649 lines
115 KiB
Plaintext
649 lines
115 KiB
Plaintext
14x10F (14x10F.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 0.1170 0.0558 0.002 0.144 0.137 1.707 0.016 0.610 36.463 0.05 21212. 0.5722
|
|
0.39 0.0300 0.0613 0.1158 0.0567 0.002 0.146 0.136 1.733 0.017 0.604 35.542 0.05 21231. 0.5549
|
|
0.79 0.0600 0.1193 0.1145 0.0575 0.002 0.149 0.134 1.759 0.017 0.597 34.613 0.05 21251. 0.5373
|
|
1.18 0.0899 0.1742 0.1130 0.0583 0.002 0.151 0.133 1.784 0.017 0.589 33.683 0.05 21274. 0.5194
|
|
1.57 0.1199 0.2258 0.1113 0.0591 0.002 0.153 0.131 1.808 0.017 0.581 32.755 0.05 21298. 0.5014
|
|
1.97 0.1499 0.2743 0.1095 0.0598 0.002 0.155 0.128 1.830 0.017 0.571 31.834 0.06 21325. 0.4833
|
|
2.36 0.1799 0.3198 0.1075 0.0605 0.002 0.156 0.126 1.849 0.018 0.561 30.921 0.06 21354. 0.4651
|
|
2.75 0.2098 0.3622 0.1053 0.0610 0.003 0.158 0.123 1.865 0.018 0.549 30.021 0.06 21386. 0.4469
|
|
3.15 0.2398 0.4017 0.1028 0.0614 0.003 0.159 0.121 1.877 0.018 0.536 29.135 0.06 21420. 0.4286
|
|
3.54 0.2698 0.4384 0.1001 0.0616 0.003 0.159 0.117 1.884 0.018 0.522 28.264 0.06 21457. 0.4103
|
|
3.93 0.2998 0.4724 0.0972 0.0617 0.003 0.159 0.114 1.886 0.018 0.507 27.409 0.06 21497. 0.3920
|
|
4.32 0.3297 0.5037 0.0940 0.0615 0.003 0.159 0.110 1.881 0.018 0.490 26.568 0.06 21539. 0.3736
|
|
4.72 0.3597 0.5324 0.0905 0.0611 0.003 0.158 0.106 1.869 0.018 0.472 25.741 0.06 21583. 0.3552
|
|
5.11 0.3897 0.5584 0.0867 0.0605 0.002 0.156 0.102 1.850 0.018 0.452 24.923 0.06 21631. 0.3366
|
|
5.50 0.4197 0.5818 0.0826 0.0596 0.002 0.154 0.097 1.823 0.017 0.431 24.111 0.06 21681. 0.3179
|
|
5.90 0.4496 0.6023 0.0783 0.0584 0.002 0.151 0.092 1.787 0.017 0.408 23.298 0.06 21734. 0.2990
|
|
6.29 0.4796 0.6199 0.0736 0.0570 0.002 0.147 0.086 1.742 0.017 0.384 22.477 0.06 21790. 0.2798
|
|
6.68 0.5096 0.6341 0.0687 0.0552 0.002 0.143 0.081 1.688 0.016 0.358 21.639 0.06 21848. 0.2602
|
|
7.08 0.5396 0.6445 0.0635 0.0532 0.002 0.137 0.075 1.627 0.016 0.331 20.775 0.06 21909. 0.2402
|
|
7.47 0.5695 0.6507 0.0582 0.0509 0.002 0.132 0.068 1.557 0.015 0.303 19.870 0.06 21972. 0.2199
|
|
7.86 0.5995 0.6518 0.0526 0.0484 0.002 0.125 0.062 1.481 0.014 0.275 18.909 0.06 22038. 0.1990
|
|
8.26 0.6295 0.6469 0.0470 0.0457 0.002 0.118 0.055 1.398 0.013 0.245 17.873 0.06 22107. 0.1777
|
|
8.65 0.6595 0.6346 0.0412 0.0428 0.002 0.111 0.048 1.309 0.013 0.215 16.736 0.06 22178. 0.1558
|
|
9.04 0.6895 0.6131 0.0353 0.0397 0.002 0.103 0.041 1.215 0.012 0.184 15.466 0.06 22252. 0.1333
|
|
9.44 0.7194 0.5798 0.0294 0.0365 0.001 0.094 0.034 1.115 0.011 0.153 14.016 0.06 22329. 0.1102
|
|
9.83 0.7494 0.5309 0.0234 0.0330 0.001 0.085 0.027 1.010 0.010 0.122 12.320 0.06 22408. 0.0865
|
|
10.22 0.7794 0.4606 0.0174 0.0295 0.001 0.076 0.020 0.902 0.009 0.091 10.278 0.06 22490. 0.0622
|
|
10.62 0.8094 0.3599 0.0115 0.0258 0.001 0.067 0.013 0.790 0.008 0.060 7.733 0.06 22574. 0.0380
|
|
11.01 0.8393 0.2133 0.0056 0.0221 0.001 0.057 0.007 0.675 0.006 0.029 4.419 0.06 22661. 0.0152
|
|
11.40 0.8693 -0.0072 -0.0002 0.0182 0.001 0.047 0.000 0.558 0.005 -0.001 -0.144 0.06 22750. 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 0.1174 0.0516 0.017 0.534 0.551 12.626 0.060 2.449 19.781 0.11 42424. 0.6219
|
|
0.80 0.0306 0.0677 0.1162 0.0525 0.017 0.543 0.545 12.855 0.061 2.424 19.229 0.11 42462. 0.6014
|
|
1.61 0.0612 0.1315 0.1148 0.0535 0.018 0.553 0.539 13.082 0.062 2.396 18.675 0.11 42504. 0.5807
|
|
2.41 0.0918 0.1914 0.1133 0.0544 0.018 0.562 0.532 13.303 0.064 2.364 18.124 0.11 42550. 0.5598
|
|
3.21 0.1225 0.2476 0.1116 0.0552 0.018 0.571 0.524 13.514 0.065 2.329 17.577 0.11 42601. 0.5389
|
|
4.02 0.1531 0.2999 0.1098 0.0560 0.018 0.579 0.515 13.709 0.065 2.291 17.038 0.11 42656. 0.5180
|
|
4.82 0.1837 0.3487 0.1077 0.0567 0.019 0.587 0.505 13.882 0.066 2.247 16.508 0.11 42716. 0.4971
|
|
5.62 0.2143 0.3941 0.1054 0.0573 0.019 0.593 0.494 14.028 0.067 2.199 15.988 0.11 42782. 0.4763
|
|
6.43 0.2449 0.4361 0.1029 0.0578 0.019 0.598 0.483 14.139 0.068 2.147 15.481 0.11 42853. 0.4556
|
|
7.23 0.2755 0.4749 0.1001 0.0581 0.019 0.600 0.469 14.209 0.068 2.088 14.987 0.11 42929. 0.4350
|
|
8.03 0.3062 0.5107 0.0970 0.0582 0.019 0.601 0.455 14.231 0.068 2.024 14.506 0.11 43011. 0.4146
|
|
8.83 0.3368 0.5437 0.0937 0.0580 0.019 0.600 0.439 14.199 0.068 1.955 14.037 0.11 43098. 0.3942
|
|
9.64 0.3674 0.5738 0.0900 0.0577 0.019 0.596 0.422 14.107 0.067 1.879 13.581 0.11 43191. 0.3739
|
|
10.44 0.3980 0.6012 0.0861 0.0570 0.019 0.589 0.404 13.949 0.067 1.797 13.134 0.11 43289. 0.3536
|
|
11.24 0.4286 0.6258 0.0819 0.0561 0.018 0.580 0.384 13.721 0.066 1.708 12.696 0.11 43393. 0.3333
|
|
12.05 0.4592 0.6476 0.0773 0.0548 0.018 0.567 0.363 13.418 0.064 1.614 12.262 0.11 43503. 0.3129
|
|
12.85 0.4899 0.6664 0.0725 0.0533 0.017 0.551 0.340 13.038 0.062 1.512 11.829 0.11 43618. 0.2922
|
|
13.65 0.5205 0.6819 0.0674 0.0514 0.017 0.532 0.316 12.581 0.060 1.406 11.393 0.11 43739. 0.2713
|
|
14.46 0.5511 0.6939 0.0620 0.0493 0.016 0.509 0.291 12.053 0.058 1.294 10.949 0.11 43865. 0.2502
|
|
15.26 0.5817 0.7016 0.0565 0.0468 0.015 0.484 0.265 11.459 0.055 1.179 10.488 0.11 43997. 0.2287
|
|
16.06 0.6123 0.7044 0.0508 0.0442 0.014 0.457 0.238 10.803 0.052 1.060 10.002 0.11 44135. 0.2068
|
|
16.87 0.6429 0.7010 0.0450 0.0412 0.014 0.426 0.211 10.089 0.048 0.938 9.481 0.11 44277. 0.1845
|
|
17.67 0.6736 0.6901 0.0390 0.0381 0.012 0.394 0.183 9.321 0.045 0.814 8.910 0.11 44426. 0.1615
|
|
18.47 0.7042 0.6694 0.0330 0.0347 0.011 0.359 0.155 8.501 0.041 0.689 8.266 0.11 44579. 0.1378
|
|
19.28 0.7348 0.6353 0.0270 0.0312 0.010 0.323 0.127 7.635 0.036 0.563 7.518 0.11 44738. 0.1133
|
|
20.08 0.7654 0.5823 0.0209 0.0275 0.009 0.284 0.098 6.727 0.032 0.436 6.616 0.11 44903. 0.0878
|
|
20.88 0.7960 0.5012 0.0149 0.0236 0.008 0.244 0.070 5.782 0.028 0.310 5.475 0.11 45072. 0.0613
|
|
21.68 0.8266 0.3746 0.0089 0.0196 0.006 0.203 0.042 4.808 0.023 0.186 3.940 0.11 45247. 0.0341
|
|
22.49 0.8573 0.1671 0.0030 0.0156 0.005 0.161 0.014 3.811 0.018 0.063 1.695 0.11 45427. 0.0086
|
|
23.29 0.8879
|
|
|
|
|
|
|
|
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 0.1177 0.0498 0.055 1.159 1.242 41.130 0.131 5.524 13.696 0.16 63635. 0.6466
|
|
1.19 0.0302 0.0693 0.1165 0.0508 0.056 1.181 1.229 41.912 0.133 5.469 13.305 0.16 63691. 0.6250
|
|
2.38 0.0604 0.1345 0.1152 0.0517 0.057 1.203 1.216 42.692 0.136 5.407 12.915 0.16 63753. 0.6032
|
|
3.56 0.0906 0.1957 0.1137 0.0526 0.058 1.224 1.200 43.454 0.138 5.338 12.526 0.16 63821. 0.5813
|
|
4.75 0.1208 0.2529 0.1121 0.0535 0.059 1.245 1.183 44.184 0.141 5.261 12.142 0.16 63896. 0.5594
|
|
5.94 0.1509 0.3063 0.1102 0.0543 0.060 1.264 1.164 44.865 0.143 5.176 11.764 0.17 63977. 0.5376
