612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x5.5MR (14x55MR.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 0.0881 0.0340 0.001 0.093 0.108 1.098 0.010 0.480 44.561 0.06 22295. 0.6135
|
|
0.24 0.0181 0.0459 0.0864 0.0341 0.001 0.093 0.106 1.099 0.010 0.470 43.645 0.06 22307. 0.5949
|
|
0.48 0.0362 0.0898 0.0845 0.0340 0.001 0.093 0.103 1.099 0.010 0.460 42.721 0.06 22320. 0.5760
|
|
0.72 0.0543 0.1318 0.0826 0.0340 0.001 0.093 0.101 1.098 0.010 0.450 41.787 0.06 22334. 0.5569
|
|
0.96 0.0723 0.1717 0.0806 0.0339 0.001 0.093 0.099 1.096 0.010 0.439 40.838 0.06 22348. 0.5376
|
|
1.20 0.0904 0.2096 0.0784 0.0338 0.001 0.092 0.096 1.092 0.010 0.427 39.879 0.06 22363. 0.5179
|
|
1.44 0.1085 0.2454 0.0762 0.0337 0.001 0.092 0.093 1.088 0.010 0.415 38.908 0.06 22378. 0.4981
|
|
1.68 0.1266 0.2790 0.0739 0.0335 0.001 0.091 0.090 1.082 0.010 0.402 37.917 0.06 22395. 0.4780
|
|
1.92 0.1447 0.3104 0.0714 0.0333 0.001 0.091 0.087 1.075 0.010 0.389 36.910 0.06 22412. 0.4575
|
|
2.16 0.1628 0.3394 0.0689 0.0330 0.001 0.090 0.084 1.067 0.010 0.375 35.880 0.06 22430. 0.4368
|
|
2.40 0.1808 0.3660 0.0663 0.0327 0.001 0.089 0.081 1.057 0.010 0.361 34.826 0.06 22449. 0.4157
|
|
2.64 0.1989 0.3901 0.0635 0.0324 0.001 0.088 0.078 1.045 0.010 0.346 33.742 0.06 22468. 0.3944
|
|
2.88 0.2170 0.4115 0.0607 0.0320 0.001 0.087 0.074 1.032 0.010 0.330 32.627 0.06 22489. 0.3726
|
|
3.12 0.2351 0.4300 0.0577 0.0315 0.001 0.086 0.071 1.018 0.010 0.314 31.468 0.06 22510. 0.3504
|
|
3.36 0.2532 0.4453 0.0546 0.0310 0.001 0.085 0.067 1.001 0.010 0.297 30.264 0.06 22532. 0.3278
|
|
3.60 0.2713 0.4574 0.0514 0.0305 0.001 0.083 0.063 0.984 0.009 0.280 29.009 0.06 22555. 0.3049
|
|
3.84 0.2893 0.4658 0.0481 0.0299 0.001 0.082 0.059 0.964 0.009 0.262 27.698 0.06 22579. 0.2817
|
|
4.08 0.3074 0.4703 0.0447 0.0292 0.001 0.080 0.055 0.944 0.009 0.244 26.322 0.06 22604. 0.2582
|
|
4.32 0.3255 0.4706 0.0413 0.0286 0.001 0.078 0.051 0.922 0.009 0.225 24.874 0.06 22630. 0.2344
|
|
4.56 0.3436 0.4662 0.0378 0.0278 0.001 0.076 0.046 0.898 0.009 0.206 23.343 0.06 22656. 0.2103
|
|
4.80 0.3617 0.4566 0.0342 0.0271 0.001 0.074 0.042 0.873 0.008 0.186 21.719 0.06 22684. 0.1861
|
|
5.03 0.3798 0.4412 0.0305 0.0262 0.001 0.072 0.037 0.847 0.008 0.166 19.988 0.06 22712. 0.1618
|
|
5.27 0.3979 0.4194 0.0268 0.0254 0.001 0.069 0.033 0.819 0.008 0.146 18.135 0.06 22742. 0.1376
|
|
5.51 0.4159 0.3902 0.0230 0.0245 0.001 0.067 0.028 0.790 0.008 0.125 16.143 0.06 22772. 0.1135
|
|
5.75 0.4340 0.3529 0.0191 0.0235 0.001 0.064 0.023 0.760 0.007 0.104 13.990 0.06 22804. 0.0898
|
|
5.99 0.4521 0.3062 0.0153 0.0226 0.001 0.062 0.019 0.728 0.007 0.083 11.652 0.06 22836. 0.0668
|
|
6.23 0.4702 0.2487 0.0114 0.0215 0.001 0.059 0.014 0.695 0.007 0.062 9.101 0.06 22869. 0.0450
|
|
6.47 0.4883 0.1789 0.0075 0.0205 0.001 0.056 0.009 0.661 0.006 0.041 6.303 0.06 22904. 0.0253
|
|
6.71 0.5064 0.0948 0.0036 0.0194 0.001 0.053 0.004 0.625 0.006 0.020 3.221 0.06 22939. 0.0090
|
|
6.95 0.5244 -0.0061 -0.0002 0.0183 0.001 0.050 0.000 0.589 0.006 -0.001 -0.200 0.06 22974. 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 0.0884 0.0313 0.011 0.342 0.433 8.087 0.039 1.925 24.276 0.11 44590. 0.6694
|
|
0.50 0.0187 0.0516 0.0866 0.0314 0.011 0.342 0.424 8.099 0.039 1.886 23.742 0.11 44615. 0.6479
|
|
0.99 0.0374 0.1009 0.0847 0.0314 0.011 0.342 0.415 8.102 0.039 1.844 23.207 0.11 44642. 0.6262
|
|
1.49 0.0561 0.1479 0.0826 0.0314 0.011 0.342 0.405 8.098 0.039 1.800 22.671 0.11 44670. 0.6045
|
|
1.98 0.0748 0.1925 0.0805 0.0313 0.011 0.342 0.394 8.085 0.039 1.754 22.130 0.11 44699. 0.5825
|
|
2.48 0.0935 0.2347 0.0783 0.0312 0.011 0.341 0.384 8.058 0.038 1.706 21.588 0.11 44730. 0.5603
|
|
2.98 0.1122 0.2745 0.0760 0.0311 0.011 0.339 0.372 8.022 0.038 1.655 21.043 0.11 44763. 0.5380
|
|
3.47 0.1309 0.3119 0.0736 0.0309 0.011 0.337 0.360 7.974 0.038 1.602 20.492 0.11 44797. 0.5155
|
|
3.97 0.1497 0.3468 0.0710 0.0306 0.011 0.334 0.348 7.913 0.038 1.547 19.936 0.11 44833. 0.4927
|
|
4.46 0.1684 0.3791 0.0684 0.0304 0.011 0.331 0.335 7.839 0.037 1.489 19.371 0.11 44871. 0.4698
|
|
4.96 0.1871 0.4088 0.0656 0.0300 0.010 0.328 0.321 7.751 0.037 1.429 18.798 0.11 44910. 0.4465
|
|
5.46 0.2058 0.4356 0.0627 0.0296 0.010 0.323 0.307 7.647 0.037 1.366 18.212 0.11 44952. 0.4230
|
|
5.95 0.2245 0.4596 0.0597 0.0292 0.010 0.318 0.292 7.529 0.036 1.300 17.613 0.11 44995. 0.3991
|
|
6.45 0.2432 0.4804 0.0566 0.0286 0.010 0.312 0.277 7.393 0.035 1.232 16.994 0.11 45040. 0.3748
|
|
6.94 0.2619 0.4978 0.0533 0.0281 0.010 0.306 0.261 7.242 0.035 1.161 16.353 0.11 45086. 0.3502
|
|
7.44 0.2806 0.5117 0.0500 0.0274 0.009 0.299 0.245 7.077 0.034 1.089 15.687 0.11 45135. 0.3253
|
|
7.94 0.2993 0.5216 0.0465 0.0267 0.009 0.291 0.228 6.896 0.033 1.014 14.993 0.11 45185. 0.3000
|
|
8.43 0.3180 0.5273 0.0430 0.0260 0.009 0.283 0.211 6.701 0.032 0.937 14.263 0.11 45238. 0.2744
|
|
8.93 0.3367 0.5281 0.0394 0.0251 0.009 0.274 0.193 6.491 0.031 0.859 13.492 0.11 45292. 0.2485
|
|
9.42 0.3554 0.5236 0.0357 0.0243 0.008 0.265 0.175 6.266 0.030 0.779 12.672 0.11 45349. 0.2222
|
|
9.92 0.3741 0.5129 0.0320 0.0233 0.008 0.255 0.157 6.026 0.029 0.697 11.794 0.11 45407. 0.1957
|
|
10.42 0.3928 0.4953 0.0282 0.0223 0.008 0.244 0.138 5.770 0.028 0.614 10.846 0.11 45467. 0.1689
|
|
10.91 0.4116 0.4695 0.0243 0.0213 0.007 0.232 0.119 5.500 0.026 0.529 9.814 0.11 45530. 0.1419
|
|
11.41 0.4303 0.4341 0.0204 0.0202 0.007 0.220 0.100 5.216 0.025 0.444 8.679 0.11 45594. 0.1149
|
|
11.90 0.4490 0.3871 0.0164 0.0190 0.007 0.208 0.080 4.917 0.023 0.358 7.418 0.11 45661. 0.0882
|
|
12.40 0.4677 0.3263 0.0124 0.0178 0.006 0.195 0.061 4.605 0.022 0.271 6.002 0.11 45729. 0.0621
|
|
12.90 0.4864 0.2483 0.0085 0.0166 0.006 0.181 0.041 4.280 0.020 0.184 4.391 0.11 45800. 0.0375
|
|
13.39 0.5051 0.1488 0.0045 0.0153 0.005 0.167 0.022 3.944 0.019 0.098 2.534 0.11 45872. 0.0158
|
|
13.89 0.5238 0.0216 0.0006 0.0139 0.005 0.152 0.003 3.598 0.017 0.013 0.356 0.11 45945. 0.0008
|
|
14.38 0.5425
|
|
|
|
|
|
|
|
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 0.0886 0.0301 0.035 0.740 0.977 26.270 0.084 4.344 16.861 0.17 66884. 0.6983
|
|
0.72 0.0182 0.0523 0.0869 0.0302 0.035 0.742 0.957 26.319 0.084 4.257 16.494 0.17 66921. 0.6763
