575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
14x10E (14x10E.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 0.1012 0.0469 0.002 0.128 0.124 1.515 0.014 0.551 37.102 0.06 18240. 0.5474
|
|
0.39 0.0296 0.0622 0.1003 0.0477 0.002 0.130 0.123 1.539 0.015 0.546 36.182 0.06 18255. 0.5314
|
|
0.78 0.0592 0.1212 0.0993 0.0485 0.002 0.132 0.122 1.564 0.015 0.541 35.247 0.06 18271. 0.5150
|
|
1.18 0.0887 0.1769 0.0981 0.0492 0.002 0.134 0.120 1.588 0.015 0.534 34.303 0.06 18289. 0.4982
|
|
1.57 0.1183 0.2294 0.0968 0.0499 0.002 0.136 0.119 1.612 0.015 0.527 33.354 0.06 18309. 0.4813
|
|
1.96 0.1479 0.2786 0.0954 0.0506 0.002 0.138 0.117 1.634 0.016 0.519 32.405 0.06 18330. 0.4641
|
|
2.35 0.1775 0.3245 0.0938 0.0513 0.002 0.140 0.115 1.655 0.016 0.511 31.462 0.06 18354. 0.4468
|
|
2.75 0.2071 0.3674 0.0920 0.0519 0.002 0.141 0.113 1.674 0.016 0.501 30.526 0.06 18380. 0.4294
|
|
3.14 0.2366 0.4071 0.0900 0.0523 0.002 0.143 0.110 1.689 0.016 0.490 29.602 0.06 18408. 0.4119
|
|
3.53 0.2662 0.4439 0.0878 0.0527 0.002 0.144 0.108 1.700 0.016 0.478 28.691 0.06 18439. 0.3943
|
|
3.92 0.2958 0.4778 0.0854 0.0529 0.002 0.144 0.105 1.707 0.016 0.465 27.794 0.06 18471. 0.3767
|
|
4.31 0.3254 0.5090 0.0828 0.0529 0.002 0.144 0.101 1.708 0.016 0.451 26.913 0.06 18506. 0.3591
|
|
4.71 0.3550 0.5373 0.0799 0.0528 0.002 0.144 0.098 1.703 0.016 0.435 26.045 0.06 18544. 0.3413
|
|
5.10 0.3845 0.5630 0.0767 0.0524 0.002 0.143 0.094 1.691 0.016 0.418 25.190 0.06 18583. 0.3235
|
|
5.49 0.4141 0.5859 0.0732 0.0518 0.002 0.141 0.090 1.671 0.016 0.399 24.342 0.06 18625. 0.3055
|
|
5.88 0.4437 0.6059 0.0695 0.0509 0.002 0.139 0.085 1.643 0.016 0.379 23.497 0.06 18670. 0.2873
|
|
6.27 0.4733 0.6230 0.0655 0.0498 0.002 0.136 0.080 1.607 0.015 0.357 22.647 0.06 18717. 0.2689
|
|
6.67 0.5029 0.6367 0.0613 0.0484 0.002 0.132 0.075 1.562 0.015 0.334 21.784 0.06 18766. 0.2501
|
|
7.06 0.5324 0.6466 0.0568 0.0468 0.002 0.128 0.070 1.509 0.014 0.309 20.895 0.06 18818. 0.2309
|
|
7.45 0.5620 0.6522 0.0521 0.0449 0.002 0.122 0.064 1.448 0.014 0.283 19.968 0.06 18872. 0.2113
|
|
7.84 0.5916 0.6528 0.0472 0.0427 0.002 0.117 0.058 1.379 0.013 0.257 18.984 0.06 18928. 0.1912
|
|
8.24 0.6212 0.6471 0.0421 0.0404 0.002 0.110 0.052 1.304 0.012 0.229 17.925 0.06 18986. 0.1705
|
|
8.63 0.6508 0.6340 0.0369 0.0379 0.002 0.103 0.045 1.223 0.012 0.201 16.763 0.06 19047. 0.1494
|
|
9.02 0.6803 0.6116 0.0316 0.0352 0.002 0.096 0.039 1.136 0.011 0.172 15.467 0.06 19110. 0.1276
|
|
9.41 0.7099 0.5772 0.0263 0.0324 0.001 0.088 0.032 1.045 0.010 0.143 13.989 0.06 19176. 0.1052
|
|
9.80 0.7395 0.5271 0.0209 0.0294 0.001 0.080 0.026 0.949 0.009 0.114 12.263 0.06 19244. 0.0823
|
|
10.20 0.7691 0.4557 0.0156 0.0263 0.001 0.072 0.019 0.849 0.008 0.085 10.194 0.06 19313. 0.0590
|
|
10.59 0.7987 0.3542 0.0102 0.0231 0.001 0.063 0.013 0.746 0.007 0.056 7.630 0.06 19386. 0.0358
|
|
10.98 0.8282 0.2081 0.0050 0.0198 0.001 0.054 0.006 0.640 0.006 0.027 4.323 0.06 19460. 0.0142
|
|
11.37 0.8578 -0.0082 -0.0002 0.0165 0.001 0.045 0.000 0.533 0.005 -0.001 -0.164 0.06 19537. 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 0.1016 0.0430 0.015 0.469 0.497 11.105 0.053 2.213 20.316 0.11 36480. 0.6005
|
|
0.80 0.0303 0.0695 0.1006 0.0438 0.015 0.478 0.493 11.315 0.054 2.192 19.754 0.11 36510. 0.5812
|
|
1.60 0.0605 0.1350 0.0996 0.0447 0.015 0.487 0.488 11.529 0.055 2.169 19.185 0.11 36543. 0.5615
|
|
2.41 0.0908 0.1964 0.0984 0.0455 0.016 0.496 0.482 11.742 0.056 2.143 18.614 0.11 36580. 0.5416
|
|
3.21 0.1211 0.2539 0.0971 0.0463 0.016 0.505 0.475 11.952 0.057 2.115 18.044 0.11 36621. 0.5215
|
|
4.01 0.1513 0.3074 0.0956 0.0471 0.016 0.514 0.468 12.152 0.058 2.083 17.477 0.11 36666. 0.5012
|
|
4.81 0.1816 0.3571 0.0940 0.0478 0.017 0.521 0.460 12.338 0.059 2.047 16.918 0.11 36715. 0.4810
|
|
5.62 0.2118 0.4031 0.0921 0.0484 0.017 0.528 0.451 12.504 0.060 2.007 16.368 0.11 36769. 0.4608
|
|
6.42 0.2421 0.4455 0.0901 0.0490 0.017 0.534 0.441 12.643 0.060 1.963 15.829 0.11 36827. 0.4407
|
|
7.22 0.2724 0.4845 0.0878 0.0494 0.017 0.539 0.430 12.749 0.061 1.913 15.302 0.11 36890. 0.4206
|
|
8.02 0.3026 0.5203 0.0853 0.0496 0.017 0.542 0.418 12.814 0.061 1.858 14.789 0.11 36958. 0.4007
|
|
8.83 0.3329 0.5530 0.0825 0.0497 0.017 0.542 0.404 12.831 0.061 1.798 14.289 0.11 37031. 0.3808
|
|
9.63 0.3632 0.5827 0.0795 0.0496 0.017 0.541 0.389 12.794 0.061 1.732 13.803 0.11 37109. 0.3610
|
|
10.43 0.3934 0.6095 0.0762 0.0492 0.017 0.537 0.373 12.695 0.061 1.659 13.329 0.11 37191. 0.3412
|
|
11.23 0.4237 0.6335 0.0726 0.0485 0.017 0.530 0.355 12.530 0.060 1.581 12.864 0.11 37279. 0.3214
|
|
12.04 0.4539 0.6547 0.0687 0.0476 0.016 0.520 0.336 12.295 0.059 1.496 12.407 0.11 37372. 0.3015
|
|
12.84 0.4842 0.6727 0.0645 0.0464 0.016 0.507 0.316 11.986 0.057 1.405 11.952 0.11 37469. 0.2815
|
|
13.64 0.5145 0.6875 0.0600 0.0449 0.016 0.490 0.294 11.601 0.055 1.308 11.496 0.11 37572. 0.2613
|
|
14.44 0.5447 0.6986 0.0553 0.0432 0.015 0.471 0.271 11.143 0.053 1.206 11.033 0.11 37680. 0.2407
|
|
15.25 0.5750 0.7054 0.0504 0.0411 0.014 0.449 0.247 10.614 0.051 1.099 10.554 0.11 37792. 0.2198
|
|
16.05 0.6053 0.7072 0.0454 0.0388 0.013 0.424 0.222 10.022 0.048 0.988 10.051 0.11 37909. 0.1985
|
|
16.85 0.6355 0.7027 0.0401 0.0363 0.013 0.396 0.197 9.371 0.045 0.874 9.512 0.11 38031. 0.1767
|
|
17.65 0.6658 0.6904 0.0348 0.0336 0.012 0.366 0.170 8.667 0.041 0.758 8.921 0.11 38158. 0.1544
|
|
18.46 0.6961 0.6680 0.0294 0.0306 0.011 0.334 0.144 7.912 0.038 0.641 8.256 0.11 38290. 0.1313
|
|
19.26 0.7263 0.6319 0.0240 0.0275 0.010 0.301 0.117 7.113 0.034 0.522 7.485 0.11 38426. 0.1075
|
|
20.06 0.7566 0.5766 0.0185 0.0243 0.008 0.265 0.091 6.274 0.030 0.403 6.556 0.11 38567. 0.0827
|
|
20.86 0.7868 0.4926 0.0131 0.0209 0.007 0.228 0.064 5.401 0.026 0.285 5.386 0.11 38713. 0.0572
|
|
