 0.206 6.018 4.736 0.29 91467. 0.2694
|
|
36.85 0.5405 0.7350 0.0519 0.0381 0.165 1.733 1.234 123.007 0.196 5.488 4.549 0.29 91712. 0.2471
|
|
38.79 0.5690 0.7408 0.0467 0.0359 0.155 1.630 1.111 115.702 0.184 4.942 4.356 0.29 91967. 0.2245
|
|
40.73 0.5974 0.7413 0.0414 0.0334 0.144 1.517 0.986 107.700 0.171 4.385 4.151 0.29 92231. 0.2015
|
|
42.67 0.6259 0.7352 0.0361 0.0307 0.133 1.395 0.858 99.042 0.158 3.817 3.930 0.29 92506. 0.1780
|
|
44.61 0.6543 0.7204 0.0306 0.0278 0.120 1.265 0.729 89.770 0.143 3.243 3.683 0.29 92791. 0.1538
|
|
46.55 0.6828 0.6937 0.0252 0.0248 0.107 1.126 0.599 79.930 0.127 2.664 3.399 0.29 93086. 0.1286
|
|
48.49 0.7112 0.6497 0.0197 0.0216 0.093 0.980 0.469 69.579 0.111 2.085 3.056 0.29 93391. 0.1023
|
|
50.43 0.7397 0.5789 0.0143 0.0182 0.079 0.828 0.339 58.781 0.094 1.509 2.618 0.29 93706. 0.0746
|
|
52.37 0.7681 0.4623 0.0089 0.0148 0.064 0.671 0.211 47.616 0.076 0.940 2.013 0.29 94032. 0.0453
|
|
54.31 0.7966 0.2565 0.0036 0.0112 0.049 0.510 0.086 36.177 0.058 0.382 1.077 0.29 94366. 0.0154
|
|
56.25 0.8250
|
|
|
|
|
|
|
|
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 0.1087 0.0419 0.288 2.591 3.521 214.620 0.293 15.661 7.441 0.33 103572. 0.6827
|
|
2.24 0.0282 0.0710 0.1075 0.0427 0.293 2.640 3.482 218.620 0.298 15.489 7.225 0.33 103656. 0.6592
|
|
4.48 0.0563 0.1377 0.1062 0.0435 0.298 2.688 3.439 222.581 0.304 15.299 7.009 0.33 103748. 0.6356
|
|
6.72 0.0845 0.2002 0.1048 0.0442 0.304 2.734 3.392 226.429 0.309 15.088 6.795 0.33 103849. 0.6120
|
|
8.96 0.1127 0.2587 0.1031 0.0449 0.309 2.778 3.340 230.083 0.314 14.856 6.584 0.33 103959. 0.5884
|
|
11.20 0.1408 0.3132 0.1014 0.0456 0.313 2.819 3.282 233.457 0.318 14.599 6.377 0.33 104079. 0.5649
|
|
13.44 0.1690 0.3639 0.0994 0.0462 0.317 2.855 3.219 236.453 0.323 14.317 6.174 0.33 104210. 0.5416
|
|
15.68 0.1972 0.4109 0.0972 0.0467 0.320 2.885 3.149 238.969 0.326 14.006 5.976 0.33 104351. 0.5185
|
|
17.92 0.2253 0.4545 0.0949 0.0470 0.323 2.909 3.072 240.897 0.329 13.664 5.784 0.33 104503. 0.4957
|
|
20.17 0.2535 0.4948 0.0923 0.0473 0.325 2.924 2.988 242.126 0.330 13.291 5.597 0.33 104667. 0.4731
|
|
22.41 0.2817 0.5321 0.0895 0.0474 0.325 2.929 2.897 242.547 0.331 12.884 5.417 0.33 104842. 0.4508
|
|
24.65 0.3098 0.5664 0.0864 0.0473 0.325 2.923 2.797 242.056 0.330 12.443 5.242 0.33 105028. 0.4287
|
|
26.89 0.3380 0.5979 0.0831 0.0470 0.323 2.905 2.690 240.557 0.328 11.965 5.072 0.34 105226. 0.4068
|
|
29.13 0.3662 0.6267 0.0795 0.0465 0.319 2.873 2.575 237.965 0.325 11.452 4.908 0.34 105436. 0.3850
|
|
31.37 0.3943 0.6528 0.0757 0.0457 0.314 2.828 2.451 234.212 0.320 10.903 4.747 0.34 105658. 0.3634
|
|
33.61 0.4225 0.6763 0.0716 0.0448 0.307 2.768 2.320 229.236 0.313 10.319 4.590 0.34 105891. 0.3419
|
|
35.85 0.4507 0.6971 0.0673 0.0435 0.299 2.692 2.181 222.988 0.304 9.700 4.436 0.34 106136. 0.3203
|
|
38.09 0.4788 0.7151 0.0628 0.0421 0.289 2.601 2.034 215.415 0.294 9.046 4.282 0.34 106393. 0.2986
|
|
40.33 0.5070 0.7300 0.0580 0.0403 0.277 2.494 1.880 206.507 0.282 8.361 4.128 0.34 106662. 0.2768
|
|
42.57 0.5352 0.7414 0.0531 0.0383 0.263 2.371 1.719 196.333 0.268 7.648 3.972 0.34 106942. 0.2547
|
|
44.81 0.5634 0.7488 0.0480 0.0361 0.248 2.233 1.554 184.972 0.252 6.914 3.811 0.34 107234. 0.2324
|
|
47.05 0.5915 0.7514 0.0428 0.0337 0.231 2.083 1.385 172.492 0.235 6.162 3.643 0.34 107538. 0.2096
|
|
49.29 0.6197 0.7481 0.0375 0.0310 0.213 1.919 1.213 158.959 0.217 5.396 3.462 0.34 107853. 0.1864
|
|
51.53 0.6479 0.7370 0.0321 0.0282 0.194 1.744 1.039 144.436 0.197 4.621 3.262 0.34 108180. 0.1626
|
|
53.77 0.6760 0.7154 0.0267 0.0252 0.173 1.558 0.863 128.996 0.176 3.839 3.035 0.34 108518. 0.1378
|
|
56.02 0.7042 0.6787 0.0212 0.0220 0.151 1.361 0.687 112.720 0.154 3.055 2.764 0.34 108867. 0.1120
|
|
58.26 0.7324 0.6189 0.0158 0.0187 0.128 1.156 0.511 95.707 0.131 2.274 2.423 0.34 109229. 0.0847
|
|
60.50 0.7605 0.5200 0.0104 0.0152 0.105 0.943 0.337 78.077 0.107 1.501 1.961 0.34 109601. 0.0557
|
|
62.74 0.7887 0.3468 0.0051 0.0117 0.080 0.724 0.167 59.971 0.082 0.741 1.261 0.34 109985. 0.0252
|
|
64.98 0.8169 0.0004 0.0000 0.0081 0.056 0.501 0.000 41.528 0.057 0.001 0.001 0.34 110377. 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 0.1091 0.0417 0.428 3.371 4.615 319.025 0.381 20.527 6.561 0.38 118364. 0.6892
|
|
2.56 0.0282 0.0715 0.1079 0.0425 0.436 3.435 4.565 325.085 0.388 20.305 6.369 0.38 118460. 0.6654
|
|
5.12 0.0564 0.1388 0.1066 0.0433 0.444 3.498 4.509 331.089 0.395 20.058 6.178 0.38 118565. 0.6415
|
|
7.69 0.0845 0.2018 0.1052 0.0441 0.452 3.560 4.448 336.927 0.402 19.785 5.988 0.38 118681. 0.6175
|
|
10.25 0.1127 0.2606 0.1036 0.0448 0.459 3.618 4.380 342.478 0.409 19.483 5.801 0.38 118807. 0.5937
|
|
12.81 0.1409 0.3155 0.1018 0.0455 0.466 3.673 4.305 347.609 0.415 19.149 5.617 0.38 118945. 0.5699
|
|