|
|
1.45 0.0364 0.1023 0.0850 0.0302 0.035 0.742 0.937 26.337 0.084 4.166 16.128 0.17 66960. 0.6542
|
|
2.17 0.0546 0.1500 0.0831 0.0302 0.035 0.742 0.915 26.331 0.084 4.070 15.763 0.17 67000. 0.6320
|
|
2.89 0.0728 0.1954 0.0810 0.0302 0.035 0.741 0.893 26.298 0.084 3.971 15.396 0.17 67043. 0.6097
|
|
3.62 0.0910 0.2384 0.0789 0.0301 0.035 0.739 0.869 26.220 0.083 3.865 15.030 0.17 67088. 0.5872
|
|
4.34 0.1092 0.2791 0.0766 0.0300 0.035 0.736 0.844 26.108 0.083 3.755 14.664 0.17 67135. 0.5647
|
|
5.07 0.1274 0.3175 0.0743 0.0298 0.035 0.732 0.818 25.964 0.083 3.640 14.295 0.17 67185. 0.5420
|
|
5.79 0.1456 0.3534 0.0718 0.0296 0.035 0.726 0.791 25.769 0.082 3.519 13.926 0.17 67237. 0.5191
|
|
6.51 0.1638 0.3870 0.0693 0.0293 0.034 0.720 0.763 25.538 0.081 3.394 13.553 0.17 67292. 0.4962
|
|
7.24 0.1820 0.4180 0.0666 0.0290 0.034 0.711 0.734 25.252 0.080 3.263 13.176 0.17 67349. 0.4730
|
|
7.96 0.2001 0.4465 0.0638 0.0286 0.033 0.702 0.703 24.922 0.079 3.127 12.794 0.17 67408. 0.4496
|
|
8.68 0.2183 0.4723 0.0609 0.0282 0.033 0.691 0.671 24.539 0.078 2.985 12.405 0.17 67470. 0.4259
|
|
9.41 0.2365 0.4952 0.0579 0.0277 0.032 0.679 0.638 24.099 0.077 2.837 12.006 0.17 67535. 0.4019
|
|
10.13 0.2547 0.5151 0.0548 0.0271 0.032 0.665 0.604 23.606 0.075 2.685 11.597 0.17 67602. 0.3776
|
|
10.86 0.2729 0.5318 0.0516 0.0265 0.031 0.650 0.568 23.062 0.073 2.527 11.174 0.17 67672. 0.3530
|
|
11.58 0.2911 0.5450 0.0483 0.0258 0.030 0.633 0.532 22.467 0.072 2.365 10.736 0.17 67744. 0.3281
|
|
12.30 0.3093 0.5543 0.0449 0.0250 0.029 0.615 0.494 21.821 0.069 2.199 10.278 0.17 67820. 0.3029
|
|
13.03 0.3275 0.5595 0.0414 0.0242 0.028 0.595 0.456 21.123 0.067 2.030 9.798 0.17 67898. 0.2774
|
|
13.75 0.3457 0.5600 0.0379 0.0234 0.027 0.574 0.417 20.373 0.065 1.856 9.291 0.17 67978. 0.2515
|
|
14.47 0.3639 0.5552 0.0343 0.0225 0.026 0.551 0.378 19.571 0.062 1.679 8.750 0.17 68062. 0.2253
|
|
15.20 0.3821 0.5442 0.0306 0.0215 0.025 0.527 0.337 18.717 0.060 1.499 8.168 0.17 68148. 0.1987
|
|
15.92 0.4003 0.5260 0.0269 0.0204 0.024 0.502 0.296 17.811 0.057 1.316 7.537 0.17 68238. 0.1718
|
|
16.64 0.4185 0.4994 0.0231 0.0193 0.023 0.475 0.254 16.853 0.054 1.131 6.844 0.17 68330. 0.1446
|
|
17.37 0.4367 0.4625 0.0193 0.0182 0.021 0.446 0.212 15.845 0.050 0.944 6.074 0.17 68425. 0.1173
|
|
18.09 0.4549 0.4131 0.0154 0.0170 0.020 0.417 0.170 14.788 0.047 0.755 5.208 0.17 68523. 0.0899
|
|
18.82 0.4731 0.3479 0.0116 0.0157 0.018 0.386 0.127 13.685 0.044 0.566 4.218 0.17 68624. 0.0631
|
|
19.54 0.4913 0.2627 0.0077 0.0144 0.017 0.353 0.085 12.540 0.040 0.377 3.066 0.17 68728. 0.0374
|
|
20.26 0.5095 0.1511 0.0039 0.0130 0.015 0.320 0.043 11.357 0.036 0.189 1.701 0.17 68834. 0.0147
|
|
20.99 0.5277 0.0027 0.0001 0.0116 0.014 0.286 0.001 10.134 0.032 0.003 0.029 0.17 68939. 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 0.0889 0.0295 0.082 1.287 1.742 60.922 0.145 7.747 12.966 0.22 89178. 0.7172
|
|
0.97 0.0183 0.0538 0.0871 0.0296 0.082 1.290 1.707 61.052 0.146 7.592 12.681 0.22 89227. 0.6944
|
|
1.94 0.0365 0.1052 0.0853 0.0296 0.082 1.291 1.670 61.104 0.146 7.429 12.397 0.22 89278. 0.6715
|
|
2.90 0.0548 0.1542 0.0833 0.0296 0.082 1.291 1.632 61.096 0.146 7.258 12.114 0.22 89333. 0.6486
|
|
3.87 0.0730 0.2008 0.0813 0.0295 0.082 1.290 1.592 61.025 0.146 7.080 11.830 0.22 89390. 0.6256
|
|
4.84 0.0913 0.2450 0.0791 0.0295 0.082 1.286 1.549 60.843 0.145 6.891 11.548 0.22 89451. 0.6024
|
|
5.81 0.1095 0.2869 0.0768 0.0293 0.081 1.280 1.505 60.578 0.145 6.693 11.267 0.22 89514. 0.5793
|
|
6.78 0.1278 0.3263 0.0745 0.0292 0.081 1.273 1.459 60.233 0.144 6.488 10.985 0.22 89581. 0.5561
|
|
7.74 0.1460 0.3633 0.0720 0.0289 0.080 1.263 1.410 59.763 0.143 6.272 10.702 0.22 89650. 0.5327
|
|
8.71 0.1643 0.3979 0.0694 0.0287 0.079 1.251 1.360 59.203 0.141 6.049 10.418 0.22 89723. 0.5092
|
|
9.68 0.1825 0.4299 0.0667 0.0283 0.078 1.236 1.307 58.511 0.140 5.814 10.132 0.22 89800. 0.4855
|
|
10.65 0.2008 0.4594 0.0639 0.0279 0.077 1.219 1.252 57.707 0.138 5.570 9.843 0.22 89880. 0.4617
|
|
11.61 0.2190 0.4863 0.0610 0.0275 0.076 1.200 1.195 56.774 0.136 5.317 9.550 0.22 89963. 0.4376
|
|
12.58 0.2373 0.5102 0.0580 0.0270 0.075 1.177 1.136 55.699 0.133 5.053 9.250 0.22 90049. 0.4132
|
|
13.55 0.2555 0.5312 0.0549 0.0264 0.073 1.151 1.074 54.494 0.130 4.779 8.943 0.22 90140. 0.3885
|
|
14.52 0.2738 0.5491 0.0516 0.0257 0.071 1.123 1.011 53.161 0.127 4.497 8.627 0.22 90233. 0.3636
|
|
15.49 0.2920 0.5635 0.0483 0.0250 0.069 1.092 0.946 51.701 0.123 4.208 8.300 0.22 90330. 0.3383
|
|
16.45 0.3103 0.5741 0.0449 0.0243 0.067 1.059 0.879 50.112 0.120 3.911 7.959 0.22 90431. 0.3128
|
|
17.42 0.3285 0.5806 0.0414 0.0234 0.065 1.023 0.811 48.395 0.116 3.608 7.602 0.22 90536. 0.2869
|
|
18.39 0.3468 0.5824 0.0378 0.0225 0.062 0.984 0.741 46.547 0.111 3.298 7.224 0.22 90644. 0.2607
|
|
19.36 0.3650 0.5789 0.0342 0.0216 0.060 0.942 0.670 44.568 0.106 2.981 6.821 0.22 90756. 0.2341
|
|
20.33 0.3833 0.5692 0.0305 0.0206 0.057 0.897 0.598 42.458 0.101 2.660 6.388 0.22 90872. 0.2070
|
|
21.29 0.4015 0.5522 0.0268 0.0195 0.054 0.850 0.525 40.218 0.096 2.333 5.915 0.22 90992. 0.1796
|
|
22.26 0.4198 0.5265 0.0230 0.0183 0.051 0.800 0.450 37.848 0.090 2.002 5.394 0.22 91115. 0.1517
|
|
23.23 0.4380 0.4900 0.0191 0.0171 0.047 0.747 0.375 35.353 0.084 1.668 4.811 0.22 91243. 0.1235
|
|
24.20 0.4563 0.4400 0.0153 0.0158 0.044 0.692 0.299 32.735 0.078 1.332 4.148 0.22 91374. 0.0951
|
|
25.16 0.4745 0.3728 0.0114 0.0145 0.040 0.634 0.224 30.002 0.072 0.994 3.379 0.22 91510. 0.0670
|
|
26.13 0.4928 0.2827 0.0075 0.0132 0.036 0.574 0.148 27.163 0.065 0.657 2.468 0.22 91649. 0.0398
|
|
27.10 0.5110 0.1617 0.0037 0.0117 0.032 0.512 0.073 24.231 0.058 0.323 1.361 0.23 91791. 0.0154
|
|
28.07 0.5293 -0.0058 -0.0001 0.0103 0.028 0.448 -0.002 21.190 0.051 -0.010 -0.047 0.23 91929. 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 0.0893 0.0291 0.157 1.985 2.732 117.431 0.224 12.151 10.551 0.28 111470. 0.7309
|
|
1.21 0.0182 0.0547 0.0875 0.0292 0.158 1.990 2.677 117.700 0.225 11.909 10.318 0.28 111531. 0.7076
|
|
2.42 0.0365 0.1070 0.0856 0.0292 0.158 1.992 2.620 117.812 0.225 11.653 10.086 0.28 111596. 0.6842