|
|
7.13 0.1811 0.3560 0.1082 0.0551 0.061 1.281 1.142 45.477 0.145 5.081 11.393 0.17 64066. 0.5159
|
|
8.32 0.2113 0.4021 0.1060 0.0557 0.062 1.296 1.119 46.001 0.146 4.976 11.031 0.17 64162. 0.4943
|
|
9.50 0.2415 0.4448 0.1035 0.0562 0.062 1.308 1.093 46.414 0.148 4.860 10.678 0.17 64266. 0.4729
|
|
10.69 0.2717 0.4844 0.1008 0.0565 0.063 1.316 1.064 46.696 0.149 4.733 10.335 0.17 64378. 0.4516
|
|
11.88 0.3019 0.5209 0.0978 0.0567 0.063 1.319 1.033 46.822 0.149 4.593 10.003 0.17 64498. 0.4306
|
|
13.07 0.3321 0.5545 0.0946 0.0566 0.063 1.318 0.998 46.772 0.149 4.440 9.680 0.17 64625. 0.4097
|
|
14.25 0.3623 0.5854 0.0910 0.0563 0.062 1.311 0.961 46.526 0.148 4.274 9.367 0.17 64761. 0.3890
|
|
15.44 0.3925 0.6136 0.0872 0.0558 0.062 1.298 0.920 46.064 0.147 4.094 9.063 0.17 64906. 0.3684
|
|
16.63 0.4226 0.6391 0.0831 0.0549 0.061 1.278 0.877 45.373 0.144 3.901 8.766 0.17 65058. 0.3478
|
|
17.82 0.4528 0.6620 0.0787 0.0538 0.060 1.252 0.830 44.436 0.141 3.693 8.475 0.17 65219. 0.3272
|
|
19.01 0.4830 0.6822 0.0739 0.0524 0.058 1.218 0.780 43.238 0.138 3.472 8.187 0.17 65387. 0.3064
|
|
20.19 0.5132 0.6994 0.0690 0.0506 0.056 1.177 0.728 41.781 0.133 3.237 7.900 0.17 65564. 0.2855
|
|
21.38 0.5434 0.7135 0.0637 0.0485 0.054 1.129 0.673 40.080 0.128 2.992 7.612 0.17 65749. 0.2645
|
|
22.57 0.5736 0.7239 0.0583 0.0462 0.051 1.075 0.615 38.150 0.121 2.737 7.317 0.17 65942. 0.2432
|
|
23.76 0.6038 0.7301 0.0527 0.0436 0.048 1.014 0.556 36.006 0.115 2.475 7.010 0.17 66143. 0.2215
|
|
24.95 0.6340 0.7312 0.0470 0.0408 0.045 0.948 0.496 33.658 0.107 2.207 6.686 0.17 66352. 0.1995
|
|
26.13 0.6642 0.7260 0.0412 0.0377 0.042 0.877 0.435 31.119 0.099 1.934 6.337 0.17 66569. 0.1770
|
|
27.32 0.6943 0.7125 0.0353 0.0344 0.038 0.800 0.372 28.401 0.090 1.657 5.949 0.17 66794. 0.1538
|
|
28.51 0.7245 0.6881 0.0293 0.0309 0.034 0.719 0.310 25.516 0.081 1.378 5.506 0.17 67026. 0.1298
|
|
29.70 0.7547 0.6481 0.0234 0.0272 0.030 0.633 0.247 22.479 0.072 1.097 4.978 0.17 67267. 0.1048
|
|
30.88 0.7849 0.5848 0.0174 0.0234 0.026 0.544 0.184 19.309 0.061 0.818 4.319 0.17 67515. 0.0785
|
|
32.07 0.8151 0.4837 0.0115 0.0194 0.021 0.452 0.122 16.025 0.051 0.541 3.440 0.17 67771. 0.0508
|
|
33.26 0.8453 0.3146 0.0057 0.0153 0.017 0.356 0.060 12.653 0.040 0.268 2.157 0.17 68034. 0.0224
|
|
34.45 0.8755 0.0017 0.0000 0.0112 0.012 0.260 0.000 9.219 0.029 0.001 0.011 0.17 68305. 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 0.1180 0.0488 0.128 2.019 2.213 95.550 0.228 9.845 10.507 0.22 84845. 0.6622
|
|
1.59 0.0302 0.0710 0.1168 0.0498 0.131 2.059 2.191 97.445 0.233 9.747 10.200 0.22 84920. 0.6397
|
|
3.17 0.0605 0.1376 0.1155 0.0507 0.133 2.099 2.167 99.334 0.237 9.638 9.894 0.22 85003. 0.6170
|
|
4.76 0.0907 0.2001 0.1140 0.0517 0.136 2.138 2.139 101.185 0.242 9.516 9.590 0.22 85094. 0.5942
|
|
6.35 0.1210 0.2585 0.1124 0.0526 0.138 2.176 2.109 102.960 0.246 9.380 9.290 0.22 85194. 0.5715
|
|
7.93 0.1512 0.3128 0.1106 0.0534 0.140 2.211 2.075 104.620 0.250 9.229 8.995 0.22 85303. 0.5489
|
|
9.52 0.1815 0.3634 0.1086 0.0542 0.142 2.242 2.037 106.119 0.253 9.060 8.706 0.22 85421. 0.5264
|
|
11.11 0.2117 0.4102 0.1063 0.0549 0.144 2.270 1.995 107.407 0.256 8.874 8.425 0.22 85550. 0.5041
|
|
12.69 0.2419 0.4536 0.1039 0.0554 0.145 2.291 1.949 108.433 0.259 8.668 8.151 0.22 85689. 0.4821
|
|
14.28 0.2722 0.4937 0.1011 0.0558 0.146 2.306 1.898 109.142 0.261 8.441 7.886 0.22 85839. 0.4602
|
|
15.87 0.3024 0.5307 0.0981 0.0559 0.147 2.313 1.842 109.480 0.261 8.191 7.629 0.22 85999. 0.4386
|
|
17.45 0.3327 0.5648 0.0949 0.0559 0.147 2.312 1.780 109.396 0.261 7.919 7.381 0.22 86170. 0.4172
|
|
19.04 0.3629 0.5961 0.0913 0.0556 0.146 2.300 1.714 108.839 0.260 7.622 7.141 0.22 86352. 0.3960
|
|
20.63 0.3932 0.6247 0.0875 0.0551 0.145 2.277 1.641 107.765 0.257 7.301 6.909 0.22 86545. 0.3750
|
|
22.21 0.4234 0.6507 0.0833 0.0542 0.142 2.243 1.564 106.137 0.253 6.955 6.682 0.22 86748. 0.3540
|
|
23.80 0.4536 0.6742 0.0789 0.0531 0.139 2.196 1.480 103.916 0.248 6.585 6.461 0.22 86963. 0.3330
|
|
25.39 0.4839 0.6949 0.0741 0.0516 0.136 2.136 1.391 101.065 0.241 6.188 6.244 0.22 87189. 0.3120
|
|
26.97 0.5141 0.7129 0.0691 0.0499 0.131 2.062 1.297 97.587 0.233 5.769 6.028 0.22 87426. 0.2909
|
|
28.56 0.5444 0.7278 0.0639 0.0478 0.125 1.976 1.198 93.518 0.223 5.331 5.813 0.22 87674. 0.2696
|
|
30.15 0.5746 0.7392 0.0584 0.0454 0.119 1.878 1.096 88.893 0.212 4.876 5.594 0.22 87932. 0.2481
|
|
31.73 0.6049 0.7467 0.0528 0.0428 0.112 1.770 0.991 83.744 0.200 4.408 5.367 0.22 88201. 0.2264
|
|
33.32 0.6351 0.7493 0.0471 0.0399 0.105 1.650 0.883 78.099 0.186 3.929 5.130 0.22 88480. 0.2042
|
|
34.91 0.6653 0.7459 0.0412 0.0368 0.097 1.521 0.774 71.986 0.172 3.441 4.874 0.22 88770. 0.1816
|
|
36.49 0.6956 0.7347 0.0353 0.0334 0.088 1.383 0.662 65.434 0.156 2.947 4.592 0.23 89071. 0.1583
|
|
38.08 0.7258 0.7128 0.0293 0.0299 0.078 1.236 0.550 58.474 0.140 2.448 4.270 0.23 89382. 0.1342
|
|
39.67 0.7561 0.6757 0.0233 0.0261 0.069 1.081 0.438 51.142 0.122 1.949 3.885 0.23 89704. 0.1090
|
|
41.25 0.7863 0.6151 0.0174 0.0222 0.058 0.919 0.326 43.482 0.104 1.450 3.401 0.23 90036. 0.0823
|
|
42.84 0.8166 0.5154 0.0115 0.0182 0.048 0.751 0.215 35.545 0.085 0.957 2.744 0.23 90378. 0.0539
|
|
44.43 0.8468 0.3413 0.0056 0.0140 0.037 0.579 0.106 27.393 0.065 0.471 1.752 0.23 90731. 0.0242
|
|
46.01 0.8770 -0.0039 0.0000 0.0098 0.026 0.403 -0.001 19.089 0.046 -0.004 -0.019 0.23 91091. 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 0.1183 0.0482 0.247 3.117 3.468 184.362 0.352 15.426 8.532 0.27 106054. 0.6732
|
|
1.98 0.0303 0.0721 0.1171 0.0492 0.252 3.180 3.434 188.123 0.359 15.275 8.280 0.27 106148. 0.6500
|
|
3.97 0.0605 0.1397 0.1158 0.0502 0.257 3.244 3.396 191.878 0.366 15.105 8.028 0.27 106251. 0.6267
|
|
5.95 0.0908 0.2030 0.1144 0.0512 0.262 3.306 3.353 195.561 0.373 14.916 7.778 0.27 106365. 0.6034
|
|
7.94 0.1211 0.2621 0.1128 0.0521 0.267 3.366 3.306 199.101 0.380 14.705 7.531 0.27 106490. 0.5801
|
|
9.92 0.1513 0.3172 0.1110 0.0529 0.271 3.422 3.253 202.416 0.387 14.469 7.289 0.28 106627. 0.5569
|
|
11.91 0.1816 0.3682 0.1089 0.0537 0.275 3.472 3.194 205.417 0.392 14.207 7.053 0.28 106775. 0.5340
|
|
13.89 0.2119 0.4156 0.1067 0.0544 0.279 3.516 3.129 208.005 0.397 13.916 6.822 0.28 106936. 0.5112
|
|
15.88 0.2421 0.4594 0.1042 0.0549 0.282 3.551 3.056 210.078 0.401 13.594 6.599 0.28 107110. 0.4887
|
|
17.86 0.2724 0.4999 0.1015 0.0553 0.284 3.576 2.976 211.529 0.404 13.239 6.382 0.28 107298. 0.4665
|
|
19.85 0.3027 0.5372 0.0985 0.0555 0.285 3.588 2.889 212.250 0.405 12.849 6.173 0.28 107498. 0.4445
|
|
21.83 0.3329 0.5716 0.0953 0.0555 0.284 3.586 2.793 212.136 0.405 12.423 5.972 0.28 107712. 0.4228
