427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20x22.5EP(CD) (20x225EP(CD).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 0.1192 0.0686 0.018 1.113 0.608 13.171 0.126 2.704 20.937 0.08 42365. 0.4790
|
|
0.84 0.0444 0.0756 0.1189 0.0698 0.018 1.133 0.606 13.399 0.128 2.697 20.525 0.08 42416. 0.4689
|
|
1.68 0.0887 0.1478 0.1186 0.0712 0.018 1.155 0.605 13.664 0.130 2.690 20.074 0.08 42476. 0.4580
|
|
2.52 0.1331 0.2164 0.1183 0.0727 0.019 1.180 0.603 13.965 0.133 2.682 19.586 0.08 42546. 0.4462
|
|
3.36 0.1774 0.2808 0.1179 0.0745 0.019 1.209 0.601 14.303 0.137 2.674 19.066 0.08 42626. 0.4337
|
|
4.20 0.2218 0.3410 0.1175 0.0764 0.020 1.240 0.599 14.673 0.140 2.665 18.519 0.08 42717. 0.4205
|
|
5.04 0.2661 0.3966 0.1170 0.0785 0.020 1.274 0.596 15.071 0.144 2.653 17.951 0.08 42819. 0.4067
|
|
5.88 0.3105 0.4477 0.1163 0.0807 0.021 1.309 0.593 15.489 0.148 2.638 17.369 0.08 42934. 0.3924
|
|
6.72 0.3548 0.4943 0.1155 0.0829 0.021 1.345 0.589 15.916 0.152 2.619 16.779 0.08 43061. 0.3777
|
|
7.56 0.3992 0.5366 0.1144 0.0851 0.022 1.381 0.583 16.338 0.156 2.594 16.190 0.08 43201. 0.3627
|
|
8.40 0.4435 0.5747 0.1130 0.0872 0.022 1.415 0.576 16.739 0.160 2.562 15.607 0.08 43353. 0.3475
|
|
9.24 0.4879 0.6090 0.1112 0.0890 0.023 1.445 0.567 17.100 0.163 2.521 15.036 0.08 43519. 0.3321
|
|
10.08 0.5322 0.6398 0.1089 0.0906 0.023 1.471 0.555 17.400 0.166 2.471 14.480 0.08 43699. 0.3166
|
|
10.92 0.5766 0.6674 0.1062 0.0918 0.024 1.489 0.542 17.619 0.168 2.409 13.942 0.08 43891. 0.3010
|
|
11.76 0.6209 0.6921 0.1029 0.0924 0.024 1.499 0.525 17.735 0.169 2.335 13.424 0.08 44097. 0.2853
|
|
12.60 0.6653 0.7140 0.0991 0.0923 0.024 1.498 0.505 17.725 0.169 2.247 12.926 0.08 44316. 0.2695
|
|
13.44 0.7096 0.7334 0.0945 0.0914 0.024 1.484 0.482 17.560 0.168 2.144 12.448 0.08 44548. 0.2535
|
|
14.28 0.7540 0.7505 0.0892 0.0897 0.023 1.455 0.455 17.217 0.164 2.024 11.988 0.08 44792. 0.2373
|
|
15.12 0.7983 0.7651 0.0833 0.0869 0.022 1.411 0.425 16.692 0.159 1.890 11.543 0.08 45049. 0.2207
|
|
15.96 0.8427 0.7770 0.0768 0.0833 0.021 1.352 0.392 15.994 0.153 1.742 11.105 0.08 45318. 0.2039
|
|
16.80 0.8870 0.7855 0.0698 0.0789 0.020 1.280 0.356 15.141 0.145 1.584 10.666 0.08 45599. 0.1867
|
|
17.64 0.9314 0.7898 0.0625 0.0737 0.019 1.196 0.319 14.151 0.135 1.417 10.214 0.08 45891. 0.1691
|
|
18.48 0.9757 0.7886 0.0549 0.0679 0.017 1.102 0.280 13.038 0.125 1.245 9.735 0.08 46194. 0.1511
|
|
19.32 1.0201 0.7801 0.0471 0.0615 0.016 0.999 0.240 11.817 0.113 1.067 9.211 0.08 46508. 0.1324
|
|
20.16 1.0644 0.7613 0.0391 0.0547 0.014 0.888 0.199 10.502 0.100 0.887 8.615 0.08 46833. 0.1129
|
|
21.00 1.1088 0.7275 0.0311 0.0474 0.012 0.770 0.159 9.105 0.087 0.706 7.902 0.08 47169. 0.0923
|
|
21.84 1.1531 0.6698 0.0231 0.0398 0.010 0.646 0.118 7.642 0.073 0.524 6.996 0.08 47514. 0.0705
|
|
22.68 1.1975 0.5707 0.0152 0.0319 0.008 0.518 0.078 6.127 0.059 0.345 5.740 0.08 47870. 0.0469
|
|
23.52 1.2418 0.3886 0.0075 0.0238 0.006 0.387 0.038 4.580 0.044 0.169 3.769 0.09 48235. 0.0216
|
|
24.36 1.2862 -0.0027 0.0000 0.0157 0.004 0.255 0.000 3.017 0.029 -0.001 -0.026 0.09 48610. 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 0.1195 0.0654 0.135 4.245 2.438 100.436 0.480 10.843 11.009 0.16 84729. 0.5043
|
|
1.69 0.0446 0.0798 0.1192 0.0666 0.137 4.323 2.432 102.294 0.488 10.816 10.782 0.16 84832. 0.4933
|
|
3.38 0.0892 0.1560 0.1189 0.0680 0.140 4.414 2.426 104.450 0.499 10.790 10.534 0.16 84953. 0.4813
|
|
5.07 0.1337 0.2280 0.1186 0.0696 0.143 4.518 2.420 106.910 0.510 10.763 10.266 0.16 85093. 0.4685
|
|
6.75 0.1783 0.2955 0.1183 0.0714 0.147 4.635 2.413 109.667 0.524 10.733 9.980 0.16 85254. 0.4548
|
|
8.44 0.2229 0.3583 0.1179 0.0734 0.151 4.763 2.405 112.699 0.538 10.698 9.680 0.16 85438. 0.4404
|
|
10.13 0.2675 0.4161 0.1174 0.0755 0.156 4.901 2.395 115.965 0.554 10.654 9.369 0.16 85644. 0.4254
|
|
11.82 0.3120 0.4690 0.1168 0.0777 0.160 5.046 2.382 119.402 0.570 10.597 9.050 0.16 85875. 0.4098
|
|
13.51 0.3566 0.5170 0.1160 0.0800 0.165 5.195 2.366 122.922 0.587 10.523 8.729 0.16 86132. 0.3939
|
|
15.20 0.4012 0.5603 0.1149 0.0823 0.170 5.342 2.344 126.414 0.604 10.425 8.409 0.16 86414. 0.3777
|
|
16.89 0.4458 0.5991 0.1135 0.0845 0.174 5.483 2.315 129.742 0.619 10.298 8.094 0.16 86722. 0.3613
|
|
18.57 0.4904 0.6340 0.1117 0.0864 0.178 5.610 2.279 132.753 0.634 10.136 7.786 0.16 87058. 0.3448
|
|
