686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x6.5E(F2B) (13x65E(F2B).dat)
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v2022-0915
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Simulation Date: 09/22/2022
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AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
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====== PERFORMANCE DATA (versus advance ratio and MPH) ======
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DEFINITIONS:
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J=V/nD (advance ratio)
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Ct=T/(rho * n**2 * D**4) (thrust coef.)
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Cp=P/(rho * n**3 * D**5) (power coef.)
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Pe=Ct*J/Cp (efficiency)
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V (model speed in MPH)
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Mach (at prop tip)
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Reyn (at 75% of span)
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FOM (Figure of Merit)
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PROP RPM = 1000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0892 0.0378 0.001 0.070 0.080 0.825 0.008 0.356 43.944 0.05 16670. 0.5631
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0.27 0.0219 0.0505 0.0878 0.0380 0.001 0.070 0.079 0.830 0.008 0.350 42.959 0.05 16680. 0.5459
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0.54 0.0438 0.0987 0.0862 0.0382 0.001 0.071 0.077 0.835 0.008 0.344 41.966 0.05 16691. 0.5285
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0.80 0.0656 0.1445 0.0845 0.0384 0.001 0.071 0.076 0.839 0.008 0.337 40.968 0.05 16703. 0.5109
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1.07 0.0875 0.1880 0.0827 0.0385 0.001 0.071 0.074 0.841 0.008 0.330 39.965 0.05 16716. 0.4931
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1.34 0.1094 0.2291 0.0808 0.0386 0.001 0.071 0.072 0.843 0.008 0.322 38.958 0.05 16729. 0.4751
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1.61 0.1313 0.2678 0.0788 0.0386 0.001 0.071 0.071 0.844 0.008 0.314 37.949 0.05 16744. 0.4569
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1.88 0.1531 0.3041 0.0766 0.0386 0.001 0.071 0.069 0.843 0.008 0.305 36.936 0.05 16759. 0.4386
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2.15 0.1750 0.3379 0.0743 0.0385 0.001 0.071 0.067 0.841 0.008 0.296 35.920 0.05 16775. 0.4201
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2.41 0.1969 0.3694 0.0719 0.0383 0.001 0.071 0.064 0.838 0.008 0.287 34.898 0.05 16793. 0.4014
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2.68 0.2188 0.3983 0.0694 0.0381 0.001 0.070 0.062 0.832 0.008 0.276 33.868 0.05 16811. 0.3826
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2.95 0.2406 0.4247 0.0666 0.0378 0.001 0.070 0.060 0.825 0.008 0.266 32.829 0.05 16831. 0.3635
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3.22 0.2625 0.4484 0.0638 0.0373 0.001 0.069 0.057 0.816 0.008 0.254 31.775 0.05 16851. 0.3443
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3.49 0.2844 0.4694 0.0608 0.0368 0.001 0.068 0.054 0.805 0.008 0.242 30.703 0.05 16872. 0.3248
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3.76 0.3063 0.4875 0.0577 0.0362 0.001 0.067 0.052 0.792 0.008 0.230 29.608 0.05 16895. 0.3050
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4.02 0.3281 0.5024 0.0544 0.0355 0.001 0.066 0.049 0.776 0.007 0.217 28.480 0.05 16919. 0.2849
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4.29 0.3500 0.5139 0.0510 0.0347 0.001 0.064 0.046 0.759 0.007 0.203 27.312 0.05 16943. 0.2646
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4.56 0.3719 0.5217 0.0475 0.0338 0.001 0.062 0.043 0.739 0.007 0.189 26.095 0.05 16969. 0.2438
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4.83 0.3938 0.5254 0.0438 0.0328 0.001 0.061 0.039 0.718 0.007 0.175 24.818 0.05 16996. 0.2228
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5.10 0.4156 0.5244 0.0401 0.0318 0.001 0.059 0.036 0.694 0.007 0.160 23.469 0.05 17024. 0.2015
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5.37 0.4375 0.5182 0.0362 0.0306 0.001 0.057 0.032 0.669 0.006 0.144 22.032 0.05 17053. 0.1799
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5.63 0.4594 0.5060 0.0323 0.0294 0.001 0.054 0.029 0.642 0.006 0.129 20.491 0.05 17084. 0.1581
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5.90 0.4813 0.4870 0.0284 0.0280 0.001 0.052 0.025 0.613 0.006 0.113 18.824 0.05 17115. 0.1360
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6.17 0.5031 0.4599 0.0244 0.0266 0.001 0.049 0.022 0.582 0.006 0.097 17.003 0.05 17148. 0.1138
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6.44 0.5250 0.4233 0.0203 0.0252 0.001 0.047 0.018 0.550 0.005 0.081 14.997 0.05 17181. 0.0917
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6.71 0.5469 0.3752 0.0162 0.0236 0.001 0.044 0.015 0.517 0.005 0.065 12.763 0.05 17216. 0.0697
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6.97 0.5688 0.3133 0.0122 0.0221 0.001 0.041 0.011 0.482 0.005 0.048 10.246 0.05 17252. 0.0484
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7.24 0.5906 0.2342 0.0081 0.0204 0.001 0.038 0.007 0.446 0.004 0.032 7.377 0.05 17289. 0.0285
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7.51 0.6125 0.1338 0.0041 0.0187 0.001 0.035 0.004 0.409 0.004 0.016 4.062 0.05 17328. 0.0111
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7.78 0.6344 0.0057 0.0002 0.0170 0.000 0.031 0.000 0.372 0.004 0.001 0.168 0.05 17367. 0.0001
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0895 0.0341 0.008 0.252 0.321 5.960 0.028 1.428 24.429 0.10 33340. 0.6271
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0.54 0.0220 0.0565 0.0881 0.0344 0.008 0.254 0.316 6.008 0.029 1.404 23.834 0.10 33361. 0.6068
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1.08 0.0441 0.1101 0.0865 0.0346 0.008 0.256 0.310 6.052 0.029 1.379 23.238 0.10 33383. 0.5863
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1.62 0.0661 0.1610 0.0848 0.0348 0.008 0.257 0.304 6.090 0.029 1.352 22.645 0.10 33407. 0.5658
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2.16 0.0882 0.2090 0.0830 0.0350 0.008 0.259 0.298 6.121 0.029 1.324 22.053 0.10 33432. 0.5451
