612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x11 (14x11.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 0.1179 0.0616 0.003 0.168 0.144 1.987 0.019 0.642 32.949 0.06 24289. 0.5246
|
|
0.44 0.0329 0.0614 0.1169 0.0627 0.003 0.171 0.143 2.023 0.019 0.637 32.093 0.06 24312. 0.5089
|
|
0.87 0.0658 0.1194 0.1158 0.0638 0.003 0.174 0.142 2.059 0.020 0.631 31.224 0.06 24337. 0.4928
|
|
1.31 0.0987 0.1741 0.1146 0.0649 0.003 0.177 0.140 2.096 0.020 0.624 30.349 0.06 24365. 0.4763
|
|
1.74 0.1316 0.2254 0.1131 0.0660 0.003 0.180 0.139 2.131 0.020 0.616 29.473 0.06 24396. 0.4597
|
|
2.18 0.1645 0.2734 0.1115 0.0671 0.003 0.183 0.137 2.165 0.021 0.607 28.599 0.06 24431. 0.4429
|
|
2.62 0.1974 0.3181 0.1097 0.0681 0.003 0.186 0.134 2.197 0.021 0.597 27.733 0.06 24469. 0.4260
|
|
3.05 0.2303 0.3597 0.1077 0.0689 0.003 0.188 0.132 2.224 0.021 0.586 26.877 0.06 24510. 0.4090
|
|
3.49 0.2632 0.3982 0.1054 0.0696 0.003 0.190 0.129 2.248 0.021 0.574 26.034 0.06 24556. 0.3919
|
|
3.93 0.2961 0.4337 0.1028 0.0702 0.003 0.191 0.126 2.265 0.022 0.560 25.204 0.06 24605. 0.3748
|
|
4.36 0.3290 0.4663 0.1000 0.0705 0.003 0.192 0.122 2.276 0.022 0.544 24.388 0.06 24657. 0.3576
|
|
4.80 0.3618 0.4960 0.0968 0.0706 0.003 0.193 0.119 2.280 0.022 0.527 23.586 0.06 24714. 0.3404
|
|
5.23 0.3947 0.5230 0.0934 0.0705 0.003 0.192 0.114 2.275 0.022 0.509 22.796 0.06 24774. 0.3231
|
|
5.67 0.4276 0.5472 0.0896 0.0700 0.003 0.191 0.110 2.260 0.022 0.488 22.016 0.06 24838. 0.3056
|
|
6.11 0.4605 0.5686 0.0855 0.0692 0.003 0.189 0.105 2.234 0.021 0.465 21.244 0.06 24906. 0.2880
|
|
6.54 0.4934 0.5872 0.0810 0.0681 0.003 0.186 0.099 2.197 0.021 0.441 20.475 0.06 24978. 0.2702
|
|
6.98 0.5263 0.6028 0.0762 0.0665 0.003 0.182 0.093 2.148 0.021 0.415 19.705 0.06 25054. 0.2523
|
|
7.41 0.5592 0.6152 0.0712 0.0647 0.003 0.176 0.087 2.087 0.020 0.387 18.929 0.06 25133. 0.2341
|
|
7.85 0.5921 0.6242 0.0659 0.0625 0.003 0.170 0.081 2.016 0.019 0.359 18.138 0.06 25216. 0.2159
|
|
8.29 0.6250 0.6293 0.0604 0.0600 0.003 0.164 0.074 1.936 0.018 0.329 17.324 0.06 25303. 0.1974
|
|
8.72 0.6579 0.6300 0.0547 0.0572 0.002 0.156 0.067 1.845 0.018 0.298 16.475 0.06 25393. 0.1788
|
|
9.16 0.6908 0.6254 0.0490 0.0541 0.002 0.148 0.060 1.746 0.017 0.267 15.576 0.06 25487. 0.1598
|
|
9.59 0.7237 0.6144 0.0431 0.0507 0.002 0.138 0.053 1.637 0.016 0.234 14.607 0.06 25585. 0.1406
|
|
10.03 0.7566 0.5954 0.0371 0.0471 0.002 0.128 0.045 1.520 0.015 0.202 13.540 0.06 25687. 0.1209
|
|
10.47 0.7895 0.5661 0.0310 0.0432 0.002 0.118 0.038 1.395 0.013 0.169 12.338 0.06 25792. 0.1007
|
|
10.90 0.8224 0.5229 0.0248 0.0391 0.002 0.107 0.030 1.261 0.012 0.135 10.939 0.06 25900. 0.0800
|
|
11.34 0.8553 0.4599 0.0187 0.0347 0.002 0.095 0.023 1.120 0.011 0.102 9.251 0.06 26012. 0.0586
|
|
11.78 0.8882 0.3674 0.0124 0.0301 0.001 0.082 0.015 0.971 0.009 0.068 7.117 0.06 26128. 0.0368
|
|
12.21 0.9211 0.2275 0.0062 0.0253 0.001 0.069 0.008 0.816 0.008 0.034 4.249 0.06 26247. 0.0156
|
|
12.65 0.9540 0.0034 0.0001 0.0203 0.001 0.055 0.000 0.654 0.006 0.000 0.062 0.06 26369. 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 0.1184 0.0552 0.019 0.602 0.580 14.255 0.068 2.579 18.449 0.11 48579. 0.5888
|
|
0.88 0.0331 0.0690 0.1175 0.0564 0.020 0.615 0.575 14.561 0.070 2.558 17.917 0.11 48624. 0.5695
|
|
1.76 0.0663 0.1339 0.1164 0.0576 0.020 0.628 0.570 14.872 0.071 2.535 17.380 0.11 48674. 0.5499
|
|
2.64 0.0994 0.1947 0.1151 0.0588 0.020 0.642 0.564 15.183 0.072 2.508 16.843 0.11 48731. 0.5301
|
|
3.52 0.1326 0.2513 0.1137 0.0600 0.021 0.655 0.557 15.489 0.074 2.477 16.310 0.11 48794. 0.5101
|
|
4.39 0.1657 0.3040 0.1121 0.0611 0.021 0.667 0.549 15.782 0.075 2.443 15.782 0.11 48864. 0.4902
|
|
5.27 0.1989 0.3528 0.1103 0.0622 0.022 0.679 0.540 16.056 0.077 2.403 15.263 0.11 48941. 0.4702
|
|
6.15 0.2320 0.3979 0.1083 0.0631 0.022 0.689 0.530 16.302 0.078 2.359 14.754 0.11 49025. 0.4503
|
|
7.03 0.2652 0.4395 0.1060 0.0640 0.022 0.698 0.519 16.512 0.079 2.309 14.258 0.11 49117. 0.4305
|
|
7.91 0.2983 0.4776 0.1034 0.0646 0.022 0.705 0.507 16.678 0.080 2.253 13.774 0.11 49216. 0.4109
|
|
8.79 0.3314 0.5126 0.1006 0.0650 0.023 0.710 0.493 16.791 0.080 2.191 13.304 0.11 49322. 0.3913
|
|
9.67 0.3646 0.5445 0.0974 0.0652 0.023 0.712 0.477 16.842 0.080 2.122 12.847 0.11 49437. 0.3719
|
|
10.55 0.3977 0.5734 0.0939 0.0652 0.023 0.711 0.460 16.821 0.080 2.046 12.402 0.11 49559. 0.3525
|
|
11.42 0.4309 0.5994 0.0901 0.0648 0.022 0.707 0.441 16.719 0.080 1.962 11.968 0.11 49689. 0.3332
|
|
12.30 0.4640 0.6227 0.0859 0.0640 0.022 0.698 0.421 16.527 0.079 1.871 11.544 0.11 49827. 0.3138
|
|
13.18 0.4972 0.6432 0.0814 0.0629 0.022 0.686 0.398 16.238 0.078 1.772 11.129 0.11 49972. 0.2944
|
|
14.06 0.5303 0.6608 0.0765 0.0614 0.021 0.670 0.375 15.853 0.076 1.667 10.720 0.11 50126. 0.2750
|
|
14.94 0.5635 0.6756 0.0714 0.0595 0.021 0.650 0.350 15.373 0.073 1.555 10.315 0.11 50287. 0.2556
|
|
15.82 0.5966 0.6872 0.0660 0.0573 0.020 0.626 0.323 14.804 0.071 1.439 9.909 0.11 50455. 0.2362
|
|
16.70 0.6297 0.6953 0.0605 0.0548 0.019 0.598 0.296 14.149 0.068 1.318 9.498 0.11 50631. 0.2167
|
|
17.58 0.6629 0.6994 0.0548 0.0519 0.018 0.567 0.268 13.412 0.064 1.194 9.077 0.11 50814. 0.1971
|
|
18.46 0.6960 0.6989 0.0490 0.0488 0.017 0.532 0.240 12.596 0.060 1.067 8.638 0.11 51005. 0.1773
|
|
19.33 0.7292 0.6926 0.0430 0.0453 0.016 0.495 0.211 11.702 0.056 0.938 8.171 0.11 51204. 0.1572
|
|
20.21 0.7623 0.6788 0.0370 0.0416 0.014 0.454 0.181 10.733 0.051 0.806 7.661 0.11 51409. 0.1367
|
|
21.09 0.7955 0.6552 0.0309 0.0375 0.013 0.410 0.151 9.690 0.046 0.673 7.086 0.11 51622. 0.1155
|
|
21.97 0.8286 0.6175 0.0248 0.0332 0.012 0.362 0.121 8.576 0.041 0.539 6.411 0.11 51842. 0.0935
|
|
22.85 0.8618 0.5584 0.0186 0.0286 0.010 0.313 0.091 7.394 0.035 0.404 5.575 0.12 52069. 0.0704
|
|
23.73 0.8949 0.4643 0.0124 0.0238 0.008 0.260 0.061 6.149 0.029 0.269 4.463 0.12 52304. 0.0460
|
|
24.61 0.9280 0.3051 0.0062 0.0188 0.006 0.205 0.030 4.846 0.023 0.134 2.829 0.12 52545. 0.0206
|
|
25.49 0.9612 0.0023 0.0000 0.0135 0.005 0.148 0.000 3.490 0.017 0.001 0.020 0.12 52791. 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 0.1187 0.0526 0.062 1.292 1.308 45.866 0.146 5.819 12.936 0.17 72867. 0.6201
|
|
