353 lines
63 KiB
Plaintext
353 lines
63 KiB
Plaintext
26x13E (26x13E.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 0.0824 0.0283 0.027 1.707 1.199 20.195 0.193 5.335 26.938 0.10 61851. 0.6658
|
|
0.55 0.0223 0.0630 0.0810 0.0286 0.027 1.726 1.179 20.415 0.195 5.245 26.199 0.10 61887. 0.6421
|
|
1.10 0.0446 0.1225 0.0795 0.0289 0.028 1.743 1.158 20.618 0.197 5.149 25.466 0.10 61926. 0.6183
|
|
1.65 0.0669 0.1786 0.0779 0.0292 0.028 1.758 1.134 20.797 0.199 5.046 24.740 0.10 61968. 0.5947
|
|
2.20 0.0892 0.2312 0.0762 0.0294 0.028 1.771 1.110 20.948 0.200 4.935 24.024 0.10 62013. 0.5711
|
|
2.74 0.1114 0.2805 0.0744 0.0295 0.028 1.781 1.083 21.067 0.201 4.818 23.319 0.10 62061. 0.5477
|
|
3.29 0.1337 0.3266 0.0724 0.0297 0.028 1.787 1.055 21.148 0.202 4.692 22.624 0.10 62113. 0.5244
|
|
3.84 0.1560 0.3695 0.0704 0.0297 0.028 1.791 1.025 21.186 0.202 4.558 21.940 0.10 62169. 0.5012
|
|
4.39 0.1783 0.4093 0.0682 0.0297 0.028 1.790 0.993 21.177 0.202 4.417 21.267 0.10 62228. 0.4783
|
|
4.94 0.2006 0.4461 0.0659 0.0296 0.028 1.785 0.959 21.114 0.202 4.266 20.604 0.10 62290. 0.4554
|
|
5.49 0.2229 0.4800 0.0634 0.0294 0.028 1.774 0.923 20.994 0.200 4.108 19.951 0.10 62357. 0.4327
|
|
6.04 0.2452 0.5109 0.0608 0.0292 0.028 1.759 0.886 20.811 0.199 3.940 19.306 0.10 62427. 0.4101
|
|
6.59 0.2675 0.5389 0.0581 0.0288 0.028 1.738 0.846 20.558 0.196 3.764 18.668 0.10 62502. 0.3875
|
|
7.13 0.2897 0.5640 0.0552 0.0284 0.027 1.710 0.804 20.233 0.193 3.578 18.034 0.10 62580. 0.3650
|
|
7.68 0.3120 0.5861 0.0523 0.0278 0.027 1.677 0.761 19.836 0.189 3.385 17.402 0.10 62662. 0.3426
|
|
8.23 0.3343 0.6051 0.0492 0.0272 0.026 1.637 0.716 19.366 0.185 3.184 16.768 0.10 62749. 0.3202
|
|
8.78 0.3566 0.6208 0.0460 0.0264 0.025 1.591 0.669 18.823 0.180 2.977 16.128 0.10 62839. 0.2978
|
|
9.33 0.3789 0.6330 0.0427 0.0255 0.024 1.539 0.621 18.208 0.174 2.764 15.477 0.10 62934. 0.2753
|
|
9.88 0.4012 0.6413 0.0393 0.0246 0.023 1.481 0.572 17.522 0.167 2.545 14.810 0.10 63033. 0.2528
|
|
10.43 0.4235 0.6453 0.0358 0.0235 0.022 1.417 0.522 16.765 0.160 2.321 14.118 0.10 63136. 0.2302
|
|
10.98 0.4458 0.6444 0.0323 0.0224 0.021 1.347 0.471 15.939 0.152 2.093 13.392 0.10 63244. 0.2073
|
|
11.52 0.4681 0.6376 0.0287 0.0211 0.020 1.272 0.419 15.044 0.144 1.862 12.621 0.10 63355. 0.1843
|
|
12.07 0.4903 0.6239 0.0251 0.0198 0.019 1.190 0.366 14.082 0.134 1.628 11.789 0.10 63471. 0.1610
|
|
12.62 0.5126 0.6016 0.0215 0.0183 0.018 1.104 0.313 13.056 0.125 1.392 10.872 0.10 63591. 0.1373
|
|
13.17 0.5349 0.5682 0.0178 0.0168 0.016 1.012 0.260 11.970 0.114 1.155 9.841 0.10 63716. 0.1132
|
|
13.72 0.5572 0.5202 0.0142 0.0152 0.015 0.915 0.206 10.827 0.103 0.918 8.650 0.10 63845. 0.0887
|
|
14.27 0.5795 0.4520 0.0105 0.0135 0.013 0.814 0.153 9.632 0.092 0.683 7.227 0.10 63979. 0.0639
|
|
14.82 0.6018 0.3545 0.0069 0.0118 0.011 0.709 0.101 8.391 0.080 0.449 5.458 0.11 64116. 0.0391
|
|
15.37 0.6241 0.2117 0.0034 0.0100 0.010 0.601 0.049 7.112 0.068 0.219 3.143 0.11 64258. 0.0157
|
|
15.91 0.6464 -0.0080 -0.0001 0.0081 0.008 0.490 -0.001 5.798 0.055 -0.006 -0.114 0.11 64402. 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 0.0828 0.0266 0.204 6.422 4.823 151.952 0.726 21.454 14.397 0.21 123698. 0.7136
|
|
1.10 0.0223 0.0674 0.0814 0.0270 0.206 6.502 4.743 153.855 0.735 21.095 13.981 0.21 123771. 0.6871
|
|
2.20 0.0447 0.1309 0.0799 0.0273 0.209 6.576 4.656 155.610 0.743 20.709 13.571 0.21 123849. 0.6608
|
|
3.30 0.0670 0.1905 0.0783 0.0276 0.211 6.643 4.563 157.178 0.750 20.295 13.167 0.21 123933. 0.6347
|
|
