464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
20x14 (20x14.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 0.0878 0.0370 0.010 0.601 0.448 7.113 0.068 1.991 28.548 0.08 31265. 0.5604
|
|
0.58 0.0306 0.0702 0.0872 0.0380 0.010 0.616 0.445 7.290 0.070 1.978 27.673 0.08 31288. 0.5415
|
|
1.16 0.0611 0.1359 0.0866 0.0389 0.010 0.632 0.441 7.474 0.071 1.964 26.791 0.08 31314. 0.5222
|
|
1.74 0.0917 0.1972 0.0858 0.0399 0.010 0.647 0.438 7.660 0.073 1.946 25.908 0.08 31342. 0.5028
|
|
2.31 0.1222 0.2540 0.0849 0.0409 0.011 0.663 0.433 7.846 0.075 1.926 25.030 0.08 31374. 0.4832
|
|
2.89 0.1528 0.3065 0.0839 0.0418 0.011 0.678 0.428 8.027 0.077 1.902 24.162 0.08 31410. 0.4636
|
|
3.47 0.1833 0.3548 0.0826 0.0427 0.011 0.693 0.421 8.200 0.078 1.874 23.309 0.08 31450. 0.4439
|
|
4.05 0.2139 0.3991 0.0812 0.0435 0.011 0.706 0.414 8.357 0.080 1.842 22.474 0.08 31493. 0.4243
|
|
4.63 0.2444 0.4396 0.0796 0.0442 0.011 0.718 0.406 8.495 0.081 1.804 21.662 0.08 31540. 0.4048
|
|
5.21 0.2750 0.4766 0.0777 0.0448 0.012 0.727 0.396 8.605 0.082 1.761 20.873 0.08 31591. 0.3853
|
|
5.79 0.3055 0.5101 0.0755 0.0452 0.012 0.734 0.385 8.682 0.083 1.712 20.109 0.08 31647. 0.3660
|
|
6.37 0.3361 0.5405 0.0730 0.0454 0.012 0.737 0.372 8.721 0.083 1.656 19.369 0.08 31707. 0.3468
|
|
6.94 0.3666 0.5679 0.0703 0.0454 0.012 0.737 0.358 8.715 0.083 1.594 18.653 0.08 31771. 0.3276
|
|
7.52 0.3972 0.5923 0.0673 0.0451 0.012 0.732 0.343 8.664 0.083 1.526 17.959 0.08 31839. 0.3086
|
|
8.10 0.4278 0.6138 0.0640 0.0446 0.011 0.724 0.326 8.567 0.082 1.452 17.283 0.08 31912. 0.2897
|
|
8.68 0.4583 0.6325 0.0605 0.0439 0.011 0.712 0.309 8.423 0.080 1.373 16.621 0.08 31989. 0.2709
|
|
9.26 0.4889 0.6482 0.0569 0.0429 0.011 0.696 0.290 8.235 0.079 1.290 15.968 0.08 32070. 0.2522
|
|
9.84 0.5194 0.6607 0.0530 0.0417 0.011 0.676 0.270 8.002 0.076 1.202 15.319 0.08 32155. 0.2337
|
|
10.42 0.5500 0.6698 0.0490 0.0402 0.010 0.653 0.250 7.727 0.074 1.112 14.668 0.08 32244. 0.2151
|
|
10.99 0.5805 0.6752 0.0449 0.0386 0.010 0.626 0.229 7.411 0.071 1.018 14.008 0.08 32338. 0.1966
|
|
11.57 0.6111 0.6763 0.0407 0.0367 0.009 0.596 0.207 7.053 0.067 0.922 13.329 0.08 32436. 0.1780
|
|
12.15 0.6416 0.6723 0.0363 0.0347 0.009 0.563 0.185 6.656 0.064 0.824 12.620 0.08 32538. 0.1593
|
|
12.73 0.6722 0.6623 0.0319 0.0324 0.008 0.526 0.163 6.220 0.059 0.724 11.867 0.08 32644. 0.1404
|
|
13.31 0.7027 0.6445 0.0274 0.0299 0.008 0.486 0.140 5.745 0.055 0.622 11.047 0.08 32754. 0.1212
|
|
13.89 0.7333 0.6166 0.0229 0.0272 0.007 0.442 0.117 5.232 0.050 0.520 10.127 0.08 32868. 0.1016
|
|
14.47 0.7638 0.5746 0.0183 0.0244 0.006 0.396 0.094 4.684 0.045 0.416 9.060 0.08 32986. 0.0813
|
|
15.05 0.7944 0.5120 0.0138 0.0214 0.005 0.347 0.070 4.101 0.039 0.312 7.762 0.08 33109. 0.0603
|
|
15.62 0.8250 0.4170 0.0092 0.0182 0.005 0.295 0.047 3.486 0.033 0.208 6.088 0.08 33235. 0.0386
|
|
16.20 0.8555 0.2664 0.0046 0.0148 0.004 0.240 0.023 2.841 0.027 0.105 3.751 0.08 33365. 0.0169
|
|
16.78 0.8861 0.0057 0.0001 0.0113 0.003 0.183 0.000 2.169 0.021 0.002 0.077 0.08 33498. 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 0.0881 0.0334 0.069 2.168 1.798 51.308 0.245 7.996 15.891 0.16 62530. 0.6251
|
|
1.16 0.0307 0.0783 0.0876 0.0344 0.071 2.231 1.786 52.784 0.252 7.946 15.351 0.16 62575. 0.6020
|
|
2.33 0.0615 0.1511 0.0870 0.0354 0.073 2.295 1.773 54.312 0.259 7.888 14.811 0.16 62627. 0.5787
|
|
3.49 0.0922 0.2185 0.0862 0.0364 0.075 2.361 1.758 55.871 0.267 7.821 14.274 0.16 62685. 0.5553
|
|
4.66 0.1229 0.2805 0.0853 0.0374 0.077 2.427 1.740 57.433 0.274 7.741 13.743 0.16 62750. 0.5319
|
|
5.82 0.1536 0.3374 0.0843 0.0384 0.079 2.492 1.719 58.966 0.282 7.647 13.224 0.16 62822. 0.5087
|
|
6.98 0.1844 0.3893 0.0831 0.0393 0.081 2.554 1.694 60.432 0.289 7.536 12.717 0.16 62901. 0.4856
|
|
8.15 0.2151 0.4367 0.0817 0.0402 0.083 2.611 1.665 61.786 0.295 7.408 12.226 0.16 62989. 0.4629
|
|
9.31 0.2458 0.4797 0.0800 0.0410 0.084 2.662 1.632 62.980 0.301 7.258 11.751 0.16 63084. 0.4404
|
|
10.47 0.2765 0.5187 0.0781 0.0416 0.086 2.703 1.593 63.961 0.305 7.085 11.296 0.16 63188. 0.4183
|
|
11.64 0.3073 0.5541 0.0759 0.0421 0.087 2.733 1.548 64.675 0.309 6.887 10.859 0.16 63300. 0.3964
|
|
12.80 0.3380 0.5860 0.0734 0.0424 0.087 2.750 1.498 65.074 0.311 6.663 10.441 0.16 63421. 0.3749
|
|
13.97 0.3687 0.6148 0.0707 0.0424 0.087 2.752 1.442 65.119 0.311 6.412 10.041 0.16 63550. 0.3537
|
|
15.13 0.3994 0.6406 0.0676 0.0422 0.087 2.738 1.380 64.789 0.309 6.136 9.658 0.16 63688. 0.3328
|
|
16.29 0.4302 0.6636 0.0643 0.0417 0.086 2.708 1.312 64.075 0.306 5.837 9.289 0.16 63835. 0.3122
|
|
17.46 0.4609 0.6838 0.0608 0.0410 0.084 2.662 1.241 62.979 0.301 5.518 8.934 0.16 63990. 0.2919
|
|