20.26 0.5349 0.6651 0.1095 0.0881 0.181 5.717 2.233 135.279 0.646 9.933 7.487 0.16 87420. 0.3283
|
|
21.95 0.5795 0.6929 0.1067 0.0893 0.184 5.796 2.177 137.146 0.655 9.684 7.200 0.16 87809. 0.3117
|
|
23.64 0.6241 0.7177 0.1034 0.0899 0.185 5.839 2.110 138.174 0.660 9.384 6.925 0.16 88224. 0.2951
|
|
25.33 0.6687 0.7398 0.0995 0.0899 0.185 5.839 2.030 138.161 0.660 9.027 6.663 0.16 88666. 0.2785
|
|
27.02 0.7133 0.7595 0.0949 0.0891 0.184 5.785 1.935 136.880 0.654 8.608 6.413 0.16 89134. 0.2617
|
|
28.71 0.7578 0.7770 0.0895 0.0873 0.180 5.669 1.826 134.141 0.640 8.122 6.174 0.16 89628. 0.2448
|
|
30.39 0.8024 0.7923 0.0835 0.0846 0.174 5.490 1.703 129.901 0.620 7.575 5.946 0.16 90147. 0.2276
|
|
32.08 0.8470 0.8052 0.0769 0.0809 0.167 5.251 1.568 124.248 0.593 6.975 5.725 0.16 90690. 0.2103
|
|
33.77 0.8916 0.8153 0.0698 0.0764 0.157 4.958 1.424 117.314 0.560 6.335 5.506 0.16 91256. 0.1928
|
|
35.46 0.9361 0.8217 0.0624 0.0711 0.146 4.616 1.273 109.235 0.522 5.663 5.286 0.17 91846. 0.1750
|
|
37.15 0.9807 0.8236 0.0547 0.0652 0.134 4.232 1.116 100.132 0.478 4.966 5.057 0.17 92458. 0.1568
|
|
38.84 1.0253 0.8193 0.0469 0.0587 0.121 3.809 0.956 90.121 0.430 4.253 4.812 0.17 93092. 0.1381
|
|
40.53 1.0699 0.8063 0.0389 0.0516 0.106 3.352 0.794 79.309 0.379 3.530 4.538 0.17 93748. 0.1186
|
|
42.21 1.1145 0.7799 0.0309 0.0441 0.091 2.866 0.630 67.811 0.324 2.802 4.214 0.17 94425. 0.0981
|
|
43.90 1.1590 0.7316 0.0229 0.0363 0.075 2.356 0.467 55.749 0.266 2.078 3.801 0.17 95122. 0.0762
|
|
45.59 1.2036 0.6425 0.0150 0.0282 0.058 1.828 0.307 43.260 0.207 1.364 3.214 0.17 95839. 0.0522
|
|
47.28 1.2482 0.4619 0.0073 0.0199 0.041 1.289 0.150 30.495 0.146 0.666 2.228 0.17 96577. 0.0253
|
|
48.97 1.2928 -0.0081 -0.0001 0.0115 0.024 0.744 -0.001 17.616 0.084 -0.007 -0.038 0.17 97332. 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 0.1197 0.0641 0.446 9.367 5.494 332.470 1.058 24.436 7.495 0.24 127092. 0.5154
|
|
2.54 0.0447 0.0816 0.1194 0.0653 0.454 9.545 5.481 338.770 1.078 24.380 7.338 0.24 127247. 0.5040
|
|
5.07 0.0893 0.1594 0.1192 0.0668 0.464 9.751 5.469 346.092 1.102 24.325 7.167 0.24 127429. 0.4917
|
|
7.61 0.1340 0.2330 0.1189 0.0684 0.475 9.987 5.456 354.458 1.128 24.269 6.982 0.24 127639. 0.4785
|
|
10.15 0.1786 0.3019 0.1186 0.0702 0.488 10.251 5.442 363.850 1.158 24.207 6.784 0.24 127882. 0.4643
|
|
12.69 0.2233 0.3658 0.1182 0.0722 0.502 10.543 5.426 374.199 1.191 24.134 6.577 0.24 128157. 0.4494
|
|
15.22 0.2679 0.4246 0.1178 0.0743 0.517 10.857 5.405 385.370 1.227 24.042 6.362 0.24 128468. 0.4339
|
|
17.76 0.3126 0.4782 0.1172 0.0766 0.533 11.189 5.378 397.151 1.264 23.920 6.142 0.24 128815. 0.4179
|
|
20.30 0.3573 0.5268 0.1164 0.0789 0.549 11.530 5.342 409.249 1.303 23.760 5.920 0.24 129201. 0.4014
|
|
22.84 0.4019 0.5706 0.1154 0.0813 0.565 11.869 5.294 421.282 1.341 23.546 5.699 0.24 129626. 0.3847
|
|
25.37 0.4466 0.6098 0.1140 0.0835 0.580 12.193 5.231 432.789 1.378 23.267 5.482 0.24 130090. 0.3679
|
|
27.91 0.4912 0.6449 0.1122 0.0855 0.594 12.488 5.150 443.241 1.411 22.908 5.270 0.24 130594. 0.3509
|
|
30.45 0.5359 0.6762 0.1100 0.0872 0.606 12.736 5.049 452.061 1.439 22.456 5.066 0.24 131140. 0.3339
|
|
32.99 0.5806 0.7041 0.1073 0.0885 0.615 12.922 4.923 458.646 1.460 21.899 4.869 0.24 131725. 0.3170
|
|
35.52 0.6252 0.7290 0.1040 0.0892 0.620 13.027 4.772 462.368 1.472 21.225 4.681 0.24 132350. 0.3000
|
|
38.06 0.6699 0.7512 0.1000 0.0892 0.620 13.032 4.591 462.535 1.472 20.422 4.502 0.24 133016. 0.2830
|
|
40.60 0.7145 0.7711 0.0954 0.0884 0.615 12.914 4.378 458.359 1.459 19.473 4.332 0.24 133720. 0.2659
|
|
43.14 0.7592 0.7888 0.0900 0.0866 0.602 12.655 4.131 449.185 1.430 18.374 4.171 0.24 134463. 0.2487
|
|
45.67 0.8038 0.8045 0.0839 0.0839 0.583 12.252 3.852 434.861 1.384 17.134 4.018 0.25 135244. 0.2313
|
|
48.21 0.8485 0.8180 0.0773 0.0802 0.557 11.711 3.547 415.670 1.323 15.776 3.870 0.25 136062. 0.2138
|
|
50.75 0.8932 0.8289 0.0702 0.0756 0.526 11.046 3.221 392.056 1.248 14.325 3.726 0.25 136915. 0.1962
|
|
53.29 0.9378 0.8367 0.0627 0.0703 0.489 10.269 2.878 364.472 1.160 12.801 3.582 0.25 137802. 0.1783
|
|
55.82 0.9825 0.8403 0.0550 0.0643 0.447 9.391 2.524 333.336 1.061 11.225 3.434 0.25 138724. 0.1600
|
|
58.36 1.0271 0.8385 0.0471 0.0577 0.401 8.425 2.161 299.034 0.952 9.610 3.277 0.25 139678. 0.1413
|
|
60.90 1.0718 0.8288 0.0391 0.0505 0.351 7.380 1.793 261.942 0.834 7.974 3.104 0.25 140665. 0.1219
|
|