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2.70 0.1102 0.2543 0.0811 0.0351 0.008 0.260 0.291 6.143 0.029 1.293 21.465 0.10 33460. 0.5244
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3.24 0.1322 0.2969 0.0791 0.0352 0.008 0.260 0.283 6.156 0.029 1.260 20.880 0.10 33489. 0.5036
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3.78 0.1543 0.3367 0.0769 0.0352 0.008 0.260 0.276 6.158 0.029 1.226 20.298 0.10 33520. 0.4828
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4.32 0.1763 0.3738 0.0746 0.0352 0.008 0.260 0.267 6.148 0.029 1.189 19.721 0.10 33553. 0.4620
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4.86 0.1983 0.4083 0.0721 0.0350 0.008 0.259 0.259 6.124 0.029 1.150 19.146 0.10 33588. 0.4411
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5.41 0.2204 0.4401 0.0695 0.0348 0.008 0.257 0.249 6.086 0.029 1.109 18.573 0.10 33625. 0.4201
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5.95 0.2424 0.4692 0.0668 0.0345 0.008 0.255 0.239 6.033 0.029 1.065 18.001 0.10 33664. 0.3991
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6.49 0.2645 0.4956 0.0639 0.0341 0.008 0.252 0.229 5.963 0.028 1.019 17.428 0.10 33706. 0.3780
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7.03 0.2865 0.5191 0.0609 0.0336 0.008 0.248 0.218 5.875 0.028 0.971 16.851 0.10 33749. 0.3567
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7.57 0.3085 0.5397 0.0577 0.0330 0.008 0.244 0.207 5.769 0.028 0.920 16.269 0.10 33795. 0.3353
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8.11 0.3306 0.5572 0.0544 0.0323 0.008 0.239 0.195 5.644 0.027 0.868 15.676 0.10 33843. 0.3137
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8.65 0.3526 0.5713 0.0510 0.0315 0.007 0.232 0.183 5.499 0.026 0.813 15.069 0.10 33893. 0.2919
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9.19 0.3747 0.5818 0.0474 0.0305 0.007 0.226 0.170 5.336 0.025 0.756 14.443 0.10 33945. 0.2698
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9.73 0.3967 0.5882 0.0437 0.0295 0.007 0.218 0.157 5.155 0.025 0.697 13.791 0.10 34000. 0.2474
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10.27 0.4187 0.5901 0.0400 0.0284 0.007 0.209 0.143 4.956 0.024 0.637 13.106 0.10 34056. 0.2247
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10.81 0.4408 0.5867 0.0361 0.0271 0.006 0.200 0.129 4.741 0.023 0.576 12.380 0.10 34115. 0.2018
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11.35 0.4628 0.5773 0.0322 0.0258 0.006 0.191 0.115 4.509 0.022 0.513 11.602 0.10 34177. 0.1785
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11.89 0.4848 0.5608 0.0282 0.0244 0.006 0.180 0.101 4.261 0.020 0.449 10.757 0.10 34241. 0.1549
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12.43 0.5069 0.5355 0.0242 0.0229 0.005 0.169 0.087 3.997 0.019 0.385 9.827 0.10 34307. 0.1310
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12.97 0.5289 0.4997 0.0201 0.0213 0.005 0.157 0.072 3.720 0.018 0.321 8.786 0.10 34375. 0.1069
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13.51 0.5510 0.4503 0.0160 0.0196 0.005 0.145 0.057 3.429 0.016 0.256 7.602 0.10 34446. 0.0826
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14.05 0.5730 0.3836 0.0120 0.0179 0.004 0.132 0.043 3.126 0.015 0.191 6.226 0.10 34519. 0.0584
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14.59 0.5950 0.2936 0.0079 0.0161 0.004 0.119 0.028 2.812 0.013 0.127 4.589 0.10 34594. 0.0351
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15.13 0.6171 0.1717 0.0040 0.0142 0.003 0.105 0.014 2.489 0.012 0.063 2.587 0.10 34671. 0.0140
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15.67 0.6391 0.0031 0.0001 0.0124 0.003 0.091 0.000 2.159 0.010 0.001 0.046 0.10 34751. 0.0000
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PROP RPM = 3000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0898 0.0325 0.026 0.540 0.724 19.178 0.061 3.221 17.128 0.15 50010. 0.6605
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0.83 0.0226 0.0607 0.0883 0.0328 0.026 0.545 0.712 19.358 0.062 3.167 16.685 0.15 50041. 0.6380
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1.66 0.0451 0.1183 0.0867 0.0331 0.026 0.550 0.699 19.520 0.062 3.109 16.244 0.15 50075. 0.6154
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2.49 0.0677 0.1726 0.0849 0.0333 0.026 0.554 0.685 19.662 0.063 3.047 15.805 0.15 50112. 0.5928
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3.32 0.0903 0.2238 0.0831 0.0335 0.027 0.557 0.670 19.778 0.063 2.981 15.370 0.15 50152. 0.5701
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4.15 0.1129 0.2719 0.0811 0.0337 0.027 0.560 0.654 19.864 0.063 2.910 14.939 0.15 50194. 0.5475
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4.98 0.1354 0.3170 0.0790 0.0338 0.027 0.561 0.637 19.915 0.063 2.834 14.513 0.15 50239. 0.5249
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5.81 0.1580 0.3591 0.0768 0.0338 0.027 0.561 0.619 19.927 0.063 2.754 14.091 0.15 50287. 0.5024
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6.64 0.1806 0.3982 0.0744 0.0337 0.027 0.560 0.600 19.894 0.063 2.668 13.674 0.15 50339. 0.4798
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7.47 0.2031 0.4345 0.0718 0.0336 0.027 0.558 0.579 19.813 0.063 2.577 13.261 0.15 50393. 0.4573
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8.30 0.2257 0.4679 0.0691 0.0334 0.026 0.554 0.558 19.678 0.063 2.480 12.852 0.15 50451. 0.4349
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9.13 0.2483 0.4984 0.0663 0.0330 0.026 0.549 0.535 19.486 0.062 2.378 12.446 0.15 50512. 0.4124
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9.96 0.2709 0.5260 0.0633 0.0326 0.026 0.542 0.511 19.232 0.061 2.271 12.041 0.15 50577. 0.3899
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10.79 0.2934 0.5507 0.0602 0.0321 0.025 0.533 0.485 18.914 0.060 2.158 11.636 0.15 50645. 0.3673
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11.63 0.3160 0.5723 0.0569 0.0314 0.025 0.522 0.459 18.527 0.059 2.040 11.229 0.15 50716. 0.3446
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12.46 0.3386 0.5906 0.0534 0.0306 0.024 0.509 0.431 18.070 0.058 1.917 10.816 0.15 50791. 0.3217
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13.29 0.3611 0.6054 0.0498 0.0297 0.024 0.494 0.402 17.542 0.056 1.788 10.395 0.16 50869. 0.2986
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14.12 0.3837 0.6164 0.0461 0.0287 0.023 0.477 0.372 16.945 0.054 1.655 9.961 0.16 50951. 0.2753