1.32 0.0333 0.0727 0.1178 0.0538 0.063 1.322 1.298 46.923 0.149 5.773 12.545 0.17 72935. 0.5990
|
|
2.65 0.0665 0.1409 0.1167 0.0551 0.064 1.352 1.286 48.003 0.153 5.720 12.152 0.17 73011. 0.5776
|
|
3.97 0.0998 0.2046 0.1155 0.0563 0.066 1.383 1.273 49.086 0.156 5.661 11.760 0.17 73097. 0.5560
|
|
5.29 0.1330 0.2637 0.1141 0.0576 0.067 1.413 1.257 50.153 0.160 5.593 11.371 0.17 73192. 0.5344
|
|
6.61 0.1663 0.3186 0.1125 0.0587 0.069 1.442 1.240 51.179 0.163 5.515 10.988 0.17 73297. 0.5128
|
|
7.94 0.1995 0.3692 0.1107 0.0598 0.070 1.469 1.220 52.141 0.166 5.427 10.613 0.17 73413. 0.4913
|
|
9.26 0.2328 0.4159 0.1087 0.0608 0.071 1.494 1.198 53.010 0.169 5.327 10.247 0.17 73540. 0.4700
|
|
10.58 0.2660 0.4588 0.1064 0.0617 0.072 1.515 1.172 53.758 0.171 5.215 9.892 0.17 73678. 0.4489
|
|
11.90 0.2993 0.4982 0.1038 0.0624 0.073 1.531 1.144 54.356 0.173 5.089 9.547 0.17 73827. 0.4280
|
|
13.23 0.3325 0.5342 0.1010 0.0629 0.073 1.543 1.113 54.772 0.174 4.949 9.213 0.17 73988. 0.4073
|
|
14.55 0.3658 0.5670 0.0978 0.0631 0.074 1.549 1.078 54.977 0.175 4.793 8.890 0.17 74161. 0.3868
|
|
15.87 0.3991 0.5969 0.0943 0.0630 0.074 1.548 1.039 54.936 0.175 4.621 8.578 0.17 74345. 0.3665
|
|
17.19 0.4323 0.6238 0.0904 0.0627 0.073 1.539 0.996 54.617 0.174 4.432 8.275 0.17 74542. 0.3462
|
|
18.52 0.4656 0.6479 0.0862 0.0620 0.072 1.521 0.950 53.987 0.172 4.226 7.982 0.17 74750. 0.3261
|
|
19.84 0.4988 0.6693 0.0817 0.0609 0.071 1.494 0.900 53.026 0.169 4.002 7.696 0.17 74969. 0.3059
|
|
21.16 0.5321 0.6881 0.0768 0.0594 0.069 1.457 0.846 51.731 0.165 3.763 7.417 0.17 75201. 0.2859
|
|
22.48 0.5653 0.7040 0.0716 0.0575 0.067 1.412 0.789 50.111 0.160 3.510 7.142 0.17 75443. 0.2659
|
|
23.81 0.5986 0.7170 0.0662 0.0553 0.065 1.357 0.730 48.181 0.153 3.246 6.870 0.17 75698. 0.2460
|
|
25.13 0.6318 0.7269 0.0607 0.0527 0.062 1.295 0.668 45.952 0.146 2.973 6.598 0.17 75963. 0.2261
|
|
26.45 0.6651 0.7330 0.0549 0.0498 0.058 1.224 0.605 43.436 0.138 2.693 6.321 0.17 76240. 0.2061
|
|
27.77 0.6983 0.7349 0.0491 0.0466 0.055 1.145 0.541 40.642 0.129 2.405 6.035 0.17 76528. 0.1860
|
|
29.10 0.7316 0.7314 0.0431 0.0431 0.050 1.059 0.475 37.576 0.120 2.113 5.734 0.17 76827. 0.1656
|
|
30.42 0.7648 0.7212 0.0371 0.0393 0.046 0.965 0.408 34.246 0.109 1.816 5.408 0.17 77138. 0.1448
|
|
31.74 0.7981 0.7016 0.0309 0.0352 0.041 0.864 0.341 30.658 0.098 1.516 5.042 0.17 77459. 0.1234
|
|
33.07 0.8314 0.6685 0.0247 0.0308 0.036 0.756 0.273 26.822 0.085 1.213 4.611 0.17 77791. 0.1009
|
|
34.39 0.8646 0.6141 0.0185 0.0261 0.031 0.641 0.204 22.747 0.072 0.909 4.073 0.17 78134. 0.0772
|
|
35.71 0.8979 0.5227 0.0123 0.0212 0.025 0.520 0.136 18.451 0.059 0.604 3.339 0.17 78487. 0.0516
|
|
37.03 0.9311 0.3569 0.0061 0.0160 0.019 0.393 0.068 13.950 0.044 0.301 2.198 0.17 78851. 0.0240
|
|
38.36 0.9644 -0.0005 0.0000 0.0106 0.012 0.261 0.000 9.267 0.029 0.000 -0.003 0.17 79222. 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 0.1190 0.0512 0.142 2.236 2.331 105.840 0.253 10.370 9.991 0.22 97154. 0.6394
|
|
1.77 0.0333 0.0750 0.1181 0.0525 0.145 2.290 2.313 108.392 0.259 10.290 9.681 0.22 97245. 0.6171
|
|
3.53 0.0666 0.1451 0.1171 0.0537 0.149 2.346 2.293 111.001 0.265 10.199 9.369 0.22 97347. 0.5946
|
|
5.30 0.1000 0.2105 0.1159 0.0550 0.152 2.401 2.269 113.623 0.271 10.094 9.059 0.22 97461. 0.5719
|
|
7.07 0.1333 0.2712 0.1145 0.0563 0.156 2.456 2.242 116.209 0.277 9.974 8.752 0.22 97588. 0.5493
|
|
8.83 0.1666 0.3273 0.1129 0.0575 0.159 2.508 2.212 118.704 0.283 9.837 8.451 0.22 97729. 0.5267
|
|
10.60 0.1999 0.3791 0.1111 0.0586 0.162 2.558 2.177 121.045 0.289 9.682 8.156 0.22 97884. 0.5043
|
|
12.37 0.2332 0.4267 0.1091 0.0596 0.165 2.603 2.137 123.168 0.294 9.505 7.869 0.22 98053. 0.4821
|
|
14.13 0.2665 0.4704 0.1068 0.0605 0.168 2.641 2.092 125.004 0.298 9.306 7.592 0.22 98238. 0.4602
|
|
15.90 0.2999 0.5105 0.1042 0.0612 0.170 2.673 2.042 126.480 0.302 9.083 7.323 0.22 98438. 0.4386
|
|
17.67 0.3332 0.5471 0.1014 0.0617 0.171 2.695 1.986 127.524 0.304 8.833 7.063 0.22 98654. 0.4172
|
|
19.44 0.3665 0.5805 0.0982 0.0620 0.172 2.706 1.924 128.060 0.306 8.556 6.813 0.22 98885. 0.3961
|
|
21.20 0.3998 0.6109 0.0947 0.0620 0.172 2.705 1.855 128.008 0.306 8.250 6.572 0.22 99132. 0.3751
|
|
22.97 0.4331 0.6383 0.0908 0.0616 0.171 2.690 1.779 127.286 0.304 7.913 6.339 0.22 99394. 0.3544
|
|
24.74 0.4664 0.6630 0.0866 0.0609 0.169 2.659 1.696 125.819 0.300 7.544 6.114 0.22 99673. 0.3337
|
|
26.50 0.4998 0.6851 0.0820 0.0598 0.166 2.611 1.606 123.555 0.295 7.144 5.896 0.22 99967. 0.3132
|
|
28.27 0.5331 0.7045 0.0771 0.0583 0.162 2.546 1.510 120.486 0.288 6.716 5.684 0.23 100276. 0.2928
|
|
30.04 0.5664 0.7213 0.0719 0.0565 0.156 2.465 1.408 116.634 0.278 6.265 5.477 0.23 100601. 0.2724
|
|
31.80 0.5997 0.7352 0.0665 0.0542 0.150 2.367 1.303 112.030 0.267 5.794 5.273 0.23 100941. 0.2522
|
|
33.57 0.6330 0.7462 0.0609 0.0517 0.143 2.255 1.193 106.706 0.255 5.306 5.070 0.23 101297. 0.2321
|
|
35.34 0.6664 0.7537 0.0551 0.0487 0.135 2.128 1.080 100.687 0.240 4.804 4.865 0.23 101667. 0.2119
|
|
37.10 0.6997 0.7573 0.0493 0.0455 0.126 1.986 0.965 93.991 0.224 4.291 4.656 0.23 102053. 0.1917
|
|
38.87 0.7330 0.7559 0.0433 0.0419 0.116 1.831 0.847 86.636 0.207 3.769 4.436 0.23 102453. 0.1711
|
|
40.64 0.7663 0.7481 0.0372 0.0381 0.105 1.662 0.728 78.639 0.188 3.239 4.199 0.23 102868. 0.1502
|
|
42.40 0.7996 0.7316 0.0310 0.0339 0.094 1.479 0.608 70.015 0.167 2.702 3.936 0.23 103298. 0.1286
|
|
44.17 0.8329 0.7022 0.0248 0.0294 0.082 1.284 0.486 60.788 0.145 2.162 3.626 0.23 103743. 0.1060
|
|
45.94 0.8663 0.6520 0.0186 0.0247 0.068 1.077 0.364 50.983 0.122 1.619 3.237 0.23 104201. 0.0819
|
|
47.70 0.8996 0.5643 0.0123 0.0197 0.054 0.859 0.242 40.639 0.097 1.075 2.698 0.23 104674. 0.0556
|
|
49.47 0.9329 0.3965 0.0061 0.0144 0.040 0.630 0.120 29.802 0.071 0.534 1.828 0.23 105161. 0.0266
|
|
51.24 0.9662 -0.0028 0.0000 0.0090 0.025 0.391 -0.001 18.517 0.044 -0.002 -0.013 0.23 105656. 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 0.1193 0.0504 0.273 3.438 3.653 203.360 0.388 16.246 8.146 0.28 121440. 0.6525
|
|
2.21 0.0334 0.0765 0.1184 0.0517 0.279 3.523 3.625 208.420 0.398 16.124 7.889 0.28 121553. 0.6295
|
|
4.42 0.0667 0.1479 0.1174 0.0529 0.286 3.611 3.594 213.600 0.408 15.984 7.631 0.28 121681. 0.6063