|
|
23.82 0.3632 0.6032 0.0917 0.0552 0.283 3.568 2.688 211.090 0.403 11.958 5.777 0.28 107940. 0.4013
|
|
25.80 0.3935 0.6322 0.0878 0.0547 0.280 3.533 2.575 209.022 0.399 11.455 5.588 0.28 108182. 0.3799
|
|
27.79 0.4238 0.6586 0.0837 0.0538 0.276 3.480 2.453 205.856 0.393 10.913 5.406 0.28 108437. 0.3587
|
|
29.77 0.4540 0.6824 0.0792 0.0527 0.270 3.407 2.323 201.517 0.385 10.331 5.228 0.28 108706. 0.3375
|
|
31.76 0.4843 0.7036 0.0745 0.0512 0.263 3.312 2.183 195.928 0.374 9.710 5.053 0.28 108989. 0.3163
|
|
33.74 0.5146 0.7221 0.0694 0.0495 0.254 3.197 2.035 189.094 0.361 9.052 4.881 0.28 109286. 0.2950
|
|
35.73 0.5448 0.7377 0.0641 0.0474 0.243 3.061 1.880 181.084 0.346 8.364 4.710 0.28 109596. 0.2736
|
|
37.71 0.5751 0.7500 0.0587 0.0450 0.231 2.907 1.720 171.966 0.328 7.650 4.536 0.28 109919. 0.2520
|
|
39.70 0.6054 0.7584 0.0530 0.0423 0.217 2.735 1.555 161.803 0.309 6.915 4.358 0.28 110256. 0.2302
|
|
41.68 0.6356 0.7623 0.0473 0.0394 0.202 2.547 1.385 150.649 0.288 6.162 4.171 0.28 110606. 0.2080
|
|
43.67 0.6659 0.7604 0.0414 0.0362 0.186 2.342 1.213 138.558 0.265 5.397 3.972 0.28 110970. 0.1853
|
|
45.65 0.6962 0.7509 0.0354 0.0328 0.168 2.123 1.039 125.588 0.240 4.621 3.752 0.28 111346. 0.1620
|
|
47.64 0.7264 0.7313 0.0294 0.0292 0.150 1.890 0.863 111.800 0.214 3.839 3.502 0.28 111735. 0.1378
|
|
49.62 0.7567 0.6968 0.0234 0.0254 0.130 1.644 0.687 97.269 0.186 3.055 3.203 0.28 112138. 0.1125
|
|
51.61 0.7870 0.6390 0.0174 0.0215 0.110 1.388 0.511 82.080 0.157 2.273 2.824 0.28 112554. 0.0855
|
|
53.59 0.8172 0.5415 0.0115 0.0174 0.089 1.121 0.337 66.338 0.127 1.499 2.305 0.28 112982. 0.0567
|
|
55.58 0.8475 0.3654 0.0057 0.0131 0.067 0.848 0.166 50.165 0.096 0.738 1.500 0.28 113424. 0.0259
|
|
57.56 0.8778 -0.0042 0.0000 0.0088 0.045 0.569 -0.001 33.687 0.064 -0.005 -0.016 0.29 113875. 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 0.1187 0.0479 0.424 4.456 5.010 316.301 0.503 22.286 7.185 0.33 127261. 0.6813
|
|
2.38 0.0303 0.0728 0.1175 0.0489 0.433 4.549 4.962 322.895 0.514 22.070 6.970 0.33 127373. 0.6577
|
|
4.77 0.0606 0.1411 0.1162 0.0499 0.442 4.641 4.907 329.486 0.524 21.828 6.756 0.33 127498. 0.6340
|
|
7.15 0.0908 0.2050 0.1148 0.0509 0.451 4.733 4.847 335.958 0.535 21.558 6.543 0.33 127634. 0.6103
|
|
9.53 0.1211 0.2647 0.1132 0.0518 0.459 4.820 4.779 342.187 0.545 21.256 6.334 0.33 127784. 0.5866
|
|
11.91 0.1514 0.3201 0.1114 0.0527 0.467 4.903 4.703 348.029 0.554 20.919 6.129 0.33 127948. 0.5631
|
|
14.30 0.1817 0.3716 0.1094 0.0535 0.474 4.977 4.619 353.328 0.562 20.543 5.929 0.33 128127. 0.5398
|
|
16.68 0.2119 0.4193 0.1072 0.0542 0.480 5.042 4.525 357.913 0.570 20.126 5.734 0.33 128321. 0.5167
|
|
19.06 0.2422 0.4634 0.1047 0.0547 0.485 5.094 4.421 361.603 0.576 19.664 5.545 0.33 128530. 0.4939
|
|
21.44 0.2725 0.5041 0.1020 0.0551 0.488 5.131 4.306 364.210 0.580 19.153 5.362 0.33 128755. 0.4714
|
|
23.83 0.3028 0.5417 0.0990 0.0553 0.490 5.149 4.180 365.546 0.582 18.591 5.186 0.33 128996. 0.4492
|
|
26.21 0.3330 0.5764 0.0957 0.0553 0.490 5.148 4.042 365.426 0.582 17.977 5.016 0.33 129253. 0.4272
|
|
28.59 0.3633 0.6082 0.0922 0.0550 0.488 5.123 3.891 363.678 0.579 17.307 4.853 0.33 129527. 0.4055
|
|
30.97 0.3936 0.6375 0.0883 0.0545 0.483 5.073 3.728 360.144 0.573 16.580 4.695 0.33 129817. 0.3840
|
|
33.36 0.4239 0.6641 0.0841 0.0537 0.476 4.997 3.552 354.690 0.565 15.797 4.542 0.33 130124. 0.3626
|
|
35.74 0.4541 0.6883 0.0796 0.0526 0.466 4.891 3.363 347.183 0.553 14.957 4.393 0.33 130447. 0.3413
|
|
38.12 0.4844 0.7099 0.0749 0.0511 0.453 4.754 3.161 337.487 0.537 14.058 4.248 0.33 130787. 0.3199
|
|
40.50 0.5147 0.7289 0.0698 0.0493 0.437 4.587 2.947 325.608 0.518 13.107 4.105 0.33 131144. 0.2985
|
|
42.89 0.5450 0.7450 0.0645 0.0472 0.418 4.390 2.723 311.660 0.496 12.111 3.962 0.33 131516. 0.2770
|
|
45.27 0.5753 0.7580 0.0590 0.0448 0.397 4.166 2.490 295.766 0.471 11.078 3.819 0.34 131905. 0.2553
|
|
47.65 0.6055 0.7673 0.0533 0.0421 0.373 3.917 2.251 278.028 0.442 10.014 3.673 0.34 132309. 0.2335
|
|
50.04 0.6358 0.7721 0.0475 0.0391 0.347 3.642 2.007 258.545 0.411 8.925 3.520 0.34 132730. 0.2112
|
|
52.42 0.6661 0.7715 0.0416 0.0359 0.318 3.344 1.757 237.410 0.378 7.817 3.357 0.34 133166. 0.1886
|
|
54.80 0.6964 0.7637 0.0356 0.0325 0.288 3.025 1.505 214.722 0.342 6.694 3.179 0.34 133618. 0.1652
|
|
57.18 0.7266 0.7460 0.0296 0.0288 0.256 2.685 1.250 190.592 0.303 5.562 2.976 0.34 134086. 0.1410
|
|
59.57 0.7569 0.7138 0.0236 0.0250 0.221 2.326 0.995 165.149 0.263 4.427 2.734 0.34 134569. 0.1155
|
|
61.95 0.7872 0.6588 0.0176 0.0210 0.186 1.952 0.741 138.544 0.221 3.296 2.426 0.34 135068. 0.0885
|
|
64.33 0.8175 0.5638 0.0116 0.0168 0.149 1.563 0.489 110.963 0.177 2.175 1.999 0.34 135583. 0.0592
|
|
66.71 0.8477 0.3876 0.0057 0.0125 0.111 1.164 0.241 82.622 0.131 1.074 1.325 0.34 136113. 0.0276
|
|
69.10 0.8780 -0.0008 0.0000 0.0081 0.072 0.757 0.000 53.743 0.086 -0.001 -0.003 0.34 136654. 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 0.1191 0.0477 0.671 6.043 6.845 500.483 0.683 30.445 6.203 0.38 148466. 0.6875
|
|
2.78 0.0303 0.0734 0.1180 0.0487 0.685 6.171 6.780 511.110 0.697 30.156 6.016 0.38 148597. 0.6637
|
|
5.56 0.0606 0.1422 0.1167 0.0497 0.700 6.300 6.707 521.741 0.712 29.831 5.830 0.38 148742. 0.6397
|
|
8.34 0.0909 0.2065 0.1153 0.0507 0.714 6.426 6.625 532.192 0.726 29.467 5.646 0.38 148902. 0.6157
|
|
11.12 0.1212 0.2665 0.1137 0.0517 0.727 6.548 6.533 542.261 0.740 29.060 5.465 0.38 149077. 0.5917
|
|
13.91 0.1515 0.3223 0.1119 0.0526 0.740 6.662 6.431 551.719 0.753 28.604 5.287 0.39 149269. 0.5680
|
|
16.69 0.1818 0.3740 0.1099 0.0534 0.751 6.766 6.316 560.312 0.764 28.096 5.113 0.39 149477. 0.5444
|
|
19.47 0.2120 0.4220 0.1077 0.0541 0.761 6.856 6.189 567.766 0.775 27.530 4.944 0.39 149704. 0.5211
|
|
22.25 0.2423 0.4663 0.1052 0.0547 0.769 6.928 6.048 573.787 0.783 26.902 4.781 0.39 149948. 0.4981
|
|
25.03 0.2726 0.5073 0.1025 0.0551 0.775 6.980 5.892 578.074 0.789 26.208 4.623 0.39 150211. 0.4754
|
|
27.81 0.3029 0.5451 0.0995 0.0553 0.778 7.007 5.720 580.320 0.792 25.443 4.471 0.39 150492. 0.4530
|
|
30.59 0.3332 0.5799 0.0963 0.0553 0.778 7.006 5.532 580.227 0.792 24.605 4.324 0.39 150793. 0.4309
|
|
33.37 0.3635 0.6120 0.0927 0.0550 0.774 6.973 5.326 577.515 0.788 23.691 4.183 0.39 151113. 0.4090
|
|
36.15 0.3938 0.6415 0.0888 0.0545 0.767 6.906 5.103 571.932 0.780 22.699 4.047 0.39 151452. 0.3873
|
|
38.94 0.4241 0.6684 0.0846 0.0537 0.755 6.801 4.863 563.255 0.768 21.629 3.916 0.39 151811. 0.3658
|
|
41.72 0.4544 0.6928 0.0801 0.0525 0.739 6.656 4.604 551.273 0.752 20.480 3.788 0.39 152189. 0.3444
|
|