15.37 0.1691 0.3665 0.0998 0.0461 0.472 3.721 4.222 352.174 0.420 18.781 5.438 0.38 119095. 0.5464
|
|
17.93 0.1973 0.4138 0.0977 0.0466 0.477 3.761 4.131 356.017 0.425 18.375 5.263 0.38 119256. 0.5231
|
|
20.50 0.2255 0.4576 0.0953 0.0470 0.481 3.793 4.031 358.973 0.428 17.929 5.093 0.38 119430. 0.5000
|
|
23.06 0.2536 0.4982 0.0927 0.0472 0.484 3.813 3.921 360.878 0.431 17.442 4.928 0.38 119618. 0.4772
|
|
25.62 0.2818 0.5356 0.0899 0.0473 0.485 3.820 3.802 361.564 0.432 16.910 4.769 0.38 119818. 0.4547
|
|
28.18 0.3100 0.5702 0.0868 0.0472 0.484 3.813 3.672 360.872 0.431 16.332 4.615 0.38 120031. 0.4324
|
|
30.74 0.3382 0.6019 0.0835 0.0469 0.481 3.789 3.531 358.657 0.428 15.707 4.466 0.38 120258. 0.4103
|
|
33.31 0.3664 0.6309 0.0799 0.0464 0.476 3.748 3.380 354.791 0.424 15.034 4.321 0.38 120498. 0.3884
|
|
35.87 0.3946 0.6573 0.0761 0.0457 0.468 3.689 3.218 349.167 0.417 14.314 4.180 0.38 120752. 0.3667
|
|
38.43 0.4227 0.6812 0.0720 0.0447 0.458 3.610 3.046 341.696 0.408 13.548 4.043 0.38 121019. 0.3450
|
|
40.99 0.4509 0.7023 0.0677 0.0435 0.446 3.511 2.863 332.298 0.397 12.735 3.908 0.38 121300. 0.3233
|
|
43.55 0.4791 0.7206 0.0631 0.0420 0.430 3.390 2.670 320.896 0.383 11.877 3.774 0.39 121594. 0.3016
|
|
46.12 0.5073 0.7360 0.0583 0.0402 0.412 3.249 2.468 307.473 0.367 10.976 3.640 0.39 121901. 0.2796
|
|
48.68 0.5355 0.7479 0.0534 0.0382 0.392 3.086 2.257 292.130 0.349 10.040 3.505 0.39 122222. 0.2575
|
|
51.24 0.5636 0.7560 0.0482 0.0360 0.369 2.905 2.040 274.986 0.328 9.076 3.365 0.39 122556. 0.2351
|
|
53.80 0.5918 0.7594 0.0430 0.0335 0.343 2.706 1.818 256.145 0.306 8.088 3.220 0.39 122904. 0.2123
|
|
56.36 0.6200 0.7571 0.0376 0.0308 0.316 2.490 1.592 235.702 0.281 7.082 3.064 0.39 123264. 0.1890
|
|
58.93 0.6482 0.7471 0.0322 0.0280 0.287 2.258 1.363 213.757 0.255 6.063 2.892 0.39 123638. 0.1651
|
|
61.49 0.6764 0.7269 0.0268 0.0249 0.255 2.012 1.132 190.417 0.227 5.036 2.697 0.39 124025. 0.1403
|
|
64.05 0.7046 0.6918 0.0213 0.0217 0.222 1.752 0.901 165.808 0.198 4.006 2.464 0.39 124425. 0.1143
|
|
66.61 0.7327 0.6336 0.0158 0.0183 0.188 1.480 0.670 140.080 0.167 2.980 2.169 0.39 124838. 0.0868
|
|
69.17 0.7609 0.5357 0.0104 0.0148 0.152 1.198 0.442 113.415 0.135 1.965 1.767 0.39 125265. 0.0574
|
|
71.74 0.7891 0.3606 0.0051 0.0113 0.115 0.909 0.217 86.030 0.103 0.967 1.146 0.39 125704. 0.0261
|
|
74.30 0.8173 -0.0032 0.0000 0.0076 0.078 0.614 -0.001 58.132 0.069 -0.006 -0.010 0.39 126152. 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 0.1096 0.0417 0.608 4.258 5.864 453.426 0.481 26.083 5.866 0.43 133155. 0.6945
|
|
2.88 0.0282 0.0720 0.1084 0.0425 0.620 4.341 5.801 462.180 0.490 25.804 5.693 0.43 133263. 0.6705
|
|
5.77 0.0564 0.1396 0.1071 0.0433 0.631 4.422 5.732 470.861 0.500 25.495 5.521 0.43 133381. 0.6464
|
|
8.65 0.0846 0.2029 0.1056 0.0440 0.643 4.501 5.655 479.309 0.509 25.152 5.351 0.43 133512. 0.6222
|
|
11.53 0.1127 0.2620 0.1040 0.0448 0.654 4.577 5.569 487.349 0.517 24.773 5.183 0.43 133654. 0.5981
|
|
14.41 0.1409 0.3171 0.1023 0.0455 0.664 4.647 5.475 494.790 0.525 24.352 5.019 0.43 133809. 0.5742
|
|
17.30 0.1691 0.3684 0.1003 0.0461 0.672 4.709 5.370 501.421 0.532 23.888 4.858 0.43 133977. 0.5505
|
|
20.18 0.1973 0.4159 0.0982 0.0466 0.680 4.762 5.255 507.016 0.538 23.375 4.701 0.43 134160. 0.5270
|
|
23.06 0.2255 0.4600 0.0958 0.0470 0.686 4.802 5.129 511.339 0.543 22.812 4.549 0.43 134356. 0.5038
|
|
25.95 0.2537 0.5007 0.0932 0.0472 0.689 4.829 4.990 514.147 0.546 22.195 4.402 0.43 134567. 0.4808
|
|
28.83 0.2819 0.5383 0.0904 0.0473 0.691 4.838 4.838 515.203 0.547 21.521 4.260 0.43 134792. 0.4581
|
|
31.71 0.3101 0.5730 0.0873 0.0472 0.690 4.830 4.674 514.275 0.546 20.788 4.122 0.43 135033. 0.4357
|
|
34.59 0.3382 0.6050 0.0840 0.0470 0.685 4.800 4.495 511.151 0.542 19.995 3.989 0.43 135288. 0.4135
|
|
37.48 0.3664 0.6342 0.0804 0.0465 0.678 4.749 4.303 505.647 0.537 19.141 3.860 0.43 135559. 0.3916
|
|
40.36 0.3946 0.6609 0.0766 0.0457 0.667 4.673 4.098 497.607 0.528 18.227 3.735 0.43 135844. 0.3697
|
|
43.24 0.4228 0.6849 0.0725 0.0447 0.653 4.573 3.879 486.900 0.517 17.252 3.613 0.43 136145. 0.3479
|
|
46.12 0.4510 0.7064 0.0681 0.0435 0.635 4.446 3.646 473.414 0.502 16.218 3.493 0.43 136462. 0.3262
|
|
49.01 0.4792 0.7251 0.0635 0.0420 0.613 4.292 3.401 457.037 0.485 15.127 3.375 0.43 136793. 0.3043
|
|
51.89 0.5074 0.7409 0.0587 0.0402 0.587 4.111 3.143 437.743 0.464 13.980 3.257 0.43 137139. 0.2823
|
|
54.77 0.5356 0.7533 0.0537 0.0382 0.557 3.904 2.875 415.673 0.441 12.789 3.137 0.43 137500. 0.2601
|
|
57.66 0.5637 0.7621 0.0486 0.0359 0.524 3.672 2.599 390.996 0.415 11.560 3.015 0.44 137876. 0.2377
|
|
60.54 0.5919 0.7662 0.0433 0.0334 0.488 3.417 2.316 363.864 0.386 10.302 2.887 0.44 138268. 0.2148
|
|
63.42 0.6201 0.7648 0.0379 0.0307 0.448 3.141 2.028 334.414 0.355 9.020 2.751 0.44 138674. 0.1915
|
|
66.30 0.6483 0.7560 0.0324 0.0278 0.406 2.844 1.736 302.788 0.321 7.722 2.601 0.44 139094. 0.1676