|
|
6.63 0.1001 0.2144 0.1162 0.0542 0.293 3.699 3.557 218.813 0.418 15.823 7.374 0.28 121824. 0.5829
|
|
8.84 0.1334 0.2761 0.1149 0.0555 0.300 3.786 3.516 223.962 0.428 15.639 7.120 0.28 121983. 0.5596
|
|
11.06 0.1668 0.3330 0.1133 0.0567 0.307 3.870 3.468 228.936 0.437 15.427 6.872 0.28 122159. 0.5364
|
|
13.27 0.2001 0.3855 0.1116 0.0579 0.313 3.949 3.414 233.615 0.446 15.186 6.629 0.28 122353. 0.5133
|
|
15.48 0.2335 0.4338 0.1095 0.0590 0.319 4.021 3.353 237.867 0.454 14.913 6.393 0.28 122566. 0.4906
|
|
17.69 0.2668 0.4781 0.1073 0.0599 0.324 4.083 3.283 241.554 0.461 14.603 6.165 0.28 122797. 0.4682
|
|
19.90 0.3002 0.5186 0.1047 0.0606 0.328 4.134 3.205 244.535 0.467 14.255 5.944 0.28 123047. 0.4460
|
|
22.11 0.3336 0.5556 0.1019 0.0611 0.331 4.170 3.117 246.664 0.471 13.866 5.732 0.28 123318. 0.4242
|
|
24.32 0.3669 0.5894 0.0987 0.0614 0.332 4.189 3.020 247.789 0.473 13.433 5.528 0.28 123607. 0.4026
|
|
26.53 0.4003 0.6202 0.0952 0.0614 0.332 4.188 2.912 247.754 0.473 12.954 5.332 0.28 123917. 0.3813
|
|
28.74 0.4336 0.6480 0.0913 0.0611 0.330 4.165 2.794 246.396 0.471 12.426 5.142 0.28 124246. 0.3602
|
|
30.96 0.4670 0.6731 0.0870 0.0604 0.327 4.117 2.664 243.563 0.465 11.847 4.960 0.28 124595. 0.3393
|
|
33.17 0.5003 0.6956 0.0824 0.0593 0.321 4.043 2.523 239.155 0.457 11.220 4.784 0.28 124963. 0.3185
|
|
35.38 0.5337 0.7155 0.0775 0.0578 0.313 3.941 2.372 233.152 0.445 10.549 4.614 0.28 125351. 0.2978
|
|
37.59 0.5671 0.7329 0.0723 0.0559 0.303 3.814 2.212 225.596 0.431 9.840 4.448 0.28 125758. 0.2773
|
|
39.80 0.6004 0.7476 0.0668 0.0537 0.290 3.661 2.046 216.549 0.414 9.099 4.285 0.28 126185. 0.2569
|
|
42.01 0.6338 0.7595 0.0612 0.0511 0.276 3.484 1.873 206.070 0.394 8.333 4.124 0.28 126630. 0.2366
|
|
44.22 0.6671 0.7681 0.0554 0.0481 0.260 3.283 1.696 194.208 0.371 7.545 3.962 0.28 127094. 0.2163
|
|
46.43 0.7005 0.7729 0.0495 0.0449 0.243 3.060 1.515 181.001 0.346 6.740 3.797 0.28 127577. 0.1959
|
|
48.64 0.7338 0.7731 0.0435 0.0413 0.223 2.814 1.331 166.483 0.318 5.919 3.625 0.29 128079. 0.1753
|
|
50.86 0.7672 0.7674 0.0374 0.0374 0.202 2.547 1.143 150.685 0.288 5.086 3.442 0.29 128599. 0.1543
|
|
53.07 0.8005 0.7533 0.0312 0.0331 0.179 2.259 0.954 133.641 0.255 4.244 3.238 0.29 129138. 0.1326
|
|
55.28 0.8339 0.7270 0.0249 0.0286 0.155 1.951 0.763 115.394 0.220 3.395 3.000 0.29 129694. 0.1098
|
|
57.49 0.8673 0.6805 0.0187 0.0238 0.129 1.623 0.571 96.000 0.183 2.542 2.700 0.29 130269. 0.0855
|
|
59.70 0.9006 0.5967 0.0124 0.0187 0.101 1.277 0.380 75.532 0.144 1.689 2.280 0.29 130862. 0.0589
|
|
61.91 0.9340 0.4296 0.0062 0.0134 0.073 0.914 0.189 54.085 0.103 0.840 1.583 0.29 131471. 0.0288
|
|
64.12 0.9673 -0.0026 0.0000 0.0079 0.043 0.537 -0.001 31.742 0.061 -0.003 -0.009 0.29 132090. 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 0.1197 0.0499 0.467 4.901 5.275 347.895 0.554 23.464 6.877 0.33 145724. 0.6620
|
|
2.67 0.0336 0.0780 0.1188 0.0512 0.479 5.027 5.236 356.828 0.568 23.291 6.656 0.33 145860. 0.6384
|
|
5.35 0.0672 0.1508 0.1178 0.0525 0.491 5.156 5.192 365.987 0.582 23.093 6.434 0.33 146015. 0.6144
|
|
8.02 0.1008 0.2185 0.1166 0.0538 0.503 5.286 5.140 375.214 0.597 22.864 6.214 0.33 146188. 0.5904
|
|
10.70 0.1345 0.2812 0.1153 0.0551 0.515 5.414 5.081 384.336 0.612 22.600 5.996 0.33 146381. 0.5665
|
|
13.37 0.1681 0.3390 0.1137 0.0564 0.527 5.538 5.013 393.154 0.626 22.297 5.783 0.33 146595. 0.5427
|
|
16.04 0.2017 0.3921 0.1120 0.0576 0.538 5.655 4.935 401.448 0.639 21.950 5.575 0.33 146831. 0.5191
|
|
18.72 0.2353 0.4410 0.1099 0.0587 0.548 5.761 4.846 408.983 0.651 21.554 5.374 0.33 147089. 0.4958
|
|
21.39 0.2689 0.4857 0.1077 0.0596 0.557 5.853 4.745 415.512 0.661 21.105 5.179 0.33 147370. 0.4729
|
|
24.07 0.3025 0.5267 0.1051 0.0604 0.564 5.928 4.631 420.777 0.670 20.599 4.992 0.33 147675. 0.4503
|
|
26.74 0.3362 0.5641 0.1022 0.0609 0.569 5.980 4.504 424.516 0.676 20.032 4.812 0.34 148003. 0.4280
|
|
29.41 0.3698 0.5982 0.0990 0.0612 0.572 6.008 4.362 426.459 0.679 19.400 4.639 0.34 148356. 0.4060
|
|
32.09 0.4034 0.6292 0.0954 0.0612 0.572 6.006 4.204 426.323 0.679 18.699 4.473 0.34 148732. 0.3843
|
|
34.76 0.4370 0.6573 0.0914 0.0608 0.568 5.970 4.030 423.818 0.675 17.926 4.313 0.34 149133. 0.3629
|
|
37.43 0.4706 0.6826 0.0871 0.0601 0.561 5.898 3.839 418.675 0.666 17.078 4.159 0.34 149558. 0.3416
|
|
40.11 0.5042 0.7054 0.0824 0.0589 0.551 5.786 3.633 410.725 0.654 16.158 4.012 0.34 150006. 0.3204
|
|
42.78 0.5378 0.7256 0.0774 0.0574 0.536 5.634 3.411 399.944 0.637 15.173 3.869 0.34 150478. 0.2995
|
|
45.46 0.5715 0.7433 0.0721 0.0554 0.518 5.443 3.178 386.413 0.615 14.134 3.730 0.34 150974. 0.2787
|
|
48.13 0.6051 0.7584 0.0666 0.0531 0.497 5.216 2.934 370.242 0.589 13.050 3.594 0.34 151493. 0.2580
|
|
50.80 0.6387 0.7706 0.0608 0.0504 0.471 4.952 2.682 351.534 0.559 11.928 3.460 0.34 152035. 0.2375
|
|
53.48 0.6723 0.7797 0.0550 0.0474 0.443 4.654 2.422 330.372 0.526 10.775 3.326 0.34 152601. 0.2169
|
|
56.15 0.7059 0.7851 0.0489 0.0440 0.411 4.322 2.157 306.823 0.488 9.596 3.189 0.34 153188. 0.1963
|
|
58.83 0.7395 0.7859 0.0428 0.0403 0.377 3.958 1.887 280.947 0.447 8.396 3.047 0.34 153799. 0.1755
|
|
61.50 0.7731 0.7806 0.0366 0.0363 0.339 3.561 1.614 252.798 0.402 7.178 2.895 0.34 154432. 0.1542
|
|
64.17 0.8068 0.7670 0.0303 0.0319 0.298 3.134 1.337 222.442 0.354 5.947 2.726 0.34 155088. 0.1321
|
|
66.85 0.8404 0.7404 0.0240 0.0272 0.255 2.676 1.058 189.956 0.302 4.707 2.527 0.34 155765. 0.1089
|
|
69.52 0.8740 0.6921 0.0177 0.0223 0.208 2.190 0.778 155.446 0.247 3.462 2.271 0.35 156465. 0.0840
|
|
72.20 0.9076 0.6011 0.0113 0.0171 0.160 1.677 0.498 119.051 0.189 2.217 1.899 0.35 157186. 0.0562
|
|
74.87 0.9412 0.4051 0.0050 0.0116 0.109 1.140 0.220 80.951 0.129 0.980 1.234 0.35 157927. 0.0243
|
|
77.54 0.9748
|
|
|
|
|
|
|
|
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 0.1201 0.0496 0.737 6.633 7.204 549.317 0.749 32.042 5.948 0.39 170005. 0.6691
|
|
3.10 0.0334 0.0782 0.1192 0.0509 0.756 6.805 7.153 563.614 0.769 31.817 5.756 0.39 170163. 0.6453
|
|
6.20 0.0668 0.1512 0.1183 0.0522 0.776 6.983 7.094 578.292 0.789 31.556 5.564 0.39 170342. 0.6212
|
|
9.30 0.1002 0.2191 0.1171 0.0536 0.795 7.162 7.027 593.105 0.809 31.255 5.374 0.39 170542. 0.5970
|
|