44.50 0.4847 0.7148 0.0753 0.0511 0.718 6.469 4.328 535.767 0.731 19.251 3.664 0.39 152586. 0.3229
|
|
47.28 0.5150 0.7341 0.0702 0.0493 0.693 6.239 4.035 516.736 0.705 17.948 3.542 0.39 153003. 0.3014
|
|
50.06 0.5453 0.7507 0.0649 0.0471 0.663 5.969 3.728 494.365 0.674 16.584 3.421 0.39 153438. 0.2798
|
|
52.84 0.5755 0.7643 0.0593 0.0447 0.629 5.661 3.410 468.845 0.640 15.169 3.299 0.39 153892. 0.2581
|
|
55.62 0.6058 0.7743 0.0536 0.0420 0.591 5.317 3.083 440.344 0.601 13.712 3.175 0.39 154364. 0.2362
|
|
58.40 0.6361 0.7800 0.0478 0.0390 0.549 4.939 2.747 409.018 0.558 12.220 3.047 0.39 154856. 0.2139
|
|
61.19 0.6664 0.7805 0.0419 0.0357 0.503 4.528 2.406 375.017 0.512 10.701 2.910 0.39 155365. 0.1912
|
|
63.97 0.6967 0.7739 0.0358 0.0323 0.454 4.087 2.060 338.503 0.462 9.162 2.760 0.39 155893. 0.1678
|
|
66.75 0.7270 0.7578 0.0298 0.0286 0.402 3.618 1.711 299.652 0.409 7.610 2.590 0.39 156440. 0.1435
|
|
69.53 0.7573 0.7276 0.0237 0.0247 0.347 3.123 1.361 258.675 0.353 6.055 2.387 0.40 157004. 0.1180
|
|
72.31 0.7876 0.6747 0.0176 0.0206 0.289 2.606 1.013 215.818 0.294 4.505 2.128 0.40 157587. 0.0907
|
|
75.09 0.8179 0.5816 0.0116 0.0163 0.230 2.069 0.668 171.381 0.234 2.969 1.767 0.40 158188. 0.0611
|
|
77.87 0.8482 0.4042 0.0057 0.0120 0.169 1.518 0.328 125.720 0.172 1.460 1.184 0.40 158807. 0.0287
|
|
80.65 0.8785 -0.0060 -0.0001 0.0075 0.106 0.956 -0.003 79.187 0.108 -0.013 -0.017 0.40 159439. 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 0.1196 0.0477 1.001 7.887 8.978 746.531 0.891 39.933 5.455 0.44 169668. 0.6924
|
|
3.18 0.0303 0.0737 0.1185 0.0487 1.023 8.057 8.894 762.622 0.910 39.562 5.290 0.44 169818. 0.6684
|
|
6.36 0.0606 0.1428 0.1173 0.0497 1.044 8.228 8.800 778.739 0.930 39.145 5.126 0.44 169984. 0.6442
|
|
9.53 0.0909 0.2074 0.1158 0.0507 1.066 8.395 8.695 794.601 0.948 38.676 4.963 0.44 170166. 0.6200
|
|
12.71 0.1211 0.2676 0.1143 0.0517 1.086 8.557 8.577 809.902 0.967 38.150 4.803 0.44 170366. 0.5959
|
|
15.89 0.1514 0.3236 0.1125 0.0526 1.105 8.709 8.444 824.295 0.984 37.561 4.647 0.44 170586. 0.5720
|
|
19.07 0.1817 0.3756 0.1105 0.0535 1.123 8.847 8.296 837.397 1.000 36.902 4.494 0.44 170824. 0.5483
|
|
22.24 0.2120 0.4237 0.1083 0.0542 1.138 8.968 8.131 848.791 1.013 36.167 4.345 0.44 171083. 0.5249
|
|
25.42 0.2423 0.4682 0.1059 0.0548 1.151 9.065 7.948 858.032 1.024 35.351 4.201 0.44 171362. 0.5018
|
|
28.60 0.2726 0.5093 0.1032 0.0552 1.160 9.135 7.744 864.663 1.032 34.447 4.062 0.44 171663. 0.4789
|
|
31.78 0.3028 0.5473 0.1002 0.0554 1.164 9.173 7.520 868.216 1.036 33.450 3.929 0.44 171985. 0.4564
|
|
34.95 0.3331 0.5823 0.0969 0.0554 1.164 9.173 7.274 868.242 1.036 32.355 3.800 0.44 172329. 0.4342
|
|
38.13 0.3634 0.6145 0.0933 0.0552 1.159 9.132 7.005 864.312 1.032 31.160 3.676 0.44 172695. 0.4122
|
|
41.31 0.3937 0.6442 0.0894 0.0547 1.148 9.044 6.714 856.042 1.022 29.863 3.557 0.44 173083. 0.3905
|
|
44.49 0.4240 0.6713 0.0853 0.0538 1.131 8.908 6.399 843.095 1.006 28.461 3.442 0.44 173493. 0.3689
|
|
47.66 0.4543 0.6960 0.0807 0.0527 1.107 8.718 6.060 825.151 0.985 26.954 3.331 0.44 173925. 0.3474
|
|
50.84 0.4845 0.7183 0.0759 0.0512 1.075 8.472 5.697 801.876 0.957 25.341 3.223 0.44 174379. 0.3259
|
|
54.02 0.5148 0.7380 0.0708 0.0494 1.037 8.170 5.313 773.254 0.923 23.632 3.116 0.45 174855. 0.3043
|
|
57.20 0.5451 0.7551 0.0654 0.0472 0.992 7.814 4.910 739.560 0.883 21.840 3.011 0.45 175353. 0.2827
|
|
60.37 0.5754 0.7692 0.0598 0.0448 0.940 7.407 4.492 701.080 0.837 19.980 2.906 0.45 175872. 0.2609
|
|
63.55 0.6057 0.7799 0.0541 0.0420 0.882 6.953 4.061 658.071 0.786 18.064 2.799 0.45 176412. 0.2390
|
|
66.73 0.6360 0.7864 0.0482 0.0390 0.819 6.453 3.620 610.766 0.729 16.102 2.688 0.45 176973. 0.2167
|
|
69.91 0.6662 0.7879 0.0422 0.0357 0.750 5.910 3.171 559.395 0.668 14.103 2.571 0.45 177556. 0.1939
|
|
73.08 0.6965 0.7827 0.0362 0.0322 0.676 5.327 2.715 504.200 0.602 12.078 2.443 0.45 178159. 0.1705
|
|
76.26 0.7268 0.7681 0.0301 0.0284 0.597 4.706 2.256 445.451 0.532 10.037 2.298 0.45 178784. 0.1462
|
|
79.44 0.7571 0.7399 0.0239 0.0245 0.514 4.051 1.796 383.464 0.458 7.989 2.125 0.45 179429. 0.1206
|
|
82.62 0.7874 0.6895 0.0178 0.0203 0.427 3.366 1.337 318.616 0.380 5.948 1.904 0.45 180094. 0.0933
|
|
85.79 0.8177 0.5991 0.0118 0.0161 0.337 2.656 0.883 251.363 0.300 3.927 1.593 0.45 180781. 0.0634
|
|
88.97 0.8479 0.4233 0.0058 0.0116 0.244 1.926 0.436 182.248 0.218 1.939 1.085 0.46 181488. 0.0304
|
|
92.15 0.8782 0.0000 0.0000 0.0071 0.150 1.181 0.000 111.808 0.133 0.000 0.000 0.46 182210. 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 0.1202 0.0478 1.428 9.999 11.417 1064.714 1.130 50.781 4.864 0.49 190867. 0.6962
|
|
3.58 0.0303 0.0739 0.1191 0.0488 1.459 10.218 11.313 1087.992 1.154 50.322 4.716 0.49 191036. 0.6721
|
|
7.15 0.0606 0.1432 0.1179 0.0498 1.490 10.437 11.197 1111.332 1.179 49.803 4.570 0.49 191222. 0.6478
|
|
10.73 0.0909 0.2080 0.1165 0.0509 1.521 10.653 11.066 1134.331 1.204 49.220 4.425 0.49 191428. 0.6236
|
|
14.30 0.1211 0.2684 0.1149 0.0519 1.551 10.862 10.918 1156.545 1.227 48.564 4.282 0.49 191653. 0.5994
|
|
17.88 0.1514 0.3246 0.1132 0.0528 1.579 11.058 10.752 1177.473 1.249 47.827 4.142 0.50 191900. 0.5754
|
|
21.45 0.1817 0.3767 0.1112 0.0537 1.605 11.237 10.567 1196.555 1.270 47.000 4.005 0.50 192168. 0.5516
|
|
25.03 0.2120 0.4249 0.1091 0.0544 1.627 11.394 10.359 1213.188 1.287 46.077 3.873 0.50 192460. 0.5281
|
|
28.60 0.2423 0.4695 0.1066 0.0550 1.645 11.521 10.128 1226.727 1.302 45.049 3.745 0.50 192774. 0.5049
|
|
32.18 0.2726 0.5108 0.1039 0.0555 1.658 11.613 9.871 1236.507 1.312 43.908 3.621 0.50 193113. 0.4820
|
|
35.75 0.3029 0.5489 0.1009 0.0557 1.665 11.663 9.588 1241.849 1.318 42.648 3.502 0.50 193476. 0.4594
|
|
39.33 0.3331 0.5840 0.0977 0.0557 1.666 11.665 9.277 1242.096 1.318 41.262 3.387 0.50 193863. 0.4371
|
|
42.90 0.3634 0.6164 0.0941 0.0555 1.658 11.614 8.936 1236.627 1.312 39.747 3.278 0.50 194276. 0.4151
|
|
46.48 0.3937 0.6462 0.0902 0.0549 1.643 11.503 8.566 1224.886 1.300 38.100 3.172 0.50 194713. 0.3933
|
|
50.05 0.4240 0.6736 0.0860 0.0541 1.618 11.330 8.165 1206.379 1.280 36.318 3.070 0.50 195175. 0.3716
|
|
53.63 0.4543 0.6985 0.0814 0.0530 1.583 11.088 7.734 1180.647 1.253 34.402 2.971 0.50 195662. 0.3501
|
|
57.20 0.4846 0.7210 0.0766 0.0515 1.538 10.774 7.273 1147.205 1.217 32.349 2.875 0.50 196173. 0.3285
|
|
60.78 0.5149 0.7411 0.0714 0.0496 1.483 10.387 6.783 1106.014 1.174 30.170 2.782 0.50 196709. 0.3069
|
|
64.35 0.5451 0.7586 0.0660 0.0474 1.418 9.931 6.269 1057.460 1.122 27.886 2.689 0.50 197270. 0.2852
|
|
67.93 0.5754 0.7732 0.0604 0.0449 1.344 9.410 5.736 1001.962 1.063 25.514 2.597 0.50 197854. 0.2635
|
|