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14.95 0.4063 0.6232 0.0423 0.0276 0.022 0.459 0.341 16.283 0.052 1.519 9.510 0.16 51036. 0.2518
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15.78 0.4289 0.6251 0.0384 0.0264 0.021 0.438 0.310 15.556 0.050 1.379 9.037 0.16 51125. 0.2280
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16.61 0.4514 0.6213 0.0344 0.0250 0.020 0.416 0.278 14.767 0.047 1.236 8.534 0.16 51217. 0.2038
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17.44 0.4740 0.6109 0.0304 0.0236 0.019 0.392 0.245 13.916 0.044 1.091 7.992 0.16 51313. 0.1793
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18.27 0.4966 0.5924 0.0263 0.0220 0.017 0.366 0.212 13.007 0.041 0.944 7.397 0.16 51413. 0.1544
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19.10 0.5191 0.5637 0.0222 0.0204 0.016 0.339 0.179 12.042 0.038 0.795 6.733 0.16 51516. 0.1290
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19.93 0.5417 0.5220 0.0180 0.0187 0.015 0.311 0.145 11.024 0.035 0.646 5.975 0.16 51623. 0.1032
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20.76 0.5643 0.4631 0.0139 0.0169 0.013 0.281 0.112 9.958 0.032 0.497 5.088 0.16 51734. 0.0771
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21.59 0.5869 0.3803 0.0097 0.0150 0.012 0.249 0.078 8.849 0.028 0.349 4.018 0.16 51848. 0.0510
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22.42 0.6094 0.2632 0.0056 0.0131 0.010 0.217 0.045 7.704 0.025 0.202 2.678 0.16 51966. 0.0259
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23.25 0.6320 0.0935 0.0016 0.0111 0.009 0.184 0.013 6.530 0.021 0.059 0.917 0.16 52088. 0.0048
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24.08 0.6546
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PROP RPM = 4000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0901 0.0316 0.059 0.934 1.291 44.209 0.106 5.744 13.249 0.21 66679. 0.6822
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1.09 0.0221 0.0615 0.0886 0.0319 0.060 0.943 1.270 44.643 0.107 5.650 12.905 0.21 66720. 0.6590
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2.17 0.0443 0.1197 0.0870 0.0322 0.060 0.952 1.248 45.040 0.108 5.549 12.563 0.21 66765. 0.6358
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3.26 0.0664 0.1747 0.0853 0.0325 0.061 0.959 1.223 45.389 0.108 5.441 12.224 0.21 66813. 0.6126
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4.35 0.0886 0.2265 0.0835 0.0327 0.061 0.965 1.197 45.680 0.109 5.326 11.889 0.21 66864. 0.5894
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5.43 0.1107 0.2752 0.0816 0.0328 0.062 0.970 1.170 45.902 0.110 5.202 11.557 0.21 66919. 0.5663
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6.52 0.1329 0.3209 0.0795 0.0329 0.062 0.973 1.140 46.046 0.110 5.071 11.230 0.21 66978. 0.5433
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7.61 0.1550 0.3637 0.0773 0.0330 0.062 0.974 1.109 46.100 0.110 4.931 10.908 0.21 67041. 0.5204
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8.69 0.1772 0.4035 0.0750 0.0329 0.062 0.973 1.075 46.053 0.110 4.783 10.590 0.21 67107. 0.4976
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9.78 0.1993 0.4405 0.0725 0.0328 0.062 0.970 1.040 45.895 0.110 4.625 10.276 0.21 67178. 0.4748
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10.86 0.2215 0.4747 0.0699 0.0326 0.061 0.964 1.002 45.615 0.109 4.458 9.966 0.21 67253. 0.4521
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11.95 0.2436 0.5061 0.0671 0.0323 0.061 0.955 0.963 45.204 0.108 4.282 9.660 0.21 67332. 0.4295
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13.04 0.2658 0.5347 0.0642 0.0319 0.060 0.944 0.921 44.651 0.107 4.097 9.356 0.21 67416. 0.4068
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14.12 0.2879 0.5606 0.0612 0.0314 0.059 0.929 0.877 43.949 0.105 3.902 9.053 0.21 67503. 0.3842
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15.21 0.3101 0.5835 0.0580 0.0308 0.058 0.911 0.831 43.090 0.103 3.698 8.750 0.21 67596. 0.3615
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16.30 0.3322 0.6034 0.0546 0.0301 0.056 0.889 0.783 42.068 0.100 3.484 8.446 0.21 67692. 0.3387
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17.38 0.3544 0.6201 0.0511 0.0292 0.055 0.864 0.733 40.879 0.098 3.262 8.137 0.21 67793. 0.3157
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18.47 0.3765 0.6334 0.0475 0.0283 0.053 0.835 0.682 39.528 0.094 3.032 7.822 0.21 67899. 0.2926
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19.56 0.3987 0.6428 0.0438 0.0272 0.051 0.803 0.628 38.020 0.091 2.795 7.497 0.21 68009. 0.2693
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20.64 0.4208 0.6479 0.0400 0.0260 0.049 0.768 0.574 36.359 0.087 2.553 7.159 0.21 68124. 0.2458
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21.73 0.4430 0.6481 0.0361 0.0247 0.046 0.730 0.518 34.549 0.082 2.305 6.803 0.21 68243. 0.2219
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22.82 0.4651 0.6424 0.0322 0.0233 0.044 0.689 0.462 32.592 0.078 2.053 6.423 0.21 68367. 0.1977
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23.90 0.4873 0.6297 0.0282 0.0218 0.041 0.644 0.404 30.494 0.073 1.797 6.010 0.21 68495. 0.1731
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24.99 0.5094 0.6083 0.0241 0.0202 0.038 0.597 0.346 28.261 0.067 1.539 5.553 0.21 68629. 0.1480
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26.08 0.5316 0.5757 0.0201 0.0185 0.035 0.547 0.288 25.898 0.062 1.279 5.036 0.21 68767. 0.1224
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27.16 0.5537 0.5282 0.0160 0.0167 0.031 0.495 0.229 23.416 0.056 1.019 4.436 0.21 68909. 0.0962
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28.25 0.5759 0.4604 0.0119 0.0149 0.028 0.440 0.171 20.826 0.050 0.759 3.718 0.21 69057. 0.0696
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29.33 0.5980 0.3630 0.0079 0.0130 0.024 0.383 0.113 18.141 0.043 0.502 2.823 0.21 69209. 0.0430
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30.42 0.6202 0.2203 0.0039 0.0110 0.021 0.325 0.056 15.380 0.037 0.249 1.652 0.21 69365. 0.0177
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31.51 0.6423 0.0012 0.0000 0.0090 0.017 0.265 0.000 12.552 0.030 0.001 0.008 0.21 69524. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0904 0.0311 0.114 1.434 2.025 84.834 0.162 9.005 10.824 0.26 83347. 0.6979