12.40 0.1336 0.2819 0.1158 0.0549 0.815 7.339 6.949 607.777 0.829 30.908 5.186 0.39 170765. 0.5729
|
|
15.50 0.1670 0.3399 0.1143 0.0562 0.834 7.510 6.859 621.994 0.849 30.507 5.001 0.39 171013. 0.5490
|
|
18.60 0.2004 0.3932 0.1126 0.0574 0.852 7.672 6.755 635.409 0.867 30.047 4.822 0.39 171285. 0.5253
|
|
21.70 0.2338 0.4422 0.1106 0.0585 0.869 7.820 6.637 647.646 0.884 29.522 4.648 0.39 171583. 0.5019
|
|
24.80 0.2672 0.4871 0.1084 0.0595 0.883 7.949 6.503 658.313 0.898 28.924 4.480 0.39 171908. 0.4788
|
|
27.90 0.3006 0.5282 0.1059 0.0603 0.894 8.054 6.351 667.004 0.910 28.249 4.319 0.39 172260. 0.4562
|
|
31.00 0.3340 0.5658 0.1030 0.0608 0.903 8.130 6.180 673.301 0.919 27.491 4.163 0.39 172640. 0.4338
|
|
34.10 0.3674 0.6001 0.0999 0.0611 0.908 8.172 5.990 676.779 0.923 26.644 4.015 0.39 173047. 0.4118
|
|
37.20 0.4008 0.6314 0.0963 0.0612 0.908 8.174 5.779 676.994 0.924 25.704 3.872 0.39 173482. 0.3901
|
|
40.30 0.4342 0.6598 0.0924 0.0608 0.903 8.132 5.545 673.486 0.919 24.665 3.735 0.39 173945. 0.3686
|
|
43.40 0.4677 0.6855 0.0882 0.0601 0.893 8.040 5.289 665.828 0.908 23.525 3.603 0.39 174435. 0.3473
|
|
46.50 0.5011 0.7087 0.0835 0.0591 0.877 7.893 5.010 653.724 0.892 22.286 3.476 0.39 174953. 0.3261
|
|
49.60 0.5345 0.7294 0.0785 0.0576 0.854 7.693 4.712 637.113 0.869 20.958 3.354 0.39 175498. 0.3052
|
|
52.70 0.5679 0.7477 0.0733 0.0557 0.826 7.439 4.396 616.108 0.840 19.553 3.236 0.40 176071. 0.2844
|
|
55.80 0.6013 0.7635 0.0678 0.0534 0.792 7.135 4.066 590.881 0.806 18.085 3.121 0.40 176670. 0.2638
|
|
58.90 0.6347 0.7766 0.0621 0.0507 0.753 6.781 3.724 561.597 0.766 16.565 3.008 0.40 177296. 0.2433
|
|
62.00 0.6681 0.7868 0.0562 0.0477 0.709 6.380 3.372 528.392 0.721 15.000 2.895 0.40 177948. 0.2228
|
|
65.10 0.7015 0.7936 0.0502 0.0444 0.659 5.933 3.013 491.376 0.670 13.400 2.781 0.40 178626. 0.2023
|
|
68.20 0.7349 0.7963 0.0441 0.0407 0.604 5.441 2.646 450.642 0.615 11.770 2.663 0.40 179331. 0.1816
|
|
71.30 0.7683 0.7935 0.0379 0.0367 0.545 4.906 2.274 406.278 0.554 10.115 2.539 0.40 180062. 0.1604
|
|
74.40 0.8017 0.7833 0.0316 0.0324 0.481 4.327 1.898 358.382 0.489 8.440 2.402 0.40 180818. 0.1387
|
|
77.50 0.8351 0.7618 0.0253 0.0277 0.412 3.708 1.518 307.073 0.419 6.753 2.242 0.40 181600. 0.1158
|
|
80.60 0.8685 0.7216 0.0190 0.0228 0.339 3.049 1.137 252.509 0.344 5.057 2.042 0.40 182407. 0.0913
|
|
83.70 0.9019 0.6452 0.0126 0.0176 0.261 2.353 0.756 194.901 0.266 3.361 1.758 0.40 183239. 0.0641
|
|
86.80 0.9353 0.4824 0.0063 0.0122 0.180 1.624 0.376 134.524 0.184 1.672 1.268 0.41 184095. 0.0326
|
|
89.90 0.9687 -0.0018 0.0000 0.0065 0.096 0.864 -0.001 71.580 0.098 -0.003 -0.005 0.41 184958. 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 0.1205 0.0495 1.097 8.643 9.443 818.020 0.976 42.004 5.236 0.44 194284. 0.6744
|
|
3.55 0.0334 0.0787 0.1197 0.0508 1.126 8.872 9.380 839.705 1.002 41.721 5.067 0.44 194464. 0.6503
|
|
7.09 0.0669 0.1522 0.1188 0.0522 1.156 9.107 9.306 862.004 1.029 41.394 4.897 0.44 194669. 0.6261
|
|
10.64 0.1003 0.2204 0.1177 0.0535 1.186 9.345 9.221 884.544 1.056 41.013 4.728 0.44 194897. 0.6017
|
|
14.18 0.1337 0.2836 0.1164 0.0549 1.216 9.582 9.121 906.908 1.083 40.571 4.562 0.44 195152. 0.5774
|
|
17.73 0.1671 0.3418 0.1149 0.0562 1.245 9.811 9.006 928.613 1.108 40.060 4.399 0.44 195435. 0.5533
|
|
21.27 0.2006 0.3954 0.1133 0.0574 1.273 10.028 8.874 949.127 1.133 39.470 4.241 0.45 195747. 0.5294
|
|
24.82 0.2340 0.4447 0.1113 0.0586 1.298 10.226 8.722 967.877 1.155 38.793 4.087 0.45 196088. 0.5059
|
|
28.36 0.2674 0.4898 0.1091 0.0596 1.320 10.399 8.548 984.257 1.175 38.021 3.939 0.45 196460. 0.4827
|
|
31.91 0.3008 0.5311 0.1066 0.0604 1.338 10.540 8.351 997.649 1.191 37.146 3.797 0.45 196863. 0.4599
|
|
35.45 0.3343 0.5689 0.1038 0.0610 1.351 10.644 8.130 1007.414 1.203 36.160 3.660 0.45 197298. 0.4374
|
|
39.00 0.3677 0.6034 0.1006 0.0613 1.358 10.702 7.881 1012.904 1.209 35.057 3.529 0.45 197764. 0.4153
|
|
42.54 0.4011 0.6348 0.0971 0.0613 1.359 10.707 7.605 1013.448 1.210 33.829 3.404 0.45 198262. 0.3934
|
|
46.09 0.4345 0.6634 0.0932 0.0610 1.352 10.654 7.300 1008.352 1.204 32.470 3.284 0.45 198792. 0.3718
|
|
49.63 0.4680 0.6894 0.0889 0.0603 1.337 10.533 6.964 996.962 1.190 30.976 3.168 0.45 199354. 0.3504
|
|
53.18 0.5014 0.7128 0.0842 0.0592 1.313 10.342 6.599 978.829 1.168 29.350 3.058 0.45 199947. 0.3292
|
|
56.72 0.5348 0.7339 0.0792 0.0577 1.279 10.078 6.206 953.853 1.139 27.605 2.951 0.45 200572. 0.3081
|
|
60.27 0.5682 0.7525 0.0739 0.0558 1.237 9.743 5.791 922.200 1.101 25.759 2.848 0.45 201227. 0.2873
|
|
63.81 0.6017 0.7688 0.0684 0.0535 1.186 9.341 5.357 884.134 1.055 23.827 2.748 0.45 201913. 0.2666
|
|
67.36 0.6351 0.7825 0.0626 0.0508 1.126 8.874 4.907 839.907 1.003 21.825 2.650 0.45 202630. 0.2460
|
|
70.90 0.6685 0.7933 0.0567 0.0478 1.059 8.344 4.444 789.729 0.943 19.766 2.552 0.45 203377. 0.2255
|
|
74.45 0.7019 0.8009 0.0507 0.0444 0.984 7.752 3.970 733.764 0.876 17.658 2.454 0.46 204154. 0.2049
|
|
77.99 0.7354 0.8045 0.0445 0.0407 0.901 7.102 3.487 672.156 0.802 15.509 2.353 0.46 204960. 0.1841
|
|
81.54 0.7688 0.8030 0.0382 0.0366 0.811 6.392 2.996 605.039 0.722 13.328 2.246 0.46 205797. 0.1630
|
|
85.08 0.8022 0.7943 0.0319 0.0322 0.714 5.627 2.500 532.560 0.636 11.121 2.129 0.46 206662. 0.1411
|
|
88.63 0.8356 0.7748 0.0255 0.0275 0.610 4.806 2.000 454.902 0.543 8.896 1.994 0.46 207557. 0.1182
|
|
92.17 0.8691 0.7371 0.0191 0.0225 0.499 3.933 1.497 372.302 0.444 6.660 1.824 0.46 208481. 0.0936
|
|
95.72 0.9025 0.6639 0.0127 0.0173 0.382 3.012 0.994 285.083 0.340 4.423 1.582 0.46 209433. 0.0661
|
|
99.26 0.9359 0.5031 0.0063 0.0117 0.260 2.046 0.494 193.664 0.231 2.196 1.156 0.46 210412. 0.0340
|
|
102.81 0.9693 -0.0072 0.0000 0.0060 0.132 1.039 -0.003 98.321 0.117 -0.015 -0.016 0.46 211397. 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 0.1210 0.0495 1.562 10.941 12.000 1165.039 1.236 53.375 4.672 0.50 218559. 0.6783
|
|
4.02 0.0337 0.0796 0.1202 0.0509 1.605 11.238 11.923 1196.674 1.270 53.033 4.519 0.50 218764. 0.6540
|
|
8.04 0.0674 0.1538 0.1193 0.0522 1.648 11.545 11.833 1229.276 1.304 52.633 4.366 0.50 218995. 0.6295
|
|
12.06 0.1010 0.2227 0.1183 0.0537 1.693 11.855 11.728 1262.292 1.339 52.166 4.214 0.50 219255. 0.6049
|
|