71.50 0.6057 0.7845 0.0546 0.0422 1.260 8.827 5.186 939.888 0.997 23.068 2.503 0.50 198462. 0.2415
|
|
75.08 0.6360 0.7918 0.0487 0.0391 1.169 8.185 4.623 871.578 0.925 20.563 2.406 0.50 199095. 0.2191
|
|
78.65 0.6663 0.7942 0.0426 0.0358 1.069 7.488 4.049 797.366 0.846 18.010 2.303 0.51 199750. 0.1963
|
|
82.23 0.6966 0.7900 0.0365 0.0322 0.962 6.739 3.467 717.602 0.761 15.423 2.192 0.51 200430. 0.1729
|
|
85.80 0.7269 0.7769 0.0303 0.0284 0.848 5.942 2.881 632.679 0.671 12.814 2.065 0.51 201132. 0.1485
|
|
89.38 0.7571 0.7503 0.0241 0.0244 0.728 5.100 2.293 543.055 0.576 10.198 1.915 0.51 201858. 0.1228
|
|
92.95 0.7874 0.7019 0.0180 0.0201 0.602 4.219 1.706 449.280 0.477 7.589 1.722 0.51 202608. 0.0953
|
|
96.53 0.8177 0.6135 0.0118 0.0158 0.472 3.306 1.125 352.015 0.373 5.005 1.450 0.51 203380. 0.0651
|
|
100.10 0.8480 0.4375 0.0058 0.0113 0.338 2.367 0.554 252.058 0.267 2.464 0.997 0.51 204176. 0.0314
|
|
103.68 0.8783 -0.0046 0.0000 0.0067 0.201 1.410 -0.003 150.178 0.159 -0.015 -0.010 0.51 204988. 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 0.1208 0.0479 1.966 12.392 14.170 1466.125 1.400 63.028 4.384 0.55 212063. 0.6991
|
|
3.97 0.0303 0.0740 0.1198 0.0490 2.010 12.667 14.046 1498.610 1.431 62.476 4.251 0.55 212250. 0.6750
|
|
7.94 0.0606 0.1434 0.1186 0.0501 2.053 12.942 13.905 1531.221 1.462 61.851 4.119 0.55 212457. 0.6507
|
|
11.91 0.0908 0.2083 0.1172 0.0511 2.097 13.214 13.747 1563.399 1.493 61.146 3.988 0.55 212685. 0.6264
|
|
15.89 0.1211 0.2688 0.1157 0.0521 2.138 13.477 13.568 1594.524 1.523 60.350 3.859 0.55 212936. 0.6023
|
|
19.86 0.1514 0.3250 0.1140 0.0531 2.178 13.726 13.366 1623.894 1.551 59.454 3.733 0.55 213210. 0.5782
|
|
23.83 0.1817 0.3772 0.1120 0.0540 2.214 13.952 13.140 1650.727 1.576 58.446 3.610 0.55 213509. 0.5544
|
|
27.80 0.2120 0.4255 0.1099 0.0547 2.245 14.151 12.886 1674.174 1.599 57.316 3.491 0.55 213832. 0.5309
|
|
31.77 0.2422 0.4702 0.1075 0.0554 2.271 14.312 12.602 1693.334 1.617 56.055 3.376 0.55 214182. 0.5077
|
|
35.74 0.2725 0.5115 0.1048 0.0558 2.289 14.430 12.287 1707.268 1.630 54.653 3.264 0.55 214559. 0.4848
|
|
39.71 0.3028 0.5497 0.1018 0.0561 2.300 14.496 11.938 1715.031 1.638 53.101 3.157 0.55 214963. 0.4621
|
|
43.69 0.3331 0.5850 0.0985 0.0561 2.301 14.502 11.554 1715.699 1.638 51.391 3.054 0.55 215394. 0.4398
|
|
47.66 0.3634 0.6175 0.0949 0.0559 2.291 14.440 11.133 1708.400 1.631 49.518 2.956 0.55 215852. 0.4178
|
|
51.63 0.3936 0.6475 0.0910 0.0553 2.269 14.304 10.674 1692.349 1.616 47.479 2.861 0.55 216339. 0.3960
|
|
55.60 0.4239 0.6751 0.0868 0.0545 2.235 14.089 10.178 1666.862 1.592 45.270 2.769 0.55 216852. 0.3743
|
|
59.57 0.4542 0.7002 0.0822 0.0533 2.188 13.788 9.643 1631.297 1.558 42.892 2.681 0.56 217394. 0.3527
|
|
63.54 0.4845 0.7230 0.0773 0.0518 2.125 13.397 9.070 1584.983 1.514 40.343 2.595 0.56 217963. 0.3311
|
|
67.52 0.5148 0.7435 0.0721 0.0500 2.049 12.914 8.461 1527.825 1.459 37.634 2.512 0.56 218559. 0.3095
|
|
71.49 0.5450 0.7613 0.0667 0.0477 1.958 12.343 7.822 1460.360 1.395 34.791 2.429 0.56 219182. 0.2878
|
|
75.46 0.5753 0.7764 0.0610 0.0452 1.855 11.691 7.157 1383.171 1.321 31.837 2.347 0.56 219832. 0.2660
|
|
79.43 0.6056 0.7883 0.0552 0.0424 1.739 10.961 6.472 1296.773 1.238 28.789 2.264 0.56 220508. 0.2440
|
|
83.40 0.6359 0.7963 0.0492 0.0393 1.611 10.157 5.770 1201.648 1.147 25.665 2.178 0.56 221211. 0.2216
|
|
87.37 0.6662 0.7996 0.0431 0.0359 1.473 9.283 5.054 1098.260 1.049 22.482 2.087 0.56 221940. 0.1988
|
|
91.34 0.6964 0.7965 0.0369 0.0323 1.324 8.343 4.329 987.101 0.943 19.254 1.989 0.56 222695. 0.1753
|
|
95.32 0.7267 0.7847 0.0307 0.0284 1.165 7.343 3.597 868.718 0.830 15.998 1.878 0.56 223476. 0.1509
|
|
99.29 0.7570 0.7597 0.0244 0.0243 0.997 6.286 2.862 743.755 0.710 12.731 1.745 0.57 224282. 0.1251
|
|
103.26 0.7873 0.7133 0.0182 0.0200 0.822 5.181 2.130 612.979 0.585 9.473 1.576 0.57 225115. 0.0974
|
|
107.23 0.8176 0.6271 0.0120 0.0156 0.640 4.034 1.404 477.323 0.456 6.245 1.334 0.57 225973. 0.0670
|
|
111.20 0.8478 0.4518 0.0059 0.0110 0.453 2.856 0.691 337.904 0.323 3.071 0.927 0.57 226857. 0.0326
|
|
115.17 0.8781 -0.0069 -0.0001 0.0064 0.263 1.655 -0.006 195.802 0.187 -0.026 -0.014 0.57 227758. 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 0.1215 0.0482 2.632 15.083 17.248 1962.937 1.704 76.718 3.985 0.60 233254. 0.7012
|
|
4.37 0.0303 0.0740 0.1205 0.0493 2.691 15.421 17.102 2006.997 1.742 76.072 3.865 0.60 233459. 0.6772
|
|
8.73 0.0605 0.1434 0.1194 0.0504 2.751 15.762 16.938 2051.299 1.781 75.339 3.745 0.60 233687. 0.6530
|
|
13.10 0.0908 0.2083 0.1180 0.0515 2.810 16.098 16.751 2095.078 1.819 74.508 3.626 0.60 233938. 0.6288
|
|
17.47 0.1211 0.2688 0.1166 0.0525 2.866 16.424 16.539 2137.496 1.856 73.566 3.510 0.60 234214. 0.6047
|
|
21.84 0.1513 0.3250 0.1149 0.0535 2.920 16.732 16.300 2177.596 1.890 72.501 3.395 0.61 234515. 0.5807
|
|
26.20 0.1816 0.3772 0.1130 0.0544 2.969 17.014 16.030 2214.313 1.922 71.300 3.283 0.61 234844. 0.5569
|
|
30.57 0.2119 0.4255 0.1108 0.0552 3.013 17.262 15.726 2246.487 1.950 69.950 3.175 0.61 235201. 0.5334
|
|
34.94 0.2422 0.4703 0.1084 0.0558 3.048 17.465 15.386 2272.887 1.973 68.437 3.070 0.61 235586. 0.5102
|
|
39.30 0.2724 0.5117 0.1058 0.0563 3.074 17.613 15.007 2292.231 1.990 66.751 2.969 0.61 236000. 0.4873
|
|
43.67 0.3027 0.5499 0.1028 0.0566 3.089 17.698 14.586 2303.232 1.999 64.879 2.872 0.61 236445. 0.4647
|
|
48.04 0.3330 0.5853 0.0995 0.0566 3.091 17.708 14.122 2304.620 2.001 62.813 2.779 0.61 236920. 0.4425
|
|
52.40 0.3632 0.6180 0.0959 0.0564 3.078 17.636 13.612 2295.212 1.993 60.545 2.690 0.61 237425. 0.4204
|
|
56.77 0.3935 0.6481 0.0920 0.0559 3.049 17.473 13.055 2273.936 1.974 58.071 2.604 0.61 237960. 0.3986
|
|
61.14 0.4238 0.6759 0.0878 0.0550 3.004 17.211 12.452 2239.857 1.944 55.387 2.522 0.61 238526. 0.3770
|
|
65.51 0.4540 0.7013 0.0832 0.0538 2.940 16.844 11.802 2192.116 1.903 52.494 2.442 0.61 239122. 0.3554
|
|
69.87 0.4843 0.7243 0.0782 0.0523 2.856 16.365 11.104 2129.802 1.849 49.389 2.365 0.61 239749. 0.3338
|
|
74.24 0.5146 0.7451 0.0730 0.0504 2.753 15.773 10.361 2052.743 1.782 46.085 2.289 0.61 240405. 0.3122
|
|
78.61 0.5448 0.7634 0.0675 0.0482 2.631 15.073 9.581 1961.649 1.703 42.614 2.215 0.61 241091. 0.2905
|
|
82.97 0.5751 0.7790 0.0618 0.0456 2.491 14.271 8.769 1857.313 1.612 39.004 2.141 0.61 241806. 0.2686
|
|
87.34 0.6054 0.7914 0.0559 0.0428 2.334 13.373 7.931 1740.451 1.511 35.277 2.067 0.62 242551. 0.2466
|
|
91.71 0.6357 0.8001 0.0498 0.0396 2.161 12.384 7.072 1611.710 1.399 31.455 1.990 0.62 243324. 0.2242
|
|
96.08 0.6659 0.8042 0.0437 0.0362 1.974 11.309 6.196 1471.731 1.278 27.558 1.909 0.62 244126. 0.2013
|
|