|
|
69.19 0.6765 0.7371 0.0269 0.0247 0.361 2.528 1.442 269.141 0.286 6.414 2.430 0.44 139530. 0.1427
|
|
72.07 0.7047 0.7035 0.0214 0.0215 0.313 2.194 1.147 233.657 0.248 5.102 2.227 0.44 139980. 0.1166
|
|
74.95 0.7329 0.6470 0.0159 0.0181 0.264 1.846 0.853 196.553 0.209 3.795 1.969 0.44 140445. 0.0889
|
|
77.84 0.7611 0.5505 0.0105 0.0145 0.212 1.485 0.562 158.092 0.168 2.501 1.613 0.44 140925. 0.0592
|
|
80.72 0.7892 0.3744 0.0052 0.0109 0.159 1.114 0.277 118.592 0.126 1.231 1.058 0.44 141419. 0.0272
|
|
83.60 0.8174 -0.0042 0.0000 0.0072 0.105 0.736 -0.002 78.349 0.083 -0.009 -0.011 0.44 141924. 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 0.1100 0.0417 0.834 5.259 7.271 622.154 0.594 32.344 5.301 0.48 147944. 0.6990
|
|
3.20 0.0282 0.0722 0.1089 0.0425 0.851 5.362 7.195 634.344 0.606 32.004 5.145 0.48 148064. 0.6748
|
|
6.41 0.0564 0.1401 0.1076 0.0433 0.867 5.464 7.110 646.443 0.617 31.627 4.989 0.48 148196. 0.6505
|
|
9.61 0.0846 0.2037 0.1062 0.0441 0.883 5.563 7.016 658.226 0.629 31.208 4.835 0.48 148340. 0.6262
|
|
12.81 0.1128 0.2630 0.1046 0.0448 0.898 5.658 6.912 669.452 0.639 30.743 4.683 0.48 148499. 0.6020
|
|
16.02 0.1409 0.3183 0.1028 0.0455 0.912 5.746 6.796 679.853 0.649 30.227 4.534 0.48 148671. 0.5779
|
|
19.22 0.1691 0.3697 0.1009 0.0462 0.924 5.825 6.667 689.136 0.658 29.657 4.388 0.48 148859. 0.5541
|
|
22.42 0.1973 0.4174 0.0988 0.0467 0.935 5.891 6.526 696.986 0.666 29.026 4.247 0.48 149061. 0.5304
|
|
25.63 0.2255 0.4616 0.0964 0.0471 0.943 5.943 6.370 703.074 0.671 28.332 4.109 0.48 149280. 0.5071
|
|
28.83 0.2537 0.5025 0.0938 0.0474 0.948 5.976 6.198 707.062 0.675 27.571 3.976 0.48 149514. 0.4841
|
|
32.03 0.2819 0.5403 0.0910 0.0475 0.950 5.989 6.011 708.619 0.677 26.738 3.848 0.48 149765. 0.4613
|
|
35.24 0.3101 0.5752 0.0879 0.0474 0.949 5.979 5.808 707.418 0.676 25.832 3.724 0.48 150032. 0.4388
|
|
38.44 0.3383 0.6073 0.0845 0.0471 0.943 5.943 5.587 703.167 0.671 24.851 3.604 0.48 150317. 0.4165
|
|
41.64 0.3664 0.6367 0.0809 0.0466 0.933 5.879 5.349 695.607 0.664 23.793 3.488 0.48 150618. 0.3944
|
|
44.85 0.3946 0.6636 0.0771 0.0458 0.918 5.786 5.094 684.518 0.654 22.659 3.375 0.48 150936. 0.3725
|
|
48.05 0.4228 0.6879 0.0730 0.0449 0.898 5.661 4.822 669.722 0.640 21.450 3.266 0.48 151270. 0.3507
|
|
51.25 0.4510 0.7097 0.0686 0.0436 0.873 5.503 4.534 651.061 0.622 20.167 3.159 0.48 151622. 0.3289
|
|
54.45 0.4792 0.7287 0.0640 0.0421 0.843 5.311 4.229 628.379 0.600 18.811 3.053 0.48 151990. 0.3070
|
|
57.66 0.5074 0.7449 0.0592 0.0403 0.807 5.085 3.909 601.638 0.575 17.388 2.947 0.48 152375. 0.2849
|
|
60.86 0.5356 0.7579 0.0541 0.0382 0.766 4.826 3.576 571.028 0.545 15.907 2.841 0.48 152777. 0.2627
|
|
64.06 0.5638 0.7672 0.0489 0.0359 0.720 4.537 3.233 536.787 0.513 14.379 2.732 0.48 153195. 0.2402
|
|
67.27 0.5920 0.7721 0.0436 0.0334 0.669 4.219 2.881 499.120 0.477 12.815 2.618 0.48 153630. 0.2173
|
|
70.47 0.6201 0.7715 0.0382 0.0307 0.614 3.873 2.523 458.221 0.438 11.221 2.497 0.49 154081. 0.1939
|
|
73.67 0.6483 0.7637 0.0327 0.0277 0.556 3.502 2.160 414.286 0.396 9.606 2.365 0.49 154549. 0.1699
|
|
76.88 0.6765 0.7461 0.0271 0.0246 0.493 3.106 1.794 367.533 0.351 7.979 2.214 0.49 155033. 0.1450
|
|
80.08 0.7047 0.7140 0.0216 0.0213 0.427 2.690 1.427 318.216 0.304 6.347 2.034 0.49 155534. 0.1188
|
|
83.28 0.7329 0.6591 0.0161 0.0179 0.358 2.254 1.061 266.639 0.255 4.721 1.805 0.49 156051. 0.0909
|
|
86.49 0.7611 0.5642 0.0106 0.0143 0.286 1.802 0.699 213.171 0.204 3.111 1.488 0.49 156584. 0.0608
|
|
89.69 0.7893 0.3875 0.0052 0.0106 0.212 1.338 0.344 158.256 0.151 1.530 0.986 0.49 157133. 0.0283
|
|
92.89 0.8175 -0.0050 0.0000 0.0069 0.137 0.865 -0.003 102.306 0.098 -0.012 -0.012 0.49 157693. 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 0.1106 0.0418 1.113 6.376 8.842 829.845 0.720 39.328 4.833 0.52 162731. 0.7027
|
|
3.52 0.0282 0.0724 0.1094 0.0426 1.135 6.503 8.751 846.333 0.735 38.924 4.690 0.52 162863. 0.6784
|
|
7.05 0.0564 0.1405 0.1082 0.0434 1.157 6.629 8.650 862.709 0.749 38.474 4.548 0.52 163008. 0.6540
|
|
10.57 0.0846 0.2042 0.1068 0.0442 1.178 6.752 8.537 878.672 0.763 37.973 4.407 0.52 163167. 0.6296
|
|
14.09 0.1127 0.2637 0.1052 0.0450 1.199 6.869 8.412 893.897 0.776 37.416 4.268 0.52 163342. 0.6053
|
|
17.62 0.1409 0.3191 0.1035 0.0457 1.218 6.977 8.273 908.018 0.788 36.797 4.132 0.52 163531. 0.5812
|
|
21.14 0.1691 0.3707 0.1015 0.0463 1.235 7.074 8.118 920.641 0.799 36.111 4.000 0.52 163738. 0.5572
|
|
24.66 0.1973 0.4185 0.0994 0.0469 1.249 7.156 7.948 931.340 0.809 35.351 3.871 0.52 163961. 0.5336
|
|
28.19 0.2255 0.4628 0.0970 0.0473 1.260 7.220 7.759 939.667 0.816 34.514 3.745 0.52 164201. 0.5101
|
|
31.71 0.2537 0.5038 0.0945 0.0476 1.267 7.263 7.552 945.167 0.821 33.593 3.624 0.53 164460. 0.4870
|
|