63.44 1.1165 0.8070 0.0310 0.0429 0.298 6.267 1.423 222.454 0.708 6.331 2.902 0.25 141683. 0.1016
|
|
65.97 1.1611 0.7650 0.0230 0.0349 0.243 5.099 1.056 180.996 0.576 4.695 2.645 0.25 142732. 0.0797
|
|
68.51 1.2058 0.6840 0.0151 0.0266 0.185 3.889 0.693 138.049 0.439 3.083 2.277 0.25 143812. 0.0556
|
|
71.05 1.2504 0.5100 0.0074 0.0182 0.126 2.653 0.340 94.150 0.300 1.512 1.637 0.26 144921. 0.0280
|
|
73.58 1.2951 -0.0020 0.0000 0.0096 0.067 1.405 -0.001 49.855 0.159 -0.003 -0.006 0.26 146057. 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 0.1199 0.0636 1.048 16.508 9.782 781.242 1.865 43.508 5.679 0.32 169453. 0.5211
|
|
3.39 0.0447 0.0826 0.1196 0.0648 1.068 16.824 9.760 796.180 1.901 43.415 5.560 0.32 169660. 0.5097
|
|
6.78 0.0894 0.1613 0.1194 0.0662 1.091 17.191 9.740 813.578 1.942 43.325 5.430 0.32 169903. 0.4972
|
|
10.16 0.1341 0.2357 0.1191 0.0678 1.118 17.612 9.720 833.495 1.990 43.235 5.289 0.32 170184. 0.4838
|
|
13.55 0.1789 0.3053 0.1189 0.0696 1.148 18.086 9.698 855.905 2.043 43.136 5.139 0.32 170507. 0.4695
|
|
16.94 0.2236 0.3699 0.1185 0.0717 1.181 18.609 9.671 880.654 2.102 43.018 4.981 0.32 170875. 0.4545
|
|
20.33 0.2683 0.4292 0.1181 0.0738 1.217 19.175 9.638 907.432 2.166 42.868 4.817 0.32 171290. 0.4387
|
|
23.71 0.3130 0.4834 0.1176 0.0761 1.255 19.773 9.593 935.747 2.234 42.668 4.650 0.32 171754. 0.4225
|
|
27.10 0.3577 0.5323 0.1168 0.0785 1.294 20.389 9.532 964.906 2.304 42.398 4.481 0.32 172270. 0.4058
|
|
30.49 0.4024 0.5764 0.1158 0.0809 1.333 21.004 9.450 994.000 2.373 42.036 4.312 0.32 172837. 0.3889
|
|
33.88 0.4472 0.6158 0.1145 0.0832 1.370 21.594 9.343 1021.918 2.440 41.556 4.147 0.32 173457. 0.3718
|
|
37.26 0.4919 0.6510 0.1128 0.0852 1.405 22.132 9.203 1047.380 2.500 40.933 3.985 0.32 174132. 0.3547
|
|
40.65 0.5366 0.6824 0.1106 0.0870 1.434 22.588 9.025 1068.983 2.552 40.143 3.829 0.32 174860. 0.3375
|
|
44.04 0.5813 0.7104 0.1079 0.0883 1.455 22.932 8.805 1085.258 2.591 39.163 3.680 0.32 175643. 0.3203
|
|
47.43 0.6260 0.7354 0.1046 0.0891 1.468 23.131 8.537 1094.675 2.613 37.971 3.537 0.32 176479. 0.3032
|
|
50.81 0.6707 0.7577 0.1007 0.0891 1.469 23.150 8.216 1095.548 2.615 36.544 3.401 0.32 177368. 0.2860
|
|
54.20 0.7155 0.7777 0.0961 0.0884 1.456 22.947 7.836 1085.972 2.593 34.856 3.273 0.33 178310. 0.2688
|
|
57.59 0.7602 0.7956 0.0906 0.0866 1.427 22.490 7.395 1064.355 2.541 32.893 3.151 0.33 179304. 0.2514
|
|
60.98 0.8049 0.8116 0.0845 0.0838 1.382 21.771 6.897 1030.302 2.460 30.676 3.036 0.33 180348. 0.2339
|
|
64.36 0.8496 0.8255 0.0778 0.0801 1.320 20.802 6.350 984.466 2.350 28.245 2.926 0.33 181441. 0.2163
|
|
67.75 0.8943 0.8371 0.0707 0.0755 1.244 19.607 5.766 927.897 2.215 25.645 2.818 0.33 182581. 0.1985
|
|
71.14 0.9390 0.8457 0.0631 0.0701 1.156 18.208 5.152 861.678 2.057 22.915 2.712 0.33 183768. 0.1806
|
|
74.53 0.9838 0.8506 0.0554 0.0640 1.055 16.626 4.516 786.808 1.878 20.088 2.603 0.33 185000. 0.1623
|
|
77.91 1.0285 0.8504 0.0474 0.0573 0.944 14.881 3.865 704.218 1.681 17.194 2.490 0.33 186275. 0.1436
|
|
81.30 1.0732 0.8430 0.0393 0.0500 0.824 12.992 3.206 614.822 1.468 14.260 2.365 0.34 187594. 0.1242
|
|
84.69 1.1179 0.8244 0.0312 0.0423 0.697 10.979 2.544 519.575 1.240 11.314 2.220 0.34 188955. 0.1039
|
|
88.08 1.1626 0.7867 0.0231 0.0341 0.563 8.865 1.885 419.523 1.002 8.382 2.037 0.34 190357. 0.0821
|
|
91.47 1.2073 0.7114 0.0151 0.0257 0.424 6.674 1.235 315.842 0.754 5.495 1.774 0.34 191800. 0.0579
|
|
94.85 1.2521 0.5419 0.0074 0.0171 0.281 4.434 0.603 209.854 0.501 2.682 1.303 0.34 193283. 0.0297
|
|
98.24 1.2968 -0.0121 -0.0001 0.0084 0.138 2.175 -0.006 102.915 0.246 -0.028 -0.028 0.34 194800. 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 0.1201 0.0634 2.041 25.725 15.309 1521.796 2.906 68.092 4.563 0.40 211812. 0.5237
|
|
4.23 0.0447 0.0830 0.1199 0.0646 2.080 26.216 15.278 1550.859 2.962 67.958 4.468 0.40 212071. 0.5124
|
|
8.47 0.0894 0.1621 0.1196 0.0660 2.125 26.790 15.250 1584.790 3.027 67.832 4.365 0.40 212374. 0.5000
|
|
12.70 0.1342 0.2368 0.1194 0.0676 2.177 27.448 15.222 1623.733 3.101 67.708 4.252 0.40 212725. 0.4867
|
|
16.94 0.1789 0.3068 0.1192 0.0695 2.236 28.191 15.192 1667.665 3.185 67.573 4.132 0.40 213129. 0.4725
|
|
21.17 0.2236 0.3718 0.1189 0.0715 2.302 29.013 15.156 1716.318 3.278 67.413 4.005 0.40 213589. 0.4575
|
|
25.41 0.2683 0.4315 0.1185 0.0737 2.372 29.906 15.109 1769.122 3.379 67.204 3.874 0.40 214107. 0.4417