16.08 0.1347 0.2864 0.1170 0.0550 1.737 12.163 11.605 1295.094 1.374 51.620 4.064 0.50 219544. 0.5803
|
|
20.09 0.1684 0.3451 0.1156 0.0564 1.779 12.462 11.462 1326.963 1.408 50.983 3.918 0.50 219866. 0.5559
|
|
24.11 0.2021 0.3991 0.1139 0.0577 1.820 12.745 11.296 1357.098 1.440 50.245 3.775 0.50 220220. 0.5318
|
|
28.13 0.2358 0.4486 0.1120 0.0589 1.857 13.004 11.104 1384.633 1.469 49.392 3.638 0.50 220609. 0.5080
|
|
32.15 0.2695 0.4940 0.1098 0.0599 1.889 13.229 10.885 1408.663 1.495 48.415 3.505 0.50 221033. 0.4846
|
|
36.17 0.3031 0.5355 0.1072 0.0607 1.915 13.413 10.634 1428.255 1.515 47.302 3.377 0.50 221493. 0.4616
|
|
40.19 0.3368 0.5735 0.1044 0.0613 1.934 13.547 10.351 1442.459 1.530 46.043 3.255 0.50 221989. 0.4389
|
|
44.21 0.3705 0.6081 0.1012 0.0616 1.945 13.620 10.034 1450.308 1.539 44.629 3.138 0.50 222521. 0.4166
|
|
48.23 0.4042 0.6397 0.0976 0.0617 1.946 13.625 9.679 1450.811 1.539 43.052 3.026 0.50 223089. 0.3946
|
|
52.24 0.4379 0.6685 0.0936 0.0613 1.935 13.551 9.286 1442.939 1.531 41.302 2.919 0.50 223694. 0.3728
|
|
56.26 0.4715 0.6946 0.0893 0.0606 1.912 13.390 8.852 1425.743 1.513 39.375 2.816 0.51 224336. 0.3512
|
|
60.28 0.5052 0.7182 0.0845 0.0594 1.876 13.135 8.380 1398.593 1.484 37.276 2.718 0.51 225013. 0.3297
|
|
64.30 0.5389 0.7395 0.0794 0.0579 1.826 12.785 7.874 1361.378 1.444 35.022 2.623 0.51 225726. 0.3085
|
|
68.32 0.5726 0.7584 0.0740 0.0559 1.763 12.344 7.337 1314.376 1.395 32.637 2.532 0.51 226474. 0.2875
|
|
72.34 0.6063 0.7749 0.0683 0.0535 1.687 11.814 6.777 1257.980 1.335 30.142 2.443 0.51 227257. 0.2666
|
|
76.36 0.6400 0.7888 0.0625 0.0507 1.599 11.200 6.196 1192.564 1.265 27.558 2.356 0.51 228075. 0.2458
|
|
80.38 0.6736 0.7999 0.0564 0.0475 1.500 10.504 5.598 1118.433 1.187 24.899 2.270 0.51 228928. 0.2251
|
|
84.40 0.7073 0.8078 0.0503 0.0440 1.389 9.728 4.986 1035.828 1.099 22.177 2.183 0.51 229814. 0.2043
|
|
88.41 0.7410 0.8116 0.0440 0.0402 1.267 8.874 4.362 944.956 1.003 19.404 2.094 0.51 230735. 0.1833
|
|
92.43 0.7747 0.8102 0.0376 0.0360 1.135 7.945 3.729 846.021 0.898 16.589 1.999 0.51 231689. 0.1618
|
|
96.45 0.8084 0.8015 0.0312 0.0314 0.991 6.943 3.089 739.243 0.784 13.741 1.895 0.52 232676. 0.1396
|
|
100.47 0.8420 0.7812 0.0246 0.0266 0.838 5.869 2.444 624.906 0.663 10.870 1.774 0.52 233697. 0.1162
|
|
104.49 0.8757 0.7411 0.0181 0.0214 0.675 4.727 1.795 503.379 0.534 7.986 1.618 0.52 234751. 0.0909
|
|
108.51 0.9094 0.6598 0.0116 0.0159 0.503 3.523 1.147 375.166 0.398 5.103 1.387 0.52 235837. 0.0623
|
|
112.53 0.9431 0.4667 0.0051 0.0102 0.323 2.263 0.502 240.919 0.256 2.235 0.946 0.52 236953. 0.0281
|
|
116.55 0.9768
|
|
|
|
|
|
|
|
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 0.1215 0.0496 2.149 13.542 14.879 1602.193 1.530 66.184 4.212 0.56 242832. 0.6810
|
|
4.46 0.0336 0.0797 0.1208 0.0510 2.208 13.915 14.790 1646.327 1.572 65.788 4.075 0.56 243058. 0.6568
|
|
8.92 0.0673 0.1539 0.1200 0.0524 2.269 14.301 14.686 1691.925 1.616 65.322 3.937 0.56 243313. 0.6323
|
|
13.38 0.1009 0.2229 0.1190 0.0539 2.331 14.692 14.563 1738.216 1.660 64.775 3.800 0.56 243601. 0.6078
|
|
17.84 0.1346 0.2866 0.1178 0.0553 2.393 15.082 14.418 1784.322 1.704 64.132 3.665 0.56 243922. 0.5833
|
|
22.30 0.1682 0.3454 0.1164 0.0567 2.453 15.461 14.248 1829.225 1.747 63.376 3.533 0.56 244278. 0.5589
|
|
26.76 0.2018 0.3994 0.1148 0.0580 2.510 15.821 14.050 1871.794 1.787 62.494 3.405 0.56 244671. 0.5348
|
|
31.22 0.2355 0.4490 0.1129 0.0592 2.562 16.151 13.819 1910.812 1.825 61.469 3.280 0.56 245103. 0.5111
|
|
35.68 0.2691 0.4944 0.1107 0.0603 2.608 16.440 13.554 1944.989 1.857 60.287 3.161 0.56 245573. 0.4877
|
|
40.14 0.3028 0.5360 0.1082 0.0611 2.646 16.676 13.250 1973.008 1.884 58.935 3.046 0.56 246083. 0.4647
|
|
44.60 0.3364 0.5741 0.1054 0.0618 2.673 16.850 12.905 1993.532 1.904 57.399 2.936 0.56 246633. 0.4420
|
|
49.06 0.3700 0.6088 0.1022 0.0621 2.689 16.949 12.515 2005.212 1.915 55.669 2.831 0.56 247224. 0.4197
|
|
53.52 0.4037 0.6406 0.0987 0.0622 2.691 16.961 12.080 2006.662 1.916 53.732 2.730 0.56 247855. 0.3977
|
|
57.98 0.4373 0.6696 0.0947 0.0619 2.677 16.875 11.596 1996.469 1.906 51.577 2.634 0.56 248527. 0.3760
|
|
62.44 0.4710 0.6959 0.0903 0.0611 2.646 16.679 11.061 1973.299 1.884 49.200 2.542 0.56 249239. 0.3544
|
|
66.90 0.5046 0.7198 0.0856 0.0600 2.597 16.366 10.478 1936.253 1.849 46.604 2.454 0.56 249991. 0.3330
|
|
71.36 0.5382 0.7414 0.0805 0.0584 2.528 15.934 9.850 1885.141 1.800 43.812 2.370 0.56 250783. 0.3117
|
|
75.82 0.5719 0.7606 0.0750 0.0564 2.441 15.386 9.185 1820.339 1.738 40.853 2.288 0.56 251613. 0.2907
|
|
80.28 0.6055 0.7776 0.0693 0.0540 2.337 14.727 8.488 1742.402 1.664 37.754 2.209 0.57 252483. 0.2698
|
|
84.74 0.6392 0.7921 0.0634 0.0512 2.215 13.962 7.765 1651.862 1.577 34.540 2.132 0.57 253390. 0.2490
|
|
89.20 0.6728 0.8038 0.0574 0.0480 2.077 13.094 7.021 1549.157 1.479 31.230 2.056 0.57 254336. 0.2283
|
|
93.66 0.7064 0.8125 0.0511 0.0445 1.924 12.126 6.259 1434.633 1.370 27.841 1.979 0.57 255320. 0.2075
|
|
98.12 0.7401 0.8174 0.0448 0.0405 1.755 11.060 5.482 1308.581 1.250 24.385 1.900 0.57 256341. 0.1865
|
|
102.58 0.7737 0.8173 0.0383 0.0363 1.571 9.900 4.693 1171.282 1.118 20.876 1.817 0.57 257399. 0.1650
|
|
107.04 0.8074 0.8102 0.0318 0.0317 1.372 8.647 3.895 1023.045 0.977 17.323 1.727 0.57 258495. 0.1428
|
|
111.50 0.8410 0.7924 0.0252 0.0268 1.159 7.305 3.089 864.253 0.825 13.740 1.621 0.57 259627. 0.1194
|
|
115.96 0.8746 0.7558 0.0186 0.0215 0.933 5.878 2.280 695.416 0.664 10.140 1.487 0.58 260795. 0.0941
|
|
120.42 0.9083 0.6805 0.0120 0.0160 0.694 4.372 1.470 517.227 0.494 6.538 1.289 0.58 262000. 0.0655
|
|
124.88 0.9419 0.4987 0.0054 0.0102 0.443 2.794 0.664 330.588 0.316 2.953 0.911 0.58 263238. 0.0311
|
|
129.34 0.9756
|
|
|
|
|
|
|
|
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 0.1221 0.0499 2.873 16.464 18.089 2142.630 1.860 80.458 3.829 0.61 267100. 0.6826
|
|
4.88 0.0335 0.0792 0.1214 0.0513 2.953 16.921 17.990 2202.116 1.912 80.018 3.705 0.61 267346. 0.6587
|
|
9.76 0.0669 0.1532 0.1207 0.0527 3.036 17.395 17.873 2263.782 1.965 79.498 3.581 0.61 267625. 0.6345
|
|
14.63 0.1004 0.2218 0.1197 0.0542 3.120 17.877 17.734 2326.605 2.020 78.883 3.457 0.61 267938. 0.6102
|
|