35.23 0.2819 0.5417 0.0916 0.0477 1.270 7.280 7.326 947.386 0.822 32.586 3.507 0.53 164736. 0.4642
|
|
38.76 0.3100 0.5767 0.0885 0.0476 1.268 7.268 7.079 945.888 0.821 31.488 3.395 0.53 165030. 0.4416
|
|
42.28 0.3382 0.6090 0.0852 0.0473 1.261 7.225 6.811 940.270 0.816 30.297 3.286 0.53 165343. 0.4193
|
|
45.80 0.3664 0.6386 0.0816 0.0468 1.247 7.147 6.523 930.182 0.808 29.013 3.181 0.53 165675. 0.3972
|
|
49.32 0.3946 0.6657 0.0777 0.0461 1.227 7.033 6.213 915.329 0.795 27.635 3.079 0.53 166025. 0.3752
|
|
52.85 0.4228 0.6903 0.0736 0.0451 1.201 6.881 5.882 895.467 0.777 26.164 2.979 0.53 166394. 0.3533
|
|
56.37 0.4510 0.7123 0.0692 0.0438 1.167 6.688 5.531 870.385 0.756 24.603 2.882 0.53 166781. 0.3315
|
|
59.89 0.4792 0.7317 0.0645 0.0423 1.126 6.453 5.160 839.876 0.729 22.952 2.787 0.53 167186. 0.3095
|
|
63.42 0.5073 0.7483 0.0597 0.0404 1.078 6.177 4.770 803.879 0.698 21.218 2.691 0.53 167610. 0.2874
|
|
66.94 0.5355 0.7617 0.0546 0.0384 1.023 5.860 4.364 762.649 0.662 19.413 2.596 0.53 168052. 0.2652
|
|
70.46 0.5637 0.7716 0.0493 0.0361 0.961 5.506 3.946 716.505 0.622 17.551 2.498 0.53 168513. 0.2426
|
|
73.99 0.5919 0.7772 0.0440 0.0335 0.893 5.115 3.517 665.724 0.578 15.643 2.396 0.53 168991. 0.2197
|
|
77.51 0.6201 0.7774 0.0385 0.0307 0.819 4.692 3.080 610.567 0.530 13.698 2.288 0.53 169488. 0.1963
|
|
81.03 0.6483 0.7706 0.0330 0.0277 0.739 4.236 2.637 551.300 0.479 11.728 2.169 0.53 170002. 0.1722
|
|
84.56 0.6765 0.7542 0.0274 0.0246 0.655 3.751 2.190 488.217 0.424 9.741 2.035 0.54 170535. 0.1472
|
|
88.08 0.7046 0.7236 0.0218 0.0212 0.565 3.240 1.742 421.660 0.366 7.749 1.874 0.54 171086. 0.1209
|
|
91.60 0.7328 0.6704 0.0162 0.0177 0.472 2.705 1.296 352.045 0.306 5.763 1.669 0.54 171654. 0.0929
|
|
95.13 0.7610 0.5770 0.0107 0.0141 0.375 2.150 0.854 279.872 0.243 3.797 1.384 0.54 172241. 0.0625
|
|
98.65 0.7892 0.4001 0.0052 0.0104 0.276 1.581 0.420 205.742 0.179 1.867 0.925 0.54 172845. 0.0293
|
|
102.17 0.8174 -0.0057 0.0000 0.0066 0.175 1.001 -0.004 130.212 0.113 -0.016 -0.013 0.54 173460. 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 0.1112 0.0419 1.450 7.618 10.580 1081.517 0.861 47.058 4.437 0.57 177516. 0.7057
|
|
3.84 0.0282 0.0725 0.1101 0.0428 1.480 7.771 10.474 1103.296 0.878 46.587 4.306 0.57 177660. 0.6814
|
|
7.69 0.0564 0.1407 0.1088 0.0436 1.509 7.924 10.355 1124.948 0.895 46.060 4.175 0.57 177818. 0.6570
|
|
11.53 0.0845 0.2045 0.1074 0.0444 1.537 8.072 10.223 1146.075 0.912 45.473 4.046 0.57 177992. 0.6325
|
|
15.37 0.1127 0.2641 0.1059 0.0452 1.564 8.214 10.076 1166.245 0.928 44.818 3.919 0.57 178182. 0.6082
|
|
19.21 0.1409 0.3196 0.1042 0.0459 1.589 8.346 9.912 1184.977 0.943 44.088 3.794 0.57 178389. 0.5841
|
|
23.06 0.1691 0.3712 0.1022 0.0466 1.612 8.465 9.730 1201.747 0.956 43.278 3.672 0.57 178614. 0.5601
|
|
26.90 0.1973 0.4191 0.1001 0.0471 1.631 8.565 9.528 1215.993 0.968 42.379 3.554 0.57 178858. 0.5364
|
|
30.74 0.2254 0.4635 0.0978 0.0476 1.646 8.643 9.304 1227.124 0.977 41.386 3.439 0.57 179121. 0.5129
|
|
34.58 0.2536 0.5046 0.0952 0.0478 1.656 8.695 9.059 1234.535 0.982 40.293 3.328 0.57 179403. 0.4898
|
|
38.43 0.2818 0.5426 0.0924 0.0480 1.660 8.717 8.789 1237.625 0.985 39.094 3.221 0.57 179704. 0.4669
|
|
42.27 0.3100 0.5778 0.0893 0.0479 1.657 8.705 8.495 1235.817 0.983 37.786 3.118 0.57 180026. 0.4444
|
|
46.11 0.3382 0.6102 0.0859 0.0476 1.648 8.654 8.176 1228.576 0.978 36.366 3.018 0.57 180368. 0.4220
|
|
49.95 0.3663 0.6400 0.0823 0.0471 1.630 8.561 7.831 1215.437 0.967 34.831 2.922 0.58 180730. 0.3999
|
|
53.80 0.3945 0.6673 0.0784 0.0464 1.604 8.424 7.460 1196.011 0.952 33.184 2.829 0.58 181112. 0.3779
|
|
57.64 0.4227 0.6921 0.0742 0.0453 1.569 8.241 7.065 1169.977 0.931 31.424 2.739 0.58 181515. 0.3560
|
|
61.48 0.4509 0.7144 0.0698 0.0441 1.525 8.009 6.644 1137.056 0.905 29.554 2.650 0.58 181937. 0.3341
|
|
65.32 0.4790 0.7341 0.0652 0.0425 1.471 7.727 6.200 1096.982 0.873 27.576 2.563 0.58 182380. 0.3121
|
|
69.17 0.5072 0.7511 0.0602 0.0407 1.408 7.393 5.732 1049.668 0.835 25.496 2.477 0.58 182843. 0.2900
|
|
73.01 0.5354 0.7650 0.0551 0.0386 1.335 7.011 5.245 995.441 0.792 23.331 2.390 0.58 183325. 0.2676
|
|
76.85 0.5636 0.7754 0.0498 0.0362 1.253 6.584 4.743 934.719 0.744 21.096 2.301 0.58 183828. 0.2451
|
|
80.70 0.5918 0.7816 0.0444 0.0336 1.164 6.113 4.228 867.871 0.691 18.804 2.209 0.58 184350. 0.2221
|
|
84.54 0.6199 0.7826 0.0389 0.0308 1.066 5.601 3.703 795.240 0.633 16.469 2.112 0.58 184892. 0.1987
|
|
88.38 0.6481 0.7768 0.0333 0.0278 0.962 5.051 3.170 717.177 0.571 14.101 2.005 0.58 185453. 0.1746
|
|
92.22 0.6763 0.7616 0.0277 0.0246 0.850 4.466 2.633 634.070 0.505 11.713 1.884 0.58 186034. 0.1495
|
|
96.07 0.7045 0.7324 0.0220 0.0212 0.733 3.848 2.095 546.372 0.435 9.318 1.739 0.59 186635. 0.1231
|
|
99.91 0.7327 0.6809 0.0164 0.0176 0.610 3.202 1.558 454.631 0.362 6.931 1.555 0.59 187255. 0.0949
|
|