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1.36 0.0222 0.0628 0.0889 0.0314 0.115 1.449 1.992 85.707 0.164 8.858 10.539 0.26 83398. 0.6739
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2.72 0.0443 0.1222 0.0873 0.0317 0.116 1.462 1.956 86.506 0.165 8.700 10.256 0.26 83454. 0.6499
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4.08 0.0665 0.1783 0.0856 0.0319 0.117 1.474 1.918 87.211 0.167 8.532 9.976 0.26 83514. 0.6260
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5.44 0.0887 0.2312 0.0838 0.0321 0.118 1.484 1.877 87.802 0.168 8.351 9.699 0.26 83579. 0.6022
|
|
6.80 0.1108 0.2808 0.0819 0.0323 0.118 1.492 1.834 88.259 0.169 8.158 9.426 0.26 83648. 0.5784
|
|
8.16 0.1330 0.3274 0.0798 0.0324 0.119 1.497 1.788 88.559 0.169 7.952 9.157 0.26 83722. 0.5548
|
|
9.52 0.1552 0.3709 0.0776 0.0325 0.119 1.499 1.739 88.682 0.169 7.733 8.892 0.26 83800. 0.5313
|
|
10.87 0.1774 0.4115 0.0753 0.0324 0.119 1.498 1.686 88.606 0.169 7.500 8.632 0.26 83884. 0.5079
|
|
12.23 0.1995 0.4492 0.0728 0.0323 0.118 1.493 1.631 88.310 0.169 7.253 8.375 0.26 83972. 0.4846
|
|
13.59 0.2217 0.4840 0.0702 0.0321 0.118 1.484 1.572 87.771 0.168 6.992 8.123 0.26 84066. 0.4614
|
|
14.95 0.2439 0.5161 0.0674 0.0318 0.117 1.470 1.510 86.972 0.166 6.715 7.874 0.26 84165. 0.4384
|
|
16.31 0.2660 0.5454 0.0645 0.0314 0.115 1.452 1.444 85.893 0.164 6.424 7.627 0.26 84270. 0.4153
|
|
17.67 0.2882 0.5719 0.0614 0.0309 0.113 1.429 1.376 84.516 0.161 6.119 7.383 0.26 84380. 0.3923
|
|
19.03 0.3104 0.5956 0.0582 0.0303 0.111 1.400 1.304 82.827 0.158 5.798 7.139 0.26 84495. 0.3693
|
|
20.39 0.3325 0.6162 0.0548 0.0296 0.108 1.366 1.228 80.813 0.154 5.464 6.894 0.26 84616. 0.3462
|
|
21.75 0.3547 0.6338 0.0513 0.0287 0.105 1.326 1.150 78.467 0.150 5.115 6.647 0.26 84743. 0.3230
|
|
23.11 0.3769 0.6479 0.0477 0.0277 0.102 1.281 1.069 75.798 0.145 4.754 6.396 0.26 84875. 0.2996
|
|
24.47 0.3990 0.6584 0.0440 0.0267 0.098 1.231 0.985 72.814 0.139 4.383 6.138 0.26 85013. 0.2761
|
|
25.83 0.4212 0.6646 0.0402 0.0255 0.093 1.175 0.900 69.523 0.133 4.002 5.870 0.26 85157. 0.2523
|
|
27.19 0.4434 0.6661 0.0363 0.0241 0.088 1.115 0.812 65.933 0.126 3.613 5.589 0.26 85306. 0.2282
|
|
28.55 0.4656 0.6618 0.0323 0.0227 0.083 1.049 0.723 62.050 0.119 3.218 5.289 0.26 85461. 0.2038
|
|
29.90 0.4877 0.6507 0.0283 0.0212 0.078 0.978 0.633 57.882 0.111 2.817 4.963 0.26 85622. 0.1790
|
|
31.26 0.5099 0.6309 0.0242 0.0196 0.072 0.903 0.542 53.442 0.102 2.412 4.603 0.26 85789. 0.1536
|
|
32.62 0.5321 0.5999 0.0201 0.0178 0.065 0.824 0.451 48.743 0.093 2.005 4.194 0.26 85962. 0.1276
|
|
33.98 0.5542 0.5539 0.0160 0.0160 0.059 0.740 0.359 43.804 0.084 1.597 3.718 0.26 86140. 0.1009
|
|
35.34 0.5764 0.4867 0.0119 0.0141 0.052 0.653 0.268 38.647 0.074 1.191 3.141 0.26 86325. 0.0736
|
|
36.70 0.5986 0.3882 0.0079 0.0122 0.045 0.563 0.177 33.302 0.064 0.788 2.413 0.26 86515. 0.0460
|
|
38.06 0.6207 0.2399 0.0039 0.0102 0.037 0.470 0.088 27.803 0.053 0.392 1.438 0.26 86711. 0.0193
|
|
39.42 0.6429 0.0028 0.0000 0.0081 0.030 0.375 0.001 22.168 0.042 0.004 0.016 0.26 86909. 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 0.0907 0.0307 0.194 2.042 2.927 144.955 0.231 13.019 9.158 0.31 100013. 0.7100
|
|
1.63 0.0222 0.0638 0.0892 0.0310 0.196 2.064 2.879 146.499 0.233 12.807 8.914 0.31 100076. 0.6854
|
|
3.27 0.0444 0.1242 0.0877 0.0313 0.198 2.084 2.828 147.913 0.235 12.579 8.672 0.31 100143. 0.6608
|
|
4.90 0.0666 0.1811 0.0860 0.0316 0.200 2.101 2.773 149.162 0.237 12.336 8.433 0.31 100215. 0.6363
|
|
6.53 0.0888 0.2347 0.0841 0.0318 0.201 2.116 2.715 150.213 0.239 12.075 8.197 0.31 100293. 0.6120
|
|
8.17 0.1110 0.2851 0.0822 0.0320 0.203 2.128 2.652 151.029 0.240 11.796 7.965 0.31 100376. 0.5877
|
|
9.80 0.1332 0.3323 0.0801 0.0321 0.203 2.135 2.585 151.572 0.241 11.499 7.736 0.31 100465. 0.5636
|
|
11.43 0.1554 0.3764 0.0779 0.0322 0.204 2.138 2.514 151.804 0.242 11.182 7.511 0.31 100559. 0.5397
|
|
13.06 0.1776 0.4176 0.0756 0.0321 0.203 2.137 2.438 151.687 0.241 10.845 7.291 0.31 100660. 0.5159
|
|
14.70 0.1998 0.4558 0.0731 0.0320 0.203 2.130 2.358 151.184 0.241 10.488 7.074 0.31 100766. 0.4922
|
|
16.33 0.2219 0.4912 0.0705 0.0318 0.201 2.117 2.273 150.256 0.239 10.110 6.861 0.31 100879. 0.4687
|
|
17.96 0.2441 0.5238 0.0677 0.0315 0.200 2.097 2.183 148.871 0.237 9.710 6.651 0.31 100999. 0.4453
|
|
19.60 0.2663 0.5536 0.0647 0.0311 0.197 2.071 2.088 146.993 0.234 9.289 6.444 0.31 101124. 0.4220
|
|
21.23 0.2885 0.5806 0.0616 0.0306 0.194 2.037 1.989 144.593 0.230 8.846 6.239 0.31 101257. 0.3987
|
|
22.86 0.3107 0.6049 0.0584 0.0300 0.190 1.995 1.885 141.644 0.225 8.383 6.035 0.31 101396. 0.3754
|
|
24.50 0.3329 0.6261 0.0550 0.0293 0.185 1.946 1.776 138.124 0.220 7.898 5.831 0.31 101541. 0.3520
|
|
26.13 0.3551 0.6443 0.0515 0.0284 0.180 1.888 1.662 134.021 0.213 7.393 5.625 0.31 101694. 0.3286
|
|
27.76 0.3773 0.6592 0.0479 0.0274 0.173 1.822 1.545 129.347 0.206 6.871 5.417 0.31 101853. 0.3050
|
|
29.39 0.3995 0.6705 0.0441 0.0263 0.166 1.748 1.424 124.118 0.198 6.333 5.203 0.31 102019. 0.2813
|
|
31.03 0.4217 0.6776 0.0403 0.0251 0.159 1.667 1.300 118.347 0.188 5.782 4.982 0.31 102192. 0.2574
|
|
32.66 0.4439 0.6801 0.0364 0.0237 0.150 1.578 1.173 112.046 0.178 5.219 4.750 0.31 102371. 0.2331
|
|
34.29 0.4661 0.6769 0.0324 0.0223 0.141 1.482 1.045 105.229 0.167 4.647 4.503 0.31 102558. 0.2085
|
|
35.93 0.4883 0.6670 0.0283 0.0207 0.131 1.379 0.914 97.909 0.156 4.066 4.235 0.31 102752. 0.1835
|
|
37.56 0.5105 0.6485 0.0243 0.0191 0.121 1.269 0.782 90.107 0.143 3.480 3.939 0.31 102952. 0.1579
|
|
39.19 0.5327 0.6189 0.0201 0.0173 0.110 1.153 0.650 81.847 0.130 2.891 3.602 0.31 103160. 0.1316
|
|
40.83 0.5549 0.5740 0.0160 0.0155 0.098 1.031 0.517 73.161 0.116 2.301 3.207 0.31 103375. 0.1045
|
|
42.46 0.5771 0.5073 0.0119 0.0136 0.086 0.903 0.385 64.093 0.102 1.713 2.726 0.31 103597. 0.0766
|
|
44.09 0.5993 0.4077 0.0079 0.0116 0.073 0.770 0.254 54.693 0.087 1.131 2.109 0.31 103826. 0.0482
|
|
45.72 0.6215 0.2537 0.0039 0.0095 0.060 0.634 0.126 45.023 0.072 0.559 1.266 0.31 104061. 0.0203
|
|
47.36 0.6436 -0.0017 0.0000 0.0074 0.047 0.495 -0.001 35.106 0.056 -0.003 -0.008 0.31 104299. 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 0.0911 0.0305 0.307 2.761 4.002 228.652 0.312 17.802 7.939 0.36 116679. 0.7197
|
|
1.91 0.0222 0.0646 0.0897 0.0308 0.310 2.791 3.937 231.149 0.315 17.513 7.726 0.36 116752. 0.6946
|