19.51 0.1338 0.2853 0.1186 0.0556 3.204 18.360 17.570 2389.397 2.074 78.153 3.335 0.61 268287. 0.5860
|
|
24.39 0.1673 0.3439 0.1173 0.0571 3.287 18.831 17.376 2450.780 2.128 77.290 3.216 0.61 268676. 0.5618
|
|
29.27 0.2007 0.3977 0.1158 0.0584 3.365 19.280 17.148 2509.213 2.178 76.274 3.100 0.61 269104. 0.5380
|
|
34.15 0.2342 0.4472 0.1140 0.0597 3.437 19.694 16.881 2563.026 2.225 75.085 2.987 0.61 269574. 0.5144
|
|
39.03 0.2676 0.4926 0.1119 0.0608 3.501 20.058 16.570 2610.464 2.266 73.706 2.879 0.61 270087. 0.4912
|
|
43.90 0.3011 0.5342 0.1095 0.0617 3.553 20.360 16.213 2649.728 2.300 72.117 2.775 0.61 270643. 0.4684
|
|
48.78 0.3345 0.5723 0.1067 0.0624 3.593 20.585 15.806 2679.009 2.326 70.304 2.676 0.61 271244. 0.4459
|
|
53.66 0.3680 0.6072 0.1036 0.0628 3.616 20.719 15.344 2696.481 2.341 68.252 2.581 0.62 271888. 0.4238
|
|
58.54 0.4014 0.6391 0.1001 0.0629 3.621 20.749 14.826 2700.303 2.344 65.947 2.490 0.62 272577. 0.4019
|
|
63.42 0.4349 0.6683 0.0962 0.0626 3.605 20.659 14.248 2688.591 2.334 63.376 2.404 0.62 273310. 0.3803
|
|
68.30 0.4683 0.6949 0.0919 0.0619 3.567 20.436 13.608 2659.555 2.309 60.530 2.321 0.62 274087. 0.3588
|
|
73.17 0.5018 0.7191 0.0871 0.0608 3.503 20.069 12.908 2611.899 2.267 57.414 2.242 0.62 274907. 0.3375
|
|
78.05 0.5352 0.7410 0.0820 0.0593 3.413 19.558 12.152 2545.277 2.210 54.052 2.166 0.62 275770. 0.3164
|
|
82.93 0.5687 0.7607 0.0766 0.0573 3.299 18.903 11.349 2460.125 2.136 50.479 2.092 0.62 276676. 0.2954
|
|
87.81 0.6021 0.7782 0.0709 0.0549 3.161 18.112 10.506 2357.202 2.046 46.730 2.022 0.62 277624. 0.2746
|
|
92.69 0.6356 0.7933 0.0650 0.0521 3.000 17.191 9.630 2237.248 1.942 42.836 1.952 0.62 278614. 0.2539
|
|
97.57 0.6690 0.8059 0.0589 0.0489 2.817 16.143 8.727 2100.877 1.824 38.820 1.884 0.62 279646. 0.2333
|
|
102.44 0.7025 0.8156 0.0527 0.0454 2.613 14.973 7.802 1948.575 1.692 34.703 1.816 0.63 280718. 0.2126
|
|
107.32 0.7359 0.8218 0.0463 0.0415 2.388 13.683 6.857 1780.746 1.546 30.501 1.747 0.63 281831. 0.1917
|
|
112.20 0.7694 0.8234 0.0398 0.0372 2.143 12.277 5.897 1597.763 1.387 26.230 1.674 0.63 282984. 0.1704
|
|
117.08 0.8028 0.8188 0.0332 0.0326 1.877 10.758 4.924 1400.028 1.215 21.903 1.595 0.63 284178. 0.1484
|
|
121.96 0.8363 0.8047 0.0266 0.0277 1.593 9.129 3.942 1188.035 1.031 17.534 1.505 0.63 285411. 0.1252
|
|
126.84 0.8697 0.7741 0.0199 0.0224 1.291 7.395 2.954 962.430 0.836 13.140 1.392 0.63 286684. 0.1003
|
|
131.71 0.9032 0.7106 0.0133 0.0169 0.971 5.564 1.965 724.097 0.629 8.739 1.231 0.64 287996. 0.0723
|
|
136.59 0.9366 0.5605 0.0066 0.0110 0.636 3.644 0.979 474.204 0.412 4.353 0.936 0.64 289345. 0.0388
|
|
141.47 0.9701 -0.0021 0.0000 0.0050 0.286 1.639 -0.002 213.363 0.185 -0.007 -0.003 0.64 290693. 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 0.1227 0.0504 3.768 19.792 21.632 2809.911 2.236 96.219 3.492 0.67 291364. 0.6807
|
|
5.32 0.0335 0.0789 0.1221 0.0518 3.873 20.340 21.526 2887.727 2.298 95.746 3.381 0.67 291632. 0.6574
|
|
10.65 0.0669 0.1526 0.1214 0.0532 3.981 20.910 21.399 2968.676 2.362 95.184 3.269 0.67 291934. 0.6339
|
|
15.97 0.1004 0.2211 0.1205 0.0547 4.092 21.493 21.248 3051.434 2.428 94.511 3.158 0.67 292275. 0.6102
|
|
21.29 0.1339 0.2846 0.1195 0.0562 4.203 22.078 21.066 3134.455 2.494 93.704 3.048 0.67 292655. 0.5864
|
|
26.62 0.1673 0.3431 0.1183 0.0577 4.313 22.651 20.849 3215.921 2.559 92.738 2.941 0.67 293078. 0.5627
|
|
31.94 0.2008 0.3971 0.1168 0.0591 4.417 23.200 20.591 3293.796 2.621 91.588 2.835 0.67 293545. 0.5393
|
|
37.27 0.2342 0.4466 0.1151 0.0604 4.514 23.707 20.285 3365.848 2.678 90.230 2.734 0.67 294058. 0.5160
|
|
42.59 0.2677 0.4921 0.1130 0.0615 4.599 24.157 19.928 3429.718 2.729 88.638 2.635 0.67 294618. 0.4931
|
|
47.91 0.3012 0.5337 0.1107 0.0625 4.671 24.532 19.512 3482.961 2.772 86.791 2.541 0.67 295226. 0.4704
|
|
53.24 0.3346 0.5719 0.1080 0.0632 4.725 24.815 19.035 3523.078 2.804 84.667 2.451 0.67 295882. 0.4481
|
|
58.56 0.3681 0.6069 0.1049 0.0636 4.757 24.987 18.491 3547.567 2.823 82.249 2.364 0.67 296587. 0.4261
|
|
63.88 0.4016 0.6390 0.1014 0.0637 4.766 25.032 17.878 3553.905 2.828 79.519 2.282 0.67 297340. 0.4043
|
|
69.21 0.4350 0.6683 0.0975 0.0635 4.747 24.931 17.190 3539.549 2.817 76.462 2.203 0.67 298142. 0.3828
|
|
74.53 0.4685 0.6951 0.0932 0.0628 4.696 24.667 16.427 3502.117 2.787 73.067 2.127 0.67 298991. 0.3614
|
|
79.86 0.5019 0.7196 0.0884 0.0617 4.613 24.229 15.589 3439.869 2.737 69.339 2.055 0.67 299888. 0.3401
|
|
85.18 0.5354 0.7418 0.0833 0.0601 4.496 23.612 14.682 3352.299 2.668 65.307 1.987 0.68 300832. 0.3190
|
|
90.50 0.5689 0.7619 0.0778 0.0581 4.345 22.821 13.717 3239.981 2.578 61.013 1.920 0.68 301823. 0.2981
|
|
95.83 0.6023 0.7798 0.0721 0.0557 4.162 21.863 12.702 3103.945 2.470 56.500 1.856 0.68 302860. 0.2773
|
|
101.15 0.6358 0.7954 0.0661 0.0528 3.950 20.745 11.647 2945.210 2.344 51.806 1.794 0.68 303942. 0.2566
|
|
106.47 0.6693 0.8085 0.0599 0.0496 3.707 19.473 10.558 2764.630 2.200 46.961 1.732 0.68 305069. 0.2359
|
|
111.80 0.7027 0.8189 0.0535 0.0460 3.437 18.052 9.440 2562.871 2.039 41.991 1.671 0.68 306241. 0.2151
|
|
117.12 0.7362 0.8258 0.0471 0.0420 3.139 16.485 8.299 2340.474 1.862 36.915 1.608 0.68 307457. 0.1942
|
|
122.44 0.7697 0.8284 0.0405 0.0376 2.813 14.777 7.138 2097.936 1.669 31.751 1.543 0.69 308717. 0.1728
|
|
127.77 0.8031 0.8250 0.0338 0.0329 2.462 12.930 5.961 1835.791 1.461 26.517 1.473 0.69 310021. 0.1507
|
|
133.09 0.8366 0.8124 0.0271 0.0279 2.085 10.951 4.773 1554.694 1.237 21.229 1.392 0.69 311368. 0.1275
|
|
138.42 0.8700 0.7840 0.0203 0.0225 1.684 8.843 3.576 1255.520 0.999 15.907 1.292 0.69 312758. 0.1024
|
|
143.74 0.9035 0.7232 0.0135 0.0168 1.260 6.618 2.377 939.543 0.748 10.574 1.148 0.69 314191. 0.0742
|
|
149.06 0.9370 0.5756 0.0067 0.0109 0.816 4.286 1.182 608.511 0.484 5.256 0.881 0.70 315664. 0.0401
|
|
154.39 0.9704 -0.0093 0.0000 0.0047 0.353 1.855 -0.008 263.391 0.210 -0.036 -0.014 0.70 317129. 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 0.1233 0.0517 4.914 23.823 25.510 3664.135 2.692 113.470 3.158 0.72 315625. 0.6685
|
|
5.77 0.0335 0.0774 0.1228 0.0531 5.045 24.462 25.400 3762.329 2.764 112.981 3.062 0.72 315912. 0.6468
|
|
11.54 0.0669 0.1500 0.1221 0.0545 5.183 25.127 25.269 3864.615 2.839 112.396 2.966 0.72 316239. 0.6248
|
|