103.75 0.7608 0.5892 0.0108 0.0139 0.482 2.532 1.027 359.511 0.286 4.567 1.295 0.59 187895. 0.0642
|
|
107.59 0.7890 0.4124 0.0053 0.0101 0.351 1.844 0.505 261.810 0.208 2.245 0.874 0.59 188554. 0.0304
|
|
111.44 0.8172 -0.0063 0.0000 0.0063 0.218 1.143 -0.005 162.262 0.129 -0.020 -0.013 0.59 189225. 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 0.1118 0.0421 1.854 8.990 12.491 1382.703 1.016 55.559 4.097 0.62 192298. 0.7081
|
|
4.16 0.0282 0.0725 0.1108 0.0430 1.892 9.173 12.369 1410.916 1.036 55.018 3.976 0.62 192453. 0.6838
|
|
8.32 0.0563 0.1407 0.1095 0.0439 1.930 9.356 12.233 1438.999 1.057 54.413 3.856 0.62 192625. 0.6594
|
|
12.48 0.0845 0.2045 0.1082 0.0447 1.967 9.534 12.081 1466.430 1.077 53.736 3.737 0.62 192813. 0.6351
|
|
16.65 0.1127 0.2641 0.1067 0.0455 2.002 9.705 11.911 1492.650 1.096 52.978 3.619 0.62 193019. 0.6108
|
|
20.81 0.1409 0.3197 0.1049 0.0462 2.034 9.863 11.720 1517.036 1.114 52.133 3.504 0.62 193244. 0.5866
|
|
24.97 0.1690 0.3713 0.1031 0.0469 2.064 10.006 11.509 1538.905 1.130 51.190 3.392 0.62 193488. 0.5627
|
|
29.13 0.1972 0.4192 0.1009 0.0475 2.089 10.127 11.273 1557.526 1.144 50.143 3.283 0.62 193752. 0.5390
|
|
33.29 0.2254 0.4637 0.0986 0.0479 2.108 10.222 11.013 1572.133 1.155 48.984 3.177 0.62 194037. 0.5155
|
|
37.45 0.2535 0.5049 0.0960 0.0482 2.121 10.285 10.725 1581.940 1.162 47.704 3.075 0.62 194343. 0.4924
|
|
41.61 0.2817 0.5430 0.0932 0.0484 2.127 10.313 10.409 1586.167 1.165 46.299 2.976 0.62 194670. 0.4696
|
|
45.78 0.3099 0.5783 0.0901 0.0483 2.124 10.299 10.064 1584.059 1.164 44.763 2.882 0.62 195019. 0.4470
|
|
49.94 0.3380 0.6108 0.0867 0.0480 2.112 10.240 9.688 1574.922 1.157 43.092 2.790 0.62 195390. 0.4246
|
|
54.10 0.3662 0.6408 0.0831 0.0475 2.090 10.131 9.282 1558.152 1.145 41.284 2.702 0.62 195783. 0.4025
|
|
58.26 0.3944 0.6683 0.0792 0.0467 2.056 9.969 8.845 1533.244 1.126 39.341 2.616 0.62 196197. 0.3805
|
|
62.42 0.4226 0.6933 0.0750 0.0457 2.011 9.751 8.377 1499.784 1.102 37.263 2.534 0.62 196634. 0.3586
|
|
66.58 0.4507 0.7159 0.0706 0.0444 1.954 9.476 7.881 1457.418 1.071 35.054 2.453 0.63 197092. 0.3367
|
|
70.75 0.4789 0.7360 0.0659 0.0429 1.885 9.140 7.355 1405.803 1.033 32.714 2.373 0.63 197572. 0.3147
|
|
74.91 0.5071 0.7533 0.0609 0.0410 1.803 8.744 6.802 1344.820 0.988 30.253 2.294 0.63 198073. 0.2925
|
|
79.07 0.5352 0.7677 0.0557 0.0389 1.710 8.289 6.225 1274.881 0.936 27.689 2.215 0.63 198596. 0.2702
|
|
83.23 0.5634 0.7787 0.0504 0.0365 1.605 7.779 5.630 1196.528 0.879 25.041 2.134 0.63 199141. 0.2476
|
|
87.39 0.5916 0.7855 0.0449 0.0338 1.489 7.218 5.019 1110.236 0.816 22.324 2.050 0.63 199707. 0.2246
|
|
91.55 0.6197 0.7874 0.0394 0.0310 1.363 6.609 4.396 1016.454 0.747 19.554 1.962 0.63 200294. 0.2011
|
|
95.71 0.6479 0.7825 0.0337 0.0279 1.228 5.953 3.765 915.632 0.673 16.745 1.865 0.63 200902. 0.1769
|
|
99.88 0.6761 0.7684 0.0280 0.0246 1.084 5.255 3.128 808.274 0.594 13.911 1.755 0.63 201532. 0.1518
|
|
104.04 0.7043 0.7407 0.0223 0.0212 0.932 4.518 2.488 694.967 0.510 11.068 1.624 0.63 202182. 0.1253
|
|
108.20 0.7324 0.6908 0.0166 0.0176 0.773 3.748 1.851 576.421 0.423 8.232 1.456 0.64 202854. 0.0969
|
|
112.36 0.7606 0.6008 0.0109 0.0138 0.608 2.949 1.220 453.499 0.333 5.424 1.220 0.64 203546. 0.0659
|
|
116.52 0.7888 0.4243 0.0054 0.0100 0.439 2.128 0.599 327.240 0.240 2.666 0.831 0.64 204260. 0.0314
|
|
120.68 0.8169 -0.0069 -0.0001 0.0061 0.266 1.291 -0.006 198.595 0.146 -0.025 -0.013 0.64 204986. 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 0.1126 0.0425 2.333 10.505 14.581 1740.082 1.187 64.857 3.801 0.67 207077. 0.7096
|
|
4.48 0.0282 0.0724 0.1115 0.0433 2.382 10.722 14.444 1775.893 1.211 64.248 3.689 0.67 207244. 0.6856
|
|
8.96 0.0563 0.1405 0.1103 0.0442 2.429 10.937 14.290 1811.626 1.236 63.564 3.578 0.67 207429. 0.6613
|
|
13.44 0.0845 0.2043 0.1090 0.0451 2.476 11.149 14.118 1846.611 1.260 62.796 3.468 0.67 207631. 0.6371
|
|
17.92 0.1126 0.2639 0.1075 0.0459 2.521 11.351 13.924 1880.129 1.282 61.934 3.359 0.67 207853. 0.6129
|
|
22.40 0.1408 0.3194 0.1058 0.0466 2.563 11.540 13.707 1911.370 1.304 60.968 3.253 0.67 208096. 0.5888
|
|
26.88 0.1689 0.3710 0.1040 0.0473 2.601 11.709 13.464 1939.451 1.323 59.889 3.149 0.67 208359. 0.5650
|
|
31.36 0.1971 0.4190 0.1019 0.0479 2.633 11.854 13.194 1963.426 1.339 58.686 3.048 0.67 208644. 0.5413
|
|
35.84 0.2253 0.4635 0.0995 0.0484 2.658 11.968 12.893 1982.310 1.352 57.349 2.950 0.67 208950. 0.5180
|
|
40.32 0.2534 0.5047 0.0970 0.0487 2.675 12.045 12.561 1995.102 1.361 55.872 2.856 0.67 209280. 0.4949
|
|
44.80 0.2816 0.5429 0.0942 0.0488 2.683 12.079 12.195 2000.799 1.365 54.245 2.765 0.67 209633. 0.4721
|
|
49.28 0.3097 0.5783 0.0911 0.0488 2.680 12.065 11.795 1998.439 1.363 52.462 2.677 0.67 210009. 0.4495
|
|
53.75 0.3379 0.6109 0.0877 0.0485 2.665 11.997 11.358 1987.130 1.355 50.520 2.592 0.67 210409. 0.4272