21.67 0.8171 0.3629 0.0077 0.0174 0.006 0.190 0.038 4.502 0.021 0.169 3.820 0.11 38864. 0.0312
|
|
22.47 0.8474 0.1529 0.0025 0.0139 0.005 0.151 0.012 3.585 0.017 0.055 1.552 0.12 39019. 0.0072
|
|
23.27 0.8776
|
|
|
|
|
|
|
|
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 0.1018 0.0413 0.048 1.014 1.122 36.008 0.115 4.990 14.132 0.17 54720. 0.6274
|
|
1.19 0.0298 0.0714 0.1009 0.0421 0.049 1.035 1.112 36.725 0.117 4.945 13.731 0.17 54764. 0.6068
|
|
2.37 0.0596 0.1385 0.0999 0.0430 0.050 1.055 1.101 37.457 0.119 4.895 13.326 0.17 54813. 0.5859
|
|
3.56 0.0894 0.2015 0.0987 0.0438 0.051 1.076 1.088 38.190 0.122 4.839 12.921 0.17 54867. 0.5648
|
|
4.74 0.1192 0.2602 0.0975 0.0447 0.052 1.096 1.074 38.912 0.124 4.777 12.517 0.17 54927. 0.5436
|
|
5.93 0.1490 0.3149 0.0960 0.0455 0.053 1.116 1.058 39.608 0.126 4.707 12.117 0.17 54993. 0.5224
|
|
7.11 0.1788 0.3656 0.0944 0.0462 0.054 1.134 1.041 40.260 0.128 4.629 11.723 0.17 55065. 0.5012
|
|
8.30 0.2087 0.4125 0.0927 0.0469 0.055 1.151 1.021 40.848 0.130 4.541 11.337 0.17 55144. 0.4801
|
|
9.48 0.2385 0.4557 0.0907 0.0475 0.055 1.165 0.999 41.352 0.132 4.444 10.959 0.17 55229. 0.4591
|
|
10.67 0.2683 0.4954 0.0885 0.0479 0.056 1.176 0.975 41.750 0.133 4.337 10.592 0.17 55322. 0.4383
|
|
11.86 0.2981 0.5319 0.0861 0.0482 0.056 1.184 0.948 42.018 0.134 4.217 10.235 0.17 55421. 0.4177
|
|
13.04 0.3279 0.5653 0.0834 0.0484 0.057 1.187 0.919 42.133 0.134 4.086 9.889 0.17 55527. 0.3972
|
|
14.23 0.3577 0.5958 0.0804 0.0483 0.056 1.185 0.886 42.070 0.134 3.941 9.553 0.17 55641. 0.3769
|
|
15.41 0.3875 0.6234 0.0772 0.0480 0.056 1.178 0.851 41.810 0.133 3.783 9.227 0.17 55762. 0.3567
|
|
16.60 0.4173 0.6484 0.0737 0.0474 0.055 1.165 0.812 41.333 0.132 3.612 8.911 0.17 55890. 0.3365
|
|
17.78 0.4471 0.6706 0.0699 0.0466 0.054 1.145 0.770 40.623 0.129 3.427 8.601 0.17 56025. 0.3164
|
|
18.97 0.4769 0.6900 0.0659 0.0455 0.053 1.118 0.726 39.670 0.126 3.228 8.297 0.17 56168. 0.2962
|
|
20.15 0.5067 0.7064 0.0615 0.0441 0.052 1.084 0.678 38.466 0.122 3.016 7.995 0.17 56318. 0.2759
|
|
21.34 0.5365 0.7196 0.0570 0.0425 0.050 1.043 0.628 37.009 0.118 2.792 7.692 0.17 56475. 0.2554
|
|
22.53 0.5663 0.7292 0.0522 0.0405 0.047 0.995 0.575 35.311 0.112 2.557 7.384 0.17 56639. 0.2347
|
|
23.71 0.5962 0.7344 0.0472 0.0383 0.045 0.941 0.520 33.392 0.106 2.314 7.065 0.17 56810. 0.2136
|
|
24.90 0.6260 0.7345 0.0421 0.0359 0.042 0.881 0.464 31.266 0.100 2.063 6.730 0.17 56988. 0.1921
|
|
26.08 0.6558 0.7281 0.0369 0.0332 0.039 0.816 0.406 28.950 0.092 1.808 6.368 0.17 57173. 0.1701
|
|
27.27 0.6856 0.7134 0.0316 0.0304 0.035 0.745 0.348 26.458 0.084 1.548 5.968 0.17 57366. 0.1476
|
|
28.45 0.7154 0.6875 0.0263 0.0273 0.032 0.671 0.289 23.805 0.076 1.287 5.512 0.17 57565. 0.1242
|
|
29.64 0.7452 0.6459 0.0209 0.0241 0.028 0.592 0.230 21.007 0.067 1.024 4.971 0.17 57770. 0.1000
|
|
30.82 0.7750 0.5808 0.0156 0.0208 0.024 0.509 0.171 18.083 0.058 0.762 4.298 0.17 57983. 0.0746
|
|
32.01 0.8048 0.4780 0.0103 0.0173 0.020 0.424 0.113 15.057 0.048 0.503 3.406 0.17 58203. 0.0480
|
|
33.19 0.8346 0.3085 0.0051 0.0137 0.016 0.337 0.056 11.953 0.038 0.248 2.120 0.17 58429. 0.0210
|
|
34.38 0.8644 0.0013 0.0000 0.0101 0.012 0.248 0.000 8.800 0.028 0.001 0.009 0.17 58662. 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 0.1021 0.0404 0.112 1.762 1.999 83.403 0.199 8.893 10.873 0.22 72959. 0.6444
|
|
1.58 0.0299 0.0733 0.1012 0.0412 0.114 1.799 1.982 85.140 0.203 8.814 10.556 0.22 73018. 0.6228
|
|
3.17 0.0597 0.1422 0.1001 0.0421 0.117 1.837 1.962 86.912 0.207 8.726 10.237 0.22 73083. 0.6010
|
|
4.75 0.0896 0.2066 0.0990 0.0429 0.119 1.874 1.939 88.692 0.212 8.627 9.918 0.22 73156. 0.5789
|
|
6.34 0.1195 0.2667 0.0977 0.0438 0.121 1.911 1.915 90.448 0.216 8.516 9.601 0.22 73236. 0.5568
|
|
7.92 0.1493 0.3224 0.0963 0.0446 0.124 1.947 1.887 92.143 0.220 8.392 9.288 0.22 73324. 0.5347
|
|
9.50 0.1792 0.3741 0.0947 0.0454 0.126 1.981 1.856 93.734 0.224 8.254 8.979 0.22 73421. 0.5127
|
|
11.09 0.2091 0.4217 0.0930 0.0461 0.128 2.011 1.821 95.176 0.227 8.099 8.677 0.22 73526. 0.4908
|
|
12.67 0.2389 0.4657 0.0910 0.0467 0.129 2.037 1.782 96.418 0.230 7.927 8.383 0.22 73640. 0.4690
|
|
14.25 0.2688 0.5060 0.0888 0.0472 0.131 2.058 1.739 97.406 0.233 7.735 8.097 0.22 73764. 0.4475
|
|
15.84 0.2987 0.5430 0.0863 0.0475 0.132 2.073 1.691 98.083 0.234 7.522 7.821 0.22 73896. 0.4263
|
|
17.42 0.3285 0.5769 0.0836 0.0476 0.132 2.079 1.638 98.393 0.235 7.288 7.553 0.22 74039. 0.4052
|
|
19.01 0.3584 0.6077 0.0807 0.0476 0.132 2.077 1.580 98.279 0.235 7.030 7.294 0.22 74191. 0.3843
|
|
20.59 0.3883 0.6358 0.0775 0.0473 0.131 2.064 1.517 97.687 0.233 6.748 7.044 0.22 74352. 0.3636
|
|
22.17 0.4181 0.6611 0.0739 0.0468 0.130 2.041 1.448 96.573 0.231 6.442 6.802 0.22 74524. 0.3431
|
|
23.76 0.4480 0.6838 0.0701 0.0459 0.127 2.005 1.374 94.898 0.227 6.110 6.566 0.22 74705. 0.3225
|
|
25.34 0.4778 0.7038 0.0661 0.0448 0.124 1.957 1.294 92.634 0.221 5.755 6.335 0.22 74896. 0.3020
|
|
26.92 0.5077 0.7209 0.0617 0.0435 0.120 1.897 1.209 89.763 0.214 5.376 6.107 0.23 75097. 0.2814
|
|
28.51 0.5376 0.7349 0.0571 0.0418 0.116 1.823 1.119 86.280 0.206 4.975 5.880 0.23 75307. 0.2606
|
|
30.09 0.5674 0.7454 0.0523 0.0398 0.110 1.737 1.024 82.213 0.196 4.555 5.650 0.23 75526. 0.2396
|
|
31.68 0.5973 0.7518 0.0473 0.0376 0.104 1.640 0.926 77.604 0.185 4.120 5.414 0.23 75755. 0.2184
|
|
33.26 0.6272 0.7533 0.0422 0.0351 0.097 1.532 0.826 72.494 0.173 3.673 5.167 0.23 75994. 0.1968
|
|
34.84 0.6570 0.7487 0.0369 0.0324 0.090 1.414 0.723 66.917 0.160 3.217 4.902 0.23 76242. 0.1747
|
|
36.43 0.6869 0.7362 0.0316 0.0295 0.082 1.287 0.619 60.908 0.145 2.753 4.610 0.23 76499. 0.1520
|
|
38.01 0.7168 0.7128 0.0262 0.0264 0.073 1.152 0.514 54.504 0.130 2.286 4.277 0.23 76765. 0.1285
|
|
39.59 0.7466 0.6739 0.0209 0.0231 0.064 1.009 0.409 47.744 0.114 1.818 3.883 0.23 77041. 0.1040
|
|