18.62 0.4916 0.7012 0.0571 0.0400 0.082 2.599 1.165 61.506 0.294 5.181 8.589 0.16 64154. 0.2719
|
|
19.79 0.5223 0.7157 0.0532 0.0388 0.080 2.522 1.085 59.666 0.285 4.828 8.251 0.16 64326. 0.2522
|
|
20.95 0.5531 0.7272 0.0492 0.0374 0.077 2.429 1.003 57.465 0.274 4.462 7.917 0.16 64507. 0.2326
|
|
22.11 0.5838 0.7353 0.0450 0.0357 0.074 2.321 0.918 54.909 0.262 4.084 7.585 0.16 64696. 0.2132
|
|
23.28 0.6145 0.7397 0.0407 0.0339 0.070 2.198 0.831 52.006 0.248 3.697 7.249 0.16 64894. 0.1939
|
|
24.44 0.6453 0.7397 0.0364 0.0317 0.065 2.061 0.742 48.761 0.233 3.301 6.903 0.16 65100. 0.1745
|
|
25.61 0.6760 0.7343 0.0319 0.0294 0.061 1.909 0.652 45.180 0.216 2.898 6.542 0.16 65314. 0.1549
|
|
26.77 0.7067 0.7220 0.0274 0.0269 0.055 1.744 0.560 41.268 0.197 2.490 6.153 0.16 65537. 0.1351
|
|
27.93 0.7374 0.7004 0.0229 0.0241 0.050 1.565 0.467 37.035 0.177 2.077 5.719 0.16 65768. 0.1147
|
|
29.10 0.7682 0.6651 0.0183 0.0212 0.044 1.373 0.374 32.492 0.155 1.661 5.214 0.16 66007. 0.0935
|
|
30.26 0.7989 0.6087 0.0137 0.0180 0.037 1.169 0.280 27.652 0.132 1.244 4.588 0.16 66254. 0.0712
|
|
31.42 0.8296 0.5157 0.0091 0.0147 0.030 0.952 0.186 22.535 0.108 0.827 3.744 0.16 66509. 0.0474
|
|
32.59 0.8603 0.3503 0.0045 0.0112 0.023 0.725 0.093 17.166 0.082 0.413 2.452 0.16 66773. 0.0219
|
|
33.75 0.8911 0.0012 0.0000 0.0075 0.015 0.488 0.000 11.549 0.055 0.001 0.008 0.16 67039. 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 0.0884 0.0320 0.222 4.670 4.057 165.766 0.528 18.047 11.102 0.24 93793. 0.6560
|
|
1.75 0.0308 0.0822 0.0879 0.0330 0.229 4.813 4.033 170.847 0.544 17.940 10.708 0.24 93862. 0.6309
|
|
3.50 0.0616 0.1583 0.0873 0.0340 0.236 4.962 4.005 176.118 0.561 17.814 10.314 0.24 93940. 0.6056
|
|
5.25 0.0924 0.2285 0.0865 0.0350 0.243 5.114 3.971 181.505 0.578 17.665 9.924 0.24 94027. 0.5803
|
|
7.00 0.1232 0.2929 0.0857 0.0361 0.251 5.266 3.932 186.920 0.595 17.489 9.541 0.24 94124. 0.5551
|
|
8.75 0.1540 0.3517 0.0847 0.0371 0.258 5.417 3.885 192.252 0.612 17.282 9.166 0.24 94233. 0.5301
|
|
10.50 0.1848 0.4053 0.0835 0.0381 0.265 5.561 3.830 197.369 0.628 17.038 8.803 0.24 94352. 0.5054
|
|
12.25 0.2156 0.4539 0.0821 0.0390 0.271 5.694 3.766 202.117 0.643 16.751 8.451 0.24 94484. 0.4812
|
|
14.00 0.2464 0.4981 0.0804 0.0398 0.277 5.813 3.691 206.327 0.657 16.417 8.114 0.24 94628. 0.4573
|
|
15.75 0.2773 0.5380 0.0785 0.0405 0.281 5.911 3.604 209.816 0.668 16.029 7.790 0.24 94784. 0.4339
|
|
17.50 0.3081 0.5741 0.0763 0.0410 0.285 5.984 3.504 212.401 0.676 15.584 7.482 0.24 94953. 0.4109
|
|
19.25 0.3389 0.6067 0.0739 0.0413 0.287 6.027 3.390 213.909 0.681 15.079 7.188 0.24 95135. 0.3883
|
|
21.00 0.3697 0.6362 0.0711 0.0413 0.287 6.035 3.263 214.206 0.682 14.513 6.909 0.24 95330. 0.3661
|
|
22.75 0.4005 0.6626 0.0680 0.0411 0.286 6.007 3.122 213.210 0.679 13.889 6.643 0.24 95538. 0.3444
|
|
24.50 0.4313 0.6863 0.0647 0.0407 0.283 5.942 2.970 210.892 0.671 13.212 6.388 0.24 95759. 0.3230
|
|
26.26 0.4621 0.7073 0.0612 0.0400 0.278 5.839 2.808 207.253 0.660 12.489 6.145 0.24 95993. 0.3021
|
|
28.01 0.4929 0.7256 0.0574 0.0390 0.271 5.700 2.636 202.312 0.644 11.725 5.910 0.24 96240. 0.2815
|
|
29.76 0.5237 0.7411 0.0535 0.0378 0.263 5.525 2.456 196.092 0.624 10.925 5.681 0.24 96500. 0.2612
|
|
31.51 0.5545 0.7539 0.0495 0.0364 0.253 5.314 2.270 188.617 0.600 10.096 5.458 0.24 96772. 0.2412
|
|
33.26 0.5853 0.7635 0.0453 0.0347 0.241 5.069 2.077 179.909 0.573 9.240 5.237 0.24 97058. 0.2214
|
|
35.01 0.6161 0.7698 0.0410 0.0328 0.228 4.789 1.880 169.988 0.541 8.362 5.016 0.24 97356. 0.2018
|
|
36.76 0.6469 0.7721 0.0366 0.0306 0.213 4.476 1.678 158.872 0.506 7.465 4.791 0.24 97666. 0.1821
|
|
38.51 0.6777 0.7695 0.0321 0.0283 0.197 4.130 1.473 146.581 0.467 6.552 4.558 0.24 97989. 0.1623
|
|
40.26 0.7085 0.7606 0.0276 0.0257 0.179 3.751 1.265 133.136 0.424 5.627 4.310 0.24 98325. 0.1422
|
|
42.01 0.7393 0.7431 0.0230 0.0229 0.159 3.341 1.055 118.568 0.377 4.691 4.035 0.24 98673. 0.1216
|
|
43.76 0.7701 0.7128 0.0184 0.0198 0.138 2.899 0.843 102.913 0.328 3.750 3.716 0.25 99034. 0.1001
|
|
45.51 0.8010 0.6619 0.0137 0.0166 0.116 2.429 0.631 86.225 0.274 2.805 3.318 0.25 99406. 0.0773
|
|
47.26 0.8318 0.5737 0.0091 0.0132 0.092 1.932 0.419 68.571 0.218 1.862 2.769 0.25 99791. 0.0526
|
|
49.01 0.8626 0.4047 0.0045 0.0097 0.067 1.410 0.208 50.038 0.159 0.924 1.884 0.25 100188. 0.0252
|
|
50.76 0.8934 -0.0064 0.0000 0.0059 0.041 0.862 -0.002 30.595 0.097 -0.009 -0.029 0.25 100586. 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 0.0887 0.0313 0.515 8.118 7.238 384.170 0.917 32.195 8.546 0.32 125054. 0.6745
|
|
2.35 0.0310 0.0848 0.0882 0.0323 0.532 8.377 7.197 396.454 0.946 32.013 8.234 0.32 125147. 0.6481
|
|
4.70 0.0620 0.1631 0.0876 0.0333 0.549 8.647 7.149 409.228 0.977 31.797 7.923 0.32 125251. 0.6215