|
|
3.63 0.0547 0.1568 0.0836 0.0292 0.158 1.991 2.560 117.803 0.225 11.386 9.855 0.28 111664. 0.6609
|
|
4.84 0.0730 0.2042 0.0816 0.0292 0.158 1.989 2.497 117.671 0.225 11.107 9.625 0.28 111736. 0.6374
|
|
6.05 0.0912 0.2491 0.0794 0.0291 0.157 1.983 2.430 117.318 0.224 10.810 9.396 0.28 111811. 0.6139
|
|
7.26 0.1095 0.2917 0.0771 0.0290 0.157 1.974 2.361 116.797 0.223 10.501 9.168 0.28 111891. 0.5904
|
|
8.47 0.1277 0.3318 0.0748 0.0288 0.156 1.963 2.289 116.117 0.222 10.180 8.940 0.28 111974. 0.5668
|
|
9.68 0.1460 0.3696 0.0723 0.0286 0.154 1.947 2.212 115.189 0.220 9.841 8.712 0.28 112061. 0.5431
|
|
10.89 0.1642 0.4049 0.0697 0.0283 0.153 1.928 2.134 114.080 0.218 9.491 8.483 0.28 112153. 0.5194
|
|
12.10 0.1825 0.4377 0.0670 0.0279 0.151 1.905 2.051 112.707 0.215 9.123 8.254 0.28 112248. 0.4954
|
|
13.31 0.2007 0.4679 0.0642 0.0275 0.149 1.878 1.965 111.111 0.212 8.741 8.022 0.28 112348. 0.4713
|
|
14.52 0.2190 0.4956 0.0613 0.0271 0.147 1.847 1.876 109.256 0.209 8.344 7.788 0.28 112452. 0.4471
|
|
15.73 0.2372 0.5204 0.0582 0.0266 0.144 1.811 1.783 107.117 0.205 7.930 7.549 0.28 112561. 0.4224
|
|
16.93 0.2555 0.5423 0.0551 0.0260 0.140 1.770 1.686 104.715 0.200 7.501 7.305 0.28 112673. 0.3976
|
|
18.14 0.2737 0.5611 0.0519 0.0253 0.137 1.725 1.587 102.056 0.195 7.060 7.054 0.28 112790. 0.3724
|
|
19.35 0.2920 0.5765 0.0485 0.0246 0.133 1.676 1.485 99.141 0.189 6.606 6.795 0.28 112912. 0.3471
|
|
20.56 0.3102 0.5883 0.0451 0.0238 0.129 1.622 1.381 95.966 0.183 6.141 6.526 0.28 113038. 0.3214
|
|
21.77 0.3285 0.5960 0.0416 0.0229 0.124 1.564 1.274 92.531 0.177 5.666 6.244 0.28 113169. 0.2953
|
|
22.98 0.3467 0.5991 0.0380 0.0220 0.119 1.502 1.165 88.832 0.170 5.180 5.946 0.28 113304. 0.2689
|
|
24.19 0.3650 0.5970 0.0344 0.0210 0.114 1.435 1.053 84.868 0.162 4.685 5.629 0.28 113444. 0.2421
|
|
25.40 0.3832 0.5888 0.0307 0.0200 0.108 1.363 0.940 80.640 0.154 4.181 5.287 0.28 113589. 0.2148
|
|
26.61 0.4015 0.5733 0.0270 0.0189 0.102 1.287 0.825 76.147 0.145 3.670 4.914 0.28 113739. 0.1871
|
|
27.82 0.4197 0.5490 0.0232 0.0177 0.096 1.207 0.709 71.394 0.136 3.152 4.502 0.28 113893. 0.1588
|
|
29.03 0.4380 0.5139 0.0193 0.0165 0.089 1.122 0.591 66.385 0.127 2.629 4.038 0.28 114053. 0.1301
|
|
30.24 0.4562 0.4649 0.0154 0.0152 0.082 1.033 0.473 61.129 0.117 2.102 3.506 0.28 114217. 0.1010
|
|
31.45 0.4744 0.3977 0.0116 0.0138 0.075 0.941 0.354 55.639 0.106 1.574 2.885 0.28 114386. 0.0719
|
|
32.66 0.4927 0.3061 0.0077 0.0124 0.067 0.844 0.235 49.936 0.095 1.047 2.138 0.28 114560. 0.0435
|
|
33.87 0.5109 0.1802 0.0039 0.0109 0.059 0.745 0.118 44.045 0.084 0.524 1.214 0.28 114738. 0.0175
|
|
35.08 0.5292 0.0014 0.0000 0.0094 0.051 0.641 0.001 37.936 0.072 0.003 0.009 0.28 114910. 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 0.0897 0.0289 0.270 2.837 3.952 201.393 0.321 17.579 8.901 0.33 133760. 0.7416
|
|
1.49 0.0187 0.0566 0.0878 0.0290 0.271 2.844 3.872 201.884 0.321 17.221 8.698 0.33 133835. 0.7173
|
|
2.97 0.0373 0.1107 0.0859 0.0290 0.271 2.847 3.786 202.083 0.322 16.841 8.498 0.33 133915. 0.6931
|
|
4.46 0.0560 0.1621 0.0839 0.0290 0.271 2.846 3.697 202.058 0.322 16.445 8.299 0.33 133999. 0.6688
|
|
5.94 0.0747 0.2110 0.0818 0.0289 0.271 2.843 3.604 201.796 0.321 16.030 8.101 0.33 134088. 0.6445
|
|
7.43 0.0934 0.2573 0.0795 0.0289 0.270 2.833 3.505 201.130 0.320 15.589 7.904 0.33 134181. 0.6202
|
|
8.91 0.1120 0.3011 0.0772 0.0287 0.268 2.820 3.402 200.163 0.319 15.131 7.708 0.33 134280. 0.5958
|
|
10.40 0.1307 0.3424 0.0747 0.0285 0.267 2.802 3.294 198.876 0.317 14.651 7.512 0.33 134383. 0.5714
|
|
11.88 0.1494 0.3812 0.0722 0.0283 0.264 2.777 3.181 197.148 0.314 14.147 7.317 0.33 134491. 0.5469
|
|
13.37 0.1681 0.4174 0.0695 0.0280 0.262 2.748 3.063 195.063 0.310 13.623 7.122 0.33 134605. 0.5224
|
|
14.85 0.1867 0.4510 0.0667 0.0276 0.258 2.712 2.940 192.518 0.306 13.075 6.926 0.33 134723. 0.4977
|
|
16.34 0.2054 0.4819 0.0638 0.0272 0.254 2.670 2.811 189.513 0.302 12.504 6.728 0.33 134847. 0.4728
|
|
17.82 0.2241 0.5101 0.0608 0.0267 0.249 2.621 2.678 186.044 0.296 11.910 6.528 0.33 134977. 0.4477
|
|
19.31 0.2427 0.5353 0.0576 0.0261 0.244 2.565 2.538 182.049 0.290 11.290 6.324 0.33 135112. 0.4223
|
|
20.79 0.2614 0.5575 0.0543 0.0255 0.238 2.501 2.394 177.574 0.283 10.650 6.116 0.33 135252. 0.3966
|
|
22.28 0.2801 0.5765 0.0510 0.0248 0.231 2.432 2.246 172.622 0.275 9.991 5.902 0.33 135398. 0.3707
|
|
23.76 0.2988 0.5918 0.0475 0.0240 0.224 2.355 2.094 167.191 0.266 9.314 5.681 0.33 135549. 0.3445
|
|
25.25 0.3174 0.6033 0.0440 0.0231 0.216 2.272 1.938 161.278 0.257 8.620 5.450 0.33 135706. 0.3180
|
|
26.74 0.3361 0.6104 0.0404 0.0222 0.208 2.182 1.778 154.878 0.246 7.910 5.208 0.34 135869. 0.2911
|
|
28.22 0.3548 0.6126 0.0367 0.0212 0.198 2.085 1.615 147.988 0.236 7.185 4.951 0.34 136038. 0.2637
|
|
29.71 0.3734 0.6089 0.0329 0.0202 0.189 1.981 1.449 140.605 0.224 6.447 4.676 0.34 136213. 0.2359
|
|
31.19 0.3921 0.5984 0.0291 0.0190 0.178 1.870 1.281 132.730 0.211 5.696 4.376 0.34 136394. 0.2076
|
|
32.68 0.4108 0.5797 0.0252 0.0178 0.167 1.752 1.110 124.366 0.198 4.935 4.046 0.34 136581. 0.1786
|
|
34.16 0.4295 0.5506 0.0212 0.0166 0.155 1.627 0.936 115.521 0.184 4.165 3.676 0.34 136773. 0.1491
|
|
35.65 0.4481 0.5084 0.0173 0.0152 0.142 1.496 0.762 106.209 0.169 3.388 3.253 0.34 136972. 0.1190
|
|
37.13 0.4668 0.4489 0.0133 0.0138 0.129 1.359 0.586 96.450 0.154 2.608 2.758 0.34 137178. 0.0885
|
|
38.62 0.4855 0.3658 0.0093 0.0124 0.116 1.215 0.411 86.278 0.137 1.828 2.161 0.34 137389. 0.0581
|
|
40.10 0.5042 0.2491 0.0054 0.0109 0.102 1.067 0.237 75.738 0.121 1.052 1.417 0.34 137606. 0.0289
|
|
41.59 0.5228 0.0816 0.0015 0.0093 0.087 0.914 0.064 64.867 0.103 0.285 0.448 0.34 137824. 0.0047
|
|
43.07 0.5415
|
|
|
|
|
|
|
|
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 0.0902 0.0288 0.427 3.848 5.409 318.719 0.435 24.058 7.697 0.39 156047. 0.7503
|
|
1.70 0.0183 0.0560 0.0884 0.0289 0.428 3.858 5.301 319.507 0.436 23.580 7.526 0.39 156134. 0.7262
|
|
3.39 0.0366 0.1095 0.0865 0.0289 0.429 3.862 5.187 319.833 0.436 23.072 7.356 0.39 156225. 0.7022
|
|
5.09 0.0549 0.1605 0.0845 0.0289 0.429 3.861 5.068 319.796 0.436 22.542 7.188 0.39 156321. 0.6782