41.18 0.7765 0.6115 0.0155 0.0197 0.055 0.860 0.304 40.676 0.097 1.351 3.387 0.23 77326. 0.0783
|
|
42.76 0.8064 0.5099 0.0102 0.0161 0.045 0.705 0.200 33.355 0.080 0.890 2.720 0.23 77619. 0.0510
|
|
44.35 0.8362 0.3351 0.0050 0.0125 0.035 0.546 0.098 25.847 0.062 0.437 1.724 0.23 77922. 0.0226
|
|
45.93 0.8661 -0.0039 0.0000 0.0088 0.024 0.385 -0.001 18.220 0.043 -0.003 -0.019 0.23 78233. 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 0.1024 0.0398 0.215 2.715 3.133 160.584 0.307 13.934 8.848 0.28 91197. 0.6564
|
|
1.98 0.0299 0.0746 0.1015 0.0407 0.220 2.773 3.105 164.031 0.313 13.812 8.586 0.28 91270. 0.6341
|
|
3.96 0.0598 0.1446 0.1004 0.0415 0.225 2.832 3.074 167.554 0.320 13.675 8.322 0.28 91352. 0.6116
|
|
5.94 0.0897 0.2100 0.0993 0.0424 0.229 2.892 3.040 171.095 0.327 13.522 8.059 0.28 91443. 0.5889
|
|
7.93 0.1196 0.2710 0.0981 0.0433 0.234 2.951 3.001 174.592 0.333 13.350 7.797 0.28 91543. 0.5662
|
|
9.91 0.1495 0.3275 0.0967 0.0441 0.239 3.009 2.958 177.974 0.340 13.158 7.539 0.28 91654. 0.5435
|
|
11.89 0.1794 0.3797 0.0951 0.0449 0.243 3.062 2.910 181.155 0.346 12.943 7.286 0.28 91775. 0.5209
|
|
13.87 0.2093 0.4280 0.0933 0.0456 0.247 3.111 2.856 184.046 0.352 12.702 7.038 0.28 91907. 0.4984
|
|
15.85 0.2391 0.4723 0.0913 0.0462 0.250 3.153 2.795 186.545 0.356 12.433 6.796 0.28 92050. 0.4762
|
|
17.83 0.2690 0.5131 0.0891 0.0467 0.253 3.187 2.728 188.544 0.360 12.134 6.562 0.28 92204. 0.4543
|
|
19.82 0.2989 0.5504 0.0867 0.0471 0.255 3.211 2.653 189.933 0.363 11.802 6.336 0.28 92371. 0.4326
|
|
21.80 0.3288 0.5846 0.0840 0.0472 0.256 3.222 2.571 190.596 0.364 11.435 6.118 0.28 92549. 0.4111
|
|
23.78 0.3587 0.6158 0.0810 0.0472 0.255 3.219 2.480 190.423 0.364 11.031 5.907 0.28 92740. 0.3899
|
|
25.76 0.3886 0.6442 0.0778 0.0469 0.254 3.200 2.381 189.307 0.362 10.589 5.704 0.28 92942. 0.3689
|
|
27.74 0.4185 0.6698 0.0743 0.0464 0.251 3.164 2.273 187.156 0.357 10.108 5.508 0.28 93157. 0.3480
|
|
29.72 0.4484 0.6929 0.0704 0.0456 0.247 3.109 2.156 183.893 0.351 9.589 5.317 0.28 93384. 0.3272
|
|
31.71 0.4783 0.7132 0.0663 0.0445 0.241 3.034 2.030 179.463 0.343 9.031 5.131 0.28 93623. 0.3065
|
|
33.69 0.5082 0.7309 0.0620 0.0431 0.233 2.938 1.897 173.829 0.332 8.436 4.949 0.28 93874. 0.2856
|
|
35.67 0.5381 0.7455 0.0573 0.0414 0.224 2.823 1.755 166.976 0.319 7.806 4.767 0.28 94137. 0.2647
|
|
37.65 0.5680 0.7567 0.0525 0.0394 0.213 2.687 1.607 158.960 0.304 7.147 4.585 0.28 94413. 0.2436
|
|
39.63 0.5979 0.7641 0.0475 0.0371 0.201 2.533 1.453 149.865 0.286 6.464 4.398 0.28 94700. 0.2222
|
|
41.61 0.6278 0.7669 0.0423 0.0346 0.187 2.363 1.295 139.766 0.267 5.761 4.204 0.28 94998. 0.2005
|
|
43.59 0.6577 0.7637 0.0371 0.0319 0.173 2.176 1.134 128.734 0.246 5.045 3.996 0.28 95309. 0.1784
|
|
45.58 0.6876 0.7529 0.0317 0.0290 0.157 1.975 0.971 116.836 0.223 4.318 3.768 0.28 95631. 0.1556
|
|
47.56 0.7174 0.7318 0.0263 0.0258 0.140 1.761 0.806 104.145 0.199 3.585 3.510 0.28 95964. 0.1321
|
|
49.54 0.7473 0.6955 0.0209 0.0225 0.122 1.534 0.641 90.740 0.173 2.850 3.202 0.29 96309. 0.1074
|
|
51.52 0.7772 0.6358 0.0156 0.0190 0.103 1.297 0.476 76.717 0.147 2.118 2.815 0.29 96666. 0.0814
|
|
53.50 0.8071 0.5362 0.0102 0.0154 0.083 1.051 0.313 62.187 0.119 1.394 2.286 0.29 97034. 0.0536
|
|
55.48 0.8370 0.3591 0.0050 0.0117 0.063 0.799 0.154 47.282 0.090 0.685 1.476 0.29 97413. 0.0243
|
|
57.47 0.8669 -0.0041 0.0000 0.0080 0.043 0.543 -0.001 32.141 0.061 -0.005 -0.016 0.29 97802. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 6000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1027 0.0395 0.369 3.875 4.525 275.061 0.438 20.128 7.462 0.33 109433. 0.6653
|
|
2.38 0.0299 0.0755 0.1018 0.0403 0.377 3.960 4.486 281.104 0.447 19.954 7.239 0.33 109522. 0.6426
|
|
4.76 0.0598 0.1463 0.1008 0.0412 0.385 4.047 4.442 287.284 0.457 19.760 7.014 0.33 109620. 0.6196
|
|
7.14 0.0897 0.2124 0.0997 0.0421 0.394 4.135 4.394 293.504 0.467 19.543 6.790 0.33 109729. 0.5965
|
|
9.52 0.1196 0.2739 0.0984 0.0430 0.402 4.221 4.339 299.654 0.477 19.298 6.567 0.33 109850. 0.5733
|
|
11.89 0.1495 0.3310 0.0970 0.0438 0.410 4.305 4.277 305.608 0.486 19.024 6.348 0.33 109982. 0.5502
|
|
14.27 0.1794 0.3837 0.0955 0.0446 0.417 4.384 4.208 311.221 0.495 18.716 6.132 0.33 110128. 0.5272
|
|
16.65 0.2093 0.4323 0.0937 0.0454 0.424 4.456 4.130 316.331 0.503 18.371 5.922 0.33 110286. 0.5044
|
|
19.03 0.2392 0.4770 0.0917 0.0460 0.430 4.519 4.043 320.762 0.511 17.985 5.718 0.33 110458. 0.4819
|
|
21.41 0.2691 0.5180 0.0895 0.0465 0.435 4.569 3.947 324.326 0.516 17.555 5.519 0.33 110644. 0.4596
|
|
23.79 0.2990 0.5556 0.0871 0.0469 0.438 4.604 3.839 326.827 0.520 17.077 5.328 0.33 110844. 0.4376
|
|
26.17 0.3290 0.5901 0.0844 0.0471 0.440 4.621 3.720 328.063 0.522 16.549 5.144 0.34 111058. 0.4158
|
|
28.55 0.3589 0.6215 0.0814 0.0470 0.440 4.618 3.590 327.839 0.522 15.967 4.966 0.34 111287. 0.3944
|
|
30.92 0.3888 0.6501 0.0782 0.0468 0.437 4.592 3.446 325.968 0.519 15.329 4.795 0.34 111530. 0.3731
|
|
33.30 0.4187 0.6761 0.0747 0.0462 0.432 4.540 3.290 322.286 0.513 14.635 4.631 0.34 111788. 0.3520
|
|
35.68 0.4486 0.6994 0.0708 0.0454 0.425 4.461 3.121 316.659 0.504 13.884 4.471 0.34 112061. 0.3311
|
|
38.06 0.4785 0.7201 0.0667 0.0443 0.414 4.353 2.940 308.986 0.492 13.078 4.316 0.34 112348. 0.3102
|
|
40.44 0.5084 0.7382 0.0623 0.0429 0.401 4.215 2.747 299.200 0.476 12.217 4.164 0.34 112650. 0.2892
|
|
42.82 0.5383 0.7533 0.0577 0.0412 0.385 4.047 2.542 287.275 0.457 11.306 4.013 0.34 112966. 0.2682
|
|
45.20 0.5682 0.7653 0.0528 0.0392 0.367 3.850 2.327 273.306 0.435 10.351 3.862 0.34 113297. 0.2469
|
|
47.58 0.5981 0.7735 0.0478 0.0369 0.345 3.627 2.105 257.436 0.410 9.362 3.708 0.34 113641. 0.2255
|
|
49.95 0.6280 0.7772 0.0426 0.0344 0.322 3.378 1.876 239.796 0.382 8.346 3.549 0.34 114000. 0.2037
|
|
52.33 0.6579 0.7753 0.0373 0.0316 0.296 3.106 1.643 220.508 0.351 7.308 3.379 0.34 114373. 0.1815