4.40 0.0893 0.2463 0.0766 0.0278 0.213 6.699 4.463 158.521 0.757 19.853 12.771 0.21 124024. 0.6089
|
|
5.50 0.1117 0.2985 0.0748 0.0280 0.214 6.745 4.357 159.598 0.762 19.379 12.382 0.21 124122. 0.5833
|
|
6.60 0.1340 0.3472 0.0728 0.0281 0.215 6.777 4.243 160.368 0.766 18.875 12.002 0.21 124226. 0.5580
|
|
7.70 0.1564 0.3926 0.0708 0.0282 0.216 6.795 4.123 160.788 0.768 18.338 11.630 0.21 124337. 0.5329
|
|
8.80 0.1787 0.4346 0.0686 0.0282 0.216 6.796 3.995 160.817 0.768 17.768 11.267 0.21 124456. 0.5082
|
|
9.90 0.2010 0.4735 0.0662 0.0281 0.215 6.779 3.859 160.410 0.766 17.164 10.911 0.21 124582. 0.4837
|
|
11.00 0.2234 0.5094 0.0638 0.0280 0.214 6.742 3.715 159.524 0.762 16.526 10.564 0.21 124715. 0.4595
|
|
12.10 0.2457 0.5423 0.0612 0.0277 0.212 6.682 3.564 158.113 0.755 15.851 10.223 0.21 124857. 0.4355
|
|
13.20 0.2680 0.5722 0.0584 0.0274 0.209 6.598 3.404 156.129 0.745 15.141 9.889 0.21 125006. 0.4117
|
|
14.30 0.2904 0.5993 0.0556 0.0269 0.206 6.489 3.236 153.544 0.733 14.395 9.560 0.21 125163. 0.3881
|
|
15.40 0.3127 0.6235 0.0526 0.0264 0.202 6.354 3.061 150.351 0.718 13.617 9.235 0.21 125329. 0.3647
|
|
16.50 0.3351 0.6447 0.0494 0.0257 0.197 6.193 2.880 146.547 0.700 12.809 8.913 0.21 125503. 0.3413
|
|
17.60 0.3574 0.6628 0.0462 0.0249 0.191 6.007 2.692 142.131 0.679 11.974 8.591 0.21 125685. 0.3181
|
|
18.70 0.3797 0.6777 0.0429 0.0240 0.184 5.794 2.499 137.104 0.655 11.115 8.267 0.21 125875. 0.2949
|
|
19.80 0.4021 0.6890 0.0395 0.0230 0.176 5.556 2.301 131.469 0.628 10.234 7.938 0.21 126074. 0.2717
|
|
20.90 0.4244 0.6963 0.0360 0.0220 0.168 5.292 2.098 125.230 0.598 9.334 7.600 0.21 126281. 0.2485
|
|
22.00 0.4467 0.6992 0.0325 0.0208 0.159 5.004 1.892 118.396 0.565 8.417 7.250 0.21 126496. 0.2251
|
|
23.10 0.4691 0.6967 0.0289 0.0195 0.149 4.690 1.683 110.976 0.530 7.487 6.880 0.21 126721. 0.2014
|
|
24.20 0.4914 0.6877 0.0253 0.0181 0.138 4.352 1.472 102.986 0.492 6.547 6.482 0.21 126954. 0.1775
|
|
25.30 0.5138 0.6705 0.0216 0.0166 0.127 3.991 1.259 94.447 0.451 5.599 6.045 0.21 127195. 0.1531
|
|
26.40 0.5361 0.6425 0.0179 0.0150 0.115 3.609 1.045 85.386 0.408 4.648 5.551 0.21 127446. 0.1281
|
|
27.50 0.5584 0.5994 0.0143 0.0133 0.102 3.205 0.831 75.838 0.362 3.698 4.972 0.21 127705. 0.1023
|
|
28.60 0.5808 0.5345 0.0106 0.0115 0.088 2.783 0.619 65.847 0.314 2.753 4.263 0.21 127973. 0.0757
|
|
29.70 0.6031 0.4351 0.0070 0.0097 0.074 2.344 0.409 55.465 0.265 1.818 3.341 0.21 128249. 0.0482
|
|
30.80 0.6254 0.2761 0.0035 0.0078 0.060 1.891 0.202 44.757 0.214 0.897 2.045 0.21 128534. 0.0207
|
|
31.90 0.6478 -0.0027 0.0000 0.0059 0.045 1.426 -0.001 33.735 0.161 -0.006 -0.019 0.21 128821. 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 0.0834 0.0261 0.673 14.144 10.933 502.025 1.598 48.631 9.878 0.31 185539. 0.7371
|
|
1.65 0.0224 0.0694 0.0820 0.0264 0.682 14.332 10.751 508.687 1.619 47.821 9.586 0.31 185648. 0.7094
|
|
3.30 0.0447 0.1347 0.0805 0.0267 0.690 14.505 10.556 514.844 1.639 46.951 9.299 0.31 185767. 0.6818
|
|
4.96 0.0671 0.1959 0.0789 0.0270 0.698 14.661 10.346 520.360 1.656 46.017 9.018 0.31 185894. 0.6546
|
|
6.61 0.0895 0.2533 0.0772 0.0273 0.704 14.794 10.121 525.103 1.671 45.017 8.742 0.31 186031. 0.6276
|
|
8.26 0.1118 0.3068 0.0754 0.0275 0.709 14.902 9.880 528.932 1.684 43.947 8.473 0.31 186177. 0.6010
|
|
9.91 0.1342 0.3568 0.0734 0.0276 0.713 14.980 9.624 531.704 1.692 42.806 8.210 0.31 186334. 0.5748
|
|
11.56 0.1566 0.4032 0.0713 0.0277 0.715 15.024 9.351 533.271 1.697 41.591 7.953 0.31 186502. 0.5488
|
|
13.22 0.1789 0.4463 0.0691 0.0277 0.715 15.030 9.060 533.484 1.698 40.300 7.703 0.31 186680. 0.5233
|
|