|
|
6.79 0.0732 0.2090 0.0824 0.0289 0.428 3.857 4.944 319.420 0.436 21.990 7.020 0.39 156423. 0.6542
|
|
8.49 0.0915 0.2550 0.0802 0.0288 0.427 3.845 4.812 318.418 0.434 21.402 6.854 0.39 156529. 0.6301
|
|
10.18 0.1097 0.2987 0.0779 0.0286 0.425 3.827 4.674 316.917 0.432 20.788 6.689 0.39 156642. 0.6061
|
|
11.88 0.1280 0.3399 0.0755 0.0285 0.422 3.803 4.531 314.971 0.430 20.152 6.524 0.39 156759. 0.5820
|
|
13.58 0.1463 0.3786 0.0730 0.0282 0.419 3.771 4.379 312.314 0.426 19.480 6.360 0.39 156882. 0.5578
|
|
15.28 0.1646 0.4150 0.0704 0.0279 0.415 3.733 4.223 309.133 0.422 18.784 6.196 0.39 157011. 0.5337
|
|
16.97 0.1829 0.4489 0.0677 0.0276 0.409 3.685 4.059 305.198 0.416 18.054 6.032 0.39 157146. 0.5093
|
|
18.67 0.2012 0.4802 0.0648 0.0272 0.403 3.630 3.888 300.623 0.410 17.296 5.867 0.39 157286. 0.4849
|
|
20.37 0.2195 0.5091 0.0619 0.0267 0.396 3.566 3.711 295.301 0.403 16.508 5.701 0.39 157433. 0.4603
|
|
22.07 0.2378 0.5351 0.0588 0.0261 0.388 3.492 3.526 289.166 0.394 15.685 5.531 0.39 157586. 0.4353
|
|
23.76 0.2561 0.5583 0.0556 0.0255 0.379 3.408 3.335 282.276 0.385 14.834 5.359 0.39 157745. 0.4102
|
|
25.46 0.2744 0.5785 0.0523 0.0248 0.368 3.316 3.138 274.644 0.375 13.958 5.182 0.39 157910. 0.3848
|
|
27.16 0.2927 0.5954 0.0489 0.0241 0.357 3.215 2.936 266.268 0.363 13.058 5.001 0.39 158081. 0.3591
|
|
28.86 0.3110 0.6088 0.0455 0.0232 0.345 3.105 2.728 257.143 0.351 12.136 4.812 0.39 158259. 0.3332
|
|
30.55 0.3292 0.6182 0.0419 0.0223 0.332 2.986 2.516 247.261 0.337 11.192 4.615 0.39 158443. 0.3068
|
|
32.25 0.3475 0.6232 0.0383 0.0214 0.317 2.857 2.299 236.617 0.323 10.228 4.408 0.39 158633. 0.2801
|
|
33.95 0.3658 0.6231 0.0346 0.0203 0.302 2.719 2.079 225.206 0.307 9.245 4.186 0.39 158830. 0.2530
|
|
35.65 0.3841 0.6169 0.0309 0.0192 0.286 2.572 1.854 213.027 0.291 8.246 3.947 0.39 159034. 0.2253
|
|
37.34 0.4024 0.6034 0.0271 0.0181 0.268 2.416 1.626 200.083 0.273 7.232 3.686 0.39 159245. 0.1970
|
|
39.04 0.4207 0.5811 0.0233 0.0168 0.250 2.251 1.395 186.383 0.254 6.205 3.395 0.39 159462. 0.1681
|
|
40.74 0.4390 0.5474 0.0194 0.0155 0.231 2.076 1.162 171.944 0.235 5.168 3.065 0.39 159686. 0.1385
|
|
42.44 0.4573 0.4991 0.0155 0.0142 0.210 1.893 0.927 156.792 0.214 4.125 2.683 0.39 159917. 0.1083
|
|
44.13 0.4756 0.4310 0.0115 0.0127 0.189 1.702 0.692 140.967 0.192 3.079 2.227 0.39 160155. 0.0777
|
|
45.83 0.4939 0.3350 0.0076 0.0112 0.167 1.504 0.458 124.529 0.170 2.036 1.667 0.39 160400. 0.0473
|
|
47.53 0.5122 0.1979 0.0038 0.0097 0.144 1.299 0.225 107.558 0.147 1.002 0.950 0.39 160650. 0.0189
|
|
49.23 0.5304 -0.0083 -0.0001 0.0081 0.121 1.085 -0.008 89.871 0.123 -0.034 -0.038 0.39 160885. 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 0.0907 0.0288 0.638 5.026 7.110 475.750 0.568 31.624 6.778 0.44 178332. 0.7575
|
|
1.94 0.0183 0.0563 0.0889 0.0289 0.640 5.039 6.969 476.942 0.569 30.999 6.628 0.44 178431. 0.7333
|
|
3.88 0.0365 0.1101 0.0870 0.0289 0.640 5.044 6.819 477.425 0.570 30.333 6.479 0.44 178536. 0.7091
|
|
5.81 0.0548 0.1614 0.0850 0.0289 0.640 5.043 6.663 477.336 0.570 29.637 6.331 0.44 178646. 0.6849
|
|
7.75 0.0731 0.2102 0.0830 0.0289 0.639 5.037 6.500 476.746 0.569 28.912 6.184 0.44 178762. 0.6608
|
|
9.69 0.0914 0.2566 0.0807 0.0288 0.637 5.021 6.327 475.215 0.567 28.141 6.039 0.44 178884. 0.6366
|
|
11.63 0.1096 0.3005 0.0784 0.0286 0.634 4.996 6.146 472.905 0.564 27.336 5.894 0.44 179013. 0.6124
|
|
13.57 0.1279 0.3420 0.0760 0.0284 0.630 4.965 5.958 469.935 0.561 26.501 5.750 0.44 179147. 0.5883
|
|
15.51 0.1462 0.3812 0.0735 0.0282 0.625 4.922 5.760 465.882 0.556 25.619 5.607 0.44 179288. 0.5640
|
|
17.44 0.1645 0.4179 0.0709 0.0279 0.618 4.871 5.554 461.033 0.550 24.706 5.464 0.44 179436. 0.5398
|
|
19.38 0.1827 0.4522 0.0681 0.0275 0.610 4.808 5.339 455.041 0.543 23.747 5.321 0.45 179590. 0.5153
|
|
21.32 0.2010 0.4840 0.0653 0.0271 0.601 4.734 5.115 448.082 0.535 22.752 5.178 0.45 179751. 0.4908
|
|
23.26 0.2193 0.5132 0.0623 0.0266 0.590 4.649 4.883 439.988 0.525 21.718 5.033 0.45 179919. 0.4662
|
|
25.20 0.2376 0.5398 0.0592 0.0261 0.578 4.550 4.640 430.664 0.514 20.638 4.887 0.45 180093. 0.4412
|
|
27.14 0.2558 0.5636 0.0560 0.0254 0.563 4.439 4.389 420.190 0.502 19.521 4.737 0.45 180275. 0.4160
|
|
29.07 0.2741 0.5844 0.0527 0.0247 0.548 4.317 4.130 408.590 0.488 18.371 4.585 0.45 180464. 0.3905
|
|
31.01 0.2924 0.6020 0.0493 0.0240 0.531 4.182 3.865 395.859 0.473 17.189 4.428 0.45 180659. 0.3648
|
|
32.95 0.3107 0.6161 0.0458 0.0231 0.512 4.036 3.592 381.989 0.456 15.978 4.265 0.45 180862. 0.3388
|
|
34.89 0.3289 0.6264 0.0423 0.0222 0.492 3.877 3.314 366.970 0.438 14.739 4.096 0.45 181073. 0.3125
|
|
36.83 0.3472 0.6323 0.0387 0.0212 0.470 3.706 3.029 350.793 0.419 13.474 3.917 0.45 181290. 0.2857
|
|
38.76 0.3655 0.6332 0.0350 0.0202 0.447 3.523 2.739 333.450 0.398 12.184 3.726 0.45 181516. 0.2585
|
|
40.70 0.3838 0.6282 0.0312 0.0191 0.422 3.327 2.444 314.939 0.376 10.872 3.520 0.45 181748. 0.2307
|
|
42.64 0.4020 0.6160 0.0274 0.0179 0.396 3.120 2.145 295.266 0.352 9.541 3.295 0.45 181989. 0.2023
|
|
44.58 0.4203 0.5949 0.0235 0.0166 0.368 2.900 1.842 274.445 0.328 8.193 3.044 0.45 182237. 0.1732
|
|
46.52 0.4386 0.5626 0.0196 0.0153 0.339 2.668 1.536 252.500 0.301 6.832 2.759 0.45 182493. 0.1433
|
|
48.46 0.4569 0.5156 0.0157 0.0139 0.308 2.424 1.228 229.471 0.274 5.462 2.427 0.45 182757. 0.1127
|
|
50.39 0.4751 0.4484 0.0117 0.0124 0.275 2.170 0.919 205.420 0.245 4.089 2.030 0.45 183028. 0.0816
|
|
52.33 0.4934 0.3525 0.0078 0.0109 0.242 1.906 0.611 180.436 0.215 2.719 1.537 0.45 183307. 0.0503
|
|
54.27 0.5117 0.2135 0.0039 0.0094 0.207 1.634 0.306 154.641 0.185 1.361 0.897 0.45 183592. 0.0208
|
|
56.21 0.5300 0.0005 0.0000 0.0077 0.171 1.350 0.001 127.797 0.153 0.003 0.002 0.45 183863. 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 0.0914 0.0289 0.911 6.381 9.065 679.404 0.721 40.323 6.052 0.50 200614. 0.7637
|
|
2.18 0.0183 0.0566 0.0896 0.0289 0.913 6.397 8.886 681.116 0.723 39.527 5.918 0.50 200726. 0.7394
|
|
4.37 0.0366 0.1107 0.0877 0.0290 0.914 6.403 8.696 681.782 0.723 38.679 5.785 0.50 200844. 0.7150
|
|
6.55 0.0549 0.1623 0.0857 0.0290 0.914 6.401 8.496 681.585 0.723 37.790 5.654 0.50 200969. 0.6907