|
|
54.71 0.6878 0.7661 0.0319 0.0286 0.268 2.813 1.406 199.691 0.318 6.255 3.194 0.34 114760. 0.1588
|
|
57.09 0.7177 0.7469 0.0265 0.0255 0.238 2.500 1.168 177.471 0.282 5.194 2.984 0.34 115160. 0.1351
|
|
59.47 0.7476 0.7129 0.0211 0.0221 0.207 2.169 0.928 153.991 0.245 4.130 2.735 0.34 115575. 0.1104
|
|
61.85 0.7775 0.6559 0.0157 0.0186 0.174 1.823 0.690 129.416 0.206 3.070 2.419 0.34 116003. 0.0842
|
|
64.23 0.8074 0.5588 0.0103 0.0149 0.139 1.464 0.455 103.946 0.165 2.023 1.984 0.34 116445. 0.0561
|
|
66.61 0.8373 0.3813 0.0051 0.0112 0.104 1.096 0.224 77.813 0.124 0.996 1.306 0.34 116900. 0.0259
|
|
68.98 0.8672 -0.0007 0.0000 0.0074 0.069 0.722 0.000 51.261 0.082 -0.001 -0.002 0.35 117367. 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 0.1030 0.0393 0.583 5.248 6.181 434.667 0.593 27.495 6.450 0.39 127669. 0.6721
|
|
2.78 0.0299 0.0762 0.1022 0.0401 0.596 5.366 6.129 444.401 0.606 27.263 6.256 0.39 127771. 0.6491
|
|
5.55 0.0598 0.1476 0.1012 0.0410 0.609 5.486 6.071 454.365 0.620 27.003 6.060 0.39 127886. 0.6258
|
|
8.33 0.0898 0.2142 0.1001 0.0420 0.623 5.608 6.005 464.404 0.634 26.711 5.865 0.39 128014. 0.6024
|
|
11.11 0.1197 0.2762 0.0989 0.0429 0.636 5.728 5.931 474.343 0.647 26.382 5.672 0.39 128155. 0.5789
|
|
13.88 0.1496 0.3336 0.0975 0.0437 0.649 5.844 5.848 483.976 0.660 26.013 5.481 0.39 128310. 0.5555
|
|
16.66 0.1795 0.3867 0.0959 0.0445 0.661 5.954 5.755 493.070 0.673 25.597 5.294 0.39 128479. 0.5322
|
|
19.44 0.2095 0.4356 0.0942 0.0453 0.672 6.054 5.650 501.365 0.684 25.130 5.111 0.39 128664. 0.5092
|
|
22.22 0.2394 0.4805 0.0922 0.0459 0.682 6.141 5.532 508.575 0.694 24.607 4.934 0.39 128865. 0.4864
|
|
24.99 0.2693 0.5218 0.0900 0.0465 0.690 6.211 5.401 514.398 0.702 24.023 4.762 0.39 129082. 0.4639
|
|
27.77 0.2992 0.5596 0.0876 0.0468 0.695 6.261 5.255 518.515 0.707 23.374 4.597 0.39 129316. 0.4416
|
|
30.55 0.3292 0.5942 0.0849 0.0470 0.698 6.286 5.093 520.603 0.710 22.654 4.437 0.39 129566. 0.4197
|
|
33.32 0.3591 0.6258 0.0819 0.0470 0.698 6.283 4.915 520.342 0.710 21.860 4.284 0.39 129834. 0.3980
|
|
36.10 0.3890 0.6547 0.0787 0.0467 0.694 6.248 4.719 517.431 0.706 20.990 4.137 0.39 130119. 0.3766
|
|
38.88 0.4189 0.6808 0.0751 0.0462 0.686 6.177 4.506 511.604 0.698 20.042 3.995 0.39 130420. 0.3554
|
|
41.65 0.4488 0.7045 0.0713 0.0454 0.674 6.069 4.275 502.640 0.686 19.015 3.858 0.39 130739. 0.3343
|
|
44.43 0.4788 0.7255 0.0671 0.0443 0.658 5.921 4.027 490.379 0.669 17.912 3.725 0.39 131075. 0.3133
|
|
47.21 0.5087 0.7439 0.0627 0.0429 0.637 5.732 3.762 474.709 0.648 16.734 3.595 0.39 131427. 0.2922
|
|
49.98 0.5386 0.7595 0.0580 0.0412 0.611 5.501 3.481 455.587 0.622 15.485 3.466 0.39 131797. 0.2710
|
|
52.76 0.5685 0.7720 0.0531 0.0391 0.581 5.230 3.187 433.160 0.591 14.177 3.338 0.40 132183. 0.2497
|
|
55.54 0.5985 0.7809 0.0481 0.0368 0.547 4.922 2.883 407.657 0.556 12.822 3.207 0.40 132586. 0.2282
|
|
58.32 0.6284 0.7855 0.0428 0.0343 0.509 4.580 2.569 379.290 0.517 11.428 3.072 0.40 133005. 0.2064
|
|
61.09 0.6583 0.7846 0.0375 0.0315 0.467 4.205 2.249 348.251 0.475 10.005 2.930 0.40 133441. 0.1842
|
|
63.87 0.6882 0.7767 0.0321 0.0284 0.422 3.800 1.925 314.734 0.429 8.562 2.774 0.40 133893. 0.1613
|
|
66.65 0.7181 0.7590 0.0266 0.0252 0.374 3.368 1.598 278.940 0.381 7.107 2.598 0.40 134361. 0.1376
|
|
69.42 0.7481 0.7270 0.0212 0.0218 0.323 2.911 1.270 241.104 0.329 5.648 2.389 0.40 134845. 0.1128
|
|
72.20 0.7780 0.6721 0.0157 0.0182 0.270 2.433 0.943 201.494 0.275 4.196 2.123 0.40 135345. 0.0864
|
|
74.98 0.8079 0.5767 0.0103 0.0145 0.215 1.937 0.621 160.434 0.219 2.760 1.754 0.40 135861. 0.0579
|
|
77.75 0.8378 0.3977 0.0051 0.0107 0.159 1.428 0.304 118.305 0.161 1.354 1.167 0.40 136393. 0.0270
|
|
80.53 0.8678 -0.0061 0.0000 0.0068 0.101 0.912 -0.003 75.501 0.103 -0.013 -0.017 0.40 136938. 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 0.1035 0.0392 0.869 6.843 8.107 647.660 0.773 36.058 5.677 0.44 145902. 0.6775
|
|
3.17 0.0299 0.0766 0.1026 0.0401 0.888 6.998 8.040 662.395 0.791 35.762 5.505 0.44 146019. 0.6543
|
|
6.35 0.0598 0.1484 0.1017 0.0410 0.909 7.158 7.965 677.492 0.809 35.430 5.333 0.44 146151. 0.6308
|
|
9.52 0.0898 0.2153 0.1006 0.0419 0.929 7.319 7.881 692.719 0.827 35.055 5.160 0.44 146296. 0.6072
|
|
12.69 0.1197 0.2776 0.0994 0.0428 0.949 7.478 7.786 707.813 0.845 34.633 4.989 0.44 146457. 0.5835
|
|
15.87 0.1496 0.3353 0.0980 0.0437 0.969 7.633 7.679 722.464 0.862 34.157 4.821 0.44 146634. 0.5599
|
|
19.04 0.1795 0.3886 0.0965 0.0446 0.987 7.779 7.558 736.316 0.879 33.620 4.656 0.44 146829. 0.5365
|
|
22.21 0.2094 0.4377 0.0947 0.0453 1.004 7.913 7.423 748.976 0.894 33.016 4.495 0.45 147040. 0.5133
|
|
25.38 0.2393 0.4828 0.0928 0.0460 1.019 8.030 7.270 760.010 0.907 32.337 4.339 0.45 147270. 0.4903
|
|
28.56 0.2693 0.5243 0.0906 0.0465 1.031 8.124 7.099 768.960 0.918 31.578 4.188 0.45 147518. 0.4676
|
|
31.73 0.2992 0.5622 0.0882 0.0469 1.040 8.192 6.909 775.341 0.925 30.733 4.042 0.45 147785. 0.4453
|
|
34.90 0.3291 0.5970 0.0855 0.0471 1.044 8.227 6.698 778.663 0.929 29.794 3.902 0.45 148072. 0.4232
|
|
38.08 0.3590 0.6288 0.0825 0.0471 1.044 8.224 6.465 778.438 0.929 28.758 3.767 0.45 148377. 0.4015
|
|
41.25 0.3889 0.6578 0.0793 0.0469 1.038 8.180 6.209 774.210 0.924 27.620 3.638 0.45 148703. 0.3799
|
|
44.42 0.4188 0.6842 0.0757 0.0463 1.027 8.088 5.930 765.569 0.914 26.378 3.513 0.45 149048. 0.3586
|
|
47.60 0.4488 0.7081 0.0718 0.0455 1.009 7.947 5.628 752.182 0.898 25.033 3.394 0.45 149412. 0.3374
|
|
50.77 0.4787 0.7294 0.0677 0.0444 0.984 7.753 5.302 733.802 0.876 23.585 3.277 0.45 149796. 0.3163
|
|
53.94 0.5086 0.7482 0.0632 0.0430 0.952 7.504 4.955 710.255 0.848 22.038 3.164 0.45 150199. 0.2952
|
|
57.11 0.5385 0.7642 0.0585 0.0412 0.914 7.200 4.586 681.474 0.813 20.398 3.052 0.45 150622. 0.2740
|
|