|
3.81 0.0444 0.1256 0.0881 0.0311 0.313 2.819 3.868 233.438 0.318 17.203 7.515 0.36 116830. 0.6696
|
|
5.72 0.0666 0.1832 0.0864 0.0314 0.316 2.843 3.793 235.464 0.321 16.871 7.306 0.36 116915. 0.6447
|
|
7.63 0.0888 0.2374 0.0846 0.0316 0.318 2.864 3.713 237.171 0.324 16.515 7.101 0.36 117006. 0.6199
|
|
9.53 0.1111 0.2883 0.0826 0.0318 0.320 2.880 3.627 238.499 0.325 16.134 6.898 0.36 117103. 0.5953
|
|
11.44 0.1333 0.3360 0.0805 0.0319 0.321 2.891 3.536 239.389 0.327 15.728 6.700 0.36 117207. 0.5709
|
|
13.35 0.1555 0.3806 0.0783 0.0320 0.322 2.895 3.439 239.778 0.327 15.296 6.505 0.36 117317. 0.5466
|
|
15.25 0.1777 0.4222 0.0760 0.0320 0.321 2.893 3.335 239.606 0.327 14.835 6.314 0.36 117435. 0.5225
|
|
17.16 0.1999 0.4608 0.0735 0.0319 0.320 2.884 3.225 238.811 0.326 14.347 6.126 0.36 117560. 0.4985
|
|
19.07 0.2221 0.4966 0.0708 0.0317 0.318 2.866 3.109 237.333 0.324 13.829 5.942 0.36 117692. 0.4747
|
|
20.97 0.2443 0.5297 0.0680 0.0314 0.315 2.839 2.986 235.117 0.321 13.283 5.761 0.36 117831. 0.4511
|
|
22.88 0.2665 0.5599 0.0651 0.0310 0.311 2.803 2.857 232.109 0.317 12.706 5.582 0.36 117978. 0.4275
|
|
24.79 0.2887 0.5874 0.0620 0.0305 0.306 2.756 2.721 228.259 0.311 12.101 5.406 0.36 118133. 0.4040
|
|
26.69 0.3110 0.6121 0.0587 0.0298 0.300 2.699 2.578 223.524 0.305 11.466 5.231 0.36 118296. 0.3805
|
|
28.60 0.3332 0.6339 0.0553 0.0291 0.292 2.631 2.429 217.866 0.297 10.802 5.056 0.36 118466. 0.3570
|
|
30.51 0.3554 0.6527 0.0518 0.0282 0.283 2.551 2.273 211.268 0.288 10.111 4.880 0.36 118644. 0.3334
|
|
32.41 0.3776 0.6682 0.0481 0.0272 0.273 2.460 2.112 203.749 0.278 9.396 4.702 0.36 118830. 0.3097
|
|
34.32 0.3998 0.6802 0.0443 0.0261 0.262 2.359 1.947 195.332 0.266 8.660 4.521 0.36 119024. 0.2858
|
|
36.23 0.4220 0.6881 0.0405 0.0248 0.249 2.246 1.777 186.039 0.254 7.905 4.333 0.36 119226. 0.2617
|
|
38.13 0.4442 0.6915 0.0365 0.0235 0.236 2.124 1.604 175.888 0.240 7.135 4.136 0.36 119436. 0.2374
|
|
40.04 0.4664 0.6893 0.0325 0.0220 0.221 1.991 1.428 164.900 0.225 6.351 3.927 0.36 119654. 0.2126
|
|
41.95 0.4886 0.6806 0.0284 0.0204 0.205 1.849 1.249 153.099 0.209 5.557 3.701 0.36 119880. 0.1874
|
|
43.85 0.5109 0.6633 0.0243 0.0187 0.188 1.697 1.069 140.517 0.192 4.754 3.450 0.36 120115. 0.1616
|
|
45.76 0.5331 0.6349 0.0202 0.0170 0.171 1.536 0.888 127.194 0.174 3.948 3.165 0.36 120357. 0.1351
|
|
47.67 0.5553 0.5912 0.0161 0.0151 0.152 1.367 0.706 113.183 0.154 3.140 2.829 0.37 120608. 0.1077
|
|
49.57 0.5775 0.5252 0.0120 0.0131 0.132 1.190 0.525 98.551 0.134 2.336 2.417 0.37 120868. 0.0794
|
|
51.48 0.5997 0.4249 0.0079 0.0111 0.112 1.007 0.346 83.385 0.114 1.540 1.883 0.37 121135. 0.0502
|
|
53.39 0.6219 0.2664 0.0039 0.0090 0.091 0.818 0.170 67.784 0.092 0.757 1.138 0.37 121411. 0.0213
|
|
55.29 0.6441 -0.0056 -0.0001 0.0069 0.069 0.625 -0.003 51.775 0.071 -0.012 -0.023 0.37 121687. 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 0.0916 0.0304 0.456 3.595 5.255 340.248 0.406 23.376 7.006 0.41 133342. 0.7277
|
|
2.18 0.0222 0.0652 0.0901 0.0308 0.461 3.635 5.170 344.039 0.411 22.998 6.817 0.41 133426. 0.7023
|
|
4.36 0.0445 0.1268 0.0886 0.0311 0.466 3.672 5.079 347.516 0.415 22.592 6.629 0.41 133516. 0.6770
|
|
6.54 0.0667 0.1848 0.0869 0.0313 0.470 3.704 4.981 350.595 0.418 22.157 6.444 0.41 133613. 0.6517
|
|
8.72 0.0889 0.2395 0.0850 0.0316 0.474 3.732 4.876 353.189 0.422 21.691 6.262 0.41 133717. 0.6266
|
|
10.90 0.1112 0.2908 0.0831 0.0317 0.476 3.753 4.764 355.212 0.424 21.192 6.084 0.41 133828. 0.6017
|
|
13.09 0.1334 0.3389 0.0810 0.0319 0.478 3.767 4.645 356.570 0.426 20.660 5.908 0.41 133947. 0.5770
|
|
15.27 0.1556 0.3839 0.0788 0.0319 0.479 3.774 4.517 357.170 0.426 20.092 5.736 0.41 134074. 0.5524
|
|
17.45 0.1778 0.4258 0.0764 0.0319 0.479 3.771 4.381 356.918 0.426 19.488 5.568 0.41 134209. 0.5280
|
|
19.63 0.2001 0.4649 0.0739 0.0318 0.477 3.758 4.237 355.723 0.425 18.846 5.402 0.41 134352. 0.5039
|
|
21.81 0.2223 0.5010 0.0712 0.0316 0.474 3.735 4.084 353.494 0.422 18.166 5.240 0.41 134504. 0.4799
|
|
23.99 0.2445 0.5344 0.0684 0.0313 0.470 3.699 3.923 350.145 0.418 17.448 5.081 0.41 134663. 0.4560
|
|
26.17 0.2668 0.5650 0.0654 0.0309 0.463 3.651 3.752 345.595 0.413 16.691 4.925 0.41 134832. 0.4323
|
|
28.35 0.2890 0.5929 0.0623 0.0304 0.456 3.590 3.573 339.770 0.406 15.895 4.770 0.41 135009. 0.4086
|
|
30.53 0.3112 0.6180 0.0590 0.0297 0.446 3.514 3.386 332.603 0.397 15.060 4.617 0.41 135196. 0.3850
|
|
32.71 0.3335 0.6403 0.0556 0.0290 0.435 3.424 3.190 324.037 0.387 14.187 4.465 0.41 135391. 0.3613
|
|
34.89 0.3557 0.6596 0.0520 0.0281 0.421 3.318 2.985 314.045 0.375 13.278 4.312 0.41 135595. 0.3375
|
|
37.07 0.3779 0.6756 0.0484 0.0271 0.406 3.198 2.774 302.654 0.361 12.338 4.157 0.41 135808. 0.3137
|
|
39.26 0.4001 0.6882 0.0446 0.0259 0.389 3.063 2.556 289.901 0.346 11.369 3.999 0.41 136030. 0.2897
|
|
41.44 0.4224 0.6969 0.0407 0.0247 0.370 2.914 2.333 275.817 0.329 10.376 3.836 0.41 136261. 0.2655
|
|
43.62 0.4446 0.7010 0.0367 0.0233 0.349 2.752 2.105 260.429 0.311 9.363 3.666 0.42 136502. 0.2410
|
|
45.80 0.4668 0.6998 0.0327 0.0218 0.327 2.575 1.873 243.769 0.291 8.332 3.485 0.42 136752. 0.2161
|
|
47.98 0.4891 0.6919 0.0286 0.0202 0.303 2.386 1.638 225.874 0.270 7.287 3.290 0.42 137011. 0.1908
|
|
50.16 0.5113 0.6757 0.0244 0.0185 0.277 2.185 1.401 206.791 0.247 6.232 3.073 0.42 137279. 0.1648
|
|
52.34 0.5335 0.6484 0.0203 0.0167 0.250 1.971 1.162 186.582 0.223 5.171 2.826 0.42 137557. 0.1381
|
|
54.52 0.5558 0.6057 0.0161 0.0148 0.222 1.747 0.924 165.328 0.197 4.109 2.534 0.42 137844. 0.1104
|
|
56.70 0.5780 0.5403 0.0120 0.0128 0.192 1.512 0.686 143.134 0.171 3.051 2.174 0.42 138141. 0.0816
|
|
58.88 0.6002 0.4392 0.0079 0.0107 0.161 1.269 0.451 120.131 0.143 2.004 1.701 0.42 138447. 0.0517
|
|
61.06 0.6224 0.2760 0.0038 0.0086 0.129 1.019 0.219 96.472 0.115 0.975 1.031 0.42 138763. 0.0219
|
|
63.24 0.6447 -0.0140 -0.0001 0.0065 0.097 0.762 -0.008 72.169 0.086 -0.036 -0.050 0.42 139077. 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 0.0922 0.0304 0.650 4.549 6.692 484.391 0.514 29.766 6.266 0.46 150003. 0.7345
|
|
2.48 0.0225 0.0662 0.0907 0.0308 0.657 4.601 6.583 489.925 0.520 29.283 6.095 0.46 150099. 0.7086
|
|
4.96 0.0449 0.1287 0.0891 0.0311 0.664 4.649 6.466 494.996 0.525 28.763 5.925 0.46 150202. 0.6827
|
|
7.43 0.0674 0.1877 0.0874 0.0314 0.670 4.691 6.341 499.476 0.530 28.204 5.758 0.46 150312. 0.6570