|
|
8.73 0.0732 0.2114 0.0836 0.0289 0.913 6.392 8.288 680.670 0.722 36.867 5.523 0.50 201100. 0.6664
|
|
10.91 0.0915 0.2581 0.0814 0.0288 0.910 6.371 8.067 678.406 0.720 35.884 5.394 0.50 201238. 0.6421
|
|
13.10 0.1098 0.3023 0.0790 0.0287 0.905 6.339 7.836 674.980 0.716 34.856 5.266 0.50 201383. 0.6178
|
|
15.28 0.1281 0.3442 0.0766 0.0285 0.899 6.298 7.597 670.606 0.712 33.790 5.138 0.50 201535. 0.5935
|
|
17.46 0.1463 0.3836 0.0741 0.0283 0.891 6.242 7.344 664.656 0.705 32.664 5.011 0.50 201695. 0.5692
|
|
19.64 0.1646 0.4207 0.0714 0.0279 0.882 6.175 7.082 657.545 0.698 31.499 4.885 0.50 201861. 0.5448
|
|
21.83 0.1829 0.4553 0.0686 0.0276 0.870 6.093 6.806 648.775 0.688 30.275 4.758 0.50 202036. 0.5203
|
|
24.01 0.2012 0.4875 0.0658 0.0271 0.856 5.997 6.521 638.603 0.678 29.005 4.632 0.50 202217. 0.4957
|
|
26.19 0.2195 0.5172 0.0628 0.0266 0.841 5.886 6.224 626.779 0.665 27.685 4.504 0.50 202407. 0.4710
|
|
28.38 0.2378 0.5442 0.0596 0.0261 0.822 5.759 5.914 613.172 0.651 26.306 4.375 0.50 202604. 0.4459
|
|
30.56 0.2561 0.5684 0.0564 0.0254 0.802 5.615 5.593 597.894 0.634 24.880 4.243 0.50 202809. 0.4206
|
|
32.74 0.2744 0.5898 0.0531 0.0247 0.779 5.456 5.263 580.977 0.616 23.411 4.109 0.50 203022. 0.3951
|
|
34.92 0.2927 0.6080 0.0497 0.0239 0.754 5.282 4.924 562.419 0.597 21.902 3.971 0.50 203243. 0.3693
|
|
37.11 0.3110 0.6227 0.0461 0.0230 0.727 5.092 4.576 542.205 0.575 20.355 3.828 0.50 203472. 0.3432
|
|
39.29 0.3293 0.6337 0.0426 0.0221 0.698 4.887 4.220 520.320 0.552 18.773 3.679 0.50 203709. 0.3168
|
|
41.47 0.3476 0.6403 0.0389 0.0211 0.666 4.665 3.857 496.752 0.527 17.157 3.522 0.50 203955. 0.2899
|
|
43.65 0.3659 0.6420 0.0352 0.0200 0.632 4.428 3.487 471.491 0.500 15.510 3.354 0.50 204209. 0.2625
|
|
45.84 0.3842 0.6377 0.0314 0.0189 0.596 4.175 3.110 444.534 0.472 13.835 3.174 0.50 204471. 0.2346
|
|
48.02 0.4025 0.6264 0.0275 0.0177 0.558 3.906 2.728 415.889 0.441 12.135 2.975 0.50 204743. 0.2060
|
|
50.20 0.4207 0.6061 0.0236 0.0164 0.517 3.621 2.341 385.577 0.409 10.413 2.754 0.50 205022. 0.1766
|
|
52.39 0.4390 0.5745 0.0197 0.0150 0.474 3.321 1.950 353.635 0.375 8.676 2.502 0.50 205311. 0.1464
|
|
54.57 0.4573 0.5278 0.0157 0.0136 0.429 3.006 1.557 320.122 0.340 6.927 2.206 0.51 205608. 0.1154
|
|
56.75 0.4756 0.4603 0.0117 0.0121 0.382 2.678 1.163 285.130 0.303 5.174 1.850 0.51 205915. 0.0836
|
|
58.93 0.4939 0.3627 0.0078 0.0106 0.334 2.336 0.770 248.788 0.264 3.426 1.404 0.51 206229. 0.0516
|
|
61.12 0.5122 0.2189 0.0038 0.0090 0.283 1.984 0.381 211.277 0.224 1.692 0.817 0.51 206551. 0.0211
|
|
63.30 0.5305 -0.0076 -0.0001 0.0073 0.231 1.617 -0.010 172.126 0.183 -0.046 -0.027 0.51 206849. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0922 0.0290 1.257 7.923 11.288 937.377 0.895 50.209 5.462 0.56 222891. 0.7691
|
|
2.43 0.0183 0.0568 0.0904 0.0291 1.260 7.943 11.066 939.730 0.897 49.222 5.341 0.56 223016. 0.7447
|
|
4.85 0.0366 0.1111 0.0885 0.0291 1.261 7.950 10.829 940.596 0.898 48.167 5.222 0.56 223148. 0.7202
|
|
7.28 0.0549 0.1629 0.0864 0.0291 1.261 7.947 10.580 940.207 0.898 47.061 5.104 0.56 223288. 0.6958
|
|
9.71 0.0732 0.2122 0.0843 0.0291 1.259 7.935 10.322 938.817 0.897 45.912 4.987 0.56 223434. 0.6715
|
|
12.13 0.0915 0.2591 0.0821 0.0290 1.255 7.908 10.047 935.577 0.893 44.689 4.871 0.56 223589. 0.6471
|
|
14.56 0.1098 0.3036 0.0797 0.0288 1.248 7.866 9.759 930.660 0.889 43.408 4.756 0.56 223751. 0.6227
|
|
16.99 0.1281 0.3457 0.0773 0.0286 1.240 7.813 9.461 924.426 0.883 42.082 4.642 0.56 223920. 0.5984
|
|
19.41 0.1464 0.3854 0.0747 0.0284 1.228 7.742 9.146 915.994 0.875 40.679 4.529 0.56 224098. 0.5740
|
|
21.84 0.1647 0.4227 0.0720 0.0281 1.215 7.657 8.819 905.923 0.865 39.228 4.416 0.56 224284. 0.5496
|
|
24.26 0.1830 0.4577 0.0692 0.0277 1.198 7.552 8.476 893.536 0.853 37.702 4.303 0.56 224478. 0.5250
|
|
26.69 0.2013 0.4902 0.0663 0.0272 1.179 7.431 8.121 879.191 0.840 36.121 4.189 0.56 224681. 0.5004
|
|
29.12 0.2196 0.5203 0.0633 0.0267 1.157 7.290 7.751 862.531 0.824 34.475 4.076 0.56 224892. 0.4756
|
|
31.54 0.2379 0.5477 0.0602 0.0261 1.131 7.128 7.364 843.385 0.805 32.757 3.961 0.56 225112. 0.4505
|
|
33.97 0.2562 0.5724 0.0569 0.0255 1.102 6.947 6.965 821.899 0.785 30.979 3.843 0.56 225341. 0.4251
|
|
36.40 0.2745 0.5942 0.0535 0.0247 1.070 6.746 6.553 798.122 0.762 29.148 3.724 0.56 225578. 0.3996
|
|
38.82 0.2928 0.6130 0.0501 0.0239 1.035 6.526 6.130 772.048 0.737 27.267 3.601 0.56 225824. 0.3737
|
|
41.25 0.3111 0.6283 0.0465 0.0230 0.997 6.286 5.697 743.660 0.710 25.339 3.475 0.56 226079. 0.3476
|
|
43.68 0.3294 0.6399 0.0429 0.0221 0.956 6.026 5.253 712.937 0.681 23.367 3.342 0.56 226344. 0.3211
|
|
46.10 0.3478 0.6473 0.0392 0.0211 0.912 5.746 4.800 679.862 0.649 21.353 3.203 0.56 226617. 0.2941
|
|
48.53 0.3661 0.6497 0.0354 0.0200 0.864 5.447 4.339 644.421 0.615 19.300 3.054 0.56 226900. 0.2666
|
|
50.96 0.3844 0.6463 0.0316 0.0188 0.813 5.127 3.870 606.613 0.579 17.212 2.893 0.56 227192. 0.2385
|
|
53.38 0.4027 0.6358 0.0277 0.0176 0.760 4.788 3.393 566.448 0.541 15.092 2.717 0.56 227494. 0.2098
|
|
55.81 0.4210 0.6165 0.0238 0.0162 0.703 4.429 2.911 523.955 0.500 12.947 2.520 0.56 227806. 0.1802
|
|
58.24 0.4393 0.5857 0.0198 0.0148 0.643 4.050 2.424 479.189 0.458 10.780 2.294 0.56 228127. 0.1497
|
|
60.66 0.4576 0.5396 0.0158 0.0134 0.580 3.653 1.933 432.232 0.413 8.600 2.029 0.56 228458. 0.1182
|
|
63.09 0.4759 0.4721 0.0118 0.0119 0.514 3.239 1.442 383.214 0.366 6.415 1.707 0.56 228798. 0.0859
|
|
65.52 0.4942 0.3733 0.0078 0.0103 0.446 2.809 0.952 332.319 0.317 4.236 1.300 0.56 229148. 0.0532
|
|
67.94 0.5125 0.2254 0.0038 0.0087 0.375 2.365 0.467 279.802 0.267 2.076 0.757 0.56 229506. 0.0217
|
|
70.37 0.5308 -0.0135 -0.0002 0.0070 0.302 1.900 -0.022 224.845 0.215 -0.097 -0.044 0.56 229832. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 11000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0931 0.0293 1.688 9.670 13.793 1258.418 1.092 61.353 4.972 0.61 245164. 0.7739
|
|
2.72 0.0186 0.0579 0.0913 0.0294 1.692 9.694 13.519 1261.569 1.095 60.130 4.860 0.61 245304. 0.7490
|
|
5.43 0.0372 0.1131 0.0893 0.0294 1.693 9.702 13.224 1262.607 1.096 58.821 4.751 0.61 245453. 0.7240