14.87 0.2013 0.4862 0.0668 0.0276 0.714 14.994 8.753 532.195 1.694 38.932 7.460 0.31 186870. 0.4981
|
|
16.52 0.2237 0.5231 0.0643 0.0275 0.710 14.911 8.427 529.250 1.685 37.484 7.222 0.31 187071. 0.4731
|
|
18.17 0.2460 0.5569 0.0617 0.0272 0.703 14.777 8.083 524.488 1.669 35.955 6.990 0.31 187284. 0.4485
|
|
19.83 0.2684 0.5879 0.0589 0.0269 0.694 14.587 7.721 517.743 1.648 34.342 6.764 0.31 187509. 0.4242
|
|
21.48 0.2908 0.6160 0.0560 0.0264 0.682 14.338 7.340 508.917 1.620 32.650 6.542 0.31 187746. 0.4000
|
|
23.13 0.3131 0.6412 0.0530 0.0259 0.668 14.030 6.943 497.974 1.585 30.883 6.324 0.31 187995. 0.3761
|
|
24.78 0.3355 0.6637 0.0498 0.0252 0.650 13.662 6.531 484.904 1.543 29.049 6.109 0.31 188257. 0.3523
|
|
26.43 0.3579 0.6831 0.0466 0.0244 0.630 13.233 6.105 469.701 1.495 27.153 5.895 0.31 188531. 0.3287
|
|
28.09 0.3802 0.6995 0.0432 0.0235 0.607 12.745 5.666 452.367 1.440 25.202 5.681 0.31 188817. 0.3052
|
|
29.74 0.4026 0.7125 0.0398 0.0225 0.581 12.197 5.216 432.908 1.378 23.201 5.465 0.31 189116. 0.2817
|
|
31.39 0.4250 0.7217 0.0363 0.0214 0.552 11.589 4.756 411.338 1.309 21.156 5.245 0.31 189428. 0.2581
|
|
33.04 0.4473 0.7268 0.0327 0.0201 0.520 10.923 4.288 387.682 1.234 19.075 5.017 0.31 189753. 0.2345
|
|
34.69 0.4697 0.7268 0.0291 0.0188 0.485 10.198 3.813 361.977 1.152 16.962 4.778 0.31 190090. 0.2106
|
|
36.35 0.4921 0.7207 0.0254 0.0174 0.448 9.418 3.333 334.275 1.064 14.827 4.523 0.31 190440. 0.1864
|
|
38.00 0.5144 0.7067 0.0217 0.0158 0.409 8.583 2.850 304.650 0.970 12.675 4.243 0.31 190804. 0.1616
|
|
39.65 0.5368 0.6823 0.0180 0.0142 0.366 7.697 2.364 273.197 0.870 10.516 3.925 0.31 191180. 0.1362
|
|
41.30 0.5592 0.6430 0.0143 0.0125 0.322 6.763 1.879 240.040 0.764 8.359 3.551 0.31 191570. 0.1099
|
|
42.95 0.5815 0.5812 0.0107 0.0107 0.275 5.785 1.397 205.333 0.654 6.214 3.086 0.31 191973. 0.0823
|
|
44.61 0.6039 0.4822 0.0070 0.0088 0.227 4.769 0.920 169.267 0.539 4.093 2.466 0.32 192389. 0.0534
|
|
46.26 0.6263 0.3143 0.0034 0.0069 0.177 3.721 0.451 132.064 0.420 2.007 1.550 0.32 192817. 0.0235
|
|
47.91 0.6486 -0.0103 -0.0001 0.0049 0.126 2.640 -0.010 93.698 0.298 -0.045 -0.049 0.32 193244. 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 0.0843 0.0260 1.589 25.032 19.636 1184.631 2.828 87.343 7.518 0.41 247370. 0.7519
|
|
2.20 0.0224 0.0704 0.0829 0.0263 1.610 25.375 19.313 1200.853 2.867 85.904 7.295 0.41 247516. 0.7235
|
|
4.40 0.0447 0.1366 0.0814 0.0266 1.630 25.692 18.964 1215.853 2.903 84.354 7.075 0.41 247674. 0.6953
|
|
6.61 0.0671 0.1987 0.0798 0.0269 1.649 25.976 18.590 1229.303 2.935 82.689 6.859 0.41 247845. 0.6674
|
|
8.81 0.0894 0.2567 0.0781 0.0272 1.664 26.221 18.189 1240.881 2.962 80.905 6.649 0.41 248028. 0.6399
|
|
11.01 0.1118 0.3110 0.0762 0.0274 1.677 26.419 17.760 1250.252 2.985 78.996 6.443 0.41 248224. 0.6128
|
|
13.21 0.1342 0.3616 0.0743 0.0275 1.686 26.562 17.302 1257.060 3.001 76.957 6.243 0.41 248434. 0.5860
|
|
15.41 0.1565 0.4087 0.0722 0.0276 1.691 26.645 16.813 1260.952 3.010 74.784 6.048 0.41 248658. 0.5596
|
|
17.62 0.1789 0.4524 0.0699 0.0276 1.692 26.658 16.294 1261.565 3.012 72.474 5.858 0.41 248897. 0.5336
|
|
19.82 0.2012 0.4929 0.0676 0.0276 1.688 26.594 15.743 1258.539 3.005 70.024 5.674 0.41 249151. 0.5080
|
|
22.02 0.2236 0.5304 0.0651 0.0274 1.678 26.445 15.160 1251.505 2.988 67.430 5.494 0.41 249420. 0.4828
|
|
24.22 0.2460 0.5649 0.0624 0.0272 1.663 26.203 14.543 1240.072 2.960 64.689 5.319 0.41 249704. 0.4578
|
|
26.43 0.2683 0.5965 0.0596 0.0268 1.641 25.860 13.893 1223.840 2.922 61.797 5.149 0.41 250005. 0.4331
|
|