|
|
9.91 0.0898 0.2431 0.0855 0.0316 0.675 4.726 6.206 503.241 0.534 27.606 5.594 0.46 150431. 0.6314
|
|
12.39 0.1123 0.2951 0.0835 0.0318 0.679 4.754 6.062 506.156 0.537 26.964 5.432 0.46 150558. 0.6060
|
|
14.87 0.1347 0.3438 0.0814 0.0319 0.681 4.772 5.908 508.086 0.539 26.279 5.274 0.46 150694. 0.5809
|
|
17.35 0.1572 0.3893 0.0791 0.0319 0.682 4.779 5.744 508.892 0.540 25.547 5.119 0.46 150839. 0.5559
|
|
19.82 0.1796 0.4317 0.0767 0.0319 0.682 4.775 5.568 508.433 0.539 24.768 4.968 0.46 150994. 0.5311
|
|
22.30 0.2021 0.4712 0.0741 0.0318 0.679 4.757 5.382 506.573 0.537 23.940 4.819 0.46 151157. 0.5066
|
|
24.78 0.2245 0.5077 0.0714 0.0316 0.675 4.726 5.185 503.180 0.534 23.062 4.674 0.46 151331. 0.4822
|
|
27.26 0.2470 0.5415 0.0686 0.0313 0.668 4.678 4.976 498.125 0.529 22.134 4.531 0.46 151514. 0.4580
|
|
29.74 0.2694 0.5724 0.0655 0.0308 0.659 4.614 4.756 491.290 0.521 21.155 4.391 0.46 151707. 0.4339
|
|
32.21 0.2919 0.6006 0.0623 0.0303 0.647 4.532 4.524 482.563 0.512 20.125 4.253 0.46 151910. 0.4099
|
|
34.69 0.3143 0.6260 0.0590 0.0296 0.633 4.431 4.282 471.849 0.501 19.045 4.116 0.46 152123. 0.3859
|
|
37.17 0.3368 0.6485 0.0555 0.0288 0.616 4.311 4.028 459.065 0.487 17.915 3.979 0.46 152346. 0.3619
|
|
39.65 0.3592 0.6679 0.0518 0.0279 0.596 4.171 3.763 444.182 0.471 16.738 3.843 0.47 152580. 0.3378
|
|
42.13 0.3817 0.6842 0.0481 0.0268 0.573 4.012 3.490 427.245 0.453 15.521 3.705 0.47 152824. 0.3136
|
|
44.60 0.4042 0.6968 0.0442 0.0256 0.548 3.835 3.208 408.307 0.433 14.269 3.564 0.47 153079. 0.2892
|
|
47.08 0.4266 0.7055 0.0402 0.0243 0.520 3.638 2.919 387.412 0.411 12.986 3.418 0.47 153344. 0.2646
|
|
49.56 0.4491 0.7095 0.0362 0.0229 0.489 3.424 2.625 364.601 0.387 11.676 3.266 0.47 153619. 0.2397
|
|
52.04 0.4715 0.7080 0.0320 0.0213 0.456 3.192 2.326 339.923 0.361 10.345 3.103 0.47 153905. 0.2144
|
|
54.52 0.4940 0.6995 0.0279 0.0197 0.420 2.944 2.022 313.433 0.333 8.996 2.927 0.47 154202. 0.1886
|
|
56.99 0.5164 0.6821 0.0236 0.0179 0.382 2.679 1.717 285.209 0.303 7.635 2.730 0.47 154510. 0.1621
|
|
59.47 0.5389 0.6526 0.0194 0.0160 0.342 2.398 1.409 255.348 0.271 6.268 2.503 0.47 154828. 0.1346
|
|
61.95 0.5613 0.6060 0.0152 0.0141 0.300 2.103 1.102 223.978 0.238 4.901 2.231 0.47 155157. 0.1061
|
|
64.43 0.5838 0.5333 0.0110 0.0120 0.256 1.796 0.796 191.266 0.203 3.541 1.888 0.47 155498. 0.0763
|
|
66.91 0.6062 0.4178 0.0068 0.0099 0.211 1.478 0.494 157.417 0.167 2.199 1.424 0.47 155848. 0.0454
|
|
69.38 0.6287 0.2229 0.0027 0.0077 0.164 1.152 0.198 122.662 0.130 0.881 0.733 0.47 156209. 0.0148
|
|
71.86 0.6511
|
|
|
|
|
|
|
|
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 0.0928 0.0305 0.893 5.630 8.319 666.149 0.636 37.004 5.664 0.51 166662. 0.7403
|
|
2.73 0.0222 0.0658 0.0914 0.0308 0.904 5.695 8.187 673.781 0.643 36.414 5.511 0.51 166767. 0.7145
|
|
5.45 0.0444 0.1280 0.0898 0.0312 0.913 5.754 8.044 680.783 0.650 35.778 5.359 0.51 166881. 0.6887
|
|
8.18 0.0667 0.1867 0.0880 0.0314 0.921 5.807 7.890 686.980 0.656 35.096 5.209 0.51 167003. 0.6630
|
|
10.90 0.0889 0.2419 0.0862 0.0317 0.928 5.851 7.726 692.205 0.661 34.364 5.062 0.51 167133. 0.6376
|
|
13.63 0.1111 0.2938 0.0842 0.0319 0.934 5.885 7.550 696.279 0.665 33.581 4.918 0.51 167273. 0.6123
|
|
16.35 0.1333 0.3424 0.0821 0.0320 0.937 5.908 7.361 699.016 0.668 32.743 4.777 0.51 167423. 0.5872
|
|
19.08 0.1556 0.3879 0.0799 0.0320 0.939 5.919 7.160 700.229 0.669 31.849 4.638 0.51 167582. 0.5624
|
|
21.80 0.1778 0.4303 0.0775 0.0320 0.938 5.914 6.946 699.730 0.668 30.897 4.503 0.51 167751. 0.5377
|
|
24.53 0.2000 0.4699 0.0750 0.0319 0.935 5.894 6.719 697.335 0.666 29.885 4.370 0.51 167931. 0.5133
|
|
27.25 0.2222 0.5066 0.0723 0.0317 0.929 5.856 6.478 692.863 0.662 28.813 4.240 0.51 168120. 0.4890
|
|
29.98 0.2445 0.5406 0.0694 0.0314 0.920 5.799 6.223 686.144 0.655 27.678 4.113 0.52 168321. 0.4649
|
|
32.70 0.2667 0.5718 0.0664 0.0310 0.908 5.722 5.953 677.012 0.646 26.481 3.989 0.52 168532. 0.4410
|
|
35.43 0.2889 0.6004 0.0633 0.0304 0.892 5.623 5.670 665.319 0.635 25.222 3.866 0.52 168755. 0.4171
|
|
38.15 0.3111 0.6262 0.0600 0.0298 0.873 5.502 5.373 650.933 0.622 23.901 3.744 0.52 168988. 0.3933
|
|
40.88 0.3333 0.6493 0.0565 0.0290 0.850 5.357 5.063 633.740 0.605 22.519 3.623 0.52 169232. 0.3694
|
|
43.60 0.3556 0.6695 0.0529 0.0281 0.823 5.187 4.739 613.681 0.586 21.079 3.503 0.52 169488. 0.3455
|
|
46.33 0.3778 0.6867 0.0491 0.0270 0.792 4.994 4.404 590.806 0.564 19.588 3.381 0.52 169755. 0.3215
|
|
49.05 0.4000 0.7004 0.0453 0.0259 0.758 4.777 4.059 565.187 0.540 18.053 3.257 0.52 170033. 0.2973
|
|
51.78 0.4222 0.7105 0.0413 0.0246 0.720 4.538 3.705 536.885 0.513 16.479 3.130 0.52 170322. 0.2730
|
|
54.50 0.4445 0.7161 0.0373 0.0232 0.679 4.276 3.343 505.958 0.483 14.871 2.997 0.52 170623. 0.2483
|
|
57.23 0.4667 0.7167 0.0332 0.0216 0.634 3.993 2.976 472.465 0.451 13.236 2.857 0.52 170936. 0.2233
|
|
59.95 0.4889 0.7109 0.0290 0.0200 0.585 3.689 2.603 436.481 0.417 11.578 2.705 0.52 171260. 0.1977
|
|
62.68 0.5111 0.6970 0.0248 0.0182 0.534 3.365 2.226 398.102 0.380 9.903 2.537 0.52 171595. 0.1715
|
|
65.40 0.5333 0.6723 0.0206 0.0164 0.479 3.021 1.848 357.453 0.341 8.219 2.345 0.52 171943. 0.1444
|
|
68.13 0.5556 0.6323 0.0164 0.0144 0.422 2.660 1.469 314.698 0.301 6.533 2.117 0.52 172302. 0.1163
|
|
70.85 0.5778 0.5694 0.0122 0.0124 0.362 2.283 1.091 270.048 0.258 4.854 1.833 0.52 172673. 0.0868
|
|
73.58 0.6000 0.4693 0.0080 0.0102 0.300 1.891 0.718 223.767 0.214 3.192 1.455 0.52 173056. 0.0558
|
|
76.30 0.6222 0.3018 0.0039 0.0081 0.236 1.489 0.350 176.170 0.168 1.558 0.902 0.52 173450. 0.0242
|
|
79.03 0.6445 -0.0132 -0.0001 0.0058 0.171 1.076 -0.011 127.252 0.122 -0.048 -0.038 0.52 173841. 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 0.0936 0.0306 1.195 6.847 10.146 891.136 0.774 45.129 5.164 0.57 183318. 0.7453
|
|
2.99 0.0222 0.0659 0.0921 0.0310 1.209 6.927 9.985 901.445 0.783 44.415 5.024 0.57 183434. 0.7194
|
|
5.99 0.0444 0.1282 0.0905 0.0313 1.222 6.999 9.813 910.898 0.791 43.647 4.886 0.57 183559. 0.6935
|
|
8.98 0.0666 0.1870 0.0888 0.0316 1.233 7.063 9.627 919.265 0.798 42.821 4.750 0.57 183693. 0.6678
|
|
11.97 0.0888 0.2423 0.0869 0.0318 1.242 7.118 9.428 926.317 0.804 41.935 4.616 0.57 183837. 0.6423
|
|
14.97 0.1110 0.2943 0.0850 0.0320 1.250 7.160 9.214 931.813 0.809 40.986 4.485 0.57 183991. 0.6169
|
|