|
|
29.64 0.3130 0.4859 0.1180 0.0760 2.448 30.853 15.046 1825.145 3.486 66.923 3.739 0.40 214687. 0.4255
|
|
33.88 0.3578 0.5351 0.1173 0.0785 2.525 31.832 14.958 1883.047 3.596 66.535 3.603 0.40 215331. 0.4088
|
|
38.11 0.4025 0.5794 0.1164 0.0809 2.603 32.813 14.839 1941.053 3.707 66.005 3.468 0.40 216040. 0.3919
|
|
42.35 0.4472 0.6190 0.1152 0.0832 2.678 33.758 14.679 1996.973 3.814 65.292 3.334 0.40 216815. 0.3748
|
|
46.58 0.4919 0.6543 0.1135 0.0853 2.747 34.625 14.469 2048.251 3.912 64.356 3.204 0.40 217658. 0.3575
|
|
50.82 0.5366 0.6858 0.1114 0.0872 2.806 35.365 14.199 2092.077 3.996 63.156 3.078 0.40 218569. 0.3403
|
|
55.05 0.5813 0.7139 0.1087 0.0886 2.850 35.930 13.861 2125.486 4.059 61.655 2.958 0.40 219547. 0.3231
|
|
59.29 0.6261 0.7390 0.1055 0.0894 2.877 36.267 13.448 2145.405 4.097 59.818 2.843 0.40 220593. 0.3059
|
|
63.52 0.6708 0.7614 0.1016 0.0895 2.881 36.319 12.951 2148.466 4.103 57.607 2.734 0.41 221705. 0.2887
|
|
67.76 0.7155 0.7815 0.0970 0.0888 2.858 36.021 12.360 2130.875 4.070 54.979 2.631 0.41 222883. 0.2714
|
|
71.99 0.7602 0.7996 0.0916 0.0870 2.802 35.320 11.671 2089.401 3.990 51.913 2.534 0.41 224126. 0.2539
|
|
76.23 0.8049 0.8159 0.0854 0.0843 2.713 34.200 10.890 2023.145 3.864 48.439 2.441 0.41 225431. 0.2364
|
|
80.46 0.8497 0.8302 0.0787 0.0805 2.593 32.682 10.032 1933.313 3.692 44.622 2.354 0.41 226798. 0.2187
|
|
84.69 0.8944 0.8423 0.0715 0.0759 2.443 30.799 9.112 1821.958 3.480 40.532 2.269 0.41 228225. 0.2009
|
|
88.93 0.9391 0.8517 0.0639 0.0705 2.268 28.589 8.145 1691.213 3.230 36.231 2.185 0.41 229709. 0.1829
|
|
93.16 0.9838 0.8576 0.0560 0.0643 2.069 26.085 7.143 1543.067 2.947 31.774 2.100 0.42 231249. 0.1646
|
|
97.40 1.0285 0.8588 0.0480 0.0575 1.850 23.318 6.117 1379.375 2.634 27.207 2.011 0.42 232845. 0.1459
|
|
101.63 1.0733 0.8534 0.0398 0.0501 1.612 20.319 5.076 1201.962 2.296 22.576 1.915 0.42 234494. 0.1266
|
|
105.87 1.1180 0.8375 0.0316 0.0422 1.358 17.120 4.029 1012.738 1.934 17.922 1.805 0.42 236196. 0.1063
|
|
110.10 1.1627 0.8038 0.0234 0.0339 1.091 13.757 2.988 813.798 1.554 13.290 1.665 0.42 237949. 0.0845
|
|
114.34 1.2074 0.7342 0.0154 0.0253 0.815 10.270 1.962 607.514 1.160 8.727 1.465 0.42 239753. 0.0602
|
|
118.57 1.2521 0.5722 0.0075 0.0165 0.532 6.704 0.962 396.552 0.757 4.281 1.101 0.43 241607. 0.0317
|
|
122.81 1.2968 -0.0008 0.0000 0.0077 0.246 3.105 -0.001 183.656 0.351 -0.003 -0.001 0.43 243502. 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 0.1203 0.0635 3.532 37.105 22.083 2633.989 4.192 98.227 3.803 0.48 254168. 0.5243
|
|
5.08 0.0447 0.0830 0.1201 0.0647 3.599 37.808 22.044 2683.882 4.272 98.051 3.725 0.48 254478. 0.5132
|
|
10.17 0.0895 0.1622 0.1199 0.0661 3.678 38.631 22.008 2742.314 4.365 97.893 3.640 0.48 254842. 0.5010
|
|
15.25 0.1342 0.2371 0.1197 0.0677 3.768 39.579 21.974 2809.590 4.472 97.742 3.547 0.48 255263. 0.4879
|
|
20.33 0.1789 0.3074 0.1195 0.0696 3.870 40.652 21.938 2885.732 4.593 97.582 3.448 0.48 255748. 0.4738
|
|
25.41 0.2236 0.3725 0.1193 0.0716 3.983 41.844 21.895 2970.352 4.727 97.390 3.343 0.48 256299. 0.4590
|
|
30.50 0.2684 0.4324 0.1190 0.0738 4.107 43.142 21.838 3062.538 4.874 97.138 3.234 0.48 256921. 0.4434
|
|
35.58 0.3131 0.4871 0.1185 0.0762 4.239 44.526 21.759 3160.745 5.030 96.785 3.122 0.48 257617. 0.4273
|
|
40.66 0.3578 0.5365 0.1179 0.0787 4.375 45.962 21.647 3262.701 5.193 96.287 3.009 0.48 258389. 0.4108
|
|
45.75 0.4026 0.5809 0.1171 0.0811 4.513 47.408 21.490 3365.346 5.356 95.589 2.896 0.48 259239. 0.3939
|
|
50.83 0.4473 0.6206 0.1159 0.0835 4.646 48.809 21.275 3464.838 5.514 94.631 2.785 0.48 260170. 0.3769
|
|
55.91 0.4920 0.6560 0.1143 0.0857 4.770 50.103 20.987 3556.649 5.661 93.350 2.676 0.48 261182. 0.3597
|
|
61.00 0.5368 0.6876 0.1123 0.0877 4.876 51.217 20.613 3635.754 5.786 91.686 2.572 0.48 262275. 0.3425
|
|
66.08 0.5815 0.7158 0.1097 0.0891 4.958 52.078 20.140 3696.831 5.884 89.581 2.471 0.48 263449. 0.3253
|
|
71.16 0.6262 0.7410 0.1065 0.0900 5.008 52.606 19.555 3734.355 5.943 86.982 2.375 0.49 264705. 0.3081
|
|
76.24 0.6709 0.7635 0.1027 0.0902 5.019 52.719 18.847 3742.332 5.956 83.832 2.284 0.49 266041. 0.2909
|
|
81.33 0.7157 0.7838 0.0981 0.0895 4.981 52.320 18.001 3714.044 5.911 80.068 2.198 0.49 267456. 0.2736
|
|
86.41 0.7604 0.8021 0.0927 0.0878 4.886 51.329 17.009 3643.661 5.799 75.655 2.117 0.49 268949. 0.2562
|
|