17.30 0.1004 0.2177 0.1214 0.0560 5.323 25.807 25.110 3969.264 2.916 111.690 2.869 0.72 316606. 0.6026
|
|
23.07 0.1339 0.2806 0.1204 0.0575 5.464 26.490 24.917 4074.241 2.993 110.831 2.774 0.72 317016. 0.5803
|
|
28.84 0.1673 0.3388 0.1193 0.0589 5.602 27.159 24.683 4177.160 3.068 109.790 2.680 0.72 317473. 0.5581
|
|
34.61 0.2008 0.3927 0.1179 0.0603 5.733 27.797 24.400 4275.383 3.141 108.532 2.589 0.72 317978. 0.5359
|
|
40.37 0.2343 0.4424 0.1163 0.0616 5.855 28.387 24.061 4366.066 3.207 107.025 2.500 0.72 318533. 0.5139
|
|
46.14 0.2677 0.4882 0.1144 0.0627 5.963 28.908 23.660 4446.263 3.266 105.238 2.414 0.72 319139. 0.4920
|
|
51.91 0.3012 0.5303 0.1121 0.0636 6.052 29.342 23.188 4512.918 3.315 103.141 2.331 0.73 319798. 0.4704
|
|
57.68 0.3346 0.5691 0.1094 0.0644 6.119 29.667 22.641 4562.925 3.352 100.708 2.251 0.73 320510. 0.4488
|
|
63.44 0.3681 0.6046 0.1064 0.0648 6.159 29.863 22.013 4593.132 3.374 97.915 2.174 0.73 321275. 0.4275
|
|
69.21 0.4016 0.6372 0.1029 0.0649 6.169 29.910 21.300 4600.351 3.379 94.740 2.100 0.73 322092. 0.4062
|
|
74.98 0.4350 0.6670 0.0991 0.0646 6.144 29.786 20.496 4581.311 3.365 91.166 2.029 0.73 322963. 0.3850
|
|
80.75 0.4685 0.6942 0.0947 0.0639 6.079 29.471 19.599 4532.830 3.330 87.178 1.961 0.73 323885. 0.3639
|
|
86.51 0.5020 0.7191 0.0900 0.0628 5.971 28.949 18.611 4452.478 3.271 82.784 1.896 0.73 324859. 0.3428
|
|
92.28 0.5354 0.7417 0.0848 0.0612 5.819 28.213 17.539 4339.340 3.188 78.015 1.833 0.73 325885. 0.3218
|
|
98.05 0.5689 0.7621 0.0792 0.0591 5.624 27.268 16.395 4193.953 3.081 72.924 1.773 0.73 326960. 0.3009
|
|
103.82 0.6024 0.7805 0.0734 0.0567 5.388 26.121 15.189 4017.519 2.951 67.562 1.715 0.74 328085. 0.2801
|
|
109.58 0.6358 0.7966 0.0673 0.0538 5.111 24.781 13.934 3811.392 2.800 61.977 1.658 0.74 329260. 0.2594
|
|
115.35 0.6693 0.8103 0.0611 0.0504 4.796 23.255 12.636 3576.722 2.627 56.205 1.602 0.74 330483. 0.2387
|
|
121.12 0.7028 0.8213 0.0546 0.0467 4.445 21.549 11.303 3314.420 2.435 50.277 1.547 0.74 331754. 0.2180
|
|
126.89 0.7362 0.8291 0.0480 0.0427 4.057 19.669 9.941 3025.200 2.222 44.219 1.490 0.74 333074. 0.1970
|
|
132.65 0.7697 0.8327 0.0413 0.0382 3.634 17.618 8.554 2709.738 1.990 38.050 1.432 0.74 334441. 0.1755
|
|
138.42 0.8032 0.8305 0.0345 0.0334 3.177 15.402 7.147 2368.888 1.740 31.792 1.369 0.75 335854. 0.1533
|
|
144.19 0.8366 0.8192 0.0277 0.0283 2.687 13.028 5.725 2003.776 1.472 25.465 1.296 0.75 337315. 0.1300
|
|
149.96 0.8701 0.7920 0.0207 0.0228 2.167 10.507 4.292 1615.979 1.187 19.091 1.205 0.75 338822. 0.1046
|
|
155.72 0.9035 0.7319 0.0138 0.0170 1.620 7.852 2.855 1207.707 0.887 12.698 1.072 0.75 340374. 0.0759
|
|
161.49 0.9370 0.5830 0.0069 0.0110 1.049 5.084 1.420 781.925 0.574 6.314 0.823 0.75 341970. 0.0411
|
|
167.26 0.9705 -0.0104 -0.0001 0.0048 0.457 2.215 -0.011 340.657 0.250 -0.047 -0.014 0.76 343555. 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 0.1238 0.0545 6.475 29.151 29.715 4828.507 3.293 132.173 2.791 0.78 339881. 0.6377
|
|
6.21 0.0335 0.0739 0.1234 0.0559 6.637 29.880 29.606 4949.301 3.376 131.688 2.713 0.78 340189. 0.6187
|
|
12.42 0.0669 0.1434 0.1228 0.0573 6.806 30.640 29.475 5075.096 3.462 131.106 2.634 0.78 340537. 0.5994
|
|
18.63 0.1004 0.2087 0.1222 0.0588 6.978 31.415 29.316 5203.522 3.549 130.396 2.555 0.78 340930. 0.5799
|
|
24.84 0.1338 0.2698 0.1214 0.0602 7.150 32.189 29.119 5331.740 3.637 129.523 2.477 0.78 341370. 0.5603
|
|
31.05 0.1673 0.3267 0.1203 0.0616 7.317 32.942 28.877 5456.418 3.722 128.447 2.400 0.78 341859. 0.5406
|
|
37.26 0.2007 0.3799 0.1191 0.0629 7.475 33.652 28.580 5573.929 3.802 127.123 2.326 0.78 342401. 0.5211
|
|
43.47 0.2342 0.4294 0.1176 0.0641 7.618 34.295 28.217 5680.515 3.875 125.510 2.253 0.78 342997. 0.5016
|
|
49.68 0.2677 0.4754 0.1158 0.0652 7.741 34.850 27.780 5772.444 3.937 123.564 2.183 0.78 343649. 0.4822
|
|
55.89 0.3011 0.5182 0.1136 0.0660 7.840 35.295 27.259 5846.121 3.988 121.248 2.115 0.78 344358. 0.4628
|
|
62.10 0.3346 0.5579 0.1111 0.0666 7.909 35.608 26.647 5897.990 4.023 118.528 2.049 0.78 345125. 0.4434
|
|
68.31 0.3680 0.5947 0.1081 0.0669 7.945 35.768 25.938 5924.517 4.041 115.371 1.986 0.78 345949. 0.4239
|
|
74.52 0.4015 0.6286 0.1047 0.0669 7.942 35.753 25.124 5922.071 4.039 111.752 1.924 0.78 346832. 0.4042
|
|
80.73 0.4349 0.6599 0.1009 0.0665 7.895 35.541 24.201 5886.939 4.015 107.645 1.865 0.78 347771. 0.3844
|
|
86.94 0.4684 0.6886 0.0965 0.0657 7.799 35.110 23.164 5815.479 3.967 103.035 1.807 0.79 348767. 0.3644
|
|
93.15 0.5019 0.7148 0.0918 0.0644 7.650 34.442 22.016 5704.826 3.891 97.928 1.750 0.79 349818. 0.3442
|
|
99.36 0.5353 0.7387 0.0865 0.0627 7.448 33.531 20.765 5553.896 3.788 92.362 1.696 0.79 350925. 0.3239
|
|
105.57 0.5688 0.7602 0.0810 0.0606 7.192 32.380 19.424 5363.301 3.658 86.399 1.643 0.79 352085. 0.3034
|
|
111.78 0.6022 0.7796 0.0751 0.0580 6.885 30.998 18.008 5134.380 3.502 80.102 1.591 0.79 353300. 0.2829
|
|
117.99 0.6357 0.7966 0.0689 0.0550 6.529 29.393 16.530 4868.539 3.321 73.527 1.540 0.79 354567. 0.2624
|
|
124.20 0.6691 0.8111 0.0625 0.0516 6.124 27.572 15.000 4566.936 3.115 66.721 1.490 0.79 355886. 0.2418
|
|
130.41 0.7026 0.8229 0.0560 0.0478 5.673 25.542 13.427 4230.688 2.886 59.722 1.439 0.80 357257. 0.2211
|
|
136.62 0.7361 0.8314 0.0492 0.0436 5.177 23.309 11.816 3860.814 2.633 52.559 1.388 0.80 358679. 0.2000
|
|
142.83 0.7695 0.8355 0.0424 0.0391 4.638 20.880 10.175 3458.419 2.359 45.258 1.334 0.80 360153. 0.1784
|
|
149.04 0.8030 0.8334 0.0355 0.0342 4.057 18.264 8.508 3025.255 2.064 37.842 1.276 0.80 361676. 0.1559
|
|
155.25 0.8364 0.8212 0.0284 0.0289 3.438 15.478 6.820 2563.664 1.749 30.334 1.207 0.80 363250. 0.1321
|
|
161.46 0.8699 0.7910 0.0213 0.0235 2.785 12.538 5.117 2076.751 1.417 22.760 1.118 0.81 364873. 0.1060
|
|
167.67 0.9033 0.7239 0.0142 0.0177 2.104 9.470 3.406 1568.618 1.070 15.151 0.985 0.81 366546. 0.0762
|
|
173.88 0.9368 0.5612 0.0071 0.0118 1.401 6.305 1.695 1044.364 0.712 7.540 0.736 0.81 368264. 0.0402
|
|
180.08 0.9703 -0.0087 -0.0001 0.0057 0.681 3.068 -0.012 508.112 0.347 -0.055 -0.011 0.81 369976. 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 0.1242 0.0598 8.734 36.698 34.220 6512.779 4.146 152.208 2.383 0.83 364132. 0.5843
|
|