60.29 0.5684 0.7773 0.0536 0.0392 0.869 6.843 4.199 647.672 0.773 18.679 2.941 0.45 151063. 0.2526
|
|
63.46 0.5983 0.7868 0.0485 0.0369 0.817 6.436 3.799 609.192 0.727 16.896 2.828 0.45 151524. 0.2310
|
|
66.63 0.6283 0.7922 0.0432 0.0343 0.759 5.984 3.386 566.353 0.676 15.063 2.712 0.45 152003. 0.2092
|
|
69.81 0.6582 0.7924 0.0378 0.0314 0.697 5.488 2.965 519.448 0.620 13.190 2.589 0.45 152501. 0.1869
|
|
72.98 0.6881 0.7858 0.0324 0.0284 0.629 4.953 2.538 468.766 0.560 11.291 2.456 0.45 153017. 0.1640
|
|
76.15 0.7180 0.7697 0.0269 0.0251 0.556 4.381 2.108 414.616 0.495 9.375 2.306 0.46 153552. 0.1403
|
|
79.33 0.7479 0.7397 0.0214 0.0216 0.479 3.776 1.676 357.351 0.427 7.454 2.127 0.46 154105. 0.1154
|
|
82.50 0.7778 0.6872 0.0159 0.0180 0.399 3.142 1.246 297.383 0.355 5.541 1.900 0.46 154677. 0.0889
|
|
85.67 0.8078 0.5945 0.0105 0.0142 0.315 2.485 0.821 235.203 0.281 3.651 1.583 0.46 155267. 0.0601
|
|
88.84 0.8377 0.4169 0.0052 0.0104 0.230 1.811 0.404 171.394 0.205 1.799 1.070 0.46 155874. 0.0285
|
|
92.02 0.8676 -0.0002 0.0000 0.0064 0.143 1.126 0.000 106.558 0.127 -0.001 -0.001 0.46 156496. 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 0.1039 0.0392 1.238 8.667 10.307 922.855 0.979 45.846 5.066 0.50 164133. 0.6816
|
|
3.57 0.0299 0.0769 0.1031 0.0401 1.266 8.867 10.225 944.151 1.002 45.481 4.912 0.50 164265. 0.6583
|
|
7.14 0.0598 0.1489 0.1022 0.0411 1.295 9.072 10.133 966.001 1.025 45.071 4.758 0.50 164413. 0.6347
|
|
10.71 0.0898 0.2162 0.1011 0.0420 1.325 9.279 10.029 988.069 1.048 44.608 4.604 0.50 164577. 0.6110
|
|
14.28 0.1197 0.2787 0.0999 0.0429 1.354 9.485 9.911 1009.970 1.072 44.083 4.451 0.50 164758. 0.5873
|
|
17.85 0.1496 0.3365 0.0986 0.0438 1.383 9.685 9.778 1031.257 1.094 43.490 4.300 0.50 164958. 0.5636
|
|
21.42 0.1795 0.3900 0.0971 0.0447 1.410 9.874 9.627 1051.417 1.116 42.820 4.153 0.50 165176. 0.5400
|
|
24.99 0.2094 0.4392 0.0954 0.0455 1.435 10.048 9.457 1069.875 1.135 42.063 4.009 0.50 165414. 0.5167
|
|
28.56 0.2394 0.4845 0.0934 0.0462 1.456 10.199 9.265 1086.004 1.152 41.212 3.870 0.50 165673. 0.4937
|
|
32.13 0.2693 0.5261 0.0913 0.0467 1.474 10.322 9.050 1099.134 1.166 40.256 3.735 0.50 165953. 0.4709
|
|
35.70 0.2992 0.5642 0.0888 0.0471 1.487 10.411 8.811 1108.564 1.176 39.189 3.605 0.50 166254. 0.4485
|
|
39.27 0.3291 0.5991 0.0862 0.0473 1.493 10.458 8.544 1113.580 1.182 38.003 3.480 0.50 166576. 0.4263
|
|
42.84 0.3591 0.6311 0.0832 0.0473 1.493 10.457 8.249 1113.474 1.181 36.691 3.360 0.50 166921. 0.4045
|
|
46.41 0.3890 0.6603 0.0799 0.0471 1.485 10.402 7.924 1107.578 1.175 35.247 3.245 0.50 167287. 0.3829
|
|
49.98 0.4189 0.6869 0.0763 0.0466 1.469 10.286 7.570 1095.299 1.162 33.670 3.135 0.50 167676. 0.3615
|
|
53.55 0.4488 0.7110 0.0725 0.0457 1.443 10.107 7.185 1076.147 1.142 31.959 3.028 0.50 168086. 0.3402
|
|
57.12 0.4787 0.7326 0.0683 0.0446 1.408 9.859 6.771 1049.761 1.114 30.116 2.925 0.51 168519. 0.3190
|
|
60.69 0.5087 0.7517 0.0638 0.0432 1.362 9.541 6.328 1015.894 1.078 28.145 2.825 0.51 168973. 0.2978
|
|
64.26 0.5386 0.7681 0.0591 0.0414 1.307 9.151 5.858 974.438 1.034 26.054 2.726 0.51 169449. 0.2766
|
|
67.83 0.5685 0.7816 0.0541 0.0393 1.241 8.694 5.364 925.697 0.982 23.861 2.628 0.51 169946. 0.2551
|
|
71.40 0.5984 0.7918 0.0489 0.0370 1.167 8.172 4.853 870.161 0.923 21.585 2.529 0.51 170464. 0.2335
|
|
74.97 0.6283 0.7979 0.0436 0.0344 1.084 7.591 4.326 808.289 0.858 19.243 2.428 0.51 171004. 0.2116
|
|
78.54 0.6583 0.7990 0.0382 0.0315 0.993 6.954 3.788 740.507 0.786 16.851 2.320 0.51 171564. 0.1893
|
|
82.11 0.6882 0.7935 0.0327 0.0284 0.895 6.266 3.243 667.234 0.708 14.423 2.204 0.51 172146. 0.1664
|
|
85.68 0.7181 0.7788 0.0271 0.0250 0.790 5.531 2.692 588.919 0.625 11.974 2.073 0.51 172748. 0.1426
|
|
89.25 0.7480 0.7504 0.0216 0.0215 0.679 4.753 2.140 506.075 0.537 9.518 1.918 0.51 173370. 0.1176
|
|
92.82 0.7780 0.6999 0.0160 0.0178 0.562 3.938 1.590 419.301 0.445 7.072 1.720 0.51 174014. 0.0909
|
|
96.39 0.8079 0.6092 0.0106 0.0140 0.442 3.093 1.047 329.316 0.349 4.655 1.441 0.52 174678. 0.0618
|
|
99.96 0.8378 0.4312 0.0052 0.0101 0.318 2.225 0.514 236.972 0.251 2.287 0.984 0.52 175361. 0.0296
|
|
103.53 0.8677 -0.0046 0.0000 0.0061 0.192 1.344 -0.003 143.141 0.152 -0.014 -0.010 0.52 176061. 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 0.1045 0.0393 1.703 10.732 12.790 1269.764 1.213 56.890 4.569 0.56 182362. 0.6848
|
|
3.97 0.0299 0.0770 0.1037 0.0403 1.743 10.983 12.692 1299.451 1.241 56.455 4.430 0.56 182509. 0.6615
|
|
7.93 0.0598 0.1492 0.1028 0.0412 1.783 11.241 12.582 1329.954 1.270 55.964 4.291 0.56 182673. 0.6379
|
|
11.90 0.0898 0.2166 0.1018 0.0422 1.825 11.502 12.457 1360.804 1.299 55.408 4.152 0.56 182855. 0.6142
|
|
15.87 0.1197 0.2792 0.1006 0.0431 1.866 11.761 12.315 1391.471 1.329 54.776 4.014 0.56 183056. 0.5904
|
|
19.83 0.1496 0.3372 0.0993 0.0440 1.906 12.013 12.154 1421.327 1.357 54.059 3.878 0.56 183278. 0.5667
|
|
23.80 0.1795 0.3908 0.0978 0.0449 1.944 12.253 11.971 1449.649 1.384 53.246 3.745 0.56 183521. 0.5431
|
|
27.76 0.2094 0.4401 0.0961 0.0457 1.979 12.472 11.764 1475.635 1.409 52.324 3.616 0.56 183785. 0.5198
|
|
31.73 0.2393 0.4855 0.0942 0.0464 2.009 12.665 11.530 1498.405 1.431 51.284 3.490 0.56 184073. 0.4967
|
|
35.70 0.2693 0.5272 0.0920 0.0470 2.034 12.822 11.267 1517.017 1.449 50.114 3.369 0.56 184384. 0.4739
|
|
39.66 0.2992 0.5654 0.0896 0.0474 2.052 12.936 10.972 1530.489 1.462 48.803 3.252 0.56 184719. 0.4514
|
|
43.63 0.3291 0.6004 0.0869 0.0476 2.062 12.998 10.643 1537.815 1.469 47.342 3.139 0.56 185078. 0.4292
|
|
47.60 0.3590 0.6325 0.0840 0.0477 2.062 13.000 10.279 1538.005 1.469 45.722 3.031 0.56 185461. 0.4073
|
|
51.56 0.3889 0.6619 0.0807 0.0474 2.052 12.933 9.878 1530.117 1.461 43.937 2.928 0.56 185868. 0.3857
|
|
55.53 0.4188 0.6887 0.0771 0.0469 2.029 12.791 9.439 1513.318 1.445 41.984 2.829 0.56 186301. 0.3643
|
|