28.63 0.2907 0.6253 0.0567 0.0264 1.613 25.411 13.210 1202.556 2.871 58.760 4.983 0.41 250321. 0.4087
|
|
30.83 0.3130 0.6514 0.0536 0.0258 1.577 24.852 12.497 1176.127 2.808 55.588 4.820 0.41 250654. 0.3845
|
|
33.03 0.3354 0.6747 0.0505 0.0251 1.535 24.184 11.757 1144.521 2.732 52.293 4.659 0.41 251003. 0.3605
|
|
35.23 0.3578 0.6951 0.0472 0.0243 1.485 23.407 10.991 1107.726 2.645 48.886 4.500 0.42 251369. 0.3367
|
|
37.44 0.3801 0.7126 0.0438 0.0234 1.429 22.520 10.202 1065.742 2.544 45.378 4.342 0.42 251751. 0.3130
|
|
39.64 0.4025 0.7268 0.0403 0.0223 1.366 21.523 9.393 1018.581 2.432 41.780 4.183 0.42 252150. 0.2893
|
|
41.84 0.4248 0.7376 0.0368 0.0212 1.296 20.418 8.566 966.278 2.307 38.103 4.021 0.42 252566. 0.2656
|
|
44.04 0.4472 0.7443 0.0332 0.0199 1.219 19.205 7.725 908.890 2.170 34.359 3.855 0.42 252999. 0.2418
|
|
46.24 0.4696 0.7463 0.0295 0.0186 1.135 17.887 6.870 846.505 2.021 30.558 3.681 0.42 253449. 0.2177
|
|
48.45 0.4919 0.7425 0.0258 0.0171 1.045 16.466 6.006 779.253 1.860 26.715 3.496 0.42 253916. 0.1934
|
|
50.65 0.5143 0.7312 0.0220 0.0155 0.949 14.946 5.136 707.308 1.689 22.843 3.293 0.42 254401. 0.1684
|
|
52.85 0.5366 0.7099 0.0183 0.0138 0.846 13.331 4.262 630.905 1.506 18.957 3.064 0.42 254903. 0.1427
|
|
55.05 0.5590 0.6741 0.0145 0.0121 0.738 11.629 3.389 550.344 1.314 15.074 2.793 0.42 255422. 0.1160
|
|
57.25 0.5814 0.6159 0.0108 0.0102 0.625 9.847 2.521 466.006 1.113 11.213 2.454 0.42 255959. 0.0879
|
|
59.46 0.6037 0.5195 0.0071 0.0083 0.507 7.995 1.662 378.360 0.903 7.395 1.993 0.42 256513. 0.0580
|
|
61.66 0.6261 0.3485 0.0035 0.0063 0.386 6.085 0.818 287.949 0.687 3.640 1.289 0.42 257084. 0.0263
|
|
63.86 0.6484 -0.0083 -0.0001 0.0043 0.261 4.113 -0.013 194.635 0.465 -0.057 -0.030 0.42 257650. 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 0.0854 0.0261 3.124 39.375 31.100 2329.248 4.449 138.332 6.056 0.52 309186. 0.7622
|
|
2.77 0.0225 0.0713 0.0840 0.0265 3.167 39.928 30.591 2361.972 4.511 136.069 5.874 0.52 309371. 0.7333
|
|
5.54 0.0450 0.1383 0.0825 0.0268 3.208 40.439 30.042 2392.204 4.569 133.627 5.696 0.52 309571. 0.7046
|
|
8.31 0.0675 0.2010 0.0809 0.0271 3.244 40.897 29.452 2419.278 4.620 131.001 5.522 0.52 309786. 0.6763
|
|
11.07 0.0900 0.2598 0.0792 0.0274 3.275 41.290 28.817 2442.530 4.665 128.179 5.351 0.52 310018. 0.6483
|
|
13.84 0.1124 0.3147 0.0773 0.0276 3.301 41.607 28.138 2461.271 4.701 125.156 5.185 0.52 310266. 0.6207
|
|
16.61 0.1349 0.3658 0.0753 0.0278 3.319 41.835 27.411 2474.784 4.726 121.922 5.024 0.52 310532. 0.5936
|
|
19.38 0.1574 0.4134 0.0732 0.0279 3.329 41.963 26.635 2482.337 4.741 118.471 4.867 0.52 310816. 0.5668
|
|
22.15 0.1799 0.4577 0.0709 0.0279 3.330 41.977 25.809 2483.198 4.743 114.797 4.714 0.52 311118. 0.5405
|
|
24.92 0.2024 0.4987 0.0685 0.0278 3.321 41.866 24.931 2476.631 4.730 110.895 4.566 0.52 311440. 0.5145
|
|
27.68 0.2249 0.5367 0.0659 0.0276 3.301 41.617 24.002 2461.888 4.702 106.760 4.422 0.52 311780. 0.4889
|
|
30.45 0.2474 0.5717 0.0632 0.0274 3.270 41.216 23.019 2438.184 4.657 102.386 4.282 0.52 312140. 0.4636
|
|
33.22 0.2699 0.6038 0.0604 0.0270 3.225 40.650 21.980 2404.701 4.593 97.769 4.146 0.52 312521. 0.4387
|
|
35.99 0.2923 0.6332 0.0574 0.0265 3.166 39.910 20.889 2360.929 4.509 92.915 4.013 0.52 312922. 0.4139
|
|
38.76 0.3148 0.6598 0.0542 0.0259 3.093 38.993 19.749 2306.683 4.405 87.844 3.883 0.52 313343. 0.3895
|
|
41.53 0.3373 0.6837 0.0510 0.0252 3.006 37.898 18.564 2241.901 4.282 82.573 3.756 0.52 313785. 0.3652
|
|
44.29 0.3598 0.7048 0.0476 0.0243 2.905 36.625 17.338 2166.559 4.138 77.120 3.630 0.52 314247. 0.3411
|
|