|
|
58.23 0.3660 0.6411 0.0840 0.0480 2.637 11.870 10.885 1966.095 1.341 48.416 2.511 0.67 210832. 0.4051
|
|
62.71 0.3942 0.6688 0.0801 0.0472 2.594 11.680 10.376 1934.690 1.320 46.150 2.432 0.67 211279. 0.3831
|
|
67.19 0.4224 0.6941 0.0759 0.0462 2.538 11.425 9.830 1892.388 1.291 43.725 2.356 0.67 211750. 0.3612
|
|
71.67 0.4505 0.7169 0.0714 0.0449 2.466 11.101 9.250 1838.751 1.254 41.143 2.282 0.67 212243. 0.3393
|
|
76.15 0.4787 0.7373 0.0667 0.0433 2.378 10.706 8.635 1773.351 1.210 38.408 2.209 0.67 212761. 0.3173
|
|
80.63 0.5068 0.7551 0.0617 0.0414 2.274 10.239 7.987 1696.024 1.157 35.527 2.136 0.68 213301. 0.2952
|
|
85.11 0.5350 0.7699 0.0565 0.0392 2.155 9.704 7.312 1607.280 1.096 32.523 2.063 0.68 213865. 0.2728
|
|
89.59 0.5631 0.7814 0.0511 0.0368 2.022 9.103 6.614 1507.811 1.028 29.419 1.990 0.68 214451. 0.2502
|
|
94.07 0.5913 0.7890 0.0455 0.0341 1.875 8.442 5.898 1398.222 0.954 26.233 1.913 0.68 215061. 0.2272
|
|
98.55 0.6195 0.7916 0.0399 0.0312 1.715 7.722 5.167 1279.085 0.872 22.982 1.832 0.68 215693. 0.2036
|
|
103.03 0.6476 0.7877 0.0342 0.0281 1.543 6.949 4.425 1150.975 0.785 19.684 1.744 0.68 216348. 0.1794
|
|
107.51 0.6758 0.7748 0.0284 0.0248 1.361 6.125 3.677 1014.532 0.692 16.356 1.644 0.68 217026. 0.1541
|
|
111.99 0.7039 0.7485 0.0226 0.0212 1.167 5.256 2.926 870.506 0.594 13.015 1.525 0.68 217726. 0.1275
|
|
116.47 0.7321 0.7003 0.0168 0.0176 0.965 4.346 2.177 719.811 0.491 9.682 1.372 0.68 218449. 0.0989
|
|
120.95 0.7602 0.6121 0.0111 0.0138 0.756 3.403 1.434 563.580 0.384 6.380 1.154 0.69 219195. 0.0676
|
|
125.43 0.7884 0.4360 0.0054 0.0098 0.541 2.434 0.705 403.193 0.275 3.135 0.793 0.69 219962. 0.0326
|
|
129.91 0.8166 -0.0074 -0.0001 0.0059 0.322 1.449 -0.007 239.948 0.164 -0.030 -0.013 0.69 220744. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1134 0.0431 2.910 12.229 16.857 2170.200 1.382 74.979 3.523 0.71 221852. 0.7073
|
|
4.80 0.0281 0.0720 0.1124 0.0439 2.969 12.474 16.706 2213.665 1.409 74.306 3.423 0.71 222031. 0.6841
|
|
9.59 0.0563 0.1397 0.1112 0.0448 3.027 12.719 16.535 2257.130 1.437 73.547 3.323 0.71 222229. 0.6606
|
|
14.39 0.0844 0.2033 0.1099 0.0456 3.084 12.959 16.342 2299.804 1.464 72.690 3.223 0.71 222446. 0.6371
|
|
19.19 0.1126 0.2628 0.1085 0.0464 3.139 13.190 16.125 2340.811 1.490 71.725 3.125 0.71 222684. 0.6135
|
|
23.98 0.1407 0.3183 0.1068 0.0472 3.191 13.406 15.881 2379.181 1.515 70.639 3.028 0.71 222943. 0.5900
|
|
28.78 0.1688 0.3700 0.1050 0.0479 3.237 13.601 15.607 2413.826 1.537 69.419 2.933 0.72 223225. 0.5665
|
|
33.58 0.1970 0.4180 0.1029 0.0485 3.277 13.769 15.300 2443.577 1.556 68.055 2.840 0.72 223530. 0.5432
|
|
38.37 0.2251 0.4626 0.1006 0.0490 3.309 13.902 14.958 2467.187 1.571 66.535 2.750 0.72 223859. 0.5201
|
|
43.17 0.2533 0.5039 0.0981 0.0493 3.330 13.993 14.579 2483.365 1.581 64.849 2.663 0.72 224213. 0.4972
|
|
47.96 0.2814 0.5422 0.0952 0.0494 3.340 14.035 14.161 2490.803 1.586 62.987 2.579 0.72 224591. 0.4745
|
|
52.76 0.3095 0.5777 0.0921 0.0494 3.337 14.021 13.701 2488.226 1.584 60.942 2.497 0.72 224995. 0.4520
|
|
57.56 0.3377 0.6105 0.0888 0.0491 3.318 13.943 13.199 2474.451 1.575 58.709 2.419 0.72 225424. 0.4298
|
|
62.35 0.3658 0.6408 0.0851 0.0486 3.283 13.797 12.654 2448.454 1.559 56.285 2.344 0.72 225878. 0.4077
|
|
67.15 0.3939 0.6687 0.0812 0.0478 3.231 13.577 12.066 2409.417 1.534 53.670 2.271 0.72 226357. 0.3858
|
|
71.95 0.4221 0.6942 0.0769 0.0468 3.160 13.280 11.436 2356.684 1.500 50.867 2.201 0.72 226861. 0.3639
|
|
76.74 0.4502 0.7174 0.0724 0.0454 3.071 12.902 10.764 2289.710 1.458 47.880 2.132 0.72 227391. 0.3421
|
|
81.54 0.4784 0.7381 0.0676 0.0438 2.961 12.442 10.052 2207.978 1.406 44.711 2.065 0.72 227946. 0.3201
|
|
86.34 0.5065 0.7563 0.0626 0.0419 2.831 11.897 9.301 2111.266 1.344 41.371 1.998 0.72 228525. 0.2980
|
|
91.13 0.5346 0.7716 0.0573 0.0397 2.682 11.271 8.517 2000.197 1.273 37.884 1.931 0.72 229129. 0.2756
|
|
95.93 0.5628 0.7837 0.0518 0.0372 2.515 10.569 7.706 1875.634 1.194 34.278 1.864 0.73 229758. 0.2530
|
|
100.73 0.5909 0.7920 0.0462 0.0345 2.331 9.795 6.874 1738.355 1.107 30.574 1.793 0.73 230411. 0.2299
|
|
105.52 0.6191 0.7954 0.0405 0.0315 2.131 8.954 6.024 1589.085 1.012 26.794 1.719 0.73 231088. 0.2063
|
|
110.32 0.6472 0.7924 0.0347 0.0283 1.916 8.050 5.161 1428.587 0.909 22.955 1.639 0.73 231789. 0.1820
|
|
115.11 0.6753 0.7806 0.0288 0.0250 1.687 7.087 4.289 1257.724 0.801 19.079 1.547 0.73 232515. 0.1566
|
|
119.91 0.7035 0.7555 0.0230 0.0214 1.445 6.072 3.414 1077.538 0.686 15.186 1.437 0.73 233265. 0.1298
|
|
124.71 0.7316 0.7084 0.0171 0.0176 1.193 5.011 2.541 889.314 0.566 11.300 1.296 0.73 234039. 0.1010
|
|
129.50 0.7598 0.6208 0.0113 0.0138 0.932 3.914 1.675 694.649 0.442 7.449 1.093 0.73 234837. 0.0692
|
|
134.30 0.7879 0.4437 0.0055 0.0098 0.664 2.792 0.823 495.488 0.315 3.662 0.754 0.74 235659. 0.0334
|