59.50 0.4488 0.7130 0.0732 0.0461 1.994 12.568 8.961 1486.920 1.420 39.861 2.734 0.56 186757. 0.3430
|
|
63.46 0.4787 0.7349 0.0690 0.0449 1.945 12.259 8.447 1450.414 1.385 37.571 2.641 0.56 187238. 0.3218
|
|
67.43 0.5086 0.7543 0.0645 0.0435 1.882 11.862 7.896 1403.452 1.340 35.121 2.552 0.56 187743. 0.3005
|
|
71.39 0.5385 0.7712 0.0597 0.0417 1.805 11.376 7.311 1345.880 1.285 32.519 2.464 0.56 188272. 0.2792
|
|
75.36 0.5684 0.7851 0.0547 0.0396 1.714 10.803 6.697 1278.104 1.220 29.787 2.377 0.56 188825. 0.2578
|
|
79.33 0.5983 0.7959 0.0495 0.0372 1.610 10.150 6.059 1200.807 1.147 26.950 2.289 0.57 189402. 0.2361
|
|
83.29 0.6283 0.8027 0.0441 0.0345 1.495 9.421 5.402 1114.629 1.064 24.029 2.198 0.57 190001. 0.2141
|
|
87.26 0.6582 0.8047 0.0386 0.0316 1.368 8.623 4.731 1020.163 0.974 21.044 2.104 0.57 190624. 0.1918
|
|
91.23 0.6881 0.8002 0.0331 0.0284 1.231 7.759 4.050 917.998 0.877 18.014 2.001 0.57 191270. 0.1688
|
|
95.19 0.7180 0.7869 0.0275 0.0251 1.085 6.836 3.362 808.762 0.772 14.955 1.886 0.57 191939. 0.1449
|
|
99.16 0.7479 0.7602 0.0218 0.0215 0.930 5.859 2.673 693.172 0.662 11.887 1.749 0.57 192631. 0.1198
|
|
103.12 0.7779 0.7117 0.0162 0.0177 0.767 4.835 1.986 572.073 0.546 8.832 1.574 0.57 193346. 0.0930
|
|
107.09 0.8078 0.6231 0.0107 0.0138 0.599 3.774 1.306 446.472 0.426 5.811 1.327 0.57 194083. 0.0636
|
|
111.06 0.8377 0.4457 0.0052 0.0098 0.426 2.684 0.641 317.573 0.303 2.851 0.915 0.57 194843. 0.0307
|
|
115.02 0.8676 -0.0068 0.0000 0.0058 0.250 1.577 -0.006 186.599 0.178 -0.025 -0.014 0.58 195620. 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 0.1051 0.0395 2.278 13.054 15.564 1698.823 1.475 69.227 4.155 0.61 200587. 0.6871
|
|
4.36 0.0299 0.0771 0.1043 0.0405 2.332 13.362 15.450 1739.035 1.510 68.724 4.030 0.61 200749. 0.6639
|
|
8.72 0.0598 0.1493 0.1034 0.0414 2.388 13.680 15.322 1780.420 1.546 68.152 3.903 0.61 200929. 0.6404
|
|
13.09 0.0897 0.2167 0.1024 0.0424 2.444 14.003 15.176 1822.354 1.582 67.502 3.777 0.61 201129. 0.6167
|
|
17.45 0.1196 0.2793 0.1013 0.0434 2.500 14.324 15.009 1864.114 1.618 66.761 3.652 0.61 201351. 0.5930
|
|
21.81 0.1495 0.3374 0.1000 0.0443 2.554 14.637 14.819 1904.844 1.654 65.916 3.529 0.61 201594. 0.5693
|
|
26.17 0.1795 0.3910 0.0986 0.0452 2.606 14.934 14.603 1943.562 1.687 64.953 3.408 0.61 201862. 0.5458
|
|
30.53 0.2094 0.4404 0.0969 0.0461 2.654 15.208 14.356 1979.171 1.718 63.858 3.290 0.61 202153. 0.5225
|
|
34.89 0.2393 0.4858 0.0950 0.0468 2.696 15.448 14.077 2010.468 1.745 62.616 3.176 0.61 202470. 0.4994
|
|
39.26 0.2692 0.5276 0.0929 0.0474 2.731 15.646 13.762 2036.167 1.768 61.214 3.066 0.61 202812. 0.4766
|
|
43.62 0.2991 0.5659 0.0905 0.0478 2.756 15.790 13.408 2054.922 1.784 59.639 2.959 0.61 203181. 0.4542
|
|
47.98 0.3290 0.6010 0.0878 0.0481 2.770 15.870 13.012 2065.364 1.793 57.877 2.858 0.61 203576. 0.4320
|
|
52.34 0.3589 0.6333 0.0849 0.0481 2.771 15.876 12.572 2066.135 1.794 55.920 2.760 0.61 203998. 0.4101
|
|
56.70 0.3888 0.6628 0.0816 0.0479 2.757 15.798 12.086 2055.950 1.785 53.758 2.666 0.62 204446. 0.3885
|
|
61.06 0.4187 0.6898 0.0780 0.0473 2.727 15.626 11.553 2033.668 1.765 51.386 2.577 0.62 204922. 0.3670
|
|
65.43 0.4486 0.7143 0.0741 0.0465 2.680 15.355 10.972 1998.346 1.735 48.805 2.490 0.62 205425. 0.3457
|
|
69.79 0.4785 0.7365 0.0698 0.0454 2.614 14.978 10.345 1949.289 1.692 46.016 2.407 0.62 205954. 0.3245
|
|
74.15 0.5085 0.7562 0.0653 0.0439 2.529 14.492 9.674 1886.023 1.637 43.028 2.326 0.62 206510. 0.3033
|
|
78.51 0.5384 0.7735 0.0605 0.0421 2.425 13.895 8.959 1808.332 1.570 39.852 2.247 0.62 207093. 0.2819
|
|
82.87 0.5683 0.7879 0.0554 0.0400 2.302 13.191 8.209 1716.749 1.490 36.513 2.169 0.62 207701. 0.2604
|
|
87.23 0.5982 0.7993 0.0501 0.0375 2.162 12.388 7.429 1612.189 1.400 33.042 2.090 0.62 208335. 0.2387
|
|
91.60 0.6281 0.8068 0.0447 0.0348 2.006 11.491 6.625 1495.530 1.298 29.467 2.009 0.62 208995. 0.2167
|
|
95.96 0.6580 0.8096 0.0392 0.0318 1.834 10.508 5.803 1367.575 1.187 25.811 1.925 0.62 209681. 0.1943
|
|
100.32 0.6879 0.8062 0.0335 0.0286 1.648 9.444 4.968 1229.124 1.067 22.097 1.833 0.63 210392. 0.1713
|
|
104.68 0.7178 0.7942 0.0278 0.0252 1.450 8.307 4.125 1081.034 0.938 18.346 1.731 0.63 211127. 0.1473
|
|
109.04 0.7477 0.7691 0.0221 0.0215 1.239 7.102 3.279 924.282 0.802 14.584 1.609 0.63 211888. 0.1221
|
|
113.41 0.7776 0.7227 0.0164 0.0177 1.019 5.840 2.436 760.017 0.660 10.834 1.454 0.63 212675. 0.0951
|
|
117.77 0.8075 0.6363 0.0108 0.0137 0.791 4.531 1.602 589.621 0.512 7.126 1.232 0.63 213485. 0.0654
|
|
122.13 0.8375 0.4597 0.0053 0.0097 0.556 3.187 0.785 414.739 0.360 3.492 0.859 0.63 214321. 0.0319
|
|
126.49 0.8674 -0.0091 -0.0001 0.0055 0.318 1.821 -0.009 237.045 0.206 -0.038 -0.016 0.63 215175. 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 0.1057 0.0399 2.982 15.662 18.637 2223.606 1.769 82.898 3.802 0.67 218810. 0.6878
|
|
4.75 0.0299 0.0769 0.1050 0.0408 3.053 16.033 18.510 2276.315 1.811 82.330 3.688 0.67 218985. 0.6650
|
|
9.51 0.0598 0.1490 0.1042 0.0418 3.126 16.417 18.364 2330.750 1.855 81.684 3.574 0.67 219182. 0.6419
|
|
14.26 0.0896 0.2163 0.1032 0.0428 3.200 16.807 18.198 2386.101 1.899 80.944 3.459 0.67 219400. 0.6185
|
|
19.01 0.1195 0.2789 0.1021 0.0438 3.274 17.196 18.007 2441.425 1.943 80.097 3.345 0.67 219641. 0.5950
|
|
23.77 0.1494 0.3369 0.1009 0.0447 3.347 17.578 17.789 2495.592 1.986 79.126 3.233 0.67 219907. 0.5715
|
|
28.52 0.1793 0.3905 0.0995 0.0457 3.416 17.942 17.539 2547.280 2.027 78.013 3.123 0.67 220198. 0.5482
|
|
33.28 0.2092 0.4399 0.0979 0.0465 3.480 18.278 17.253 2595.010 2.065 76.740 3.016 0.67 220516. 0.5250
|
|
38.03 0.2390 0.4854 0.0960 0.0473 3.536 18.575 16.927 2637.147 2.099 75.290 2.911 0.67 220861. 0.5020
|
|
42.78 0.2689 0.5272 0.0939 0.0479 3.583 18.820 16.557 2671.951 2.126 73.646 2.811 0.67 221234. 0.4793
|
|