|
|
7.04 0.0930 0.2352 0.0869 0.0344 0.566 8.924 7.091 422.314 1.008 31.541 7.616 0.32 125368. 0.5950
|
|
9.39 0.1240 0.3011 0.0861 0.0354 0.584 9.202 7.023 435.499 1.040 31.237 7.314 0.32 125499. 0.5686
|
|
11.74 0.1550 0.3613 0.0851 0.0365 0.601 9.477 6.941 448.512 1.071 30.875 7.020 0.32 125645. 0.5426
|
|
14.09 0.1859 0.4159 0.0839 0.0375 0.618 9.742 6.845 461.027 1.101 30.447 6.734 0.32 125806. 0.5169
|
|
16.43 0.2169 0.4654 0.0825 0.0385 0.634 9.988 6.731 472.669 1.128 29.942 6.459 0.32 125983. 0.4917
|
|
18.78 0.2479 0.5102 0.0809 0.0393 0.648 10.206 6.598 483.017 1.153 29.349 6.196 0.32 126177. 0.4669
|
|
21.13 0.2789 0.5507 0.0790 0.0400 0.659 10.388 6.443 491.619 1.174 28.659 5.945 0.32 126387. 0.4427
|
|
23.48 0.3099 0.5872 0.0768 0.0405 0.668 10.523 6.264 498.021 1.189 27.864 5.705 0.32 126615. 0.4189
|
|
25.83 0.3409 0.6202 0.0743 0.0408 0.673 10.603 6.061 501.796 1.198 26.958 5.478 0.32 126861. 0.3957
|
|
28.17 0.3719 0.6500 0.0715 0.0409 0.674 10.620 5.832 502.612 1.200 25.941 5.263 0.32 127124. 0.3729
|
|
30.52 0.4029 0.6769 0.0684 0.0407 0.671 10.571 5.580 500.270 1.194 24.818 5.059 0.32 127404. 0.3506
|
|
32.87 0.4339 0.7010 0.0650 0.0403 0.663 10.453 5.306 494.695 1.181 23.599 4.864 0.32 127703. 0.3287
|
|
35.22 0.4649 0.7224 0.0614 0.0395 0.652 10.267 5.012 485.890 1.160 22.295 4.679 0.32 128018. 0.3073
|
|
37.56 0.4959 0.7412 0.0576 0.0386 0.636 10.014 4.702 473.899 1.131 20.916 4.501 0.32 128351. 0.2863
|
|
39.91 0.5268 0.7574 0.0537 0.0373 0.615 9.694 4.378 458.777 1.095 19.474 4.328 0.32 128701. 0.2657
|
|
42.26 0.5578 0.7708 0.0495 0.0359 0.591 9.310 4.041 440.583 1.052 17.976 4.160 0.32 129069. 0.2454
|
|
44.61 0.5888 0.7813 0.0453 0.0341 0.562 8.861 3.694 419.368 1.001 16.431 3.995 0.32 129454. 0.2253
|
|
46.96 0.6198 0.7886 0.0409 0.0322 0.530 8.350 3.338 395.180 0.943 14.847 3.831 0.32 129855. 0.2053
|
|
49.30 0.6508 0.7921 0.0365 0.0299 0.494 7.777 2.974 368.063 0.879 13.228 3.665 0.32 130274. 0.1854
|
|
51.65 0.6818 0.7910 0.0319 0.0275 0.453 7.144 2.604 338.065 0.807 11.581 3.493 0.32 130710. 0.1654
|
|
54.00 0.7128 0.7839 0.0273 0.0248 0.409 6.450 2.228 305.242 0.729 9.912 3.311 0.33 131163. 0.1450
|
|
56.35 0.7438 0.7683 0.0227 0.0219 0.362 5.698 1.849 269.667 0.644 8.225 3.110 0.33 131632. 0.1241
|
|
58.69 0.7748 0.7401 0.0180 0.0188 0.310 4.890 1.468 231.437 0.553 6.528 2.876 0.33 132118. 0.1022
|
|
61.04 0.8058 0.6906 0.0133 0.0155 0.256 4.029 1.085 190.687 0.455 4.826 2.581 0.33 132621. 0.0789
|
|
63.39 0.8368 0.6004 0.0086 0.0120 0.198 3.119 0.703 147.592 0.352 3.127 2.161 0.33 133140. 0.0531
|
|
65.74 0.8677 0.4134 0.0040 0.0083 0.137 2.163 0.324 102.368 0.244 1.440 1.435 0.33 133674. 0.0239
|
|
68.09 0.8987
|
|
|
|
|
|
|
|
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 0.0891 0.0309 0.995 12.539 11.355 741.763 1.417 50.509 6.944 0.40 156314. 0.6865
|
|
2.92 0.0309 0.0857 0.0886 0.0319 1.027 12.949 11.296 765.983 1.463 50.243 6.689 0.40 156429. 0.6595
|
|
5.85 0.0618 0.1650 0.0881 0.0330 1.061 13.375 11.224 791.232 1.511 49.927 6.434 0.40 156558. 0.6324
|
|
8.77 0.0926 0.2378 0.0874 0.0340 1.096 13.814 11.140 817.171 1.561 49.549 6.183 0.40 156704. 0.6054
|
|
11.70 0.1235 0.3044 0.0866 0.0351 1.131 14.257 11.038 843.385 1.611 49.098 5.936 0.40 156867. 0.5786
|
|
14.62 0.1544 0.3651 0.0856 0.0362 1.166 14.696 10.917 869.349 1.660 48.560 5.696 0.40 157048. 0.5521
|
|
17.54 0.1853 0.4202 0.0845 0.0373 1.199 15.120 10.773 894.429 1.708 47.918 5.463 0.40 157248. 0.5261
|
|
20.47 0.2161 0.4701 0.0832 0.0382 1.231 15.516 10.602 917.881 1.753 47.156 5.239 0.40 157468. 0.5004
|
|
23.39 0.2470 0.5152 0.0816 0.0391 1.259 15.871 10.400 938.872 1.793 46.257 5.024 0.40 157708. 0.4753
|
|
26.32 0.2779 0.5560 0.0797 0.0398 1.283 16.169 10.163 956.508 1.827 45.206 4.819 0.40 157970. 0.4508
|
|
29.24 0.3088 0.5928 0.0776 0.0404 1.301 16.395 9.889 969.874 1.852 43.988 4.625 0.40 158253. 0.4267
|
|
32.16 0.3396 0.6261 0.0751 0.0407 1.312 16.535 9.576 978.115 1.868 42.595 4.441 0.40 158558. 0.4032
|
|
35.09 0.3705 0.6563 0.0724 0.0409 1.315 16.576 9.223 980.543 1.873 41.025 4.266 0.40 158885. 0.3801
|
|
38.01 0.4014 0.6834 0.0693 0.0407 1.310 16.511 8.832 976.738 1.865 39.285 4.101 0.40 159234. 0.3576
|
|
40.94 0.4323 0.7079 0.0659 0.0403 1.296 16.339 8.406 966.527 1.846 37.390 3.945 0.40 159605. 0.3356
|
|
43.86 0.4632 0.7298 0.0624 0.0396 1.274 16.058 7.949 949.903 1.814 35.359 3.796 0.40 159997. 0.3140
|
|
46.78 0.4940 0.7492 0.0586 0.0386 1.243 15.670 7.466 926.946 1.770 33.207 3.653 0.40 160411. 0.2928
|
|
49.71 0.5249 0.7661 0.0546 0.0374 1.204 15.176 6.959 897.768 1.715 30.952 3.516 0.40 160846. 0.2721
|
|
52.63 0.5558 0.7804 0.0505 0.0359 1.157 14.580 6.432 862.484 1.647 28.608 3.382 0.40 161303. 0.2517
|
|