91.49 0.8051 0.8186 0.0865 0.0851 4.733 49.719 15.880 3529.372 5.617 70.636 2.041 0.49 270517. 0.2386
|
|
96.58 0.8499 0.8333 0.0797 0.0813 4.523 47.518 14.636 3373.148 5.369 65.103 1.968 0.49 272159. 0.2209
|
|
101.66 0.8946 0.8459 0.0725 0.0766 4.262 44.776 13.300 3178.546 5.059 59.160 1.898 0.49 273873. 0.2031
|
|
106.74 0.9393 0.8559 0.0648 0.0711 3.955 41.547 11.893 2949.320 4.694 52.901 1.829 0.50 275656. 0.1851
|
|
111.82 0.9841 0.8627 0.0568 0.0648 3.606 37.880 10.433 2688.989 4.280 46.404 1.760 0.50 277506. 0.1668
|
|
116.91 1.0288 0.8651 0.0487 0.0579 3.220 33.821 8.935 2400.851 3.821 39.741 1.688 0.50 279422. 0.1480
|
|
121.99 1.0735 0.8612 0.0404 0.0503 2.800 29.416 7.414 2088.148 3.323 32.977 1.610 0.50 281403. 0.1286
|
|
127.07 1.1182 0.8476 0.0321 0.0423 2.353 24.713 5.885 1754.274 2.792 26.176 1.522 0.51 283447. 0.1083
|
|
132.16 1.1630 0.8170 0.0238 0.0338 1.881 19.764 4.362 1402.969 2.233 19.402 1.410 0.51 285552. 0.0864
|
|
137.24 1.2077 0.7518 0.0156 0.0250 1.393 14.629 2.861 1038.472 1.653 12.725 1.249 0.51 287718. 0.0620
|
|
142.32 1.2524 0.5944 0.0076 0.0160 0.893 9.376 1.398 665.590 1.059 6.218 0.953 0.51 289944. 0.0330
|
|
147.41 1.2972 -0.0115 -0.0001 0.0070 0.388 4.074 -0.011 289.230 0.460 -0.051 -0.018 0.51 292218. 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 0.1205 0.0638 5.639 50.769 30.116 4204.638 5.736 133.955 3.249 0.56 296521. 0.5230
|
|
5.93 0.0447 0.0828 0.1203 0.0650 5.744 51.716 30.068 4283.042 5.843 133.744 3.184 0.56 296882. 0.5123
|
|
11.86 0.0894 0.1618 0.1202 0.0664 5.867 52.829 30.028 4375.210 5.969 133.563 3.113 0.56 297306. 0.5005
|
|
17.78 0.1341 0.2367 0.1200 0.0680 6.010 54.115 29.991 4481.731 6.114 133.400 3.035 0.56 297797. 0.4877
|
|
23.71 0.1789 0.3069 0.1199 0.0699 6.172 55.577 29.954 4602.769 6.279 133.235 2.952 0.56 298361. 0.4740
|
|
29.64 0.2236 0.3721 0.1197 0.0719 6.354 57.208 29.909 4737.852 6.463 133.037 2.863 0.56 299003. 0.4594
|
|
35.57 0.2683 0.4321 0.1195 0.0742 6.552 58.993 29.849 4885.688 6.665 132.769 2.771 0.56 299727. 0.4442
|
|
41.50 0.3130 0.4869 0.1191 0.0766 6.764 60.904 29.761 5043.991 6.881 132.378 2.676 0.56 300538. 0.4283
|
|
47.43 0.3577 0.5364 0.1186 0.0791 6.986 62.900 29.632 5209.265 7.106 131.802 2.580 0.56 301437. 0.4120
|
|
53.35 0.4024 0.5810 0.1178 0.0816 7.210 64.922 29.443 5376.701 7.335 130.964 2.484 0.56 302428. 0.3954
|
|
59.28 0.4472 0.6208 0.1168 0.0841 7.429 66.895 29.177 5540.138 7.558 129.780 2.389 0.56 303513. 0.3785
|
|
65.21 0.4919 0.6564 0.1153 0.0864 7.633 68.731 28.813 5692.187 7.765 128.160 2.296 0.56 304692. 0.3616
|
|
71.14 0.5366 0.6880 0.1134 0.0884 7.811 70.329 28.331 5824.541 7.946 126.014 2.206 0.56 305966. 0.3445
|
|
77.07 0.5813 0.7163 0.1109 0.0900 7.950 71.583 27.711 5928.356 8.087 123.258 2.120 0.56 307336. 0.3274
|
|
83.00 0.6260 0.7416 0.1078 0.0910 8.039 72.381 26.937 5994.438 8.178 119.814 2.038 0.57 308800. 0.3103
|
|
88.92 0.6707 0.7643 0.1040 0.0913 8.063 72.604 25.989 6012.916 8.203 115.601 1.960 0.57 310359. 0.2932
|
|
94.85 0.7155 0.7847 0.0995 0.0907 8.010 72.119 24.849 5972.792 8.148 110.529 1.887 0.57 312010. 0.2760
|
|
100.78 0.7602 0.8032 0.0941 0.0890 7.864 70.809 23.504 5864.318 8.000 104.544 1.818 0.57 313751. 0.2586
|
|
106.71 0.8049 0.8199 0.0879 0.0863 7.622 68.633 21.965 5684.055 7.754 97.700 1.753 0.57 315581. 0.2410
|
|
112.64 0.8496 0.8350 0.0811 0.0825 7.288 65.624 20.262 5434.853 7.414 90.124 1.691 0.58 317498. 0.2233
|
|
118.57 0.8943 0.8481 0.0737 0.0778 6.869 61.851 18.426 5122.368 6.988 81.959 1.632 0.58 319498. 0.2055
|
|
124.49 0.9390 0.8587 0.0660 0.0722 6.373 57.387 16.487 4752.701 6.484 73.335 1.573 0.58 321578. 0.1874
|
|
130.42 0.9838 0.8664 0.0579 0.0658 5.809 52.303 14.471 4331.627 5.909 64.368 1.515 0.58 323737. 0.1691
|
|
136.35 1.0285 0.8699 0.0496 0.0587 5.182 46.663 12.400 3864.544 5.272 55.155 1.455 0.58 325973. 0.1504
|
|
142.28 1.0732 0.8676 0.0412 0.0510 4.502 40.532 10.294 3356.774 4.579 45.788 1.391 0.59 328284. 0.1309
|
|
148.21 1.1179 0.8561 0.0327 0.0427 3.773 33.977 8.174 2813.879 3.839 36.358 1.318 0.59 330667. 0.1105
|
|
154.13 1.1626 0.8284 0.0243 0.0340 3.007 27.071 6.060 2241.992 3.058 26.956 1.226 0.59 333123. 0.0885
|
|
160.06 1.2073 0.7676 0.0159 0.0250 2.210 19.900 3.975 1648.110 2.248 17.680 1.094 0.59 335650. 0.0640
|
|
165.99 1.2520 0.6159 0.0078 0.0158 1.395 12.560 1.941 1040.210 1.419 8.634 0.846 0.60 338245. 0.0346
|
|