47.54 0.2988 0.5655 0.0916 0.0484 3.618 19.001 16.140 2697.606 2.147 71.790 2.714 0.67 221636. 0.4569
|
|
52.29 0.3287 0.6008 0.0889 0.0486 3.637 19.104 15.672 2712.282 2.158 69.708 2.621 0.67 222067. 0.4348
|
|
57.04 0.3586 0.6331 0.0859 0.0487 3.640 19.117 15.150 2714.170 2.160 67.387 2.532 0.67 222527. 0.4130
|
|
61.80 0.3884 0.6628 0.0827 0.0484 3.623 19.028 14.572 2701.549 2.150 64.816 2.447 0.67 223017. 0.3914
|
|
66.55 0.4183 0.6900 0.0791 0.0479 3.584 18.827 13.936 2672.890 2.127 61.988 2.365 0.67 223536. 0.3700
|
|
71.31 0.4482 0.7148 0.0751 0.0471 3.523 18.503 13.243 2626.932 2.090 58.904 2.287 0.67 224084. 0.3487
|
|
76.06 0.4781 0.7372 0.0709 0.0460 3.437 18.051 12.492 2562.744 2.039 55.566 2.211 0.67 224662. 0.3275
|
|
80.81 0.5080 0.7573 0.0663 0.0445 3.325 17.466 11.687 2479.698 1.973 51.983 2.138 0.68 225268. 0.3063
|
|
85.57 0.5379 0.7750 0.0614 0.0426 3.188 16.746 10.829 2377.496 1.892 48.169 2.066 0.68 225903. 0.2849
|
|
90.32 0.5677 0.7900 0.0563 0.0405 3.026 15.896 9.927 2256.795 1.796 44.154 1.995 0.68 226567. 0.2634
|
|
95.07 0.5976 0.8019 0.0510 0.0380 2.841 14.924 8.987 2118.812 1.686 39.976 1.924 0.68 227258. 0.2417
|
|
99.83 0.6275 0.8102 0.0455 0.0352 2.635 13.838 8.019 1964.707 1.563 35.669 1.851 0.68 227978. 0.2197
|
|
104.58 0.6574 0.8139 0.0399 0.0322 2.408 12.647 7.028 1795.550 1.429 31.260 1.775 0.68 228725. 0.1972
|
|
109.34 0.6873 0.8117 0.0341 0.0289 2.162 11.357 6.020 1612.407 1.283 26.777 1.693 0.68 229499. 0.1741
|
|
114.09 0.7171 0.8011 0.0284 0.0254 1.899 9.977 5.002 1416.414 1.127 22.248 1.602 0.68 230301. 0.1501
|
|
118.84 0.7470 0.7779 0.0226 0.0217 1.621 8.515 3.979 1208.870 0.962 17.700 1.493 0.68 231130. 0.1248
|
|
123.60 0.7769 0.7339 0.0168 0.0178 1.329 6.982 2.960 991.318 0.789 13.167 1.354 0.69 231987. 0.0977
|
|
128.35 0.8068 0.6506 0.0111 0.0137 1.027 5.393 1.952 765.639 0.609 8.681 1.156 0.69 232870. 0.0677
|
|
133.10 0.8367 0.4771 0.0055 0.0096 0.716 3.762 0.963 534.118 0.425 4.282 0.818 0.69 233780. 0.0336
|
|
137.86 0.8665 0.0016 0.0000 0.0054 0.401 2.107 0.002 299.155 0.238 0.008 0.003 0.69 234711. 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 0.1064 0.0407 3.867 18.750 22.017 2883.776 2.118 97.933 3.463 0.72 237028. 0.6810
|
|
5.15 0.0299 0.0759 0.1057 0.0416 3.955 19.175 21.878 2949.247 2.166 97.312 3.365 0.72 237218. 0.6596
|
|
10.29 0.0597 0.1473 0.1050 0.0425 4.046 19.616 21.718 3016.994 2.216 96.600 3.265 0.72 237430. 0.6377
|
|
15.44 0.0896 0.2142 0.1041 0.0435 4.138 20.064 21.534 3086.023 2.267 95.783 3.165 0.72 237666. 0.6156
|
|
20.58 0.1194 0.2766 0.1031 0.0445 4.231 20.514 21.322 3155.179 2.318 94.839 3.065 0.72 237927. 0.5932
|
|
25.73 0.1493 0.3346 0.1019 0.0455 4.322 20.956 21.077 3223.074 2.368 93.750 2.966 0.72 238214. 0.5707
|
|
30.88 0.1792 0.3883 0.1005 0.0464 4.409 21.378 20.794 3288.076 2.415 92.493 2.868 0.72 238530. 0.5482
|
|
36.02 0.2090 0.4379 0.0989 0.0472 4.490 21.770 20.469 3348.332 2.460 91.046 2.773 0.72 238874. 0.5258
|
|
41.17 0.2389 0.4836 0.0971 0.0480 4.562 22.118 20.096 3401.806 2.499 89.387 2.679 0.72 239248. 0.5034
|
|
46.32 0.2687 0.5257 0.0951 0.0486 4.622 22.407 19.670 3446.275 2.532 87.494 2.589 0.72 239652. 0.4812
|
|
51.46 0.2986 0.5643 0.0927 0.0491 4.666 22.622 19.187 3479.392 2.556 85.346 2.501 0.73 240088. 0.4592
|
|
56.61 0.3285 0.5998 0.0901 0.0493 4.692 22.748 18.643 3498.732 2.570 82.924 2.417 0.73 240555. 0.4374
|
|
61.75 0.3583 0.6324 0.0872 0.0494 4.696 22.768 18.033 3501.837 2.572 80.212 2.336 0.73 241054. 0.4157
|
|
66.90 0.3882 0.6622 0.0839 0.0492 4.675 22.667 17.356 3486.354 2.561 77.197 2.258 0.73 241584. 0.3942
|
|
72.05 0.4180 0.6896 0.0803 0.0487 4.627 22.432 16.608 3450.137 2.534 73.872 2.183 0.73 242147. 0.3729
|
|
77.19 0.4479 0.7146 0.0763 0.0478 4.548 22.050 15.790 3391.406 2.491 70.234 2.112 0.73 242742. 0.3517
|
|
82.34 0.4777 0.7374 0.0720 0.0467 4.437 21.513 14.903 3308.878 2.431 66.288 2.043 0.73 243368. 0.3305
|
|
87.49 0.5076 0.7579 0.0674 0.0452 4.294 20.817 13.949 3201.735 2.352 62.045 1.976 0.73 244025. 0.3093
|
|
92.63 0.5375 0.7760 0.0625 0.0433 4.116 19.958 12.932 3069.578 2.255 57.519 1.911 0.73 244713. 0.2880
|
|
97.78 0.5673 0.7915 0.0573 0.0411 3.907 18.941 11.859 2913.220 2.140 52.749 1.846 0.73 245432. 0.2665
|
|
102.92 0.5972 0.8040 0.0519 0.0386 3.667 17.777 10.742 2734.236 2.008 47.778 1.782 0.73 246181. 0.2448
|
|
108.07 0.6270 0.8130 0.0463 0.0357 3.398 16.476 9.588 2534.158 1.861 42.647 1.716 0.74 246960. 0.2227
|
|
113.22 0.6569 0.8177 0.0406 0.0326 3.104 15.048 8.406 2314.416 1.700 37.390 1.647 0.74 247770. 0.2002
|
|
118.36 0.6868 0.8165 0.0348 0.0293 2.785 13.501 7.203 2076.469 1.525 32.040 1.573 0.74 248608. 0.1770
|
|
123.51 0.7166 0.8070 0.0289 0.0257 2.443 11.846 5.987 1821.926 1.338 26.630 1.490 0.74 249477. 0.1528
|
|
128.66 0.7465 0.7851 0.0230 0.0219 2.082 10.095 4.765 1552.676 1.141 21.194 1.392 0.74 250374. 0.1273
|
|
133.80 0.7763 0.7421 0.0171 0.0179 1.704 8.264 3.545 1271.010 0.934 15.769 1.265 0.74 251301. 0.0998
|
|
138.95 0.8062 0.6592 0.0113 0.0138 1.314 6.370 2.338 979.745 0.720 10.398 1.082 0.75 252257. 0.0693
|
|
144.09 0.8361 0.4840 0.0056 0.0096 0.915 4.436 1.152 682.302 0.501 5.126 0.766 0.75 253242. 0.0345
|
|
149.24 0.8659 -0.0002 0.0000 0.0054 0.513 2.485 0.000 382.279 0.281 -0.001 0.000 0.75 254249. 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 0.1071 0.0426 5.062 22.790 25.706 3774.806 2.575 114.339 3.089 0.78 255242. 0.6563
|
|
5.54 0.0298 0.0730 0.1065 0.0435 5.166 23.256 25.558 3851.995 2.627 113.681 3.009 0.78 255446. 0.6376
|
|
11.07 0.0596 0.1421 0.1058 0.0444 5.272 23.737 25.387 3931.657 2.682 112.922 2.929 0.78 255673. 0.6185
|
|
16.61 0.0895 0.2073 0.1050 0.0453 5.381 24.225 25.190 4012.543 2.737 112.045 2.847 0.78 255926. 0.5990
|
|
22.14 0.1193 0.2685 0.1040 0.0462 5.489 24.712 24.961 4093.193 2.792 111.024 2.766 0.78 256207. 0.5792
|
|