47.06 0.3823 0.7230 0.0442 0.0233 2.790 35.173 16.076 2080.663 3.974 71.505 3.504 0.52 314731. 0.3171
|
|
49.83 0.4048 0.7381 0.0406 0.0223 2.661 33.543 14.781 1984.247 3.790 65.745 3.379 0.52 315236. 0.2931
|
|
52.60 0.4273 0.7497 0.0370 0.0211 2.518 31.736 13.457 1877.380 3.586 59.857 3.251 0.52 315762. 0.2692
|
|
55.37 0.4498 0.7574 0.0333 0.0198 2.360 29.755 12.109 1760.190 3.362 53.860 3.120 0.52 316309. 0.2450
|
|
58.14 0.4722 0.7604 0.0295 0.0183 2.190 27.603 10.741 1632.866 3.119 47.774 2.983 0.52 316878. 0.2207
|
|
60.90 0.4947 0.7576 0.0257 0.0168 2.006 25.284 9.357 1495.682 2.857 41.620 2.838 0.52 317469. 0.1959
|
|
63.67 0.5172 0.7474 0.0219 0.0151 1.809 22.804 7.963 1349.011 2.576 35.421 2.677 0.52 318081. 0.1705
|
|
66.44 0.5397 0.7268 0.0180 0.0134 1.600 20.173 6.565 1193.351 2.279 29.202 2.495 0.52 318715. 0.1443
|
|
69.21 0.5622 0.6910 0.0142 0.0115 1.380 17.401 5.169 1029.343 1.966 22.991 2.278 0.52 319372. 0.1169
|
|
71.98 0.5847 0.6309 0.0104 0.0096 1.150 14.501 3.781 857.800 1.638 16.819 1.999 0.52 320050. 0.0877
|
|
74.75 0.6072 0.5270 0.0066 0.0076 0.912 11.490 2.410 679.717 1.298 10.720 1.608 0.53 320751. 0.0563
|
|
77.51 0.6297 0.3304 0.0029 0.0056 0.665 8.389 1.064 496.229 0.948 4.731 0.972 0.53 321471. 0.0226
|
|
80.28 0.6521
|
|
|
|
|
|
|
|
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 0.0869 0.0266 5.487 57.638 45.573 4091.532 6.512 202.707 5.052 0.62 370980. 0.7697
|
|
3.29 0.0223 0.0708 0.0855 0.0269 5.564 58.453 44.847 4149.428 6.604 199.480 4.902 0.62 371202. 0.7409
|
|
6.59 0.0446 0.1374 0.0840 0.0273 5.636 59.207 44.063 4202.917 6.689 195.993 4.755 0.62 371441. 0.7124
|
|
9.88 0.0669 0.1998 0.0824 0.0276 5.700 59.882 43.218 4250.831 6.765 192.235 4.611 0.62 371699. 0.6842
|
|
13.18 0.0892 0.2583 0.0807 0.0279 5.756 60.462 42.310 4292.018 6.831 188.194 4.471 0.62 371976. 0.6564
|
|
16.47 0.1115 0.3131 0.0788 0.0281 5.800 60.930 41.335 4325.265 6.884 183.857 4.335 0.62 372273. 0.6289
|
|
19.77 0.1338 0.3642 0.0769 0.0282 5.833 61.269 40.290 4349.328 6.922 179.212 4.202 0.62 372591. 0.6019
|
|
23.06 0.1561 0.4118 0.0747 0.0283 5.851 61.461 39.175 4362.932 6.944 174.249 4.073 0.62 372930. 0.5753
|
|
26.36 0.1784 0.4562 0.0725 0.0283 5.853 61.487 37.985 4364.803 6.947 168.959 3.947 0.62 373290. 0.5490
|
|
29.65 0.2007 0.4974 0.0700 0.0283 5.838 61.330 36.721 4353.665 6.929 163.336 3.826 0.62 373673. 0.5232
|
|
32.95 0.2230 0.5356 0.0675 0.0281 5.804 60.972 35.380 4328.238 6.889 157.371 3.708 0.62 374079. 0.4977
|
|
36.24 0.2453 0.5709 0.0648 0.0278 5.749 60.394 33.961 4287.186 6.823 151.058 3.593 0.62 374508. 0.4725
|
|
39.54 0.2677 0.6035 0.0619 0.0275 5.671 59.575 32.461 4229.084 6.731 144.388 3.481 0.62 374960. 0.4476
|
|
42.83 0.2900 0.6334 0.0589 0.0270 5.569 58.503 30.883 4152.933 6.610 137.368 3.373 0.62 375437. 0.4230
|
|
46.13 0.3123 0.6607 0.0558 0.0264 5.442 57.170 29.232 4058.343 6.459 130.022 3.267 0.62 375937. 0.3986
|
|
49.42 0.3346 0.6854 0.0525 0.0256 5.291 55.576 27.513 3945.209 6.279 122.378 3.163 0.62 376462. 0.3744
|
|
52.72 0.3569 0.7074 0.0491 0.0248 5.114 53.721 25.734 3813.495 6.069 114.464 3.061 0.62 377012. 0.3504
|
|
56.01 0.3792 0.7267 0.0456 0.0238 4.912 51.604 23.899 3663.214 5.830 106.305 2.959 0.62 377586. 0.3265
|
|
59.31 0.4015 0.7430 0.0420 0.0227 4.686 49.226 22.016 3494.426 5.562 97.926 2.858 0.62 378184. 0.3026
|
|
62.60 0.4238 0.7561 0.0383 0.0215 4.435 46.590 20.089 3307.257 5.264 89.355 2.755 0.62 378808. 0.2787
|
|
65.90 0.4461 0.7656 0.0346 0.0201 4.160 43.697 18.124 3101.913 4.937 80.617 2.650 0.63 379457. 0.2546
|
|