17.96 0.1331 0.3430 0.0829 0.0322 1.255 7.188 8.986 935.505 0.812 39.970 4.357 0.57 184156. 0.5918
|
|
20.95 0.1553 0.3887 0.0806 0.0322 1.257 7.201 8.742 937.138 0.814 38.885 4.231 0.57 184331. 0.5669
|
|
23.95 0.1775 0.4313 0.0782 0.0322 1.256 7.196 8.482 936.462 0.813 37.730 4.108 0.57 184517. 0.5422
|
|
26.94 0.1997 0.4711 0.0757 0.0321 1.251 7.171 8.206 933.227 0.810 36.500 3.988 0.57 184715. 0.5177
|
|
29.93 0.2219 0.5080 0.0730 0.0319 1.243 7.124 7.913 927.193 0.805 35.197 3.871 0.57 184924. 0.4934
|
|
32.93 0.2441 0.5422 0.0701 0.0316 1.231 7.055 7.603 918.128 0.797 33.817 3.756 0.57 185144. 0.4693
|
|
35.92 0.2663 0.5737 0.0671 0.0311 1.215 6.960 7.275 905.813 0.786 32.361 3.643 0.57 185377. 0.4453
|
|
38.91 0.2885 0.6026 0.0639 0.0306 1.194 6.839 6.931 890.047 0.773 30.829 3.532 0.57 185621. 0.4213
|
|
41.91 0.3107 0.6288 0.0606 0.0299 1.168 6.690 6.570 870.654 0.756 29.222 3.422 0.57 185878. 0.3975
|
|
44.90 0.3329 0.6523 0.0571 0.0291 1.136 6.512 6.191 847.480 0.736 27.539 3.314 0.57 186147. 0.3736
|
|
47.89 0.3551 0.6729 0.0535 0.0282 1.100 6.304 5.797 820.440 0.712 25.786 3.205 0.57 186427. 0.3496
|
|
50.89 0.3773 0.6906 0.0497 0.0271 1.059 6.067 5.389 789.600 0.685 23.970 3.096 0.57 186721. 0.3256
|
|
53.88 0.3994 0.7050 0.0458 0.0260 1.013 5.802 4.968 755.056 0.655 22.098 2.984 0.57 187026. 0.3014
|
|
56.88 0.4216 0.7157 0.0418 0.0246 0.961 5.508 4.537 716.890 0.622 20.179 2.870 0.57 187344. 0.2770
|
|
59.87 0.4438 0.7222 0.0378 0.0232 0.905 5.188 4.096 675.179 0.586 18.219 2.752 0.57 187675. 0.2523
|
|
62.86 0.4660 0.7237 0.0336 0.0217 0.845 4.841 3.648 630.004 0.547 16.225 2.626 0.57 188018. 0.2273
|
|
65.86 0.4882 0.7191 0.0294 0.0200 0.780 4.468 3.193 581.467 0.505 14.202 2.491 0.57 188374. 0.2017
|
|
68.85 0.5104 0.7065 0.0252 0.0182 0.710 4.070 2.734 529.694 0.460 12.159 2.341 0.57 188742. 0.1754
|
|
71.84 0.5326 0.6834 0.0209 0.0163 0.637 3.649 2.272 474.853 0.412 10.104 2.170 0.57 189124. 0.1482
|
|
74.84 0.5548 0.6452 0.0167 0.0143 0.559 3.205 1.809 417.164 0.362 8.046 1.967 0.57 189518. 0.1199
|
|
77.83 0.5770 0.5845 0.0124 0.0123 0.479 2.742 1.348 356.909 0.310 5.995 1.713 0.57 189925. 0.0901
|
|
80.82 0.5992 0.4866 0.0082 0.0101 0.395 2.262 0.892 294.444 0.256 3.965 1.373 0.58 190345. 0.0588
|
|
83.82 0.6214 0.3205 0.0041 0.0079 0.309 1.769 0.443 230.194 0.200 1.969 0.872 0.58 190777. 0.0263
|
|
86.81 0.6435 0.0020 0.0000 0.0056 0.220 1.262 0.002 164.222 0.143 0.008 0.005 0.58 191209. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0944 0.0309 1.563 8.211 12.182 1165.692 0.928 54.188 4.740 0.62 199970. 0.7497
|
|
3.26 0.0222 0.0660 0.0929 0.0312 1.581 8.306 11.992 1179.304 0.938 53.339 4.612 0.62 200097. 0.7237
|
|
6.53 0.0444 0.1284 0.0913 0.0316 1.598 8.394 11.786 1191.781 0.948 52.424 4.486 0.62 200233. 0.6978
|
|
9.79 0.0666 0.1873 0.0896 0.0319 1.613 8.472 11.565 1202.818 0.957 51.440 4.361 0.62 200380. 0.6720
|
|
13.06 0.0887 0.2427 0.0878 0.0321 1.625 8.538 11.327 1212.109 0.965 50.383 4.239 0.62 200538. 0.6464
|
|
16.32 0.1109 0.2947 0.0858 0.0323 1.635 8.588 11.072 1219.337 0.970 49.249 4.119 0.62 200707. 0.6210
|
|
19.59 0.1331 0.3436 0.0837 0.0324 1.642 8.623 10.799 1224.175 0.974 48.035 4.001 0.62 200887. 0.5958
|
|
22.85 0.1553 0.3894 0.0814 0.0325 1.644 8.637 10.508 1226.286 0.976 46.738 3.886 0.62 201079. 0.5708
|
|
26.12 0.1775 0.4322 0.0790 0.0325 1.643 8.631 10.197 1225.339 0.975 45.354 3.774 0.62 201282. 0.5461
|
|
29.38 0.1997 0.4721 0.0765 0.0323 1.637 8.600 9.866 1221.007 0.972 43.882 3.665 0.62 201498. 0.5216
|
|
32.65 0.2219 0.5092 0.0737 0.0321 1.627 8.544 9.514 1212.973 0.965 42.320 3.558 0.62 201727. 0.4972
|
|
35.91 0.2440 0.5436 0.0708 0.0318 1.610 8.459 9.142 1200.931 0.956 40.666 3.453 0.62 201968. 0.4731
|
|
39.18 0.2662 0.5754 0.0678 0.0314 1.589 8.344 8.750 1184.598 0.943 38.919 3.350 0.62 202223. 0.4490
|
|
42.44 0.2884 0.6046 0.0646 0.0308 1.561 8.197 8.336 1163.706 0.926 37.080 3.249 0.62 202490. 0.4251
|
|
45.71 0.3106 0.6311 0.0612 0.0301 1.526 8.016 7.902 1138.027 0.906 35.150 3.150 0.62 202770. 0.4012
|
|
48.97 0.3328 0.6550 0.0577 0.0293 1.485 7.800 7.448 1107.361 0.881 33.129 3.051 0.62 203064. 0.3773
|
|
52.24 0.3550 0.6760 0.0540 0.0284 1.437 7.548 6.974 1071.590 0.853 31.022 2.952 0.62 203371. 0.3533
|
|
55.50 0.3772 0.6942 0.0502 0.0273 1.382 7.260 6.484 1030.800 0.820 28.839 2.853 0.62 203691. 0.3292
|
|
58.77 0.3994 0.7091 0.0463 0.0261 1.321 6.939 5.978 985.118 0.784 26.589 2.752 0.62 204025. 0.3049
|
|
62.03 0.4215 0.7204 0.0423 0.0248 1.253 6.583 5.459 934.654 0.744 24.282 2.649 0.62 204372. 0.2805
|
|
65.30 0.4437 0.7276 0.0382 0.0233 1.179 6.195 4.929 879.507 0.700 21.924 2.542 0.62 204733. 0.2557
|
|
68.56 0.4659 0.7299 0.0340 0.0217 1.099 5.774 4.389 819.791 0.652 19.524 2.429 0.62 205107. 0.2305
|
|
71.83 0.4881 0.7262 0.0298 0.0200 1.013 5.322 3.842 755.632 0.601 17.090 2.306 0.62 205496. 0.2048
|
|
75.09 0.5103 0.7147 0.0255 0.0182 0.922 4.840 3.289 687.205 0.547 14.631 2.171 0.62 205898. 0.1784
|
|
78.36 0.5325 0.6927 0.0212 0.0163 0.824 4.330 2.733 614.728 0.489 12.157 2.017 0.63 206314. 0.1511
|
|
81.62 0.5547 0.6558 0.0169 0.0143 0.722 3.793 2.176 538.493 0.429 9.679 1.833 0.63 206744. 0.1225
|
|
84.89 0.5768 0.5962 0.0126 0.0122 0.615 3.232 1.621 458.872 0.365 7.210 1.602 0.63 207188. 0.0924
|
|
88.15 0.5990 0.4989 0.0083 0.0100 0.505 2.651 1.071 376.340 0.299 4.765 1.291 0.63 207646. 0.0605
|
|
91.41 0.6212 0.3310 0.0041 0.0077 0.391 2.053 0.531 291.457 0.232 2.360 0.826 0.63 208117. 0.0273
|
|
94.68 0.6434 -0.0005 0.0000 0.0054 0.274 1.439 -0.001 204.278 0.163 -0.002 -0.001 0.63 208587. 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 0.0312 2.008 9.734 14.442 1497.174 1.100 64.238 4.375 0.67 216618. 0.7534
|
|
3.54 0.0222 0.0660 0.0939 0.0316 2.031 9.849 14.218 1514.805 1.113 63.243 4.257 0.67 216755. 0.7274
|
|
7.07 0.0444 0.1284 0.0923 0.0319 2.053 9.954 13.977 1530.954 1.125 62.170 4.141 0.67 216904. 0.7015
|
|
10.61 0.0665 0.1872 0.0906 0.0322 2.072 10.047 13.717 1545.224 1.135 61.014 4.026 0.67 217064. 0.6757
|
|
14.14 0.0887 0.2427 0.0887 0.0324 2.088 10.125 13.438 1557.223 1.144 59.771 3.914 0.67 217235. 0.6501
|
|
17.68 0.1109 0.2948 0.0867 0.0326 2.101 10.185 13.138 1566.533 1.151 58.436 3.804 0.67 217419. 0.6247
|
|
21.21 0.1331 0.3437 0.0846 0.0328 2.109 10.225 12.816 1572.733 1.155 57.006 3.696 0.67 217614. 0.5996
|
|