100.44 0.6962 0.8022 0.0374 0.0325 1.772 10.152 5.307 1321.177 1.147 23.604 1.822 0.62 244956. 0.1778
|
|
104.81 0.7265 0.7917 0.0311 0.0285 1.557 8.919 4.410 1160.799 1.008 19.614 1.723 0.62 245815. 0.1533
|
|
109.18 0.7567 0.7684 0.0247 0.0244 1.330 7.618 3.509 991.466 0.861 15.609 1.605 0.62 246702. 0.1274
|
|
113.54 0.7870 0.7240 0.0184 0.0200 1.092 6.256 2.611 814.228 0.707 11.614 1.454 0.62 247618. 0.0996
|
|
117.91 0.8173 0.6400 0.0121 0.0155 0.845 4.844 1.721 630.352 0.547 7.654 1.238 0.62 248561. 0.0688
|
|
122.28 0.8475 0.4657 0.0060 0.0108 0.592 3.391 0.845 441.371 0.383 3.761 0.869 0.63 249533. 0.0338
|
|
126.65 0.8778 -0.0092 -0.0001 0.0061 0.334 1.911 -0.009 248.748 0.216 -0.040 -0.017 0.63 250523. 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 0.1223 0.0486 3.446 18.098 20.661 2569.425 2.045 91.901 3.647 0.66 254440. 0.7023
|
|
4.76 0.0302 0.0738 0.1214 0.0497 3.524 18.507 20.496 2627.583 2.091 91.165 3.538 0.66 254664. 0.6786
|
|
9.52 0.0605 0.1431 0.1202 0.0508 3.602 18.921 20.307 2686.224 2.138 90.326 3.429 0.66 254912. 0.6546
|
|
14.28 0.0907 0.2078 0.1190 0.0519 3.680 19.330 20.092 2744.341 2.184 89.370 3.321 0.66 255185. 0.6306
|
|
19.03 0.1209 0.2682 0.1175 0.0530 3.756 19.728 19.848 2800.809 2.229 88.282 3.214 0.66 255485. 0.6066
|
|
23.79 0.1512 0.3244 0.1159 0.0540 3.828 20.105 19.570 2854.341 2.271 87.046 3.110 0.66 255814. 0.5828
|
|
28.55 0.1814 0.3765 0.1140 0.0549 3.894 20.451 19.255 2903.503 2.311 85.646 3.008 0.66 256172. 0.5592
|
|
33.31 0.2116 0.4248 0.1119 0.0558 3.952 20.755 18.900 2946.734 2.345 84.065 2.909 0.66 256561. 0.5358
|
|
38.07 0.2419 0.4696 0.1095 0.0564 3.999 21.007 18.500 2982.384 2.373 82.288 2.814 0.66 256981. 0.5127
|
|
42.83 0.2721 0.5110 0.1069 0.0569 4.035 21.192 18.053 3008.751 2.394 80.300 2.722 0.66 257433. 0.4899
|
|
47.59 0.3023 0.5493 0.1040 0.0572 4.055 21.300 17.555 3024.107 2.407 78.087 2.633 0.66 257918. 0.4674
|
|
52.35 0.3326 0.5848 0.1007 0.0573 4.059 21.319 17.005 3026.765 2.409 75.636 2.548 0.66 258436. 0.4452
|
|
57.10 0.3628 0.6176 0.0971 0.0570 4.043 21.237 16.398 3015.143 2.399 72.940 2.467 0.66 258987. 0.4232
|
|
61.86 0.3931 0.6478 0.0932 0.0565 4.007 21.045 15.736 2987.807 2.378 69.992 2.389 0.66 259571. 0.4014
|
|
66.62 0.4233 0.6758 0.0889 0.0557 3.947 20.733 15.016 2943.519 2.342 66.790 2.314 0.67 260189. 0.3798
|
|
71.38 0.4535 0.7014 0.0843 0.0545 3.864 20.294 14.238 2881.153 2.293 63.331 2.241 0.67 260839. 0.3583
|
|
76.14 0.4838 0.7248 0.0794 0.0530 3.754 19.718 13.402 2799.514 2.228 59.613 2.171 0.67 261522. 0.3368
|
|
80.90 0.5140 0.7459 0.0741 0.0511 3.618 19.005 12.512 2698.286 2.147 55.653 2.103 0.67 262238. 0.3152
|
|
85.66 0.5442 0.7646 0.0685 0.0488 3.458 18.161 11.575 2578.379 2.052 51.485 2.036 0.67 262986. 0.2935
|
|
90.41 0.5745 0.7807 0.0628 0.0462 3.273 17.192 10.599 2440.855 1.942 47.145 1.970 0.67 263766. 0.2717
|
|
95.17 0.6047 0.7938 0.0568 0.0433 3.066 16.106 9.591 2286.669 1.820 42.661 1.902 0.67 264577. 0.2496
|
|
99.93 0.6349 0.8032 0.0507 0.0400 2.839 14.909 8.556 2116.697 1.684 38.058 1.833 0.67 265420. 0.2272
|
|
104.69 0.6652 0.8082 0.0444 0.0366 2.591 13.607 7.500 1931.786 1.537 33.361 1.761 0.67 266294. 0.2043
|
|
109.45 0.6954 0.8074 0.0381 0.0328 2.324 12.205 6.428 1732.822 1.379 28.594 1.683 0.68 267199. 0.1807
|
|
114.21 0.7256 0.7983 0.0317 0.0288 2.039 10.712 5.346 1520.794 1.210 23.779 1.594 0.68 268134. 0.1562
|
|
118.97 0.7559 0.7769 0.0252 0.0245 1.739 9.134 4.259 1296.855 1.032 18.944 1.490 0.68 269101. 0.1302
|
|
123.73 0.7861 0.7350 0.0188 0.0201 1.425 7.483 3.174 1062.396 0.845 14.117 1.355 0.68 270098. 0.1023
|
|
128.48 0.8163 0.6543 0.0124 0.0155 1.098 5.770 2.098 819.135 0.652 9.331 1.162 0.68 271126. 0.0713
|
|
133.24 0.8466 0.4838 0.0062 0.0108 0.763 4.009 1.039 569.187 0.453 4.623 0.828 0.68 272183. 0.0358
|
|
138.00 0.8768 0.0050 0.0000 0.0060 0.422 2.216 0.006 314.678 0.250 0.026 0.008 0.68 273263. 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 0.1232 0.0494 4.453 21.588 24.421 3320.353 2.439 108.623 3.336 0.71 275621. 0.6984
|
|
5.15 0.0302 0.0732 0.1223 0.0505 4.550 22.062 24.237 3393.248 2.493 107.806 3.240 0.71 275862. 0.6757
|
|
10.30 0.0604 0.1420 0.1212 0.0516 4.649 22.541 24.026 3466.937 2.547 106.870 3.143 0.71 276130. 0.6527
|
|
15.46 0.0906 0.2065 0.1200 0.0527 4.747 23.017 23.785 3540.180 2.600 105.796 3.047 0.71 276426. 0.6296
|
|
20.61 0.1209 0.2667 0.1186 0.0537 4.843 23.482 23.509 3611.598 2.653 104.567 2.952 0.71 276751. 0.6064
|
|
25.76 0.1511 0.3229 0.1170 0.0548 4.934 23.924 23.193 3679.588 2.703 103.162 2.859 0.72 277107. 0.5833
|
|
30.91 0.1813 0.3750 0.1152 0.0557 5.019 24.332 22.833 3742.350 2.749 101.562 2.767 0.72 277495. 0.5602
|
|
36.06 0.2115 0.4234 0.1131 0.0565 5.093 24.693 22.425 3797.890 2.790 99.745 2.678 0.72 277916. 0.5373
|
|
41.22 0.2417 0.4683 0.1108 0.0572 5.155 24.993 21.963 3844.059 2.824 97.693 2.592 0.72 278372. 0.5145
|
|
46.37 0.2719 0.5098 0.1082 0.0577 5.201 25.218 21.445 3878.586 2.849 95.386 2.508 0.72 278862. 0.4920
|
|
51.52 0.3022 0.5482 0.1053 0.0580 5.229 25.351 20.865 3899.152 2.864 92.808 2.427 0.72 279388. 0.4697
|
|
56.67 0.3324 0.5838 0.1020 0.0581 5.235 25.379 20.221 3903.454 2.867 89.943 2.350 0.72 279949. 0.4476
|
|
61.82 0.3626 0.6167 0.0984 0.0579 5.216 25.287 19.510 3889.311 2.857 86.781 2.275 0.72 280547. 0.4258
|
|
66.98 0.3928 0.6471 0.0945 0.0574 5.169 25.063 18.731 3854.749 2.832 83.315 2.204 0.72 281180. 0.4041
|
|
72.13 0.4230 0.6753 0.0902 0.0565 5.093 24.694 17.882 3798.101 2.790 79.540 2.135 0.72 281850. 0.3826
|
|
77.28 0.4532 0.7011 0.0856 0.0553 4.986 24.173 16.964 3717.918 2.731 75.456 2.070 0.72 282555. 0.3611
|
|
82.43 0.4834 0.7248 0.0806 0.0538 4.845 23.489 15.975 3612.665 2.654 71.058 2.006 0.72 283296. 0.3396
|
|
87.58 0.5137 0.7463 0.0753 0.0518 4.669 22.638 14.920 3481.830 2.558 66.364 1.944 0.72 284073. 0.3180
|
|
92.74 0.5439 0.7654 0.0697 0.0495 4.461 21.628 13.808 3326.549 2.444 61.418 1.883 0.72 284884. 0.2964
|
|
97.89 0.5741 0.7820 0.0638 0.0469 4.222 20.469 12.648 3148.231 2.313 56.260 1.822 0.73 285729. 0.2746
|
|
103.04 0.6043 0.7957 0.0578 0.0439 3.954 19.168 11.449 2948.139 2.166 50.925 1.761 0.73 286608. 0.2525
|
|
108.19 0.6345 0.8059 0.0515 0.0406 3.658 17.733 10.217 2727.426 2.003 45.444 1.699 0.73 287521. 0.2301
|
|
113.34 0.6647 0.8117 0.0452 0.0370 3.335 16.171 8.958 2487.230 1.827 39.846 1.634 0.73 288468. 0.2071
|
|
118.49 0.6950 0.8119 0.0387 0.0332 2.989 14.491 7.680 2228.773 1.637 34.159 1.563 0.73 289448. 0.1835
|
|
123.65 0.7252 0.8039 0.0322 0.0291 2.620 12.701 6.388 1953.467 1.435 28.412 1.483 0.73 290462. 0.1588
|
|
128.80 0.7554 0.7838 0.0257 0.0247 2.230 10.812 5.089 1663.003 1.222 22.637 1.388 0.73 291508. 0.1327