69.19 0.4684 0.7709 0.0308 0.0187 3.860 40.553 16.129 2878.714 4.582 71.742 2.541 0.63 380131. 0.2303
|
|
72.49 0.4907 0.7709 0.0269 0.0171 3.538 37.163 14.109 2638.113 4.199 62.758 2.426 0.63 380830. 0.2056
|
|
75.78 0.5130 0.7642 0.0230 0.0155 3.193 33.538 12.073 2380.733 3.789 53.699 2.300 0.63 381555. 0.1804
|
|
79.08 0.5353 0.7482 0.0191 0.0137 2.826 29.687 10.027 2107.408 3.354 44.601 2.158 0.63 382306. 0.1542
|
|
82.37 0.5576 0.7187 0.0152 0.0118 2.440 25.627 7.982 1819.213 2.895 35.503 1.990 0.63 383083. 0.1269
|
|
85.67 0.5799 0.6675 0.0113 0.0099 2.035 21.377 5.947 1517.517 2.415 26.451 1.777 0.63 383885. 0.0978
|
|
88.96 0.6022 0.5779 0.0075 0.0078 1.615 16.961 3.933 1204.015 1.916 17.494 1.482 0.63 384713. 0.0663
|
|
92.26 0.6245 0.4067 0.0037 0.0057 1.181 12.406 1.952 880.693 1.402 8.684 1.005 0.63 385566. 0.0317
|
|
95.55 0.6468 0.0003 0.0000 0.0036 0.733 7.705 0.001 546.968 0.871 0.004 0.001 0.63 386409. 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 0.0889 0.0273 8.964 80.710 63.427 6684.254 9.119 282.123 4.304 0.72 432744. 0.7736
|
|
3.84 0.0223 0.0703 0.0875 0.0277 9.088 81.827 62.447 6776.778 9.245 277.766 4.180 0.72 433004. 0.7454
|
|
7.68 0.0446 0.1366 0.0860 0.0281 9.203 82.863 61.385 6862.537 9.362 273.039 4.057 0.72 433286. 0.7174
|
|
11.52 0.0668 0.1988 0.0844 0.0284 9.306 83.793 60.236 6939.565 9.467 267.930 3.937 0.72 433589. 0.6896
|
|
15.36 0.0891 0.2571 0.0827 0.0286 9.395 84.594 58.997 7005.895 9.557 262.417 3.820 0.72 433914. 0.6621
|
|
19.20 0.1114 0.3118 0.0808 0.0289 9.467 85.240 57.663 7059.467 9.630 256.485 3.705 0.72 434263. 0.6349
|
|
23.03 0.1337 0.3629 0.0788 0.0290 9.519 85.707 56.231 7098.119 9.683 250.115 3.593 0.72 434636. 0.6081
|
|
26.87 0.1559 0.4105 0.0767 0.0291 9.548 85.967 54.697 7119.645 9.713 243.292 3.485 0.72 435033. 0.5816
|
|
30.71 0.1782 0.4550 0.0744 0.0291 9.551 85.993 53.059 7121.813 9.715 236.005 3.379 0.72 435456. 0.5555
|
|
34.55 0.2005 0.4964 0.0719 0.0290 9.525 85.759 51.314 7102.439 9.689 228.243 3.277 0.72 435906. 0.5298
|
|
38.39 0.2228 0.5348 0.0693 0.0289 9.467 85.240 49.459 7059.415 9.630 219.995 3.178 0.72 436381. 0.5044
|
|
42.23 0.2450 0.5705 0.0666 0.0286 9.375 84.409 47.494 6990.595 9.536 211.253 3.082 0.72 436884. 0.4793
|
|
46.07 0.2673 0.6035 0.0636 0.0282 9.245 83.238 45.414 6893.667 9.404 202.003 2.988 0.72 437415. 0.4544
|
|
49.91 0.2896 0.6339 0.0606 0.0277 9.075 81.708 43.222 6766.885 9.231 192.252 2.897 0.72 437973. 0.4298
|
|
53.75 0.3119 0.6617 0.0574 0.0270 8.864 79.808 40.925 6609.575 9.017 182.033 2.808 0.73 438558. 0.4055
|
|
57.59 0.3341 0.6871 0.0540 0.0263 8.611 77.538 38.531 6421.560 8.760 171.386 2.722 0.73 439173. 0.3812
|
|
61.43 0.3564 0.7099 0.0505 0.0254 8.318 74.897 36.049 6202.833 8.462 160.348 2.636 0.73 439815. 0.3572
|
|
65.27 0.3787 0.7300 0.0469 0.0243 7.984 71.886 33.489 5953.449 8.122 148.957 2.551 0.73 440486. 0.3332
|
|
69.10 0.4010 0.7473 0.0432 0.0232 7.608 68.506 30.857 5673.533 7.740 137.250 2.467 0.73 441185. 0.3092
|
|
72.94 0.4232 0.7616 0.0395 0.0219 7.192 64.760 28.162 5363.327 7.317 125.263 2.382 0.73 441914. 0.2852
|
|
76.78 0.4455 0.7724 0.0356 0.0205 6.736 60.654 25.412 5023.224 6.853 113.033 2.295 0.73 442671. 0.2610
|
|
80.62 0.4678 0.7791 0.0317 0.0190 6.241 56.193 22.617 4653.836 6.349 100.600 2.204 0.73 443457. 0.2366
|
|
84.46 0.4901 0.7808 0.0277 0.0174 5.707 51.390 19.786 4256.040 5.806 88.007 2.109 0.73 444273. 0.2117
|
|
88.30 0.5123 0.7759 0.0237 0.0157 5.137 46.258 16.929 3831.026 5.226 75.299 2.004 0.73 445119. 0.1861
|
|
92.14 0.5346 0.7619 0.0197 0.0138 4.533 40.817 14.058 3380.403 4.611 62.528 1.886 0.73 445994. 0.1596
|