171.92 1.2968 -0.0150 -0.0001 0.0065 0.572 5.149 -0.019 426.449 0.582 -0.083 -0.020 0.60 340896. 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 0.1208 0.0644 8.497 66.946 39.415 6336.440 7.564 175.319 2.821 0.63 338870. 0.5197
|
|
6.77 0.0447 0.0821 0.1206 0.0656 8.651 68.160 39.362 6451.270 7.701 175.082 2.767 0.63 339282. 0.5094
|
|
13.54 0.0894 0.1607 0.1205 0.0670 8.833 69.593 39.320 6586.925 7.863 174.895 2.708 0.63 339765. 0.4981
|
|
20.31 0.1341 0.2353 0.1204 0.0686 9.044 71.257 39.286 6744.468 8.051 174.744 2.642 0.64 340325. 0.4858
|
|
27.08 0.1787 0.3053 0.1203 0.0704 9.286 73.158 39.254 6924.374 8.265 174.604 2.571 0.64 340968. 0.4726
|
|
33.85 0.2234 0.3705 0.1202 0.0725 9.556 75.291 39.218 7126.218 8.506 174.441 2.496 0.64 341700. 0.4586
|
|
40.62 0.2681 0.4305 0.1200 0.0747 9.854 77.638 39.165 7348.400 8.772 174.205 2.417 0.64 342526. 0.4438
|
|
47.40 0.3128 0.4854 0.1198 0.0772 10.175 80.168 39.081 7587.850 9.057 173.832 2.336 0.64 343450. 0.4285
|
|
54.17 0.3575 0.5351 0.1194 0.0797 10.513 82.828 38.948 7839.669 9.358 173.240 2.253 0.64 344475. 0.4126
|
|
60.94 0.4022 0.5798 0.1187 0.0824 10.858 85.546 38.743 8096.890 9.665 172.329 2.170 0.64 345605. 0.3963
|
|
67.71 0.4469 0.6198 0.1178 0.0849 11.198 88.224 38.440 8350.313 9.967 170.982 2.088 0.64 346842. 0.3798
|
|
74.48 0.4916 0.6554 0.1165 0.0874 11.518 90.741 38.011 8588.616 10.252 169.074 2.007 0.64 348187. 0.3631
|
|
81.25 0.5362 0.6872 0.1147 0.0895 11.799 92.962 37.428 8798.819 10.503 166.478 1.929 0.64 349641. 0.3463
|
|
88.02 0.5809 0.7156 0.1123 0.0912 12.025 94.738 36.662 8966.875 10.703 163.073 1.854 0.65 351204. 0.3294
|
|
94.79 0.6256 0.7410 0.1094 0.0923 12.174 95.914 35.689 9078.188 10.836 158.745 1.783 0.65 352876. 0.3125
|
|
101.56 0.6703 0.7638 0.1057 0.0927 12.227 96.327 34.483 9117.307 10.883 153.382 1.715 0.65 354656. 0.2955
|
|
108.33 0.7150 0.7844 0.1012 0.0922 12.159 95.798 33.017 9067.185 10.823 146.861 1.652 0.65 356542. 0.2784
|
|
115.10 0.7597 0.8031 0.0958 0.0906 11.952 94.161 31.273 8912.309 10.638 139.101 1.592 0.65 358531. 0.2611
|
|
121.87 0.8044 0.8202 0.0897 0.0879 11.595 91.352 29.263 8646.449 10.321 130.162 1.535 0.66 360623. 0.2436
|
|
128.64 0.8490 0.8356 0.0828 0.0841 11.095 87.410 27.025 8273.296 9.876 120.209 1.482 0.66 362812. 0.2260
|
|
135.41 0.8937 0.8492 0.0754 0.0793 10.462 82.423 24.603 7801.282 9.312 109.433 1.430 0.66 365097. 0.2082
|
|
142.18 0.9384 0.8605 0.0675 0.0736 9.709 76.490 22.035 7239.776 8.642 98.012 1.380 0.66 367475. 0.1901
|
|
148.96 0.9831 0.8690 0.0593 0.0671 8.848 69.707 19.357 6597.725 7.875 86.102 1.331 0.67 369942. 0.1718
|
|
155.73 1.0278 0.8737 0.0509 0.0598 7.890 62.161 16.600 5883.534 7.023 73.837 1.280 0.67 372496. 0.1530
|
|
162.50 1.0725 0.8728 0.0423 0.0519 6.846 53.940 13.791 5105.424 6.094 61.342 1.225 0.67 375135. 0.1335
|
|
169.27 1.1172 0.8633 0.0336 0.0435 5.729 45.135 10.958 4272.016 5.099 48.740 1.163 0.67 377858. 0.1130
|
|
176.04 1.1619 0.8386 0.0249 0.0345 4.550 35.846 8.128 3392.827 4.050 36.154 1.087 0.68 380662. 0.0909
|
|
182.81 1.2065 0.7820 0.0163 0.0252 3.324 26.190 5.333 2478.857 2.959 23.721 0.976 0.68 383547. 0.0661
|
|
189.58 1.2512 0.6361 0.0080 0.0157 2.069 16.303 2.604 1543.089 1.842 11.582 0.765 0.68 386510. 0.0362
|
|
196.35 1.2959 -0.0186 -0.0001 0.0061 0.804 6.331 -0.029 599.209 0.715 -0.127 -0.022 0.69 389535. 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 0.0661 12.417 86.957 49.978 9259.247 9.824 222.302 2.448 0.71 381214. 0.5078
|
|
7.65 0.0449 0.0807 0.1209 0.0673 12.630 88.447 49.920 9417.902 9.993 222.046 2.404 0.71 381680. 0.4984
|
|
15.31 0.0898 0.1581 0.1208 0.0686 12.883 90.219 49.880 9606.609 10.193 221.868 2.355 0.71 382225. 0.4880
|
|
22.96 0.1347 0.2316 0.1207 0.0702 13.178 92.290 49.855 9827.126 10.427 221.753 2.301 0.71 382858. 0.4767
|
|
30.62 0.1796 0.3010 0.1207 0.0720 13.518 94.669 49.837 10080.383 10.696 221.677 2.242 0.72 383586. 0.4644
|
|
38.27 0.2245 0.3657 0.1206 0.0741 13.901 97.352 49.820 10366.058 10.999 221.598 2.180 0.72 384414. 0.4514
|
|
45.93 0.2694 0.4256 0.1205 0.0763 14.325 100.320 49.788 10682.156 11.334 221.458 2.114 0.72 385349. 0.4376
|
|
53.58 0.3143 0.4805 0.1204 0.0788 14.784 103.536 49.726 11024.598 11.697 221.179 2.046 0.72 386396. 0.4232
|
|
61.23 0.3592 0.5305 0.1201 0.0813 15.270 106.936 49.608 11386.653 12.082 220.657 1.976 0.72 387557. 0.4083
|
|
68.89 0.4042 0.5756 0.1196 0.0840 15.768 110.428 49.407 11758.483 12.476 219.762 1.906 0.72 388838. 0.3930