|
|
8.15 0.0559 0.1658 0.0872 0.0294 1.692 9.696 12.915 1261.825 1.095 57.445 4.642 0.61 245610. 0.6992
|
|
10.86 0.0745 0.2159 0.0850 0.0293 1.689 9.679 12.593 1259.602 1.093 56.014 4.535 0.61 245776. 0.6744
|
|
13.58 0.0931 0.2636 0.0827 0.0292 1.683 9.642 12.251 1254.790 1.089 54.491 4.428 0.61 245950. 0.6496
|
|
16.29 0.1117 0.3088 0.0803 0.0290 1.673 9.586 11.892 1247.613 1.083 52.894 4.323 0.61 246133. 0.6248
|
|
19.01 0.1303 0.3515 0.0778 0.0288 1.661 9.517 11.519 1238.520 1.075 51.237 4.218 0.61 246324. 0.6001
|
|
21.72 0.1489 0.3918 0.0751 0.0285 1.645 9.423 11.125 1226.346 1.065 49.485 4.115 0.61 246525. 0.5752
|
|
24.44 0.1676 0.4297 0.0723 0.0282 1.625 9.311 10.717 1211.823 1.052 47.669 4.011 0.61 246736. 0.5504
|
|
27.15 0.1862 0.4652 0.0695 0.0278 1.601 9.175 10.288 1194.079 1.037 45.761 3.908 0.61 246956. 0.5253
|
|
29.87 0.2048 0.4981 0.0664 0.0273 1.574 9.017 9.842 1173.467 1.019 43.779 3.804 0.61 247185. 0.5002
|
|
32.58 0.2234 0.5285 0.0633 0.0268 1.542 8.834 9.379 1149.640 0.998 41.718 3.700 0.61 247424. 0.4750
|
|
35.30 0.2420 0.5563 0.0600 0.0261 1.505 8.624 8.895 1122.302 0.974 39.564 3.595 0.61 247673. 0.4493
|
|
38.01 0.2607 0.5812 0.0567 0.0254 1.464 8.389 8.394 1091.706 0.948 37.337 3.488 0.61 247932. 0.4235
|
|
40.73 0.2793 0.6031 0.0532 0.0246 1.419 8.129 7.879 1057.897 0.918 35.045 3.378 0.61 248200. 0.3974
|
|
43.44 0.2979 0.6219 0.0496 0.0238 1.369 7.844 7.349 1020.862 0.886 32.689 3.265 0.61 248479. 0.3710
|
|
46.16 0.3165 0.6371 0.0459 0.0228 1.315 7.535 6.807 980.575 0.851 30.276 3.148 0.61 248768. 0.3443
|
|
48.87 0.3351 0.6484 0.0422 0.0218 1.257 7.200 6.251 937.009 0.813 27.806 3.026 0.61 249068. 0.3171
|
|
51.59 0.3538 0.6551 0.0384 0.0207 1.194 6.840 5.685 890.140 0.773 25.285 2.897 0.61 249378. 0.2895
|
|
54.30 0.3724 0.6565 0.0345 0.0196 1.126 6.454 5.107 839.955 0.729 22.717 2.758 0.62 249698. 0.2612
|
|
57.02 0.3910 0.6516 0.0305 0.0183 1.055 6.043 4.520 786.458 0.683 20.105 2.607 0.62 250029. 0.2323
|
|
59.73 0.4096 0.6388 0.0265 0.0170 0.979 5.607 3.924 729.673 0.633 17.455 2.439 0.62 250371. 0.2025
|
|
62.45 0.4282 0.6160 0.0224 0.0156 0.898 5.146 3.322 669.655 0.581 14.775 2.250 0.62 250724. 0.1719
|
|
65.16 0.4468 0.5798 0.0183 0.0141 0.813 4.660 2.714 606.497 0.527 12.072 2.030 0.62 251088. 0.1401
|
|
67.88 0.4655 0.5254 0.0142 0.0126 0.725 4.152 2.103 540.344 0.469 9.356 1.766 0.62 251464. 0.1073
|
|
70.60 0.4841 0.4444 0.0101 0.0110 0.632 3.622 1.492 471.410 0.409 6.639 1.436 0.62 251850. 0.0735
|
|
73.31 0.5027 0.3225 0.0060 0.0093 0.536 3.074 0.885 400.007 0.347 3.936 1.003 0.62 252246. 0.0396
|
|
76.03 0.5213 0.1314 0.0019 0.0076 0.438 2.508 0.284 326.431 0.283 1.262 0.394 0.62 252645. 0.0088
|
|
78.74 0.5399
|
|
|
|
|
|
|
|
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 0.0942 0.0296 2.216 11.641 16.602 1652.788 1.315 73.844 4.556 0.67 267430. 0.7780
|
|
2.91 0.0183 0.0568 0.0923 0.0297 2.222 11.669 16.279 1656.755 1.318 72.407 4.457 0.67 267581. 0.7536
|
|
5.82 0.0366 0.1112 0.0904 0.0297 2.223 11.678 15.933 1658.030 1.319 70.868 4.359 0.67 267742. 0.7292
|
|
8.73 0.0548 0.1630 0.0883 0.0297 2.222 11.670 15.568 1656.828 1.318 69.247 4.262 0.67 267911. 0.7048
|
|
11.63 0.0731 0.2125 0.0862 0.0297 2.218 11.648 15.190 1653.760 1.316 67.563 4.166 0.67 268088. 0.6805
|
|
14.54 0.0914 0.2595 0.0839 0.0295 2.209 11.605 14.788 1647.594 1.311 65.777 4.071 0.67 268275. 0.6561
|
|
17.45 0.1097 0.3043 0.0815 0.0294 2.197 11.539 14.365 1638.188 1.304 63.897 3.977 0.67 268471. 0.6318
|
|
20.36 0.1280 0.3467 0.0790 0.0292 2.181 11.456 13.928 1626.411 1.294 61.951 3.884 0.67 268676. 0.6075
|
|
23.27 0.1463 0.3868 0.0764 0.0289 2.160 11.345 13.466 1610.760 1.282 59.895 3.792 0.67 268891. 0.5832
|
|
26.18 0.1645 0.4246 0.0737 0.0285 2.135 11.214 12.986 1592.061 1.267 57.764 3.700 0.67 269116. 0.5588
|
|
29.09 0.1828 0.4601 0.0708 0.0281 2.104 11.053 12.483 1569.266 1.249 55.524 3.608 0.67 269351. 0.5343
|
|
31.99 0.2011 0.4932 0.0678 0.0277 2.069 10.868 11.961 1542.952 1.228 53.202 3.516 0.67 269596. 0.5097
|
|
34.90 0.2194 0.5239 0.0648 0.0271 2.028 10.653 11.417 1512.463 1.204 50.785 3.424 0.67 269851. 0.4849
|
|
37.81 0.2377 0.5521 0.0615 0.0265 1.981 10.407 10.850 1477.564 1.176 48.261 3.331 0.67 270116. 0.4598
|
|
40.72 0.2560 0.5777 0.0582 0.0258 1.929 10.132 10.263 1438.448 1.145 45.648 3.236 0.67 270391. 0.4345
|
|
43.63 0.2742 0.6005 0.0548 0.0250 1.871 9.827 9.658 1395.225 1.110 42.957 3.140 0.67 270677. 0.4089
|
|
46.54 0.2925 0.6203 0.0513 0.0242 1.808 9.494 9.036 1347.894 1.073 40.192 3.041 0.67 270974. 0.3831
|
|
49.45 0.3108 0.6369 0.0476 0.0232 1.739 9.131 8.399 1296.428 1.032 37.357 2.938 0.67 271281. 0.3569
|
|
52.35 0.3291 0.6499 0.0439 0.0222 1.664 8.740 7.747 1240.794 0.987 34.457 2.832 0.67 271599. 0.3303
|
|
55.26 0.3474 0.6588 0.0402 0.0212 1.584 8.318 7.081 1180.961 0.940 31.495 2.719 0.67 271928. 0.3033
|
|
58.17 0.3656 0.6630 0.0363 0.0200 1.498 7.867 6.402 1116.910 0.889 28.475 2.600 0.67 272268. 0.2757
|
|
61.08 0.3839 0.6615 0.0324 0.0188 1.406 7.386 5.711 1048.638 0.834 25.404 2.470 0.67 272619. 0.2474
|
|
63.99 0.4022 0.6531 0.0284 0.0175 1.309 6.876 5.010 976.168 0.777 22.286 2.328 0.67 272981. 0.2184
|
|
66.90 0.4205 0.6359 0.0244 0.0161 1.206 6.336 4.300 899.553 0.716 19.128 2.168 0.67 273355. 0.1885
|
|
69.81 0.4388 0.6074 0.0203 0.0147 1.098 5.768 3.584 818.890 0.652 15.940 1.985 0.67 273740. 0.1575
|
|
72.71 0.4571 0.5635 0.0162 0.0132 0.985 5.172 2.862 734.331 0.584 12.731 1.768 0.67 274137. 0.1253
|
|
75.62 0.4753 0.4978 0.0121 0.0116 0.866 4.551 2.139 646.110 0.514 9.514 1.501 0.67 274546. 0.0920
|
|
78.53 0.4936 0.3991 0.0080 0.0099 0.744 3.906 1.417 554.568 0.441 6.304 1.159 0.67 274965. 0.0578
|
|
81.44 0.5119 0.2470 0.0040 0.0083 0.617 3.241 0.702 460.180 0.366 3.122 0.692 0.68 275393. 0.0243
|
|
84.35 0.5302 -0.0080 -0.0001 0.0065 0.485 2.547 -0.017 361.583 0.288 -0.077 -0.022 0.68 275785. 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 0.0954 0.0301 2.861 13.869 19.738 2133.128 1.567 87.796 4.197 0.72 289689. 0.7815
|
|
3.18 0.0185 0.0572 0.0935 0.0302 2.867 13.901 19.353 2138.002 1.570 86.080 4.106 0.72 289855. 0.7570
|
|