55.55 0.5867 0.7920 0.0462 0.0342 1.101 13.882 5.888 821.199 1.568 26.188 3.252 0.40 161781. 0.2315
|
|
58.48 0.6175 0.8006 0.0418 0.0322 1.038 13.084 5.329 774.010 1.478 23.703 3.123 0.40 162280. 0.2115
|
|
61.40 0.6484 0.8057 0.0373 0.0300 0.967 12.188 4.758 721.005 1.377 21.163 2.993 0.41 162800. 0.1915
|
|
64.33 0.6793 0.8067 0.0328 0.0276 0.888 11.195 4.177 662.278 1.265 18.578 2.860 0.41 163342. 0.1715
|
|
67.25 0.7102 0.8022 0.0281 0.0249 0.802 10.108 3.587 597.936 1.142 15.955 2.721 0.41 163904. 0.1512
|
|
70.17 0.7410 0.7903 0.0235 0.0220 0.708 8.928 2.991 528.119 1.009 13.305 2.569 0.41 164487. 0.1303
|
|
73.10 0.7719 0.7671 0.0188 0.0189 0.608 7.658 2.391 453.013 0.865 10.635 2.394 0.41 165091. 0.1086
|
|
76.02 0.8028 0.7252 0.0140 0.0155 0.500 6.303 1.789 372.874 0.712 7.957 2.176 0.41 165715. 0.0854
|
|
78.95 0.8337 0.6471 0.0093 0.0120 0.386 4.869 1.187 288.042 0.550 5.282 1.870 0.41 166359. 0.0598
|
|
81.87 0.8646 0.4826 0.0046 0.0083 0.267 3.363 0.590 198.939 0.380 2.623 1.345 0.41 167022. 0.0303
|
|
84.79 0.8954 -0.0113 -0.0001 0.0044 0.141 1.776 -0.007 105.053 0.201 -0.031 -0.030 0.41 167680. 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 0.0895 0.0308 1.711 17.979 16.427 1276.248 2.031 73.069 5.838 0.48 187570. 0.6942
|
|
3.51 0.0309 0.0866 0.0891 0.0318 1.768 18.577 16.348 1318.724 2.099 72.717 5.623 0.48 187708. 0.6670
|
|
7.03 0.0618 0.1666 0.0885 0.0329 1.828 19.203 16.254 1363.142 2.170 72.296 5.408 0.48 187863. 0.6397
|
|
10.54 0.0927 0.2400 0.0879 0.0340 1.889 19.848 16.140 1408.929 2.242 71.790 5.196 0.48 188038. 0.6124
|
|
14.05 0.1236 0.3072 0.0872 0.0351 1.952 20.502 16.003 1455.364 2.316 71.180 4.987 0.48 188234. 0.5853
|
|
17.56 0.1546 0.3684 0.0863 0.0362 2.014 21.152 15.837 1501.532 2.390 70.445 4.784 0.48 188451. 0.5586
|
|
21.08 0.1855 0.4238 0.0852 0.0373 2.074 21.783 15.639 1546.300 2.461 69.560 4.587 0.48 188692. 0.5322
|
|
24.59 0.2164 0.4741 0.0839 0.0383 2.130 22.375 15.401 1588.350 2.528 68.502 4.398 0.48 188956. 0.5063
|
|
28.10 0.2473 0.5195 0.0824 0.0392 2.181 22.908 15.118 1626.181 2.588 67.244 4.217 0.48 189245. 0.4810
|
|
31.61 0.2782 0.5605 0.0805 0.0400 2.224 23.359 14.784 1658.183 2.639 65.760 4.044 0.48 189560. 0.4562
|
|
35.13 0.3091 0.5975 0.0784 0.0406 2.257 23.704 14.395 1682.700 2.678 64.030 3.880 0.48 189901. 0.4319
|
|
38.64 0.3400 0.6311 0.0760 0.0409 2.277 23.922 13.948 1698.178 2.703 62.040 3.725 0.48 190268. 0.4082
|
|
42.15 0.3709 0.6614 0.0732 0.0411 2.284 23.995 13.441 1703.360 2.711 59.785 3.579 0.48 190661. 0.3850
|
|
45.67 0.4019 0.6888 0.0702 0.0409 2.276 23.912 12.877 1697.465 2.702 57.277 3.441 0.48 191081. 0.3622
|
|
49.18 0.4328 0.7136 0.0668 0.0405 2.253 23.669 12.261 1680.161 2.674 54.537 3.310 0.48 191528. 0.3400
|
|
52.69 0.4637 0.7358 0.0632 0.0398 2.215 23.264 11.599 1651.434 2.628 51.590 3.186 0.48 192000. 0.3183
|
|
56.20 0.4946 0.7556 0.0594 0.0389 2.161 22.700 10.896 1611.427 2.565 48.464 3.067 0.48 192498. 0.2970
|
|
59.72 0.5255 0.7730 0.0553 0.0376 2.092 21.981 10.158 1560.347 2.483 45.183 2.953 0.48 193022. 0.2761
|
|
63.23 0.5564 0.7879 0.0512 0.0361 2.009 21.108 9.390 1498.408 2.385 41.768 2.842 0.48 193572. 0.2555
|
|
66.74 0.5873 0.8002 0.0468 0.0344 1.912 20.085 8.597 1425.807 2.269 38.240 2.735 0.48 194147. 0.2353
|
|
70.25 0.6182 0.8096 0.0424 0.0324 1.801 18.915 7.782 1342.722 2.137 34.615 2.629 0.49 194747. 0.2151
|
|
73.77 0.6491 0.8158 0.0379 0.0301 1.675 17.599 6.949 1249.315 1.988 30.907 2.523 0.49 195374. 0.1951
|
|
77.28 0.6801 0.8181 0.0332 0.0276 1.536 16.140 6.100 1145.754 1.824 27.131 2.415 0.49 196025. 0.1750
|
|
80.79 0.7110 0.8152 0.0285 0.0249 1.384 14.541 5.238 1032.236 1.643 23.299 2.302 0.49 196701. 0.1545
|
|
84.30 0.7419 0.8053 0.0238 0.0219 1.219 12.805 4.367 909.003 1.447 19.424 2.179 0.49 197403. 0.1336
|
|
87.82 0.7728 0.7848 0.0190 0.0187 1.041 10.937 3.489 776.391 1.236 15.521 2.038 0.49 198129. 0.1117
|
|
91.33 0.8037 0.7462 0.0142 0.0153 0.851 8.943 2.609 634.852 1.010 11.603 1.864 0.49 198880. 0.0883
|
|
94.84 0.8346 0.6723 0.0094 0.0117 0.650 6.832 1.729 484.994 0.772 7.690 1.617 0.49 199655. 0.0624
|
|
98.36 0.8655 0.5101 0.0047 0.0079 0.439 4.615 0.854 327.575 0.521 3.800 1.183 0.49 200452. 0.0321
|
|
101.87 0.8964 -0.0277 -0.0001 0.0039 0.216 2.269 -0.022 161.094 0.256 -0.098 -0.062 0.49 201232. 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 0.0900 0.0308 2.721 24.497 22.475 2028.815 2.768 99.968 5.025 0.56 218823. 0.6988
|
|
4.14 0.0312 0.0877 0.0896 0.0319 2.813 25.331 22.378 2097.859 2.862 99.537 4.838 0.56 218985. 0.6715
|
|
8.27 0.0624 0.1687 0.0891 0.0330 2.911 26.206 22.261 2170.372 2.961 99.017 4.652 0.56 219168. 0.6440
|
|
12.41 0.0936 0.2431 0.0885 0.0341 3.011 27.113 22.119 2245.441 3.063 98.383 4.468 0.56 219374. 0.6165
|
|