|
95.98 0.5569 0.7345 0.0157 0.0119 3.897 35.092 11.185 2906.266 3.965 49.749 1.746 0.73 446898. 0.1317
|
|
99.82 0.5792 0.6852 0.0117 0.0099 3.234 29.116 8.324 2411.297 3.289 37.026 1.566 0.73 447833. 0.1020
|
|
103.66 0.6014 0.5961 0.0077 0.0078 2.546 22.928 5.492 1898.835 2.590 24.428 1.312 0.74 448798. 0.0694
|
|
107.50 0.6237 0.4211 0.0038 0.0056 1.841 16.576 2.705 1372.830 1.873 12.031 0.894 0.74 449791. 0.0332
|
|
111.34 0.6460 -0.0124 -0.0001 0.0034 1.116 10.045 -0.047 831.871 1.135 -0.207 -0.025 0.74 450763. 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 0.0914 0.0303 14.831 116.844 85.181 11059.220 13.201 378.886 3.494 0.83 494461. 0.7277
|
|
4.38 0.0222 0.0656 0.0901 0.0305 14.940 117.708 83.932 11141.017 13.299 373.329 3.417 0.83 494760. 0.7065
|
|
8.75 0.0444 0.1282 0.0886 0.0307 15.036 118.458 82.569 11212.013 13.383 367.268 3.340 0.83 495084. 0.6850
|
|
13.13 0.0667 0.1879 0.0870 0.0309 15.113 119.070 81.088 11269.917 13.452 360.678 3.263 0.83 495433. 0.6632
|
|
17.51 0.0889 0.2446 0.0853 0.0310 15.170 119.519 79.481 11312.432 13.503 353.533 3.187 0.83 495808. 0.6412
|
|
21.89 0.1111 0.2984 0.0834 0.0311 15.203 119.780 77.744 11337.102 13.533 345.805 3.110 0.83 496209. 0.6189
|
|
26.26 0.1333 0.3494 0.0814 0.0311 15.209 119.825 75.870 11341.336 13.538 337.470 3.034 0.83 496638. 0.5965
|
|
30.64 0.1556 0.3974 0.0792 0.0310 15.184 119.625 73.855 11322.451 13.515 328.508 2.959 0.83 497096. 0.5738
|
|
35.02 0.1778 0.4427 0.0769 0.0309 15.124 119.152 71.695 11277.624 13.462 318.900 2.883 0.83 497583. 0.5510
|
|
39.39 0.2000 0.4851 0.0744 0.0307 15.025 118.373 69.386 11203.950 13.374 308.631 2.809 0.83 498100. 0.5280
|
|
43.77 0.2222 0.5249 0.0718 0.0304 14.883 117.258 66.926 11098.419 13.248 297.688 2.735 0.83 498647. 0.5050
|
|
48.15 0.2445 0.5619 0.0690 0.0300 14.695 115.772 64.312 10957.783 13.080 286.058 2.662 0.83 499225. 0.4818
|
|
52.53 0.2667 0.5963 0.0660 0.0295 14.454 113.877 61.539 10778.405 12.866 273.725 2.590 0.83 499834. 0.4585
|
|
56.90 0.2889 0.6282 0.0629 0.0289 14.157 111.539 58.609 10557.090 12.602 260.692 2.518 0.83 500474. 0.4350
|
|
61.28 0.3111 0.6574 0.0596 0.0282 13.802 108.740 55.530 10292.196 12.285 246.998 2.447 0.83 501146. 0.4115
|
|
65.66 0.3333 0.6841 0.0561 0.0274 13.389 105.483 52.315 9983.903 11.917 232.699 2.377 0.83 501850. 0.3880
|
|
70.04 0.3556 0.7079 0.0525 0.0264 12.921 101.796 48.976 9634.946 11.501 217.846 2.306 0.83 502586. 0.3641
|
|
74.41 0.3778 0.7287 0.0488 0.0253 12.396 97.661 45.524 9243.577 11.034 202.492 2.234 0.83 503354. 0.3401
|
|
78.79 0.4000 0.7464 0.0450 0.0241 11.815 93.081 41.971 8810.094 10.516 186.687 2.161 0.83 504154. 0.3159
|
|
83.17 0.4222 0.7605 0.0411 0.0228 11.177 88.061 38.328 8334.889 9.949 170.481 2.086 0.83 504987. 0.2914
|
|
87.54 0.4445 0.7705 0.0371 0.0214 10.484 82.599 34.606 7817.956 9.332 153.928 2.008 0.83 505852. 0.2665
|
|
91.92 0.4667 0.7757 0.0331 0.0199 9.738 76.721 30.818 7261.563 8.668 137.080 1.925 0.83 506751. 0.2412
|
|
96.30 0.4889 0.7746 0.0289 0.0183 8.943 70.458 26.977 6668.836 7.960 119.993 1.835 0.83 507682. 0.2151
|
|
100.68 0.5111 0.7650 0.0248 0.0166 8.104 63.851 23.095 6043.438 7.214 102.729 1.733 0.84 508646. 0.1880
|
|
105.05 0.5333 0.7437 0.0206 0.0148 7.228 56.944 19.190 5389.726 6.434 85.355 1.615 0.84 509644. 0.1596
|
|
109.43 0.5556 0.7053 0.0164 0.0129 6.320 49.795 15.276 4713.040 5.626 67.948 1.470 0.84 510675. 0.1297
|
|
113.81 0.5778 0.6403 0.0122 0.0110 5.390 42.469 11.374 4019.671 4.798 50.592 1.283 0.84 511740. 0.0977
|
|
118.18 0.6000 0.5318 0.0081 0.0091 4.448 35.042 7.505 3316.669 3.959 33.383 1.026 0.84 512838. 0.0635