|
139.10 0.8160 -0.0075 -0.0001 0.0058 0.394 1.655 -0.008 293.677 0.187 -0.035 -0.012 0.74 236495. 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 0.1142 0.0444 3.639 14.335 19.322 2713.674 1.620 85.943 3.229 0.76 236623. 0.6941
|
|
5.11 0.0281 0.0704 0.1132 0.0452 3.706 14.600 19.158 2763.677 1.649 85.214 3.144 0.76 236813. 0.6729
|
|
10.22 0.0562 0.1371 0.1121 0.0460 3.773 14.863 18.972 2813.553 1.679 84.387 3.058 0.76 237024. 0.6514
|
|
15.33 0.0843 0.1998 0.1109 0.0468 3.838 15.121 18.761 2862.352 1.708 83.450 2.973 0.76 237255. 0.6296
|
|
20.44 0.1124 0.2588 0.1095 0.0476 3.901 15.368 18.522 2909.057 1.736 82.387 2.888 0.76 237509. 0.6077
|
|
25.55 0.1406 0.3141 0.1079 0.0483 3.959 15.597 18.252 2952.524 1.762 81.185 2.804 0.76 237785. 0.5857
|
|
30.67 0.1687 0.3658 0.1061 0.0489 4.012 15.803 17.947 2991.497 1.785 79.829 2.721 0.76 238086. 0.5637
|
|
35.78 0.1968 0.4141 0.1041 0.0495 4.056 15.978 17.604 3024.625 1.805 78.305 2.640 0.76 238412. 0.5416
|
|
40.89 0.2249 0.4590 0.1018 0.0499 4.091 16.115 17.221 3050.470 1.821 76.599 2.561 0.76 238763. 0.5196
|
|
46.00 0.2530 0.5007 0.0993 0.0502 4.114 16.205 16.794 3067.531 1.831 74.698 2.483 0.76 239140. 0.4976
|
|
51.11 0.2811 0.5395 0.0965 0.0503 4.123 16.240 16.320 3074.283 1.835 72.593 2.408 0.76 239544. 0.4756
|
|
56.22 0.3092 0.5754 0.0934 0.0502 4.116 16.214 15.799 3069.210 1.832 70.273 2.335 0.77 239975. 0.4538
|
|
61.33 0.3373 0.6087 0.0900 0.0499 4.091 16.117 15.228 3050.875 1.821 67.733 2.264 0.77 240432. 0.4320
|
|
66.44 0.3654 0.6394 0.0863 0.0493 4.047 15.943 14.606 3017.949 1.801 64.968 2.195 0.77 240917. 0.4102
|
|
71.55 0.3935 0.6677 0.0824 0.0485 3.982 15.686 13.934 2969.301 1.772 61.980 2.129 0.77 241428. 0.3885
|
|
76.66 0.4217 0.6936 0.0781 0.0475 3.894 15.341 13.213 2903.986 1.733 58.770 2.064 0.77 241967. 0.3668
|
|
81.77 0.4498 0.7171 0.0735 0.0461 3.783 14.903 12.442 2821.211 1.684 55.343 2.000 0.77 242532. 0.3450
|
|
86.89 0.4779 0.7383 0.0687 0.0445 3.648 14.370 11.624 2720.235 1.624 51.703 1.938 0.77 243124. 0.3231
|
|
92.00 0.5060 0.7569 0.0636 0.0425 3.488 13.739 10.760 2600.702 1.552 47.862 1.877 0.77 243742. 0.3010
|
|
97.11 0.5341 0.7727 0.0583 0.0403 3.303 13.013 9.858 2463.377 1.470 43.847 1.815 0.77 244386. 0.2787
|
|
102.22 0.5622 0.7854 0.0527 0.0378 3.097 12.200 8.923 2309.401 1.378 39.691 1.753 0.77 245056. 0.2560
|
|
107.33 0.5903 0.7942 0.0471 0.0350 2.870 11.304 7.963 2139.838 1.277 35.418 1.688 0.77 245752. 0.2329
|
|
112.44 0.6184 0.7981 0.0413 0.0320 2.623 10.331 6.981 1955.719 1.167 31.053 1.619 0.78 246474. 0.2092
|
|
117.55 0.6465 0.7956 0.0354 0.0287 2.358 9.288 5.984 1758.143 1.049 26.618 1.544 0.78 247222. 0.1847
|
|
122.66 0.6746 0.7839 0.0294 0.0253 2.076 8.180 4.976 1548.389 0.924 22.134 1.458 0.78 247995. 0.1590
|
|
127.77 0.7028 0.7582 0.0234 0.0217 1.781 7.015 3.963 1328.016 0.793 17.628 1.354 0.78 248794. 0.1318
|
|
132.88 0.7309 0.7095 0.0174 0.0180 1.474 5.805 2.951 1098.937 0.656 13.125 1.218 0.78 249619. 0.1023
|
|
138.00 0.7590 0.6185 0.0115 0.0141 1.158 4.561 1.946 863.479 0.515 8.657 1.022 0.78 250469. 0.0697
|
|
143.11 0.7871 0.4364 0.0057 0.0102 0.837 3.299 0.958 624.405 0.373 4.259 0.696 0.79 251344. 0.0333
|
|
148.22 0.8152 -0.0067 -0.0001 0.0063 0.515 2.030 -0.009 384.301 0.229 -0.039 -0.010 0.79 252235. 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 0.1151 0.0470 4.619 17.126 21.977 3444.491 1.935 97.754 2.894 0.81 251389. 0.6634
|
|
5.43 0.0281 0.0672 0.1142 0.0477 4.692 17.397 21.803 3499.078 1.966 96.980 2.826 0.81 251591. 0.6453
|
|
10.85 0.0562 0.1312 0.1131 0.0484 4.765 17.665 21.605 3552.957 1.996 96.098 2.758 0.81 251814. 0.6268
|
|
16.28 0.0843 0.1919 0.1119 0.0491 4.834 17.924 21.378 3604.964 2.025 95.091 2.690 0.81 252059. 0.6081
|
|
21.70 0.1123 0.2494 0.1106 0.0498 4.900 18.167 21.120 3653.869 2.052 93.942 2.622 0.81 252328. 0.5891
|
|
27.13 0.1404 0.3038 0.1091 0.0504 4.960 18.388 20.826 3698.325 2.077 92.635 2.554 0.81 252622. 0.5699
|
|
32.55 0.1685 0.3550 0.1073 0.0509 5.011 18.579 20.492 3736.883 2.099 91.150 2.487 0.81 252941. 0.5506
|
|
37.98 0.1966 0.4031 0.1053 0.0514 5.053 18.734 20.115 3768.023 2.117 89.472 2.421 0.81 253287. 0.5310
|
|
43.40 0.2247 0.4484 0.1031 0.0517 5.083 18.844 19.691 3790.154 2.129 87.584 2.356 0.81 253661. 0.5113
|
|
48.83 0.2528 0.4908 0.1006 0.0518 5.098 18.901 19.215 3801.635 2.135 85.469 2.293 0.81 254062. 0.4914
|
|
54.26 0.2809 0.5304 0.0978 0.0518 5.097 18.897 18.686 3800.764 2.135 83.115 2.230 0.81 254492. 0.4713
|
|
59.68 0.3089 0.5674 0.0948 0.0516 5.077 18.823 18.101 3785.927 2.127 80.511 2.169 0.81 254950. 0.4511
|
|
65.11 0.3370 0.6018 0.0914 0.0512 5.036 18.672 17.457 3755.575 2.110 77.649 2.108 0.81 255436. 0.4307
|
|
70.53 0.3651 0.6337 0.0877 0.0505 4.973 18.437 16.755 3708.259 2.083 74.525 2.049 0.81 255952. 0.4102
|
|