27.68 0.1491 0.3258 0.1029 0.0471 5.595 25.187 24.693 4171.883 2.846 109.836 2.685 0.78 256516. 0.5591
|
|
33.21 0.1789 0.3792 0.1016 0.0480 5.695 25.638 24.383 4246.623 2.897 108.454 2.604 0.78 256855. 0.5390
|
|
38.75 0.2088 0.4289 0.1001 0.0487 5.787 26.052 24.022 4315.176 2.943 106.850 2.525 0.78 257225. 0.5187
|
|
44.28 0.2386 0.4751 0.0984 0.0494 5.867 26.414 23.605 4375.083 2.984 104.995 2.447 0.78 257627. 0.4983
|
|
49.82 0.2684 0.5179 0.0964 0.0500 5.932 26.707 23.125 4423.720 3.017 102.862 2.371 0.78 258062. 0.4779
|
|
55.36 0.2982 0.5574 0.0941 0.0503 5.979 26.916 22.578 4458.317 3.041 100.425 2.297 0.78 258531. 0.4574
|
|
60.89 0.3281 0.5939 0.0915 0.0505 6.002 27.023 21.956 4476.014 3.053 97.660 2.225 0.78 259034. 0.4369
|
|
66.43 0.3579 0.6275 0.0886 0.0505 6.000 27.010 21.256 4473.923 3.052 94.546 2.155 0.78 259571. 0.4164
|
|
71.96 0.3877 0.6585 0.0853 0.0502 5.966 26.861 20.474 4449.219 3.035 91.067 2.087 0.78 260143. 0.3958
|
|
77.50 0.4175 0.6868 0.0817 0.0497 5.900 26.560 19.607 4399.281 3.001 87.213 2.022 0.78 260749. 0.3752
|
|
83.03 0.4474 0.7127 0.0777 0.0488 5.796 26.092 18.656 4321.839 2.948 82.980 1.958 0.79 261389. 0.3544
|
|
88.57 0.4772 0.7362 0.0734 0.0476 5.653 25.448 17.620 4215.081 2.875 78.375 1.896 0.79 262064. 0.3336
|
|
94.10 0.5070 0.7573 0.0688 0.0460 5.468 24.618 16.504 4077.701 2.781 73.409 1.836 0.79 262772. 0.3126
|
|
99.64 0.5368 0.7760 0.0638 0.0441 5.242 23.599 15.310 3908.927 2.666 68.101 1.777 0.79 263513. 0.2913
|
|
105.17 0.5667 0.7921 0.0586 0.0419 4.975 22.396 14.050 3709.579 2.530 62.493 1.718 0.79 264286. 0.2699
|
|
110.71 0.5965 0.8052 0.0531 0.0393 4.669 21.019 12.734 3481.484 2.375 56.640 1.659 0.79 265093. 0.2481
|
|
116.25 0.6263 0.8147 0.0474 0.0364 4.327 19.480 11.373 3226.666 2.201 50.588 1.599 0.79 265932. 0.2260
|
|
121.78 0.6561 0.8198 0.0416 0.0333 3.952 17.793 9.977 2947.185 2.010 44.380 1.536 0.79 266802. 0.2033
|
|
127.32 0.6860 0.8188 0.0357 0.0299 3.547 15.970 8.555 2645.258 1.804 38.053 1.467 0.80 267704. 0.1798
|
|
132.85 0.7158 0.8089 0.0297 0.0262 3.116 14.027 7.115 2323.461 1.585 31.647 1.389 0.80 268638. 0.1553
|
|
138.39 0.7456 0.7855 0.0236 0.0224 2.662 11.983 5.666 1984.820 1.354 25.202 1.295 0.80 269604. 0.1292
|
|
143.92 0.7754 0.7392 0.0176 0.0184 2.190 9.859 4.218 1632.994 1.114 18.761 1.172 0.80 270600. 0.1008
|
|
149.46 0.8052 0.6497 0.0116 0.0144 1.706 7.682 2.782 1272.388 0.868 12.373 0.992 0.80 271628. 0.0693
|
|
154.99 0.8351 0.4650 0.0057 0.0103 1.218 5.483 1.370 908.107 0.619 6.095 0.684 0.80 272686. 0.0336
|
|
160.53 0.8649 -0.0028 0.0000 0.0062 0.731 3.293 -0.005 545.375 0.372 -0.021 -0.004 0.81 273769. 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 0.1078 0.0466 6.802 28.580 29.695 5071.979 3.229 132.081 2.655 0.83 273451. 0.6065
|
|
5.93 0.0298 0.0675 0.1072 0.0474 6.920 29.075 29.543 5159.923 3.285 131.406 2.597 0.83 273669. 0.5916
|
|
11.86 0.0596 0.1319 0.1066 0.0482 7.040 29.582 29.367 5249.925 3.342 130.624 2.537 0.83 273912. 0.5763
|
|
17.79 0.0895 0.1932 0.1059 0.0490 7.161 30.091 29.162 5340.234 3.400 129.712 2.477 0.83 274182. 0.5606
|
|
23.72 0.1193 0.2513 0.1050 0.0498 7.280 30.591 28.921 5428.870 3.456 128.643 2.416 0.83 274482. 0.5446
|
|
29.65 0.1491 0.3062 0.1040 0.0506 7.394 31.068 28.639 5513.537 3.510 127.385 2.356 0.83 274812. 0.5284
|
|
35.58 0.1789 0.3582 0.1028 0.0513 7.499 31.508 28.306 5591.647 3.560 125.905 2.296 0.83 275175. 0.5120
|
|
41.51 0.2087 0.4071 0.1013 0.0520 7.591 31.895 27.916 5660.386 3.604 124.170 2.237 0.83 275572. 0.4953
|
|
47.44 0.2386 0.4531 0.0997 0.0525 7.666 32.213 27.460 5716.770 3.639 122.143 2.179 0.84 276003. 0.4785
|
|
53.37 0.2684 0.4964 0.0978 0.0529 7.721 32.444 26.931 5757.712 3.665 119.789 2.122 0.84 276469. 0.4614
|
|
59.30 0.2982 0.5370 0.0956 0.0531 7.751 32.570 26.321 5780.044 3.680 117.076 2.065 0.84 276972. 0.4441
|
|
65.23 0.3280 0.5750 0.0930 0.0531 7.752 32.573 25.623 5780.585 3.680 113.971 2.010 0.84 277512. 0.4265
|
|
71.16 0.3578 0.6104 0.0901 0.0528 7.719 32.435 24.831 5756.195 3.665 110.449 1.957 0.84 278089. 0.4086
|
|
77.09 0.3877 0.6434 0.0869 0.0524 7.649 32.140 23.941 5703.870 3.631 106.488 1.904 0.84 278703. 0.3904
|
|
83.02 0.4175 0.6740 0.0833 0.0516 7.538 31.673 22.949 5620.893 3.578 102.075 1.852 0.84 279354. 0.3718
|
|
88.95 0.4473 0.7022 0.0793 0.0505 7.382 31.019 21.854 5504.943 3.505 97.205 1.801 0.84 280041. 0.3528
|
|
94.88 0.4771 0.7279 0.0750 0.0492 7.180 30.170 20.657 5354.152 3.409 91.884 1.750 0.84 280766. 0.3334
|
|
100.81 0.5069 0.7512 0.0703 0.0474 6.929 29.116 19.363 5167.162 3.290 86.128 1.700 0.84 281526. 0.3135
|
|
106.74 0.5368 0.7719 0.0653 0.0454 6.629 27.853 17.976 4943.042 3.147 79.956 1.649 0.85 282321. 0.2931
|
|
112.67 0.5666 0.7895 0.0599 0.0430 6.281 26.394 16.506 4684.097 2.982 73.419 1.598 0.85 283152. 0.2722
|
|
118.60 0.5964 0.8036 0.0543 0.0403 5.891 24.754 14.968 4393.116 2.797 66.580 1.545 0.85 284018. 0.2506
|
|
124.53 0.6262 0.8131 0.0486 0.0374 5.463 22.953 13.376 4073.499 2.593 59.495 1.489 0.85 284918. 0.2283
|
|
130.46 0.6561 0.8170 0.0426 0.0342 4.999 21.005 11.739 3727.702 2.373 52.215 1.428 0.85 285852. 0.2051
|
|
136.39 0.6859 0.8135 0.0366 0.0308 4.502 18.916 10.069 3356.951 2.137 44.788 1.361 0.85 286819. 0.1809
|
|
142.32 0.7157 0.7994 0.0304 0.0272 3.977 16.709 8.377 2965.322 1.888 37.259 1.281 0.85 287821. 0.1554
|
|
148.26 0.7455 0.7689 0.0242 0.0235 3.430 14.414 6.672 2558.044 1.629 29.676 1.183 0.86 288856. 0.1281
|
|
154.19 0.7753 0.7113 0.0180 0.0197 2.871 12.062 4.967 2140.697 1.363 22.091 1.052 0.86 289924. 0.0983
|
|
160.12 0.8052 0.6062 0.0119 0.0158 2.306 9.691 3.275 1719.765 1.095 14.565 0.864 0.86 291025. 0.0655
|
|
166.05 0.8350 0.4083 0.0058 0.0120 1.747 7.339 1.611 1302.458 0.829 7.164 0.561 0.86 292159. 0.0298
|
|
171.98 0.8648 -0.0039 0.0000 0.0082 1.201 5.046 -0.010 895.425 0.570 -0.046 -0.005 0.86 293320. 0.0000
|
|
|
|
|
|
|