16.55 0.1248 0.3109 0.0878 0.0353 3.114 28.036 21.945 2321.899 3.167 97.611 4.287 0.56 219605. 0.5892
|
|
20.68 0.1560 0.3727 0.0870 0.0364 3.216 28.958 21.733 2398.221 3.272 96.667 4.110 0.56 219861. 0.5622
|
|
24.82 0.1872 0.4286 0.0859 0.0375 3.316 29.855 21.474 2472.507 3.373 95.517 3.939 0.56 220146. 0.5356
|
|
28.95 0.2184 0.4792 0.0847 0.0386 3.410 30.700 21.160 2542.506 3.468 94.122 3.775 0.56 220459. 0.5095
|
|
33.09 0.2496 0.5248 0.0832 0.0396 3.494 31.462 20.783 2605.646 3.555 92.443 3.618 0.56 220801. 0.4839
|
|
37.23 0.2808 0.5660 0.0814 0.0404 3.566 32.108 20.333 2659.146 3.628 90.443 3.468 0.56 221175. 0.4588
|
|
41.36 0.3120 0.6032 0.0793 0.0410 3.621 32.603 19.804 2700.164 3.684 88.089 3.327 0.56 221579. 0.4343
|
|
45.50 0.3432 0.6369 0.0768 0.0414 3.656 32.916 19.190 2726.030 3.719 85.359 3.193 0.56 222015. 0.4104
|
|
49.64 0.3744 0.6674 0.0740 0.0415 3.667 33.019 18.491 2734.608 3.731 82.247 3.067 0.56 222482. 0.3869
|
|
53.77 0.4056 0.6950 0.0709 0.0414 3.654 32.898 17.709 2724.587 3.717 78.771 2.948 0.56 222981. 0.3640
|
|
57.91 0.4368 0.7199 0.0675 0.0409 3.615 32.547 16.853 2695.447 3.677 74.960 2.836 0.56 223511. 0.3415
|
|
62.05 0.4680 0.7424 0.0638 0.0402 3.550 31.964 15.929 2647.184 3.611 70.854 2.729 0.56 224072. 0.3196
|
|
66.18 0.4992 0.7624 0.0598 0.0392 3.460 31.154 14.948 2580.081 3.520 66.490 2.628 0.56 224663. 0.2981
|
|
70.32 0.5304 0.7801 0.0557 0.0379 3.345 30.120 13.917 2494.512 3.403 61.904 2.531 0.56 225286. 0.2770
|
|
74.45 0.5616 0.7953 0.0514 0.0363 3.206 28.869 12.844 2390.867 3.262 57.129 2.437 0.56 225939. 0.2562
|
|
78.59 0.5928 0.8080 0.0470 0.0345 3.043 27.403 11.734 2269.495 3.096 52.191 2.345 0.57 226622. 0.2357
|
|
82.73 0.6240 0.8178 0.0424 0.0324 2.857 25.728 10.593 2130.709 2.907 47.116 2.255 0.57 227336. 0.2153
|
|
86.86 0.6552 0.8244 0.0377 0.0300 2.648 23.845 9.425 1974.799 2.694 41.925 2.165 0.57 228079. 0.1950
|
|
91.00 0.6864 0.8270 0.0330 0.0274 2.417 21.759 8.236 1802.056 2.458 36.636 2.073 0.57 228853. 0.1746
|
|
95.14 0.7176 0.8245 0.0281 0.0245 2.163 19.474 7.030 1612.826 2.200 31.269 1.977 0.57 229656. 0.1538
|
|
99.27 0.7488 0.8148 0.0233 0.0214 1.888 16.996 5.810 1407.544 1.920 25.842 1.872 0.57 230489. 0.1324
|
|
103.41 0.7800 0.7936 0.0183 0.0180 1.592 14.330 4.581 1186.801 1.619 20.375 1.751 0.57 231351. 0.1099
|
|
107.54 0.8112 0.7525 0.0134 0.0144 1.276 11.488 3.348 951.406 1.298 14.892 1.596 0.57 232242. 0.0857
|
|
111.68 0.8424 0.6694 0.0085 0.0107 0.942 8.482 2.117 702.449 0.958 9.418 1.367 0.57 233162. 0.0584
|
|
115.82 0.8736 0.4673 0.0036 0.0067 0.592 5.327 0.895 441.214 0.602 3.982 0.920 0.58 234107. 0.0255
|
|
119.95 0.9048
|
|
|
|
|
|
|
|
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 0.0905 0.0310 4.090 32.224 29.519 3050.022 3.641 131.298 4.390 0.63 250073. 0.6997
|
|
4.69 0.0310 0.0870 0.0901 0.0321 4.228 33.313 29.411 3153.042 3.764 130.820 4.231 0.63 250255. 0.6731
|
|
9.38 0.0619 0.1675 0.0897 0.0332 4.374 34.462 29.280 3261.765 3.893 130.237 4.072 0.63 250462. 0.6464
|
|
14.07 0.0929 0.2415 0.0892 0.0343 4.526 35.657 29.119 3374.961 4.029 129.523 3.913 0.63 250694. 0.6196
|
|
18.77 0.1239 0.3091 0.0886 0.0355 4.682 36.884 28.921 3491.010 4.167 128.641 3.758 0.64 250955. 0.5929
|
|
23.46 0.1548 0.3707 0.0879 0.0367 4.838 38.117 28.676 3607.734 4.306 127.549 3.605 0.64 251244. 0.5664
|
|
28.15 0.1858 0.4266 0.0869 0.0379 4.992 39.328 28.372 3722.348 4.443 126.199 3.457 0.64 251565. 0.5403
|
|
32.84 0.2167 0.4772 0.0858 0.0390 5.138 40.481 27.999 3831.470 4.573 124.538 3.314 0.64 251918. 0.5145
|
|
37.53 0.2477 0.5229 0.0844 0.0400 5.272 41.534 27.543 3931.186 4.693 122.510 3.178 0.64 252304. 0.4893
|
|
42.22 0.2787 0.5641 0.0827 0.0409 5.387 42.443 26.992 4017.174 4.795 120.061 3.048 0.64 252725. 0.4645
|
|
46.91 0.3096 0.6014 0.0807 0.0415 5.478 43.159 26.336 4084.953 4.876 117.144 2.924 0.64 253181. 0.4403
|
|
51.61 0.3406 0.6352 0.0783 0.0420 5.539 43.637 25.567 4130.232 4.930 113.723 2.808 0.64 253673. 0.4165
|
|
56.30 0.3716 0.6659 0.0756 0.0422 5.565 43.841 24.682 4149.480 4.953 109.786 2.698 0.64 254201. 0.3932
|
|
60.99 0.4025 0.6937 0.0726 0.0421 5.552 43.745 23.684 4140.426 4.942 105.348 2.595 0.64 254764. 0.3704
|
|
65.68 0.4335 0.7190 0.0692 0.0417 5.501 43.340 22.583 4102.076 4.896 100.449 2.497 0.64 255362. 0.3481
|
|
70.37 0.4645 0.7419 0.0655 0.0410 5.410 42.624 21.389 4034.327 4.816 95.137 2.405 0.64 255996. 0.3263
|
|
75.06 0.4954 0.7624 0.0616 0.0401 5.280 41.602 20.114 3937.599 4.700 89.465 2.317 0.64 256664. 0.3048
|
|
79.75 0.5264 0.7807 0.0575 0.0388 5.113 40.280 18.769 3812.505 4.551 83.483 2.233 0.64 257367. 0.2838
|
|
84.45 0.5573 0.7967 0.0532 0.0372 4.908 38.666 17.364 3659.699 4.368 77.234 2.152 0.64 258104. 0.2631
|
|