75.96 0.3932 0.6631 0.0837 0.0497 4.885 18.111 15.993 3642.691 2.046 71.138 1.991 0.82 256496. 0.3894
|
|
81.38 0.4213 0.6902 0.0795 0.0485 4.771 17.689 15.174 3557.777 1.998 67.492 1.934 0.82 257069. 0.3684
|
|
86.81 0.4494 0.7148 0.0749 0.0471 4.630 17.166 14.296 3452.552 1.939 63.590 1.878 0.82 257670. 0.3472
|
|
92.23 0.4774 0.7369 0.0700 0.0453 4.460 16.537 13.363 3326.118 1.868 59.440 1.822 0.82 258299. 0.3257
|
|
97.66 0.5055 0.7562 0.0648 0.0433 4.262 15.803 12.377 3178.443 1.785 55.052 1.766 0.82 258956. 0.3038
|
|
103.09 0.5336 0.7725 0.0594 0.0410 4.037 14.966 11.344 3010.119 1.691 50.458 1.709 0.82 259641. 0.2815
|
|
108.51 0.5617 0.7853 0.0538 0.0385 3.785 14.034 10.273 2822.571 1.586 45.696 1.651 0.82 260353. 0.2587
|
|
113.94 0.5898 0.7940 0.0480 0.0357 3.509 13.011 9.172 2616.910 1.470 40.796 1.590 0.82 261093. 0.2354
|
|
119.36 0.6179 0.7974 0.0421 0.0326 3.211 11.905 8.045 2394.490 1.345 35.784 1.524 0.82 261860. 0.2114
|
|
124.79 0.6460 0.7936 0.0361 0.0294 2.893 10.725 6.899 2157.135 1.212 30.687 1.451 0.83 262654. 0.1863
|
|
130.21 0.6740 0.7794 0.0301 0.0260 2.557 9.480 5.740 1906.728 1.071 25.530 1.365 0.83 263475. 0.1599
|
|
135.64 0.7021 0.7495 0.0239 0.0224 2.207 8.182 4.573 1645.676 0.924 20.341 1.260 0.83 264323. 0.1318
|
|
141.06 0.7302 0.6939 0.0178 0.0188 1.846 6.846 3.406 1376.900 0.773 15.151 1.122 0.83 265198. 0.1013
|
|
146.49 0.7583 0.5931 0.0118 0.0150 1.480 5.488 2.247 1103.729 0.620 9.997 0.924 0.83 266100. 0.0677
|
|
151.91 0.7864 0.4025 0.0058 0.0113 1.113 4.126 1.106 829.904 0.466 4.918 0.604 0.83 267029. 0.0311
|
|
157.34 0.8145 -0.0062 -0.0001 0.0076 0.749 2.778 -0.011 558.778 0.314 -0.049 -0.009 0.84 267976. 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 0.1158 0.0513 5.991 20.980 24.801 4467.858 2.370 110.315 2.518 0.86 266152. 0.6131
|
|
5.75 0.0281 0.0622 0.1150 0.0520 6.069 21.251 24.621 4525.603 2.401 109.513 2.468 0.86 266365. 0.5987
|
|
11.49 0.0562 0.1218 0.1140 0.0526 6.144 21.513 24.414 4581.431 2.431 108.593 2.417 0.86 266601. 0.5840
|
|
17.24 0.0843 0.1789 0.1129 0.0532 6.214 21.759 24.176 4633.814 2.458 107.535 2.366 0.86 266860. 0.5689
|
|
22.99 0.1124 0.2334 0.1116 0.0538 6.278 21.981 23.903 4681.135 2.483 106.320 2.316 0.86 267144. 0.5537
|
|
28.74 0.1405 0.2855 0.1102 0.0542 6.332 22.171 23.589 4721.589 2.505 104.925 2.266 0.86 267455. 0.5382
|
|
34.48 0.1686 0.3351 0.1085 0.0546 6.374 22.320 23.230 4753.368 2.522 103.329 2.217 0.86 267794. 0.5224
|
|
40.23 0.1967 0.3823 0.1066 0.0548 6.403 22.421 22.821 4774.756 2.533 101.510 2.168 0.86 268161. 0.5064
|
|
45.98 0.2248 0.4273 0.1044 0.0549 6.415 22.464 22.358 4783.984 2.538 99.448 2.120 0.86 268557. 0.4901
|
|
51.72 0.2529 0.4699 0.1020 0.0549 6.409 22.442 21.835 4779.336 2.536 97.124 2.072 0.86 268983. 0.4735
|
|
57.47 0.2810 0.5103 0.0993 0.0547 6.382 22.348 21.250 4759.170 2.525 94.522 2.025 0.86 269439. 0.4565
|
|
63.22 0.3091 0.5484 0.0962 0.0542 6.332 22.173 20.600 4721.908 2.505 91.629 1.979 0.86 269926. 0.4391
|
|
68.97 0.3372 0.5843 0.0929 0.0536 6.257 21.911 19.882 4666.093 2.475 88.435 1.933 0.86 270443. 0.4214
|
|
74.71 0.3653 0.6180 0.0892 0.0527 6.156 21.555 19.095 4590.412 2.435 84.935 1.887 0.86 270991. 0.4031
|
|
80.46 0.3934 0.6494 0.0852 0.0516 6.026 21.101 18.239 4493.732 2.384 81.128 1.841 0.86 271569. 0.3844
|
|
86.21 0.4215 0.6784 0.0809 0.0502 5.867 20.544 17.315 4375.055 2.321 77.018 1.795 0.86 272178. 0.3652
|
|
91.95 0.4496 0.7051 0.0762 0.0486 5.677 19.879 16.324 4233.396 2.246 72.610 1.749 0.87 272817. 0.3455
|
|
97.70 0.4777 0.7292 0.0713 0.0467 5.455 19.100 15.267 4067.665 2.158 67.909 1.702 0.87 273485. 0.3253
|
|
103.45 0.5057 0.7504 0.0661 0.0445 5.201 18.210 14.148 3878.102 2.057 62.929 1.655 0.87 274183. 0.3043
|
|
109.20 0.5338 0.7680 0.0606 0.0421 4.919 17.224 12.973 3668.014 1.946 57.705 1.604 0.87 274910. 0.2825
|
|
114.94 0.5619 0.7813 0.0549 0.0395 4.611 16.145 11.754 3438.159 1.824 52.281 1.551 0.87 275667. 0.2599
|
|
120.69 0.5900 0.7889 0.0490 0.0367 4.282 14.993 10.497 3192.920 1.694 46.689 1.491 0.87 276452. 0.2362
|
|
126.44 0.6181 0.7898 0.0430 0.0337 3.931 13.766 9.210 2931.629 1.555 40.966 1.425 0.87 277266. 0.2114
|
|
132.18 0.6462 0.7820 0.0369 0.0305 3.561 12.469 7.900 2655.518 1.409 35.140 1.349 0.87 278108. 0.1855
|
|
137.93 0.6743 0.7616 0.0307 0.0272 3.175 11.117 6.575 2367.530 1.256 29.244 1.260 0.88 278979. 0.1579
|
|
143.68 0.7024 0.7229 0.0245 0.0238 2.777 9.725 5.240 2071.078 1.099 23.309 1.148 0.88 279879. 0.1285
|
|
149.43 0.7305 0.6555 0.0182 0.0203 2.374 8.312 3.906 1770.238 0.939 17.373 1.001 0.88 280806. 0.0967
|
|
155.17 0.7586 0.5418 0.0121 0.0169 1.971 6.900 2.580 1469.511 0.780 11.477 0.796 0.88 281763. 0.0626
|
|
160.92 0.7867 0.3476 0.0060 0.0135 1.574 5.511 1.275 1173.610 0.623 5.671 0.493 0.88 282747. 0.0272
|
|
166.67 0.8148 0.0003 0.0000 0.0102 1.188 4.161 0.001 886.229 0.470 0.003 0.000 0.89 283752. 0.0000
|
|
|
|
|
|
|