6.36 0.0369 0.1120 0.0915 0.0302 2.869 13.910 18.939 2139.358 1.571 84.241 4.015 0.72 290032. 0.7324
|
|
9.54 0.0554 0.1643 0.0894 0.0301 2.866 13.896 18.502 2137.284 1.570 82.298 3.927 0.72 290218. 0.7079
|
|
12.72 0.0738 0.2141 0.0872 0.0301 2.860 13.866 18.048 2132.616 1.567 80.277 3.838 0.72 290414. 0.6834
|
|
15.90 0.0923 0.2615 0.0849 0.0300 2.848 13.810 17.566 2123.979 1.560 78.134 3.751 0.72 290620. 0.6589
|
|
19.08 0.1107 0.3066 0.0824 0.0298 2.831 13.725 17.058 2110.933 1.551 75.875 3.665 0.72 290836. 0.6345
|
|
22.26 0.1292 0.3494 0.0799 0.0295 2.809 13.619 16.532 2094.672 1.539 73.536 3.580 0.72 291063. 0.6101
|
|
25.45 0.1476 0.3899 0.0772 0.0292 2.780 13.480 15.976 2073.292 1.523 71.062 3.495 0.72 291300. 0.5855
|
|
28.63 0.1661 0.4280 0.0744 0.0289 2.746 13.314 15.399 2047.822 1.504 68.496 3.411 0.72 291548. 0.5610
|
|
31.81 0.1845 0.4639 0.0715 0.0284 2.705 13.113 14.793 2016.914 1.482 65.798 3.327 0.72 291807. 0.5362
|
|
34.99 0.2030 0.4973 0.0685 0.0279 2.657 12.882 14.164 1981.293 1.455 63.000 3.242 0.72 292077. 0.5114
|
|
38.17 0.2215 0.5284 0.0653 0.0274 2.602 12.614 13.508 1940.158 1.425 60.086 3.158 0.72 292359. 0.4865
|
|
41.35 0.2399 0.5569 0.0620 0.0267 2.539 12.309 12.824 1893.151 1.391 57.041 3.072 0.72 292651. 0.4611
|
|
44.53 0.2584 0.5828 0.0586 0.0260 2.468 11.967 12.116 1840.595 1.352 53.891 2.986 0.72 292955. 0.4356
|
|
47.71 0.2768 0.6060 0.0550 0.0251 2.391 11.590 11.386 1782.614 1.309 50.647 2.897 0.72 293270. 0.4097
|
|
50.89 0.2953 0.6261 0.0514 0.0242 2.305 11.178 10.637 1719.203 1.263 47.313 2.806 0.73 293597. 0.3836
|
|
54.07 0.3137 0.6429 0.0477 0.0233 2.213 10.730 9.868 1650.327 1.212 43.895 2.712 0.73 293936. 0.3571
|
|
57.25 0.3322 0.6561 0.0439 0.0222 2.113 10.246 9.082 1575.953 1.158 40.398 2.614 0.73 294287. 0.3302
|
|
60.43 0.3506 0.6650 0.0400 0.0211 2.006 9.727 8.279 1496.054 1.099 36.826 2.510 0.73 294649. 0.3027
|
|
63.61 0.3691 0.6690 0.0361 0.0199 1.892 9.171 7.461 1410.622 1.036 33.186 2.399 0.73 295024. 0.2746
|
|
66.79 0.3876 0.6671 0.0320 0.0186 1.770 8.580 6.628 1319.683 0.969 29.483 2.278 0.73 295411. 0.2458
|
|
69.97 0.4060 0.6578 0.0280 0.0173 1.640 7.954 5.784 1223.306 0.899 25.725 2.144 0.73 295810. 0.2161
|
|
73.16 0.4245 0.6392 0.0238 0.0158 1.504 7.292 4.928 1121.616 0.824 21.921 1.993 0.73 296222. 0.1854
|
|
76.34 0.4429 0.6080 0.0196 0.0143 1.361 6.598 4.065 1014.816 0.745 18.082 1.817 0.73 296647. 0.1535
|
|
79.52 0.4614 0.5596 0.0155 0.0127 1.211 5.872 3.197 903.209 0.663 14.219 1.605 0.73 297084. 0.1203
|
|
82.70 0.4798 0.4861 0.0112 0.0111 1.056 5.118 2.327 787.236 0.578 10.351 1.341 0.73 297534. 0.0857
|
|
85.88 0.4983 0.3736 0.0071 0.0094 0.895 4.340 1.461 667.512 0.490 6.497 0.992 0.73 297996. 0.0503
|
|
89.06 0.5167 0.1958 0.0029 0.0077 0.731 3.542 0.602 544.799 0.400 2.680 0.502 0.73 298465. 0.0163
|
|
92.24 0.5352
|
|
|
|
|
|
|
|
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 0.0968 0.0308 3.652 16.441 23.237 2723.234 1.857 103.357 3.870 0.78 311938. 0.7819
|
|
3.44 0.0186 0.0572 0.0949 0.0308 3.657 16.465 22.783 2727.191 1.860 101.339 3.789 0.78 312119. 0.7580
|
|
6.89 0.0371 0.1120 0.0929 0.0308 3.657 16.464 22.297 2727.033 1.860 99.177 3.709 0.78 312312. 0.7339
|
|
10.33 0.0557 0.1643 0.0908 0.0307 3.651 16.436 21.781 2722.457 1.857 96.883 3.629 0.78 312516. 0.7098
|
|
13.77 0.0742 0.2143 0.0885 0.0307 3.640 16.389 21.244 2714.548 1.852 94.493 3.550 0.78 312730. 0.6857
|
|
17.22 0.0928 0.2620 0.0862 0.0305 3.623 16.313 20.676 2701.974 1.843 91.966 3.471 0.78 312954. 0.6614
|
|
20.66 0.1113 0.3073 0.0837 0.0303 3.599 16.202 20.075 2683.683 1.831 89.293 3.393 0.78 313191. 0.6371
|
|
24.10 0.1299 0.3503 0.0811 0.0301 3.569 16.067 19.452 2661.280 1.815 86.522 3.315 0.78 313438. 0.6128
|
|
27.55 0.1484 0.3910 0.0783 0.0297 3.530 15.893 18.793 2632.461 1.796 83.593 3.238 0.78 313697. 0.5883
|
|
30.99 0.1670 0.4295 0.0755 0.0293 3.484 15.687 18.110 2598.327 1.772 80.551 3.161 0.78 313968. 0.5638
|
|
34.43 0.1855 0.4656 0.0725 0.0289 3.429 15.439 17.390 2557.255 1.744 77.353 3.084 0.78 314251. 0.5391
|
|
37.88 0.2041 0.4994 0.0694 0.0283 3.366 15.154 16.644 2510.088 1.712 74.033 3.008 0.78 314545. 0.5143
|
|
41.32 0.2226 0.5308 0.0661 0.0277 3.293 14.827 15.867 2455.831 1.675 70.575 2.930 0.78 314852. 0.4892
|
|
44.76 0.2412 0.5597 0.0627 0.0270 3.210 14.454 15.054 2394.036 1.633 66.961 2.852 0.78 315171. 0.4638
|
|
48.21 0.2597 0.5860 0.0592 0.0263 3.118 14.038 14.214 2325.178 1.586 63.222 2.773 0.78 315503. 0.4381
|
|
51.65 0.2783 0.6094 0.0556 0.0254 3.017 13.580 13.347 2249.426 1.534 59.369 2.691 0.78 315847. 0.4121
|
|
55.09 0.2968 0.6298 0.0519 0.0245 2.906 13.082 12.457 2166.817 1.478 55.410 2.608 0.78 316203. 0.3857
|
|
58.54 0.3154 0.6469 0.0481 0.0235 2.786 12.542 11.545 2077.369 1.417 51.352 2.521 0.78 316572. 0.3590
|
|
61.98 0.3339 0.6601 0.0442 0.0224 2.657 11.961 10.611 1981.116 1.351 47.198 2.429 0.78 316954. 0.3317
|
|
65.42 0.3525 0.6689 0.0402 0.0212 2.519 11.339 9.657 1878.092 1.281 42.956 2.332 0.78 317349. 0.3038
|
|
68.87 0.3710 0.6726 0.0362 0.0200 2.371 10.676 8.685 1768.390 1.206 38.632 2.228 0.78 317757. 0.2752
|
|
72.31 0.3896 0.6698 0.0321 0.0187 2.216 9.975 7.697 1652.175 1.127 34.234 2.113 0.78 318178. 0.2457
|
|
75.75 0.4081 0.6591 0.0279 0.0173 2.051 9.235 6.693 1529.692 1.043 29.770 1.985 0.78 318613. 0.2152
|
|
79.20 0.4267 0.6380 0.0237 0.0158 1.879 8.460 5.677 1401.302 0.956 25.251 1.837 0.78 319061. 0.1835
|
|
82.64 0.4452 0.6030 0.0194 0.0143 1.700 7.652 4.651 1267.479 0.865 20.689 1.664 0.79 319523. 0.1505
|
|
86.08 0.4638 0.5489 0.0151 0.0127 1.514 6.815 3.620 1128.861 0.770 16.101 1.454 0.79 319999. 0.1160
|
|
89.53 0.4824 0.4669 0.0108 0.0111 1.323 5.954 2.587 986.266 0.673 11.506 1.190 0.79 320488. 0.0802
|
|
92.97 0.5009 0.3426 0.0065 0.0095 1.127 5.076 1.558 840.752 0.573 6.931 0.841 0.79 320990. 0.0440
|
|
96.41 0.5195 0.1491 0.0022 0.0078 0.930 4.186 0.539 693.362 0.473 2.398 0.353 0.79 321498. 0.0109
|
|
99.86 0.5380
|
|
|
|
|
|
|
|
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 0.0985 0.0322 4.699 19.743 27.138 3503.678 2.231 120.709 3.513 0.83 334173. 0.7670
|
|
3.63 0.0183 0.0550 0.0966 0.0321 4.693 19.718 26.620 3499.270 2.228 118.406 3.450 0.83 334367. 0.7461