89.14 0.5883 0.8103 0.0487 0.0354 4.666 36.765 15.908 3479.779 4.154 70.758 2.074 0.65 258876. 0.2426
|
|
93.83 0.6193 0.8213 0.0442 0.0333 4.390 34.583 14.408 3273.274 3.907 64.089 1.997 0.65 259681. 0.2223
|
|
98.52 0.6502 0.8293 0.0394 0.0309 4.078 32.126 12.872 3040.663 3.630 57.254 1.920 0.65 260520. 0.2021
|
|
103.21 0.6812 0.8338 0.0346 0.0283 3.731 29.397 11.304 2782.401 3.321 50.282 1.843 0.65 261393. 0.1818
|
|
107.90 0.7122 0.8338 0.0298 0.0254 3.351 26.403 9.711 2498.999 2.983 43.196 1.763 0.65 262299. 0.1612
|
|
112.59 0.7431 0.8275 0.0248 0.0223 2.938 23.149 8.098 2191.085 2.615 36.022 1.676 0.65 263238. 0.1400
|
|
117.29 0.7741 0.8116 0.0198 0.0189 2.494 19.646 6.471 1859.494 2.220 28.784 1.578 0.65 264210. 0.1178
|
|
121.98 0.8051 0.7793 0.0148 0.0153 2.019 15.905 4.837 1505.365 1.797 21.513 1.457 0.66 265215. 0.0940
|
|
126.67 0.8360 0.7135 0.0098 0.0115 1.516 11.941 3.202 1130.248 1.349 14.242 1.285 0.66 266252. 0.0675
|
|
131.36 0.8670 0.5592 0.0048 0.0075 0.987 7.777 1.576 736.083 0.879 7.010 0.971 0.66 267319. 0.0358
|
|
136.05 0.8979 -0.0602 -0.0002 0.0032 0.422 3.329 -0.070 315.052 0.376 -0.312 -0.101 0.66 268322. 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 0.0910 0.0321 6.022 42.176 37.567 4490.933 4.765 167.099 3.794 0.71 281318. 0.6823
|
|
5.28 0.0309 0.0848 0.0907 0.0331 6.215 43.528 37.456 4634.874 4.918 166.603 3.665 0.71 281522. 0.6581
|
|
10.55 0.0619 0.1635 0.0904 0.0342 6.420 44.959 37.320 4787.298 5.079 165.997 3.536 0.71 281754. 0.6337
|
|
15.83 0.0928 0.2363 0.0900 0.0353 6.633 46.455 37.151 4946.587 5.248 165.247 3.406 0.71 282014. 0.6092
|
|
21.10 0.1238 0.3033 0.0894 0.0365 6.853 47.995 36.940 5110.526 5.422 164.308 3.278 0.71 282305. 0.5846
|
|
26.38 0.1547 0.3645 0.0888 0.0377 7.075 49.550 36.674 5276.068 5.598 163.124 3.153 0.71 282630. 0.5601
|
|
31.65 0.1857 0.4204 0.0880 0.0389 7.294 51.082 36.338 5439.257 5.771 161.631 3.030 0.72 282989. 0.5359
|
|
36.93 0.2166 0.4713 0.0870 0.0400 7.503 52.547 35.916 5595.233 5.937 159.755 2.911 0.72 283385. 0.5119
|
|
42.20 0.2476 0.5175 0.0857 0.0410 7.695 53.891 35.390 5738.334 6.089 157.416 2.797 0.72 283819. 0.4882
|
|
47.48 0.2785 0.5595 0.0841 0.0419 7.861 55.055 34.742 5862.298 6.220 154.534 2.688 0.72 284292. 0.4648
|
|
52.75 0.3095 0.5975 0.0822 0.0426 7.993 55.978 33.956 5960.606 6.324 151.038 2.584 0.72 284805. 0.4417
|
|
58.03 0.3404 0.6321 0.0799 0.0431 8.082 56.602 33.020 6026.979 6.395 146.872 2.485 0.72 285358. 0.4189
|
|
63.30 0.3714 0.6636 0.0773 0.0433 8.121 56.875 31.927 6056.103 6.426 142.011 2.391 0.72 285952. 0.3964
|
|
68.58 0.4023 0.6921 0.0743 0.0432 8.106 56.765 30.681 6044.424 6.413 136.469 2.302 0.72 286586. 0.3741
|
|
73.85 0.4333 0.7181 0.0709 0.0428 8.033 56.257 29.293 5990.236 6.356 130.295 2.218 0.72 287260. 0.3522
|
|
79.13 0.4642 0.7416 0.0673 0.0421 7.903 55.345 27.777 5893.184 6.253 123.553 2.138 0.72 287973. 0.3306
|
|
84.40 0.4951 0.7627 0.0633 0.0411 7.716 54.035 26.150 5753.664 6.105 116.315 2.061 0.72 288726. 0.3093
|
|
89.68 0.5261 0.7816 0.0591 0.0398 7.473 52.333 24.426 5572.410 5.913 108.647 1.988 0.72 289518. 0.2883
|
|
94.95 0.5570 0.7982 0.0548 0.0382 7.175 50.246 22.620 5350.190 5.677 100.613 1.918 0.73 290348. 0.2676
|
|
100.23 0.5880 0.8125 0.0502 0.0363 6.823 47.781 20.743 5087.774 5.398 92.265 1.849 0.73 291216. 0.2471
|
|
105.50 0.6189 0.8243 0.0455 0.0342 6.418 44.946 18.806 4785.919 5.078 83.651 1.782 0.73 292123. 0.2268
|
|
110.78 0.6499 0.8334 0.0407 0.0318 5.961 41.748 16.819 4445.377 4.717 74.809 1.716 0.73 293067. 0.2065
|
|
116.05 0.6808 0.8391 0.0358 0.0291 5.454 38.193 14.788 4066.862 4.315 65.776 1.649 0.73 294049. 0.1861
|
|
121.33 0.7118 0.8406 0.0308 0.0261 4.896 34.289 12.721 3651.143 3.874 56.584 1.580 0.73 295069. 0.1654
|
|
126.60 0.7427 0.8362 0.0257 0.0229 4.290 30.044 10.626 3199.147 3.394 47.267 1.507 0.73 296125. 0.1441
|
|
131.88 0.7737 0.8229 0.0206 0.0194 3.637 25.470 8.511 2712.090 2.878 37.857 1.423 0.74 297219. 0.1218
|
|
137.15 0.8046 0.7943 0.0155 0.0157 2.939 20.583 6.383 2191.689 2.325 28.393 1.321 0.74 298349. 0.0979
|
|
142.43 0.8356 0.7344 0.0103 0.0117 2.200 15.406 4.254 1640.440 1.741 18.920 1.176 0.74 299515. 0.0712
|
|
147.70 0.8665 0.5899 0.0052 0.0076 1.424 9.972 2.133 1061.806 1.127 9.487 0.911 0.74 300715. 0.0390
|
|
152.98 0.8975 -0.0010 0.0000 0.0032 0.603 4.224 -0.002 449.732 0.477 -0.007 -0.002 0.74 301877. 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 0.0914 0.0355 9.136 57.581 46.600 6812.534 6.505 207.277 3.103 0.79 312558. 0.6214
|
|
5.87 0.0310 0.0774 0.0912 0.0365 9.393 59.200 46.491 7004.112 6.688 206.793 3.011 0.79 312785. 0.6023
|
|
11.73 0.0620 0.1501 0.0909 0.0375 9.665 60.919 46.359 7207.384 6.883 206.205 2.917 0.79 313041. 0.5828
|
|