|
|
76.54 0.4491 0.6161 0.1189 0.0866 16.262 113.888 49.087 12126.812 12.867 218.339 1.836 0.72 390240. 0.3774
|
|
84.20 0.4940 0.6524 0.1177 0.0891 16.729 117.158 48.609 12475.014 13.236 216.215 1.767 0.72 391765. 0.3615
|
|
91.85 0.5389 0.6848 0.1161 0.0913 17.143 120.057 47.933 12783.745 13.564 213.206 1.701 0.72 393414. 0.3454
|
|
99.51 0.5838 0.7139 0.1138 0.0931 17.476 122.388 47.018 13031.961 13.827 209.136 1.636 0.73 395189. 0.3292
|
|
107.16 0.6287 0.7399 0.1110 0.0943 17.698 123.945 45.827 13197.749 14.003 203.840 1.575 0.73 397087. 0.3128
|
|
114.82 0.6736 0.7633 0.1073 0.0947 17.779 124.509 44.325 13257.824 14.067 197.157 1.516 0.73 399109. 0.2962
|
|
122.47 0.7185 0.7844 0.1028 0.0942 17.683 123.839 42.472 13186.453 13.991 188.915 1.461 0.73 401251. 0.2793
|
|
130.12 0.7634 0.8035 0.0974 0.0926 17.380 121.712 40.244 12959.986 13.751 179.006 1.408 0.73 403512. 0.2621
|
|
137.78 0.8083 0.8209 0.0912 0.0898 16.854 118.034 37.659 12568.337 13.335 167.506 1.359 0.74 405889. 0.2447
|
|
145.43 0.8532 0.8367 0.0842 0.0858 16.114 112.847 34.765 12016.042 12.749 154.635 1.312 0.74 408378. 0.2270
|
|
153.09 0.8981 0.8507 0.0766 0.0808 15.174 106.263 31.620 11314.984 12.006 140.648 1.268 0.74 410974. 0.2091
|
|
160.74 0.9430 0.8625 0.0685 0.0749 14.053 98.412 28.278 10479.024 11.119 125.781 1.224 0.75 413676. 0.1910
|
|
168.40 0.9879 0.8716 0.0600 0.0680 12.769 89.421 24.784 9521.604 10.103 110.240 1.181 0.75 416478. 0.1724
|
|
176.05 1.0328 0.8768 0.0513 0.0604 11.339 79.410 21.180 8455.658 8.972 94.206 1.136 0.75 419380. 0.1534
|
|
183.70 1.0777 0.8764 0.0424 0.0521 9.782 68.505 17.501 7294.467 7.740 77.846 1.088 0.75 422377. 0.1336
|
|
191.36 1.1226 0.8667 0.0334 0.0432 8.117 56.843 13.786 6052.634 6.422 61.322 1.033 0.76 425468. 0.1125
|
|
199.01 1.1675 0.8396 0.0244 0.0339 6.366 44.584 10.072 4747.314 5.037 44.800 0.962 0.76 428652. 0.0896
|
|
206.67 1.2125 0.7734 0.0155 0.0243 4.559 31.925 6.398 3399.385 3.607 28.457 0.854 0.77 431926. 0.0633
|
|
214.32 1.2574 0.5880 0.0068 0.0145 2.728 19.101 2.806 2033.922 2.158 12.483 0.626 0.77 435288. 0.0308
|
|
221.98 1.3023
|
|
|
|
|
|
|
|
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 0.1211 0.0707 18.214 114.803 61.763 13582.552 12.970 274.721 2.062 0.79 423553. 0.4755
|
|
8.51 0.0449 0.0757 0.1210 0.0718 18.495 116.572 61.698 13791.791 13.170 274.433 2.029 0.79 424069. 0.4676
|
|
17.02 0.0898 0.1486 0.1209 0.0731 18.831 118.690 61.659 14042.440 13.410 274.259 1.992 0.79 424675. 0.4588
|
|
25.52 0.1348 0.2182 0.1209 0.0747 19.227 121.182 61.643 14337.248 13.691 274.188 1.950 0.79 425377. 0.4492
|
|
34.03 0.1797 0.2842 0.1209 0.0764 19.683 124.061 61.645 14677.857 14.016 274.195 1.905 0.79 426185. 0.4388
|
|
42.54 0.2246 0.3462 0.1209 0.0784 20.201 127.326 61.655 15064.149 14.385 274.240 1.856 0.80 427104. 0.4276
|
|
51.05 0.2695 0.4039 0.1209 0.0807 20.777 130.956 61.659 15493.680 14.795 274.261 1.805 0.80 428141. 0.4158
|
|
59.55 0.3144 0.4573 0.1209 0.0831 21.404 134.906 61.639 15960.920 15.242 274.169 1.752 0.80 429302. 0.4035
|
|
68.06 0.3594 0.5063 0.1207 0.0857 22.069 139.095 61.566 16456.586 15.715 273.848 1.697 0.80 430591. 0.3906
|
|
76.57 0.4043 0.5510 0.1204 0.0884 22.753 143.407 61.408 16966.742 16.202 273.141 1.642 0.80 432011. 0.3774
|
|
85.08 0.4492 0.5918 0.1199 0.0910 23.431 147.679 61.119 17472.219 16.685 271.859 1.587 0.80 433567. 0.3639
|
|
93.58 0.4941 0.6288 0.1189 0.0935 24.069 151.705 60.651 17948.486 17.140 269.774 1.533 0.80 435259. 0.3502
|
|
102.09 0.5390 0.6626 0.1176 0.0956 24.630 155.238 59.945 18366.541 17.539 266.637 1.480 0.80 437091. 0.3363
|
|
110.60 0.5840 0.6934 0.1156 0.0974 25.070 158.014 58.947 18694.877 17.852 262.195 1.430 0.81 439062. 0.3221
|
|
119.11 0.6289 0.7217 0.1130 0.0984 25.348 159.762 57.600 18901.730 18.050 256.206 1.382 0.81 441172. 0.3078
|
|
127.61 0.6738 0.7477 0.1095 0.0987 25.419 160.214 55.853 18955.254 18.101 248.433 1.336 0.81 443420. 0.2930
|
|
136.12 0.7187 0.7715 0.1052 0.0980 25.240 159.086 53.651 18821.795 17.973 238.638 1.293 0.81 445804. 0.2778
|
|
144.63 0.7636 0.7934 0.0999 0.0962 24.769 156.118 50.957 18470.570 17.638 226.655 1.251 0.82 448321. 0.2621
|
|
153.14 0.8086 0.8134 0.0937 0.0932 23.989 151.196 47.785 17888.246 17.082 212.548 1.212 0.82 450967. 0.2457
|
|
161.64 0.8535 0.8316 0.0867 0.0890 22.907 144.381 44.195 17081.984 16.312 196.577 1.173 0.82 453738. 0.2289