|
|
7.27 0.0366 0.1080 0.0946 0.0320 4.681 19.669 26.068 3490.617 2.222 115.949 3.387 0.83 334572. 0.7248
|
|
10.90 0.0548 0.1589 0.0925 0.0319 4.662 19.590 25.479 3476.676 2.213 113.332 3.324 0.83 334789. 0.7032
|
|
14.54 0.0731 0.2078 0.0903 0.0318 4.638 19.489 24.864 3458.702 2.202 110.596 3.261 0.83 335016. 0.6814
|
|
18.17 0.0914 0.2547 0.0879 0.0315 4.608 19.363 24.218 3436.229 2.188 107.721 3.197 0.83 335255. 0.6593
|
|
21.81 0.1097 0.2995 0.0854 0.0313 4.569 19.197 23.531 3406.923 2.169 104.667 3.133 0.83 335505. 0.6369
|
|
25.44 0.1279 0.3423 0.0828 0.0310 4.523 19.005 22.819 3372.808 2.147 101.497 3.069 0.83 335767. 0.6144
|
|
29.08 0.1462 0.3829 0.0801 0.0306 4.468 18.776 22.068 3332.064 2.121 98.158 3.004 0.83 336042. 0.5914
|
|
32.71 0.1645 0.4215 0.0773 0.0302 4.405 18.510 21.285 3284.839 2.091 94.678 2.939 0.83 336328. 0.5683
|
|
36.35 0.1828 0.4579 0.0743 0.0297 4.332 18.202 20.465 3230.213 2.056 91.027 2.874 0.83 336627. 0.5448
|
|
39.98 0.2011 0.4921 0.0712 0.0291 4.249 17.855 19.613 3168.623 2.017 87.237 2.807 0.83 336938. 0.5211
|
|
43.62 0.2193 0.5239 0.0680 0.0285 4.157 17.465 18.723 3099.560 1.973 83.282 2.740 0.84 337262. 0.4969
|
|
47.25 0.2376 0.5532 0.0646 0.0278 4.054 17.033 17.796 3022.792 1.924 79.157 2.670 0.84 337599. 0.4721
|
|
50.89 0.2559 0.5798 0.0611 0.0270 3.940 16.556 16.834 2938.112 1.870 74.879 2.599 0.84 337948. 0.4469
|
|
54.52 0.2742 0.6034 0.0575 0.0261 3.817 16.040 15.843 2846.500 1.812 70.470 2.524 0.84 338310. 0.4211
|
|
58.16 0.2925 0.6240 0.0538 0.0252 3.684 15.481 14.824 2747.291 1.749 65.938 2.447 0.84 338685. 0.3949
|
|
61.79 0.3107 0.6412 0.0500 0.0242 3.541 14.879 13.779 2640.527 1.681 61.290 2.367 0.84 339073. 0.3682
|
|
65.43 0.3290 0.6545 0.0461 0.0232 3.388 14.236 12.710 2526.421 1.608 56.532 2.282 0.84 339474. 0.3409
|
|
69.06 0.3473 0.6632 0.0422 0.0221 3.226 13.554 11.617 2405.399 1.531 51.671 2.190 0.84 339888. 0.3129
|
|
72.70 0.3656 0.6665 0.0381 0.0209 3.054 12.834 10.502 2277.650 1.450 46.714 2.091 0.84 340317. 0.2841
|
|
76.33 0.3838 0.6633 0.0340 0.0197 2.875 12.079 9.368 2143.576 1.365 41.669 1.982 0.84 340758. 0.2543
|
|
79.97 0.4021 0.6520 0.0298 0.0184 2.687 11.291 8.216 2003.710 1.276 36.545 1.860 0.84 341214. 0.2234
|
|
83.60 0.4204 0.6304 0.0256 0.0171 2.493 10.474 7.049 1858.709 1.183 31.353 1.720 0.84 341683. 0.1914
|
|
87.24 0.4387 0.5956 0.0213 0.0157 2.292 9.633 5.869 1709.458 1.088 26.105 1.557 0.84 342167. 0.1581
|
|
90.87 0.4570 0.5432 0.0170 0.0143 2.088 8.773 4.681 1556.866 0.991 20.819 1.364 0.84 342664. 0.1236
|
|
94.51 0.4752 0.4675 0.0127 0.0129 1.880 7.901 3.488 1402.092 0.893 15.515 1.128 0.84 343176. 0.0883
|
|
98.14 0.4935 0.3597 0.0083 0.0114 1.672 7.024 2.297 1246.510 0.794 10.218 0.836 0.84 343701. 0.0531
|
|
101.78 0.5118 0.2068 0.0040 0.0100 1.464 6.151 1.115 1091.637 0.695 4.961 0.463 0.84 344237. 0.0205
|
|
105.41 0.5301 -0.0176 -0.0003 0.0086 1.250 5.252 -0.078 932.065 0.593 -0.347 -0.038 0.84 344718. 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 0.1003 0.0351 6.219 24.499 31.435 4637.648 2.768 139.821 3.074 0.89 356398. 0.7224
|
|
3.88 0.0183 0.0516 0.0984 0.0349 6.184 24.361 30.843 4611.467 2.752 137.190 3.034 0.89 356606. 0.7061
|
|
7.77 0.0366 0.1019 0.0964 0.0347 6.143 24.198 30.214 4580.580 2.734 134.391 2.992 0.89 356827. 0.6892
|
|
11.65 0.0549 0.1506 0.0943 0.0344 6.092 23.999 29.541 4543.048 2.711 131.396 2.949 0.89 357060. 0.6718
|
|
15.53 0.0732 0.1979 0.0920 0.0340 6.035 23.774 28.833 4500.369 2.686 128.251 2.906 0.89 357306. 0.6540
|
|
19.42 0.0915 0.2435 0.0896 0.0337 5.972 23.524 28.093 4453.054 2.658 124.955 2.861 0.89 357563. 0.6356
|
|
23.30 0.1098 0.2876 0.0871 0.0333 5.897 23.232 27.303 4397.765 2.625 121.446 2.816 0.89 357833. 0.6167
|
|
27.18 0.1281 0.3300 0.0845 0.0328 5.816 22.910 26.481 4336.822 2.588 117.790 2.770 0.89 358116. 0.5973
|
|
31.06 0.1464 0.3707 0.0817 0.0323 5.725 22.552 25.618 4269.065 2.548 113.950 2.722 0.89 358411. 0.5774
|
|
34.95 0.1648 0.4095 0.0789 0.0317 5.624 22.154 24.715 4193.715 2.503 109.932 2.673 0.89 358720. 0.5570
|
|
38.83 0.1831 0.4465 0.0758 0.0311 5.512 21.714 23.769 4110.496 2.453 105.725 2.623 0.89 359042. 0.5359
|
|
42.71 0.2014 0.4815 0.0727 0.0304 5.390 21.233 22.785 4019.353 2.399 101.347 2.571 0.89 359377. 0.5144
|
|
46.60 0.2197 0.5143 0.0694 0.0296 5.256 20.704 21.757 3919.217 2.339 96.775 2.518 0.89 359726. 0.4922
|
|
50.48 0.2380 0.5445 0.0660 0.0288 5.113 20.142 20.685 3812.907 2.276 92.006 2.461 0.89 360087. 0.4690
|
|
54.36 0.2563 0.5717 0.0624 0.0280 4.962 19.548 19.572 3700.392 2.209 87.055 2.399 0.89 360463. 0.4448
|
|
58.25 0.2746 0.5956 0.0588 0.0271 4.804 18.924 18.424 3582.279 2.138 81.948 2.333 0.89 360852. 0.4196
|
|
62.13 0.2929 0.6147 0.0550 0.0262 4.647 18.307 17.242 3465.436 2.068 76.693 2.257 0.89 361255. 0.3927
|
|
66.01 0.3112 0.6294 0.0511 0.0253 4.483 17.658 16.030 3342.713 1.995 71.301 2.175 0.89 361672. 0.3650
|
|
69.89 0.3295 0.6397 0.0472 0.0243 4.309 16.974 14.789 3213.149 1.918 65.781 2.088 0.89 362102. 0.3365
|
|
73.78 0.3478 0.6446 0.0431 0.0233 4.127 16.257 13.521 3077.393 1.837 60.143 1.993 0.89 362547. 0.3071
|
|
77.66 0.3661 0.6430 0.0390 0.0222 3.938 15.514 12.229 2936.844 1.753 54.393 1.889 0.89 363007. 0.2768
|
|
81.54 0.3844 0.6338 0.0348 0.0211 3.744 14.748 10.913 2791.771 1.666 48.542 1.773 0.90 363480. 0.2455
|
|
85.43 0.4027 0.6155 0.0306 0.0200 3.544 13.963 9.578 2643.133 1.578 42.602 1.644 0.90 363969. 0.2132
|
|
89.31 0.4210 0.5861 0.0262 0.0189 3.342 13.165 8.225 2492.057 1.487 36.586 1.497 0.90 364472. 0.1799
|
|
93.19 0.4393 0.5432 0.0219 0.0177 3.138 12.360 6.859 2339.789 1.396 30.509 1.330 0.90 364989. 0.1459
|
|
97.08 0.4576 0.4838 0.0175 0.0166 2.934 11.558 5.484 2187.921 1.306 24.392 1.137 0.90 365522. 0.1116
|
|
100.96 0.4759 0.4044 0.0131 0.0154 2.733 10.765 4.105 2037.834 1.216 18.258 0.914 0.90 366070. 0.0776
|
|
104.84 0.4943 0.3009 0.0087 0.0143 2.536 9.990 2.729 1891.174 1.129 12.141 0.655 0.90 366632. 0.0453
|
|
108.72 0.5126 0.1688 0.0044 0.0132 2.346 9.242 1.366 1749.512 1.044 6.077 0.354 0.90 367207. 0.0174
|
|
112.61 0.5309 -0.0002 0.0000 0.0121 2.154 8.483 -0.002 1605.876 0.958 -0.007 0.000 0.90 367757. 0.0000
|
|
|
|
|
|
|