6.66 0.0335 0.0678 0.1238 0.0611 8.931 37.526 34.114 6659.584 4.240 151.738 2.323 0.83 364459. 0.5688
|
|
13.31 0.0669 0.1321 0.1234 0.0625 9.136 38.388 33.988 6812.633 4.337 151.178 2.263 0.83 364830. 0.5529
|
|
19.97 0.1004 0.1928 0.1228 0.0640 9.345 39.267 33.834 6968.638 4.436 150.494 2.202 0.83 365248. 0.5369
|
|
26.63 0.1339 0.2500 0.1221 0.0654 9.553 40.140 33.643 7123.477 4.535 149.646 2.142 0.83 365716. 0.5208
|
|
33.28 0.1674 0.3040 0.1213 0.0668 9.752 40.977 33.404 7272.178 4.630 148.583 2.083 0.83 366237. 0.5047
|
|
39.94 0.2008 0.3548 0.1202 0.0680 9.936 41.750 33.105 7409.198 4.717 147.251 2.027 0.83 366815. 0.4887
|
|
46.59 0.2343 0.4028 0.1188 0.0691 10.096 42.424 32.732 7528.835 4.793 145.592 1.972 0.84 367452. 0.4728
|
|
53.25 0.2678 0.4481 0.1172 0.0700 10.226 42.969 32.273 7625.670 4.855 143.549 1.920 0.84 368149. 0.4570
|
|
59.91 0.3012 0.4910 0.1151 0.0706 10.319 43.361 31.715 7695.095 4.899 141.069 1.869 0.84 368909. 0.4412
|
|
66.56 0.3347 0.5314 0.1127 0.0710 10.370 43.575 31.049 7733.145 4.923 138.106 1.821 0.84 369731. 0.4253
|
|
73.22 0.3682 0.5696 0.1099 0.0710 10.375 43.593 30.265 7736.390 4.925 134.619 1.774 0.84 370617. 0.4091
|
|
79.88 0.4017 0.6054 0.1066 0.0707 10.328 43.397 29.356 7701.586 4.903 130.575 1.729 0.84 371565. 0.3926
|
|
86.53 0.4351 0.6389 0.1028 0.0700 10.226 42.967 28.314 7625.194 4.854 125.941 1.684 0.84 372574. 0.3756
|
|
93.19 0.4686 0.6701 0.0985 0.0689 10.062 42.280 27.135 7503.395 4.777 120.695 1.640 0.84 373645. 0.3581
|
|
99.84 0.5021 0.6990 0.0937 0.0673 9.834 41.323 25.819 7333.479 4.669 114.841 1.597 0.84 374776. 0.3401
|
|
106.50 0.5355 0.7255 0.0885 0.0653 9.541 40.091 24.376 7114.911 4.529 108.424 1.554 0.85 375967. 0.3216
|
|
113.16 0.5690 0.7498 0.0829 0.0629 9.185 38.594 22.823 6849.219 4.360 101.516 1.511 0.85 377215. 0.3026
|
|
119.81 0.6025 0.7716 0.0769 0.0600 8.768 36.844 21.177 6538.657 4.163 94.197 1.469 0.85 378521. 0.2833
|
|
126.47 0.6360 0.7910 0.0706 0.0568 8.294 34.852 19.455 6185.033 3.938 86.534 1.427 0.85 379883. 0.2637
|
|
133.13 0.6694 0.8078 0.0641 0.0532 7.764 32.623 17.667 5789.584 3.686 78.582 1.384 0.85 381301. 0.2438
|
|
139.78 0.7029 0.8215 0.0574 0.0492 7.180 30.168 15.825 5353.807 3.408 70.388 1.341 0.85 382775. 0.2235
|
|
146.44 0.7364 0.8308 0.0506 0.0448 6.549 27.519 13.935 4883.805 3.109 61.984 1.294 0.86 384303. 0.2025
|
|
153.09 0.7698 0.8337 0.0436 0.0402 5.879 24.701 12.005 4383.689 2.791 53.399 1.242 0.86 385885. 0.1804
|
|
159.75 0.8033 0.8284 0.0365 0.0354 5.164 21.699 10.042 3850.862 2.452 44.667 1.183 0.86 387521. 0.1571
|
|
166.41 0.8368 0.8099 0.0292 0.0302 4.412 18.537 8.052 3289.675 2.094 35.814 1.110 0.86 389211. 0.1320
|
|
173.06 0.8703 0.7683 0.0219 0.0248 3.629 15.248 6.042 2705.988 1.723 26.873 1.013 0.86 390953. 0.1043
|
|
179.72 0.9037 0.6819 0.0146 0.0193 2.825 11.871 4.020 2106.778 1.341 17.881 0.865 0.87 392747. 0.0727
|
|
186.38 0.9372 0.4936 0.0073 0.0138 2.012 8.453 1.998 1500.105 0.955 8.888 0.604 0.87 394591. 0.0358
|
|
193.03 0.9707 -0.0068 -0.0001 0.0082 1.197 5.029 -0.016 892.521 0.568 -0.070 -0.008 0.87 396445. 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 0.1237 0.0665 11.791 46.450 38.769 8792.886 5.248 172.443 2.000 0.89 388415. 0.5219
|
|
7.17 0.0338 0.0615 0.1234 0.0679 12.032 47.398 38.665 8972.322 5.355 171.984 1.955 0.89 388765. 0.5094
|
|
14.34 0.0676 0.1200 0.1230 0.0693 12.286 48.397 38.545 9161.565 5.468 171.450 1.908 0.89 389161. 0.4966
|
|
21.51 0.1014 0.1756 0.1225 0.0708 12.546 49.423 38.400 9355.649 5.584 170.803 1.862 0.89 389608. 0.4835
|
|
28.69 0.1352 0.2283 0.1219 0.0722 12.807 50.449 38.220 9549.982 5.700 170.003 1.815 0.89 390109. 0.4703
|
|
35.86 0.1690 0.2782 0.1212 0.0737 13.059 51.443 37.994 9738.144 5.812 168.995 1.770 0.89 390667. 0.4572
|
|
43.03 0.2029 0.3255 0.1203 0.0750 13.292 52.362 37.706 9911.986 5.916 167.716 1.725 0.89 391286. 0.4441
|
|
50.20 0.2367 0.3704 0.1191 0.0761 13.494 53.156 37.341 10062.378 6.006 166.092 1.683 0.89 391970. 0.4311
|
|
57.37 0.2705 0.4133 0.1177 0.0770 13.651 53.777 36.881 10179.847 6.076 164.045 1.643 0.89 392720. 0.4182
|
|
64.54 0.3043 0.4544 0.1158 0.0776 13.753 54.176 36.308 10255.515 6.121 161.497 1.606 0.89 393538. 0.4055
|
|
71.72 0.3381 0.4938 0.1136 0.0778 13.788 54.316 35.606 10282.037 6.137 158.377 1.571 0.89 394427. 0.3928
|
|
78.89 0.3719 0.5318 0.1109 0.0776 13.751 54.168 34.762 10254.031 6.120 154.621 1.538 0.89 395385. 0.3800
|
|
86.06 0.4057 0.5682 0.1077 0.0769 13.635 53.713 33.763 10167.742 6.068 150.178 1.506 0.90 396413. 0.3668
|
|
93.23 0.4395 0.6031 0.1040 0.0758 13.437 52.933 32.599 10020.111 5.980 145.002 1.476 0.90 397510. 0.3531
|
|
100.40 0.4733 0.6363 0.0998 0.0742 13.154 51.816 31.265 9808.681 5.854 139.065 1.446 0.90 398675. 0.3388
|
|
107.57 0.5071 0.6678 0.0950 0.0721 12.783 50.355 29.759 9532.089 5.689 132.368 1.416 0.90 399906. 0.3238
|
|
114.74 0.5409 0.6973 0.0896 0.0695 12.328 48.563 28.097 9193.012 5.487 124.973 1.386 0.90 401201. 0.3080
|
|
121.92 0.5747 0.7248 0.0839 0.0665 11.795 46.462 26.297 8795.233 5.249 116.969 1.356 0.90 402561. 0.2915
|
|
129.09 0.6086 0.7501 0.0778 0.0631 11.188 44.072 24.381 8342.807 4.979 108.448 1.326 0.91 403983. 0.2743
|
|
136.26 0.6424 0.7731 0.0714 0.0593 10.513 41.414 22.369 7839.651 4.679 99.495 1.294 0.91 405466. 0.2565
|
|
143.43 0.6762 0.7933 0.0647 0.0551 9.775 38.505 20.275 7288.895 4.350 90.183 1.262 0.91 407010. 0.2381
|
|
150.60 0.7100 0.8105 0.0578 0.0506 8.975 35.353 18.114 6692.338 3.994 80.570 1.228 0.91 408613. 0.2190
|
|
157.77 0.7438 0.8219 0.0507 0.0459 8.134 32.044 15.892 6065.832 3.620 70.686 1.188 0.91 410276. 0.1985
|
|
164.94 0.7776 0.8198 0.0434 0.0412 7.302 28.765 13.610 5445.214 3.250 60.538 1.134 0.92 411997. 0.1753
|
|
172.12 0.8114 0.8030 0.0360 0.0364 6.450 25.408 11.284 4809.653 2.871 50.192 1.064 0.92 413777. 0.1498
|
|
179.29 0.8452 0.7658 0.0285 0.0314 5.573 21.952 8.926 4155.550 2.480 39.703 0.974 0.92 415613. 0.1220
|
|
186.46 0.8790 0.6950 0.0209 0.0264 4.684 18.451 6.548 3492.762 2.085 29.124 0.850 0.92 417506. 0.0912
|
|
193.63 0.9128 0.5664 0.0133 0.0214 3.797 14.957 4.165 2831.317 1.690 18.527 0.667 0.93 419456. 0.0571
|
|
200.80 0.9466 0.3296 0.0057 0.0165 2.925 11.524 1.801 2181.405 1.302 8.010 0.374 0.93 421458. 0.0211
|
|
207.97 0.9804
|
|
|
|
|
|
|