|
|
122.56 0.6222 0.3446 0.0040 0.0072 3.502 27.594 3.693 2611.755 3.118 16.427 0.641 0.84 513969. 0.0278
|
|
126.94 0.6445 -0.0089 -0.0001 0.0052 2.551 20.100 -0.067 1902.441 2.271 -0.299 -0.016 0.84 515090. 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 0.0932 0.0390 27.152 190.147 109.914 20247.016 21.483 488.896 2.462 0.93 556176. 0.5826
|
|
4.96 0.0224 0.0528 0.0920 0.0390 27.174 190.302 108.498 20263.432 21.500 482.601 2.429 0.93 556512. 0.5709
|
|
9.93 0.0448 0.1042 0.0906 0.0390 27.151 190.145 106.929 20246.719 21.482 475.618 2.395 0.93 556876. 0.5590
|
|
14.89 0.0672 0.1542 0.0892 0.0389 27.080 189.644 105.195 20193.422 21.426 467.907 2.363 0.93 557270. 0.5469
|
|
19.85 0.0896 0.2029 0.0876 0.0387 26.955 188.771 103.287 20100.490 21.327 459.420 2.331 0.93 557695. 0.5346
|
|
24.82 0.1120 0.2501 0.0858 0.0384 26.774 187.503 101.195 19965.385 21.184 450.115 2.299 0.93 558152. 0.5219
|
|
29.78 0.1344 0.2960 0.0838 0.0381 26.533 185.817 98.910 19785.941 20.994 439.951 2.267 0.93 558641. 0.5089
|
|
34.74 0.1568 0.3406 0.0817 0.0376 26.231 183.699 96.424 19560.422 20.754 428.895 2.236 0.93 559164. 0.4955
|
|
39.71 0.1792 0.3837 0.0795 0.0371 25.865 181.135 93.732 19287.354 20.465 416.919 2.204 0.93 559722. 0.4816
|
|
44.67 0.2016 0.4254 0.0770 0.0365 25.433 178.112 90.827 18965.475 20.123 403.999 2.172 0.93 560314. 0.4672
|
|
49.63 0.2240 0.4655 0.0744 0.0358 24.934 174.618 87.707 18593.482 19.728 390.120 2.140 0.93 560941. 0.4522
|
|
54.60 0.2464 0.5041 0.0715 0.0350 24.366 170.640 84.367 18169.803 19.279 375.264 2.106 0.93 561604. 0.4366
|
|
59.56 0.2688 0.5409 0.0685 0.0340 23.725 166.153 80.803 17692.061 18.772 359.411 2.072 0.93 562303. 0.4202
|
|
64.52 0.2912 0.5759 0.0653 0.0330 23.009 161.137 77.014 17158.020 18.205 342.560 2.036 0.93 563039. 0.4032
|
|
69.49 0.3136 0.6089 0.0619 0.0319 22.218 155.593 73.014 16567.594 17.579 324.768 1.999 0.93 563810. 0.3855
|
|
74.45 0.3360 0.6399 0.0583 0.0306 21.352 149.531 68.820 15922.142 16.894 306.113 1.960 0.93 564619. 0.3670
|
|
79.41 0.3584 0.6685 0.0546 0.0293 20.414 142.965 64.451 15223.050 16.152 286.676 1.920 0.93 565464. 0.3479
|
|
84.38 0.3808 0.6932 0.0508 0.0279 19.446 136.187 59.918 14501.239 15.386 266.517 1.874 0.93 566345. 0.3274
|
|
89.34 0.4032 0.7130 0.0468 0.0265 18.458 129.264 55.240 13764.064 14.604 245.709 1.820 0.94 567263. 0.3053
|
|
94.30 0.4256 0.7266 0.0428 0.0250 17.454 122.236 50.433 13015.795 13.810 224.326 1.757 0.94 568218. 0.2817
|
|
99.27 0.4480 0.7285 0.0386 0.0237 16.533 115.781 45.503 12328.380 13.081 202.398 1.674 0.94 569209. 0.2549
|
|
104.23 0.4704 0.7207 0.0343 0.0224 15.611 109.323 40.479 11640.765 12.351 180.049 1.577 0.94 570238. 0.2265
|
|
109.19 0.4928 0.7030 0.0300 0.0210 14.656 102.641 35.385 10929.256 11.596 157.391 1.468 0.94 571304. 0.1971
|
|
114.16 0.5152 0.6729 0.0256 0.0196 13.682 95.816 30.243 10202.553 10.825 134.521 1.345 0.94 572407. 0.1669
|
|
119.12 0.5376 0.6272 0.0213 0.0182 12.702 88.952 25.081 9471.695 10.050 111.559 1.201 0.94 573548. 0.1357
|
|
124.08 0.5600 0.5622 0.0169 0.0168 11.727 82.127 19.926 8744.888 9.279 88.633 1.034 0.94 574726. 0.1041
|
|
129.05 0.5824 0.4733 0.0126 0.0155 10.769 75.418 14.813 8030.556 8.521 65.887 0.837 0.94 575943. 0.0727
|
|
134.01 0.6048 0.3551 0.0083 0.0141 9.839 68.904 9.776 7336.946 7.785 43.484 0.604 0.95 577199. 0.0426
|
|
138.97 0.6272 0.2011 0.0041 0.0128 8.944 62.638 4.853 6669.728 7.077 21.587 0.330 0.95 578493. 0.0164
|
|
143.94 0.6496 0.0006 0.0000 0.0115 8.043 56.329 0.013 5997.897 6.364 0.057 0.001 0.95 579830. 0.0000
|
|
|
|
|
|
|