|
|
133.95 0.7856 0.7430 0.0191 0.0202 1.823 8.839 3.792 1359.466 0.999 16.867 1.265 0.74 292588. 0.1044
|
|
139.10 0.8158 0.6627 0.0126 0.0156 1.402 6.797 2.505 1045.454 0.768 11.142 1.087 0.74 293700. 0.0729
|
|
144.25 0.8460 0.4903 0.0062 0.0108 0.971 4.708 1.238 724.144 0.532 5.506 0.775 0.74 294845. 0.0365
|
|
149.41 0.8763 -0.0004 0.0000 0.0059 0.535 2.593 -0.001 398.746 0.293 -0.002 -0.001 0.74 296012. 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 0.1241 0.0513 5.778 26.013 28.532 4308.750 2.939 126.909 3.003 0.77 296795. 0.6796
|
|
5.54 0.0302 0.0710 0.1233 0.0524 5.894 26.533 28.334 4394.806 2.998 126.029 2.924 0.77 297054. 0.6594
|
|
11.08 0.0604 0.1382 0.1223 0.0534 6.010 27.057 28.105 4481.547 3.057 125.013 2.844 0.77 297341. 0.6389
|
|
16.62 0.0905 0.2015 0.1211 0.0544 6.125 27.575 27.842 4567.433 3.115 123.840 2.765 0.77 297659. 0.6180
|
|
22.16 0.1207 0.2610 0.1198 0.0554 6.237 28.078 27.537 4650.795 3.172 122.486 2.686 0.77 298008. 0.5970
|
|
27.71 0.1509 0.3167 0.1183 0.0564 6.343 28.555 27.187 4729.698 3.226 120.928 2.607 0.77 298391. 0.5759
|
|
33.25 0.1811 0.3688 0.1165 0.0572 6.440 28.991 26.785 4801.990 3.275 119.140 2.530 0.77 298808. 0.5547
|
|
38.79 0.2112 0.4173 0.1145 0.0580 6.524 29.373 26.326 4865.316 3.319 117.098 2.454 0.77 299261. 0.5335
|
|
44.33 0.2414 0.4626 0.1123 0.0586 6.594 29.686 25.804 4917.113 3.354 114.775 2.380 0.77 299751. 0.5122
|
|
49.87 0.2716 0.5046 0.1097 0.0590 6.644 29.913 25.213 4954.688 3.380 112.150 2.308 0.77 300279. 0.4910
|
|
55.41 0.3018 0.5437 0.1068 0.0593 6.672 30.037 24.550 4975.261 3.394 109.199 2.238 0.77 300845. 0.4698
|
|
60.95 0.3319 0.5799 0.1036 0.0593 6.673 30.042 23.810 4976.058 3.394 105.905 2.170 0.77 301450. 0.4486
|
|
66.49 0.3621 0.6135 0.1000 0.0590 6.644 29.911 22.989 4954.403 3.379 102.254 2.105 0.77 302094. 0.4275
|
|
72.03 0.3923 0.6446 0.0961 0.0585 6.582 29.630 22.085 4907.829 3.348 98.236 2.041 0.78 302777. 0.4064
|
|
77.58 0.4225 0.6732 0.0918 0.0576 6.483 29.185 21.099 4834.120 3.297 93.847 1.980 0.78 303498. 0.3852
|
|
83.12 0.4526 0.6996 0.0871 0.0564 6.345 28.564 20.028 4731.243 3.227 89.086 1.920 0.78 304258. 0.3640
|
|
88.66 0.4828 0.7238 0.0821 0.0548 6.165 27.754 18.873 4597.038 3.136 83.948 1.862 0.78 305056. 0.3427
|
|
94.20 0.5130 0.7457 0.0767 0.0528 5.941 26.748 17.638 4430.426 3.022 78.452 1.806 0.78 305892. 0.3213
|
|
99.74 0.5432 0.7653 0.0711 0.0504 5.676 25.553 16.333 4232.585 2.887 72.648 1.750 0.78 306766. 0.2997
|
|
105.28 0.5734 0.7824 0.0651 0.0477 5.371 24.181 14.970 4005.244 2.732 66.585 1.695 0.78 307676. 0.2779
|
|
110.82 0.6035 0.7967 0.0590 0.0447 5.029 22.641 13.558 3750.130 2.558 60.305 1.640 0.78 308623. 0.2558
|
|
116.36 0.6337 0.8074 0.0527 0.0413 4.652 20.943 12.105 3468.950 2.366 53.845 1.583 0.78 309605. 0.2333
|
|
121.90 0.6639 0.8138 0.0462 0.0377 4.242 19.099 10.620 3163.483 2.158 47.240 1.523 0.79 310624. 0.2102
|
|
127.45 0.6941 0.8141 0.0396 0.0338 3.803 17.120 9.110 2835.650 1.934 40.521 1.457 0.79 311678. 0.1863
|
|
132.99 0.7242 0.8059 0.0330 0.0296 3.336 15.019 7.582 2487.731 1.697 33.724 1.382 0.79 312768. 0.1613
|
|
138.53 0.7544 0.7844 0.0263 0.0253 2.846 12.814 6.044 2122.481 1.448 26.885 1.292 0.79 313893. 0.1345
|
|
144.07 0.7846 0.7405 0.0196 0.0208 2.338 10.525 4.506 1743.251 1.189 20.043 1.172 0.79 315054. 0.1054
|
|
149.61 0.8148 0.6541 0.0130 0.0161 1.816 8.175 2.977 1354.115 0.924 13.244 0.997 0.79 316250. 0.0729
|
|
155.15 0.8449 0.4725 0.0064 0.0114 1.287 5.795 1.470 959.879 0.655 6.539 0.695 0.80 317480. 0.0357
|
|
160.69 0.8751 -0.0029 0.0000 0.0067 0.758 3.413 -0.005 565.284 0.386 -0.023 -0.004 0.80 318736. 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 0.1250 0.0554 7.663 32.197 32.988 5714.015 3.638 146.730 2.619 0.82 317960. 0.6371
|
|
5.93 0.0302 0.0666 0.1242 0.0563 7.792 32.742 32.781 5810.629 3.699 145.811 2.559 0.82 318237. 0.6207
|
|
11.87 0.0603 0.1300 0.1233 0.0572 7.921 33.284 32.541 5906.893 3.760 144.742 2.499 0.82 318544. 0.6039
|
|
17.80 0.0905 0.1903 0.1223 0.0581 8.047 33.814 32.261 6000.814 3.820 143.497 2.438 0.82 318883. 0.5868
|
|
23.73 0.1206 0.2474 0.1210 0.0590 8.167 34.317 31.935 6090.216 3.877 142.048 2.378 0.82 319256. 0.5694
|
|
29.66 0.1508 0.3016 0.1196 0.0598 8.278 34.782 31.557 6172.678 3.930 140.364 2.319 0.83 319666. 0.5518
|
|
35.60 0.1809 0.3527 0.1179 0.0605 8.375 35.193 31.118 6245.587 3.976 138.413 2.260 0.83 320112. 0.5341
|
|
41.53 0.2111 0.4009 0.1160 0.0611 8.457 35.534 30.613 6306.120 4.015 136.165 2.202 0.83 320598. 0.5161
|
|
47.46 0.2413 0.4463 0.1138 0.0615 8.517 35.789 30.033 6351.370 4.043 133.588 2.145 0.83 321123. 0.4979
|
|
53.40 0.2714 0.4890 0.1113 0.0618 8.553 35.941 29.373 6378.338 4.061 130.653 2.089 0.83 321689. 0.4796
|
|
59.33 0.3016 0.5290 0.1085 0.0618 8.561 35.972 28.627 6383.937 4.064 127.333 2.034 0.83 322296. 0.4610
|
|
65.26 0.3317 0.5665 0.1053 0.0617 8.536 35.866 27.788 6365.069 4.052 123.603 1.980 0.83 322945. 0.4422
|
|
71.20 0.3619 0.6016 0.1018 0.0612 8.474 35.606 26.854 6318.833 4.023 119.445 1.928 0.83 323636. 0.4232
|
|
77.13 0.3920 0.6343 0.0979 0.0605 8.371 35.176 25.820 6242.558 3.974 114.848 1.876 0.83 324369. 0.4039
|
|
83.06 0.4222 0.6647 0.0936 0.0594 8.226 34.563 24.686 6133.866 3.905 109.804 1.825 0.83 325144. 0.3842
|
|
88.99 0.4523 0.6928 0.0889 0.0580 8.033 33.756 23.452 5990.531 3.814 104.314 1.776 0.83 325959. 0.3643
|
|
94.93 0.4825 0.7185 0.0838 0.0563 7.791 32.739 22.116 5810.119 3.699 98.372 1.726 0.83 326816. 0.3440
|
|
100.86 0.5127 0.7419 0.0784 0.0542 7.498 31.505 20.683 5591.167 3.559 91.997 1.678 0.83 327713. 0.3233
|
|
106.79 0.5428 0.7629 0.0726 0.0517 7.154 30.062 19.166 5334.964 3.396 85.248 1.629 0.84 328650. 0.3022
|
|
112.73 0.5730 0.7809 0.0666 0.0489 6.766 28.429 17.577 5045.255 3.212 78.182 1.580 0.84 329627. 0.2807
|
|
118.66 0.6031 0.7954 0.0604 0.0458 6.336 26.625 15.928 4725.006 3.008 70.847 1.529 0.84 330642. 0.2585
|
|
124.59 0.6333 0.8057 0.0539 0.0424 5.867 24.654 14.229 4375.229 2.785 63.289 1.475 0.84 331696. 0.2357
|
|
130.52 0.6634 0.8108 0.0473 0.0387 5.361 22.527 12.489 3997.835 2.545 55.552 1.417 0.84 332788. 0.2121
|
|
136.46 0.6936 0.8088 0.0406 0.0348 4.822 20.262 10.718 3595.793 2.289 47.673 1.352 0.84 333918. 0.1875
|
|
142.39 0.7238 0.7963 0.0338 0.0307 4.255 17.879 8.924 3172.883 2.020 39.693 1.276 0.85 335086. 0.1614
|
|
148.32 0.7539 0.7677 0.0270 0.0265 3.666 15.405 7.116 2733.845 1.740 31.654 1.181 0.85 336291. 0.1334
|
|
154.26 0.7841 0.7127 0.0201 0.0221 3.063 12.869 5.306 2283.844 1.454 23.603 1.054 0.85 337534. 0.1028
|
|
160.19 0.8142 0.6105 0.0133 0.0177 2.453 10.306 3.506 1829.029 1.164 15.594 0.869 0.85 338814. 0.0690