17.60 0.0929 0.2179 0.0906 0.0386 9.951 62.717 46.195 7420.127 7.086 205.475 2.824 0.79 313329. 0.5631
|
|
23.47 0.1239 0.2809 0.0902 0.0398 10.244 64.569 45.988 7639.239 7.295 204.553 2.730 0.79 313652. 0.5432
|
|
29.34 0.1549 0.3393 0.0897 0.0409 10.541 66.437 45.722 7860.246 7.506 203.373 2.638 0.79 314011. 0.5234
|
|
35.20 0.1859 0.3933 0.0890 0.0421 10.832 68.270 45.380 8077.164 7.713 201.851 2.548 0.79 314410. 0.5036
|
|
41.07 0.2169 0.4431 0.0881 0.0431 11.107 70.005 44.939 8282.456 7.909 199.888 2.461 0.80 314849. 0.4840
|
|
46.94 0.2478 0.4891 0.0870 0.0441 11.355 71.568 44.373 8467.289 8.086 197.372 2.377 0.80 315330. 0.4645
|
|
52.81 0.2788 0.5317 0.0856 0.0449 11.562 72.875 43.657 8622.026 8.233 194.187 2.297 0.80 315856. 0.4452
|
|
58.67 0.3098 0.5711 0.0839 0.0455 11.716 73.847 42.765 8736.991 8.343 190.221 2.220 0.80 316426. 0.4259
|
|
64.54 0.3408 0.6076 0.0817 0.0458 11.805 74.408 41.678 8803.328 8.407 185.384 2.147 0.80 317042. 0.4067
|
|
70.41 0.3718 0.6414 0.0792 0.0459 11.820 74.499 40.383 8814.100 8.417 179.625 2.078 0.80 317703. 0.3874
|
|
76.28 0.4027 0.6728 0.0763 0.0456 11.754 74.086 38.883 8765.298 8.370 172.950 2.012 0.80 318410. 0.3681
|
|
82.14 0.4337 0.7017 0.0729 0.0451 11.608 73.162 37.188 8655.869 8.266 165.412 1.949 0.80 319162. 0.3486
|
|
88.01 0.4647 0.7283 0.0693 0.0442 11.381 71.733 35.318 8486.802 8.104 157.093 1.888 0.80 319959. 0.3291
|
|
93.88 0.4957 0.7524 0.0653 0.0430 11.077 69.815 33.293 8259.993 7.888 148.086 1.828 0.80 320799. 0.3095
|
|
99.74 0.5267 0.7741 0.0611 0.0415 10.698 67.427 31.134 7977.416 7.618 138.486 1.770 0.80 321683. 0.2898
|
|
105.61 0.5576 0.7932 0.0566 0.0398 10.246 64.581 28.861 7640.691 7.296 128.375 1.713 0.81 322609. 0.2700
|
|
111.48 0.5886 0.8098 0.0520 0.0378 9.724 61.287 26.490 7250.938 6.924 117.829 1.657 0.81 323578. 0.2502
|
|
117.35 0.6196 0.8237 0.0471 0.0355 9.131 57.550 24.036 6808.804 6.502 106.912 1.601 0.81 324590. 0.2303
|
|
123.21 0.6506 0.8346 0.0422 0.0329 8.468 53.373 21.511 6314.622 6.030 95.679 1.545 0.81 325643. 0.2102
|
|
129.08 0.6816 0.8421 0.0371 0.0300 7.736 48.758 18.925 5768.597 5.509 84.180 1.488 0.81 326739. 0.1899
|
|
134.95 0.7125 0.8453 0.0319 0.0269 6.934 43.707 16.290 5171.048 4.938 72.458 1.429 0.81 327875. 0.1692
|
|
140.82 0.7435 0.8422 0.0267 0.0236 6.069 38.254 13.614 4525.918 4.322 60.554 1.364 0.82 329053. 0.1477
|
|
146.68 0.7745 0.8295 0.0214 0.0200 5.143 32.413 10.907 3834.809 3.662 48.513 1.290 0.82 330272. 0.1250
|
|
152.55 0.8055 0.8000 0.0160 0.0162 4.159 26.215 8.179 3101.533 2.962 36.382 1.196 0.82 331531. 0.1004
|
|
158.42 0.8364 0.7351 0.0107 0.0121 3.128 19.717 5.444 2332.798 2.228 24.215 1.058 0.82 332830. 0.0725
|
|
164.29 0.8674 0.5768 0.0053 0.0080 2.061 12.991 2.714 1537.042 1.468 12.071 0.801 0.82 334166. 0.0387
|
|
170.15 0.8984 -0.0236 -0.0001 0.0037 0.943 5.940 -0.049 702.824 0.671 -0.218 -0.032 0.83 335446. 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 0.0912 0.0419 14.354 82.244 56.289 10703.529 9.292 250.374 2.385 0.87 343820. 0.5250
|
|
6.47 0.0310 0.0659 0.0911 0.0429 14.693 84.189 56.186 10956.654 9.512 249.916 2.326 0.87 344067. 0.5115
|
|
12.93 0.0621 0.1284 0.0909 0.0439 15.056 86.267 56.064 11227.024 9.746 249.371 2.265 0.87 344347. 0.4975
|
|
19.40 0.0931 0.1873 0.0906 0.0450 15.439 88.463 55.914 11512.776 9.994 248.708 2.203 0.87 344662. 0.4833
|
|
25.86 0.1241 0.2427 0.0903 0.0462 15.837 90.745 55.727 11809.765 10.252 247.874 2.140 0.87 345014. 0.4687
|
|
32.33 0.1552 0.2945 0.0899 0.0474 16.242 93.065 55.486 12111.797 10.514 246.800 2.078 0.87 345407. 0.4541
|
|
38.79 0.1862 0.3429 0.0894 0.0486 16.642 95.357 55.170 12410.088 10.773 245.395 2.016 0.87 345842. 0.4394
|
|
45.26 0.2172 0.3882 0.0887 0.0497 17.021 97.530 54.752 12692.864 11.019 243.538 1.957 0.87 346322. 0.4247
|
|
51.72 0.2483 0.4306 0.0879 0.0507 17.360 99.471 54.201 12945.448 11.238 241.088 1.899 0.88 346850. 0.4102
|
|
58.19 0.2793 0.4705 0.0867 0.0515 17.635 101.049 53.481 13150.787 11.416 237.882 1.845 0.88 347425. 0.3958
|
|
64.65 0.3103 0.5083 0.0852 0.0520 17.824 102.127 52.553 13291.050 11.538 233.754 1.793 0.88 348051. 0.3814
|
|
71.12 0.3414 0.5443 0.0833 0.0522 17.902 102.578 51.384 13349.770 11.589 228.554 1.746 0.88 348728. 0.3671
|
|
77.58 0.3724 0.5788 0.0810 0.0521 17.855 102.306 49.950 13314.462 11.559 222.178 1.702 0.88 349456. 0.3528
|
|
84.05 0.4034 0.6118 0.0782 0.0516 17.673 101.264 48.245 13178.856 11.441 214.594 1.660 0.88 350235. 0.3384
|
|
90.51 0.4345 0.6435 0.0750 0.0506 17.357 99.453 46.278 12943.067 11.236 205.843 1.622 0.88 351065. 0.3237
|
|
96.98 0.4655 0.6738 0.0714 0.0493 16.912 96.905 44.067 12611.477 10.948 196.009 1.585 0.88 351945. 0.3087
|
|
103.45 0.4965 0.7025 0.0675 0.0477 16.350 93.682 41.639 12192.048 10.584 185.210 1.549 0.88 352874. 0.2933
|
|