|
|
170.15 0.8984 0.8476 0.0790 0.0837 21.549 135.822 40.259 16069.346 15.345 179.072 1.136 0.83 456630. 0.2115
|
|
178.66 0.9433 0.8612 0.0707 0.0774 19.941 125.682 36.048 14869.710 14.200 160.341 1.100 0.83 459638. 0.1937
|
|
187.17 0.9882 0.8713 0.0620 0.0703 18.113 114.162 31.621 13506.653 12.898 140.652 1.062 0.83 462759. 0.1752
|
|
195.67 1.0332 0.8766 0.0530 0.0625 16.091 101.420 27.033 11999.141 11.458 120.244 1.022 0.84 465988. 0.1559
|
|
204.18 1.0781 0.8745 0.0438 0.0540 13.904 87.634 22.332 10368.153 9.901 99.335 0.977 0.84 469325. 0.1355
|
|
212.69 1.1230 0.8598 0.0345 0.0450 11.588 73.037 17.568 8641.138 8.252 78.141 0.922 0.84 472765. 0.1134
|
|
221.20 1.1679 0.8206 0.0251 0.0357 9.190 57.921 12.785 6852.721 6.544 56.867 0.846 0.85 476306. 0.0888
|
|
229.70 1.2128 0.7277 0.0158 0.0263 6.765 42.636 8.037 5044.398 4.817 35.747 0.723 0.85 479948. 0.0601
|
|
238.21 1.2578 0.4909 0.0066 0.0170 4.375 27.576 3.381 3262.590 3.116 15.040 0.470 0.85 483686. 0.0254
|
|
246.72 1.3027
|
|
|
|
|
|
|
|
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 0.1206 0.0793 27.178 155.728 74.426 20266.941 17.594 331.045 1.666 0.87 465920. 0.4216
|
|
9.31 0.0447 0.0670 0.1205 0.0803 27.539 157.796 74.342 20536.000 17.828 330.671 1.642 0.87 466483. 0.4153
|
|
18.62 0.0894 0.1319 0.1204 0.0816 27.976 160.298 74.292 20861.633 18.110 330.450 1.615 0.87 467143. 0.4085
|
|
27.94 0.1341 0.1942 0.1204 0.0831 28.494 163.266 74.275 21247.902 18.446 330.376 1.586 0.87 467908. 0.4009
|
|
37.25 0.1788 0.2536 0.1204 0.0849 29.097 166.722 74.287 21697.662 18.836 330.428 1.553 0.87 468786. 0.3927
|
|
46.56 0.2235 0.3098 0.1205 0.0869 29.786 170.672 74.319 22211.701 19.282 330.571 1.518 0.87 469786. 0.3838
|
|
55.87 0.2682 0.3625 0.1205 0.0892 30.559 175.099 74.359 22787.908 19.783 330.748 1.480 0.88 470914. 0.3744
|
|
65.19 0.3129 0.4117 0.1206 0.0916 31.407 179.958 74.388 23420.252 20.332 330.877 1.441 0.88 472175. 0.3645
|
|
74.50 0.3576 0.4572 0.1206 0.0943 32.315 185.160 74.379 24097.309 20.919 330.839 1.400 0.88 473575. 0.3542
|
|
83.81 0.4023 0.4993 0.1204 0.0970 33.253 190.537 74.294 24797.008 21.527 330.461 1.359 0.88 475118. 0.3436
|
|
93.12 0.4470 0.5381 0.1201 0.0997 34.186 195.879 74.085 25492.277 22.130 329.530 1.318 0.88 476807. 0.3329
|
|
102.44 0.4917 0.5740 0.1194 0.1023 35.068 200.935 73.696 26150.316 22.702 327.798 1.278 0.88 478645. 0.3219
|
|
111.75 0.5364 0.6074 0.1184 0.1046 35.840 205.358 73.056 26725.869 23.201 324.955 1.240 0.89 480634. 0.3109
|
|
121.06 0.5811 0.6388 0.1168 0.1063 36.433 208.757 72.091 27168.283 23.585 320.662 1.204 0.89 482777. 0.2998
|
|
130.37 0.6258 0.6685 0.1146 0.1073 36.779 210.741 70.724 27426.459 23.809 314.579 1.170 0.89 485072. 0.2886
|
|
139.69 0.6705 0.6970 0.1116 0.1074 36.807 210.896 68.871 27446.678 23.827 306.340 1.138 0.89 487520. 0.2771
|
|
149.00 0.7152 0.7242 0.1077 0.1064 36.463 208.927 66.463 27190.326 23.604 295.629 1.109 0.89 490118. 0.2652
|
|
158.31 0.7599 0.7502 0.1028 0.1041 35.697 204.537 63.438 26619.035 23.108 282.173 1.081 0.90 492863. 0.2526
|
|
167.62 0.8046 0.7749 0.0969 0.1006 34.488 197.611 59.794 25717.668 22.326 265.962 1.055 0.90 495750. 0.2392
|
|
176.94 0.8493 0.7982 0.0901 0.0959 32.855 188.255 55.587 24500.070 21.269 247.250 1.029 0.90 498776. 0.2251
|
|
186.25 0.8940 0.8197 0.0825 0.0900 30.845 176.736 50.907 23000.961 19.968 226.435 1.004 0.91 501935. 0.2101
|
|
195.56 0.9387 0.8387 0.0743 0.0832 28.504 163.324 45.845 21255.482 18.452 203.916 0.978 0.91 505221. 0.1943
|
|
204.87 0.9834 0.8539 0.0656 0.0755 25.893 148.365 40.474 19308.645 16.762 180.027 0.951 0.91 508630. 0.1775
|
|
214.19 1.0281 0.8620 0.0565 0.0674 23.094 132.323 34.857 17220.938 14.950 155.043 0.918 0.92 512158. 0.1590
|
|
223.50 1.0728 0.8558 0.0471 0.0590 20.228 115.904 29.046 15084.137 13.095 129.199 0.873 0.92 515801. 0.1381
|
|
232.81 1.1175 0.8281 0.0375 0.0506 17.328 99.285 23.114 12921.199 11.217 102.810 0.811 0.93 519557. 0.1144
|
|
242.12 1.1622 0.7682 0.0278 0.0420 14.409 82.563 17.146 10745.056 9.328 76.266 0.724 0.93 523424. 0.0879
|
|
251.44 1.2069 0.6512 0.0182 0.0337 11.567 66.275 11.234 8625.253 7.488 49.968 0.591 0.93 527398. 0.0581
|
|
260.75 1.2516 0.4289 0.0089 0.0259 8.883 50.897 5.480 6623.836 5.750 24.373 0.375 0.94 531480. 0.0258
|
|
270.06 1.2963 -0.0009 0.0000 0.0187 6.423 36.801 -0.008 4789.366 4.158 -0.036 -0.001 0.94 535675. 0.0000
|
|
|
|
|
|
|