|
|
166.12 0.8444 0.4150 0.0066 0.0133 1.846 7.756 1.729 1376.405 0.876 7.692 0.570 0.85 340131. 0.0318
|
|
172.06 0.8745 -0.0037 0.0000 0.0090 1.250 5.252 -0.010 932.016 0.593 -0.044 -0.005 0.86 341477. 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 0.1255 0.0618 10.375 40.871 37.673 7736.887 4.618 167.572 2.209 0.88 339133. 0.5743
|
|
6.34 0.0302 0.0602 0.1248 0.0627 10.525 41.462 37.468 7848.773 4.684 166.659 2.165 0.88 339426. 0.5615
|
|
12.69 0.0605 0.1180 0.1240 0.0635 10.672 42.040 37.227 7958.172 4.750 165.587 2.122 0.88 339752. 0.5484
|
|
19.03 0.0907 0.1734 0.1231 0.0644 10.811 42.589 36.943 8062.113 4.812 164.322 2.078 0.88 340112. 0.5352
|
|
25.37 0.1209 0.2264 0.1219 0.0651 10.939 43.091 36.607 8157.064 4.868 162.829 2.036 0.88 340509. 0.5218
|
|
31.71 0.1511 0.2772 0.1206 0.0658 11.049 43.527 36.212 8239.559 4.918 161.070 1.993 0.88 340945. 0.5082
|
|
38.06 0.1814 0.3257 0.1191 0.0663 11.139 43.879 35.748 8306.271 4.957 159.006 1.952 0.88 341422. 0.4944
|
|
44.40 0.2116 0.3721 0.1173 0.0667 11.202 44.129 35.206 8353.509 4.986 156.597 1.912 0.88 341940. 0.4805
|
|
50.74 0.2418 0.4165 0.1152 0.0669 11.235 44.257 34.578 8377.717 5.000 153.804 1.872 0.88 342502. 0.4664
|
|
57.09 0.2720 0.4588 0.1128 0.0669 11.232 44.245 33.855 8375.526 4.999 150.589 1.833 0.88 343108. 0.4519
|
|
63.43 0.3023 0.4993 0.1100 0.0666 11.189 44.077 33.030 8343.800 4.980 146.917 1.796 0.88 343760. 0.4372
|
|
69.77 0.3325 0.5378 0.1069 0.0661 11.103 43.738 32.095 8279.630 4.942 142.759 1.758 0.88 344456. 0.4220
|
|
76.12 0.3627 0.5744 0.1034 0.0653 10.970 43.214 31.046 8180.386 4.882 138.092 1.721 0.88 345197. 0.4063
|
|
82.46 0.3929 0.6090 0.0995 0.0642 10.787 42.492 29.878 8043.708 4.801 132.899 1.685 0.89 345984. 0.3901
|
|
88.80 0.4232 0.6417 0.0952 0.0628 10.551 41.561 28.591 7867.545 4.696 127.171 1.648 0.89 346816. 0.3734
|
|
95.14 0.4534 0.6722 0.0905 0.0611 10.259 40.412 27.182 7649.921 4.566 120.906 1.612 0.89 347692. 0.3560
|
|
101.49 0.4836 0.7006 0.0854 0.0590 9.908 39.029 25.651 7388.207 4.410 114.095 1.575 0.89 348612. 0.3379
|
|
107.83 0.5138 0.7268 0.0799 0.0565 9.496 37.408 24.002 7081.353 4.226 106.761 1.537 0.89 349576. 0.3191
|
|
114.17 0.5441 0.7504 0.0741 0.0537 9.027 35.561 22.251 6731.574 4.018 98.974 1.499 0.89 350582. 0.2996
|
|
120.52 0.5743 0.7711 0.0680 0.0506 8.508 33.515 20.414 6344.363 3.787 90.804 1.459 0.89 351631. 0.2794
|
|
126.86 0.6045 0.7870 0.0616 0.0473 7.954 31.332 18.504 5931.178 3.540 82.304 1.415 0.90 352721. 0.2579
|
|
133.20 0.6347 0.7965 0.0551 0.0439 7.372 29.039 16.530 5497.020 3.281 73.527 1.364 0.90 353852. 0.2349
|
|
139.55 0.6650 0.7973 0.0483 0.0403 6.770 26.667 14.505 5048.069 3.013 64.516 1.303 0.90 355024. 0.2103
|
|
145.89 0.6952 0.7884 0.0414 0.0365 6.138 24.180 12.440 4577.167 2.732 55.335 1.233 0.90 356236. 0.1842
|
|
152.23 0.7254 0.7661 0.0345 0.0326 5.484 21.603 10.349 4089.361 2.441 46.032 1.148 0.90 357488. 0.1564
|
|
158.57 0.7556 0.7235 0.0275 0.0287 4.817 18.976 8.243 3592.090 2.144 36.663 1.041 0.90 358780. 0.1266
|
|
164.92 0.7859 0.6504 0.0204 0.0247 4.148 16.340 6.135 3093.165 1.846 27.289 0.900 0.91 360112. 0.0944
|
|
171.26 0.8161 0.5294 0.0135 0.0208 3.488 13.738 4.043 2600.666 1.552 17.982 0.705 0.91 361484. 0.0601
|
|
177.60 0.8463 0.3300 0.0066 0.0169 2.847 11.217 1.984 2123.277 1.267 8.824 0.424 0.91 362895. 0.0253
|
|
183.95 0.8765 -0.0055 -0.0001 0.0133 2.234 8.800 -0.025 1665.871 0.994 -0.111 -0.007 0.91 364342. 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 0.1242 0.0677 13.640 50.569 42.078 10170.977 5.713 187.162 1.876 0.93 360374. 0.5157
|
|
6.87 0.0308 0.0554 0.1236 0.0687 13.847 51.340 41.891 10326.039 5.800 186.329 1.840 0.93 360684. 0.5045
|
|
13.74 0.0616 0.1086 0.1229 0.0697 14.054 52.107 41.668 10480.244 5.887 185.339 1.803 0.93 361030. 0.4931
|
|
20.61 0.0924 0.1596 0.1222 0.0707 14.254 52.846 41.401 10628.905 5.971 184.154 1.767 0.93 361414. 0.4816
|
|
27.48 0.1232 0.2085 0.1212 0.0716 14.438 53.530 41.081 10766.544 6.048 182.728 1.731 0.93 361839. 0.4699
|
|
34.35 0.1540 0.2553 0.1201 0.0725 14.600 54.129 40.696 10886.956 6.115 181.015 1.695 0.94 362307. 0.4582
|
|
41.21 0.1848 0.3002 0.1187 0.0731 14.729 54.608 40.234 10983.361 6.170 178.959 1.661 0.94 362820. 0.4465
|
|
48.08 0.2156 0.3434 0.1171 0.0735 14.817 54.934 39.682 11048.864 6.206 176.504 1.629 0.94 363380. 0.4347
|
|
54.95 0.2465 0.3850 0.1152 0.0737 14.854 55.073 39.028 11076.881 6.222 173.595 1.598 0.94 363989. 0.4229
|
|
61.82 0.2773 0.4252 0.1129 0.0736 14.834 54.997 38.259 11061.499 6.214 170.178 1.569 0.94 364648. 0.4111
|
|
68.69 0.3081 0.4641 0.1102 0.0732 14.748 54.680 37.365 10997.815 6.178 166.201 1.541 0.94 365357. 0.3991
|
|
75.56 0.3389 0.5017 0.1072 0.0724 14.593 54.104 36.336 10882.002 6.113 161.622 1.515 0.94 366118. 0.3868
|
|
82.43 0.3697 0.5381 0.1037 0.0713 14.363 53.253 35.163 10710.745 6.016 156.404 1.489 0.94 366930. 0.3741
|
|
89.30 0.4005 0.5732 0.0998 0.0698 14.057 52.117 33.840 10482.207 5.888 150.521 1.464 0.94 367793. 0.3609
|
|
96.17 0.4313 0.6070 0.0955 0.0679 13.674 50.695 32.366 10196.329 5.728 143.965 1.440 0.94 368707. 0.3470
|
|
103.04 0.4621 0.6392 0.0907 0.0656 13.213 48.988 30.741 9852.898 5.535 136.735 1.415 0.94 369670. 0.3324
|
|
109.90 0.4929 0.6697 0.0855 0.0629 12.675 46.992 28.962 9451.488 5.309 128.825 1.390 0.95 370683. 0.3169
|
|
116.77 0.5237 0.6981 0.0798 0.0599 12.061 44.716 27.041 8993.824 5.052 120.279 1.364 0.95 371743. 0.3004
|
|
123.64 0.5545 0.7243 0.0738 0.0565 11.379 42.187 24.998 8485.147 4.766 111.190 1.336 0.95 372851. 0.2830
|
|
130.51 0.5853 0.7476 0.0674 0.0528 10.637 39.439 22.851 7932.296 4.456 101.642 1.307 0.95 374005. 0.2646
|
|
137.38 0.6161 0.7648 0.0608 0.0490 9.874 36.607 20.614 7362.703 4.136 91.692 1.270 0.95 375205. 0.2443
|
|
144.25 0.6469 0.7726 0.0540 0.0452 9.111 33.780 18.300 6794.142 3.816 81.400 1.222 0.95 376450. 0.2214
|
|
151.12 0.6777 0.7624 0.0470 0.0417 8.412 31.187 15.915 6272.600 3.523 70.789 1.151 0.96 377739. 0.1945
|
|
157.99 0.7086 0.7374 0.0398 0.0382 7.705 28.568 13.488 5745.884 3.228 59.993 1.065 0.96 379072. 0.1656
|
|
164.86 0.7394 0.6936 0.0326 0.0347 6.995 25.934 11.037 5216.140 2.930 49.095 0.960 0.96 380449. 0.1351
|
|
171.73 0.7702 0.6247 0.0253 0.0312 6.294 23.335 8.586 4693.272 2.636 38.192 0.830 0.96 381870. 0.1030
|
|
178.59 0.8010 0.5222 0.0182 0.0279 5.615 20.819 6.158 4187.409 2.352 27.389 0.667 0.96 383334. 0.0701
|
|
185.46 0.8318 0.3761 0.0112 0.0247 4.971 18.429 3.780 3706.591 2.082 16.815 0.463 0.97 384843. 0.0381
|
|
192.33 0.8626 0.1740 0.0044 0.0217 4.367 16.191 1.482 3256.545 1.829 6.591 0.206 0.97 386401. 0.0106
|
|
199.20 0.8934
|
|
|
|
|
|
|