109.91 0.5276 0.7293 0.0632 0.0458 15.681 89.849 39.022 11693.272 10.151 173.570 1.514 0.88 353852. 0.2774
|
|
116.38 0.5586 0.7540 0.0587 0.0435 14.915 85.461 36.242 11122.165 9.655 161.203 1.478 0.89 354877. 0.2610
|
|
122.84 0.5896 0.7763 0.0540 0.0410 14.059 80.558 33.321 10484.078 9.101 148.213 1.442 0.89 355950. 0.2441
|
|
129.31 0.6207 0.7959 0.0491 0.0383 13.119 75.168 30.281 9782.551 8.492 134.691 1.404 0.89 357069. 0.2267
|
|
135.77 0.6517 0.8123 0.0440 0.0353 12.095 69.305 27.139 9019.574 7.830 120.716 1.365 0.89 358234. 0.2086
|
|
142.24 0.6827 0.8251 0.0388 0.0321 10.991 62.976 23.911 8195.943 7.115 106.355 1.323 0.89 359446. 0.1898
|
|
148.70 0.7138 0.8335 0.0334 0.0286 9.805 56.183 20.610 7311.876 6.348 91.674 1.278 0.89 360702. 0.1703
|
|
155.17 0.7448 0.8344 0.0280 0.0250 8.554 49.011 17.249 6378.420 5.537 76.724 1.227 0.90 362004. 0.1495
|
|
161.63 0.7758 0.8135 0.0224 0.0214 7.325 41.973 13.827 5462.470 4.742 61.501 1.148 0.90 363351. 0.1252
|
|
168.10 0.8069 0.7673 0.0168 0.0177 6.058 34.713 10.370 4517.629 3.922 46.127 1.041 0.90 364742. 0.0984
|
|
174.56 0.8379 0.6738 0.0112 0.0139 4.766 27.306 6.898 3553.665 3.085 30.682 0.880 0.90 366177. 0.0678
|
|
181.03 0.8689 0.4770 0.0056 0.0101 3.470 19.881 3.429 2587.436 2.246 15.251 0.601 0.91 367653. 0.0327
|
|
187.50 0.9000 -0.0159 -0.0001 0.0063 2.152 12.333 -0.069 1605.022 1.393 -0.305 -0.019 0.91 369108. 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 0.0887 0.0480 21.338 112.076 65.150 15911.921 12.662 289.789 1.857 0.95 375148. 0.4398
|
|
7.10 0.0313 0.0567 0.0886 0.0488 21.719 114.078 65.026 16196.179 12.889 289.235 1.821 0.95 375419. 0.4308
|
|
14.21 0.0625 0.1111 0.0884 0.0497 22.136 116.267 64.886 16506.877 13.136 288.613 1.783 0.95 375725. 0.4213
|
|
21.31 0.0938 0.1629 0.0882 0.0508 22.585 118.627 64.724 16841.971 13.402 287.894 1.743 0.95 376069. 0.4114
|
|
28.42 0.1250 0.2120 0.0879 0.0518 23.063 121.134 64.530 17197.949 13.686 287.030 1.702 0.95 376454. 0.4011
|
|
35.52 0.1563 0.2585 0.0876 0.0529 23.560 123.746 64.289 17568.781 13.981 285.957 1.660 0.95 376883. 0.3904
|
|
42.63 0.1876 0.3022 0.0871 0.0541 24.063 126.387 63.978 17943.725 14.279 284.575 1.617 0.95 377359. 0.3795
|
|
49.73 0.2188 0.3433 0.0866 0.0552 24.553 128.961 63.571 18309.166 14.570 282.762 1.575 0.95 377884. 0.3684
|
|
56.84 0.2501 0.3820 0.0858 0.0562 25.011 131.367 63.034 18650.732 14.842 280.376 1.533 0.96 378460. 0.3571
|
|
63.94 0.2813 0.4182 0.0849 0.0571 25.409 133.460 62.329 18947.838 15.078 277.237 1.492 0.96 379090. 0.3456
|
|
71.05 0.3126 0.4524 0.0836 0.0578 25.717 135.077 61.410 19177.439 15.261 273.153 1.452 0.96 379774. 0.3339
|
|
78.15 0.3439 0.4846 0.0820 0.0582 25.903 136.054 60.237 19316.102 15.371 267.935 1.414 0.96 380515. 0.3221
|
|
85.25 0.3751 0.5151 0.0801 0.0583 25.939 136.243 58.777 19342.924 15.393 261.440 1.378 0.96 381312. 0.3100
|
|
92.36 0.4064 0.5441 0.0776 0.0580 25.804 135.534 57.013 19242.336 15.313 253.593 1.344 0.96 382166. 0.2977
|
|
99.46 0.4376 0.5718 0.0748 0.0573 25.486 133.862 54.945 19004.896 15.124 244.394 1.311 0.96 383076. 0.2852
|
|
106.57 0.4689 0.5982 0.0716 0.0561 24.977 131.188 52.583 18625.354 14.822 233.888 1.281 0.96 384042. 0.2724
|
|
113.67 0.5002 0.6237 0.0680 0.0545 24.273 127.492 49.942 18100.637 14.404 222.143 1.251 0.96 385063. 0.2595
|
|
120.78 0.5314 0.6481 0.0641 0.0525 23.374 122.767 47.040 17429.781 13.870 209.234 1.224 0.97 386139. 0.2463
|
|
127.88 0.5627 0.6718 0.0598 0.0501 22.282 117.035 43.895 16615.902 13.223 195.246 1.198 0.97 387269. 0.2329
|
|
134.99 0.5939 0.6944 0.0552 0.0472 21.009 110.349 40.528 15666.774 12.467 180.270 1.173 0.97 388453. 0.2191
|
|
142.09 0.6252 0.7156 0.0503 0.0440 19.572 102.800 36.964 14594.925 11.614 164.414 1.149 0.97 389689. 0.2049
|
|
149.20 0.6565 0.7349 0.0453 0.0404 17.987 94.477 33.225 13413.256 10.674 147.786 1.124 0.97 390979. 0.1900
|
|
156.30 0.6877 0.7515 0.0400 0.0366 16.271 85.461 29.336 12133.191 9.655 130.487 1.097 0.97 392319. 0.1743
|
|
163.41 0.7190 0.7642 0.0345 0.0324 14.436 75.824 25.320 10765.110 8.567 112.624 1.067 0.98 393711. 0.1575
|
|
170.51 0.7502 0.7699 0.0289 0.0281 12.519 65.757 21.200 9335.786 7.429 94.297 1.030 0.98 395152. 0.1391
|
|
177.61 0.7815 0.7461 0.0231 0.0242 10.770 56.569 16.966 8031.284 6.391 75.463 0.958 0.98 396643. 0.1158
|
|
184.72 0.8128 0.6677 0.0172 0.0209 9.320 48.953 12.633 6950.002 5.531 56.193 0.824 0.98 398184. 0.0860
|
|
191.82 0.8440 0.5339 0.0113 0.0178 7.941 41.710 8.288 5921.725 4.712 36.867 0.635 0.99 399772. 0.0536
|
|
198.93 0.8753 0.3189 0.0054 0.0149 6.638 34.864 3.990 4949.771 3.939 17.750 0.366 0.99 401408. 0.0214
|
|
206.03 0.9065 -0.0281 -0.0004 0.0120 5.345 28.071 -0.274 3985.397 3.171 -1.217 -0.031 0.99 403085. 0.0000
|
|
|
|
|
|
|