24.75 0.1552 0.3896 0.0823 0.0328 2.113 10.243 12.472 1575.389 1.157 55.475 3.591 0.67 217823. 0.5746
|
|
28.28 0.1774 0.4325 0.0799 0.0328 2.111 10.234 12.105 1574.073 1.156 53.841 3.488 0.67 218044. 0.5499
|
|
31.82 0.1996 0.4725 0.0773 0.0327 2.103 10.197 11.713 1568.357 1.152 52.101 3.388 0.67 218279. 0.5253
|
|
35.35 0.2218 0.5098 0.0746 0.0324 2.089 10.129 11.298 1557.841 1.144 50.253 3.289 0.67 218527. 0.5010
|
|
38.89 0.2440 0.5445 0.0717 0.0321 2.068 10.026 10.858 1542.128 1.133 48.296 3.194 0.67 218790. 0.4768
|
|
42.43 0.2661 0.5765 0.0686 0.0317 2.039 9.888 10.393 1520.851 1.117 46.228 3.100 0.67 219066. 0.4528
|
|
45.96 0.2883 0.6059 0.0654 0.0311 2.003 9.711 9.903 1493.671 1.097 44.049 3.007 0.67 219356. 0.4288
|
|
49.50 0.3105 0.6328 0.0620 0.0304 1.958 9.494 9.389 1460.295 1.073 41.761 2.916 0.67 219660. 0.4049
|
|
53.03 0.3327 0.6570 0.0584 0.0296 1.905 9.235 8.850 1420.462 1.043 39.365 2.826 0.67 219979. 0.3809
|
|
56.57 0.3548 0.6785 0.0547 0.0286 1.843 8.934 8.288 1374.024 1.009 36.866 2.736 0.67 220311. 0.3569
|
|
60.10 0.3770 0.6971 0.0509 0.0275 1.772 8.589 7.706 1321.084 0.970 34.275 2.646 0.67 220659. 0.3328
|
|
63.64 0.3992 0.7126 0.0469 0.0263 1.692 8.204 7.105 1261.809 0.927 31.604 2.554 0.67 221021. 0.3085
|
|
67.17 0.4214 0.7245 0.0428 0.0249 1.604 7.778 6.489 1196.344 0.879 28.864 2.460 0.67 221397. 0.2840
|
|
70.71 0.4435 0.7324 0.0387 0.0234 1.508 7.313 5.859 1124.821 0.826 26.063 2.363 0.67 221788. 0.2592
|
|
74.25 0.4657 0.7355 0.0345 0.0218 1.405 6.810 5.218 1047.381 0.769 23.211 2.260 0.68 222194. 0.2339
|
|
77.78 0.4879 0.7327 0.0302 0.0201 1.293 6.269 4.568 964.198 0.708 20.318 2.149 0.68 222615. 0.2081
|
|
81.32 0.5101 0.7223 0.0258 0.0182 1.174 5.692 3.911 875.489 0.643 17.395 2.026 0.68 223051. 0.1815
|
|
84.85 0.5323 0.7015 0.0215 0.0163 1.048 5.081 3.249 781.544 0.574 14.453 1.886 0.68 223502. 0.1540
|
|
88.39 0.5544 0.6659 0.0171 0.0142 0.916 4.439 2.587 682.739 0.502 11.506 1.718 0.68 223967. 0.1252
|
|
91.92 0.5766 0.6075 0.0127 0.0121 0.777 3.768 1.926 579.565 0.426 8.568 1.508 0.68 224448. 0.0948
|
|
95.46 0.5988 0.5110 0.0084 0.0098 0.634 3.073 1.272 472.655 0.347 5.660 1.221 0.68 224944. 0.0624
|
|
98.99 0.6210 0.3414 0.0042 0.0076 0.486 2.359 0.629 362.760 0.266 2.798 0.787 0.68 225455. 0.0283
|
|
102.53 0.6431 -0.0027 0.0000 0.0052 0.335 1.625 -0.003 249.947 0.184 -0.015 -0.006 0.68 225963. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0964 0.0316 2.542 11.446 16.940 1895.860 1.293 75.351 4.053 0.72 233260. 0.7558
|
|
3.80 0.0222 0.0658 0.0950 0.0320 2.572 11.579 16.682 1917.838 1.308 74.202 3.945 0.72 233409. 0.7302
|
|
7.61 0.0443 0.1281 0.0934 0.0323 2.599 11.701 16.403 1938.033 1.322 72.959 3.839 0.72 233569. 0.7045
|
|
11.41 0.0665 0.1869 0.0917 0.0326 2.623 11.809 16.101 1955.927 1.334 71.619 3.734 0.72 233742. 0.6789
|
|
15.22 0.0887 0.2422 0.0898 0.0329 2.643 11.900 15.777 1970.999 1.344 70.175 3.631 0.72 233927. 0.6534
|
|
19.02 0.1108 0.2944 0.0878 0.0331 2.659 11.970 15.428 1982.702 1.352 68.623 3.529 0.72 234126. 0.6281
|
|
22.83 0.1330 0.3433 0.0857 0.0332 2.669 12.017 15.053 1990.468 1.358 66.957 3.430 0.72 234337. 0.6030
|
|
26.63 0.1551 0.3892 0.0834 0.0332 2.674 12.037 14.652 1993.716 1.360 65.172 3.333 0.72 234562. 0.5781
|
|
30.44 0.1773 0.4322 0.0810 0.0332 2.671 12.026 14.223 1991.886 1.359 63.265 3.239 0.72 234802. 0.5535
|
|
34.24 0.1995 0.4724 0.0784 0.0331 2.661 11.981 13.766 1984.434 1.354 61.233 3.146 0.72 235055. 0.5290
|
|
38.05 0.2216 0.5098 0.0756 0.0329 2.643 11.899 13.281 1970.845 1.344 59.072 3.056 0.72 235324. 0.5047
|
|
41.85 0.2438 0.5447 0.0727 0.0325 2.616 11.777 12.765 1950.624 1.331 56.781 2.968 0.72 235607. 0.4805
|
|
45.66 0.2660 0.5769 0.0696 0.0321 2.579 11.612 12.221 1923.310 1.312 54.359 2.882 0.72 235905. 0.4565
|
|
49.46 0.2881 0.6066 0.0663 0.0315 2.532 11.401 11.647 1888.472 1.288 51.806 2.797 0.72 236218. 0.4326
|
|
53.27 0.3103 0.6338 0.0629 0.0308 2.475 11.143 11.044 1845.741 1.259 49.124 2.714 0.72 236546. 0.4087
|
|
57.07 0.3324 0.6584 0.0593 0.0299 2.407 10.836 10.412 1794.793 1.224 46.313 2.631 0.72 236890. 0.3847
|
|
60.88 0.3546 0.6803 0.0555 0.0289 2.327 10.477 9.753 1735.434 1.184 43.380 2.549 0.72 237249. 0.3607
|
|
64.68 0.3768 0.6994 0.0516 0.0278 2.237 10.069 9.069 1667.787 1.138 40.337 2.466 0.72 237623. 0.3365
|
|
68.49 0.3989 0.7154 0.0476 0.0266 2.135 9.612 8.363 1592.069 1.086 37.200 2.383 0.72 238013. 0.3122
|
|
72.29 0.4211 0.7280 0.0435 0.0252 2.023 9.107 7.639 1508.471 1.029 33.979 2.297 0.73 238419. 0.2877
|
|
76.10 0.4433 0.7366 0.0393 0.0236 1.900 8.556 6.899 1417.174 0.967 30.686 2.208 0.73 238841. 0.2628
|
|
79.90 0.4654 0.7406 0.0350 0.0220 1.768 7.959 6.145 1318.373 0.899 27.333 2.114 0.73 239278. 0.2375
|
|
83.71 0.4876 0.7386 0.0306 0.0202 1.626 7.319 5.380 1212.318 0.827 23.929 2.013 0.73 239731. 0.2115
|
|
87.51 0.5098 0.7292 0.0262 0.0183 1.474 6.637 4.606 1099.323 0.750 20.489 1.901 0.73 240200. 0.1848
|
|
91.32 0.5319 0.7094 0.0218 0.0163 1.314 5.915 3.828 979.805 0.668 17.025 1.772 0.73 240686. 0.1571
|
|
95.12 0.5541 0.6747 0.0173 0.0142 1.146 5.158 3.047 854.312 0.583 13.554 1.618 0.73 241187. 0.1280
|
|
98.93 0.5762 0.6170 0.0129 0.0121 0.970 4.368 2.269 723.555 0.494 10.094 1.423 0.73 241705. 0.0971
|
|
102.73 0.5984 0.5203 0.0085 0.0098 0.789 3.553 1.499 588.435 0.401 6.666 1.155 0.73 242238. 0.0641
|
|
106.54 0.6206 0.3484 0.0042 0.0075 0.603 2.717 0.740 450.025 0.307 3.292 0.746 0.73 242787. 0.0291
|
|
110.34 0.6427 -0.0042 0.0000 0.0051 0.414 1.862 -0.006 308.458 0.210 -0.026 -0.009 0.73 243333. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0977 0.0325 3.212 13.498 19.696 2395.517 1.525 87.608 3.729 0.77 249895. 0.7499
|
|
4.07 0.0221 0.0649 0.0962 0.0328 3.244 13.632 19.401 2419.317 1.540 86.298 3.637 0.77 250056. 0.7260
|
|
8.14 0.0443 0.1266 0.0946 0.0331 3.273 13.755 19.082 2441.041 1.554 84.878 3.546 0.77 250228. 0.7018
|
|
12.22 0.0664 0.1850 0.0929 0.0334 3.299 13.862 18.737 2460.102 1.566 83.344 3.455 0.77 250414. 0.6776
|
|
16.29 0.0886 0.2403 0.0911 0.0336 3.320 13.951 18.365 2475.889 1.576 81.688 3.364 0.77 250613. 0.6533
|
|
20.36 0.1107 0.2924 0.0891 0.0337 3.336 14.018 17.964 2487.765 1.584 79.904 3.275 0.77 250826. 0.6290
|
|
24.43 0.1328 0.3414 0.0870 0.0338 3.346 14.059 17.533 2495.049 1.588 77.986 3.187 0.77 251054. 0.6047
|
|
28.51 0.1550 0.3875 0.0847 0.0339 3.349 14.070 17.070 2497.048 1.590 75.928 3.101 0.77 251296. 0.5805
|
|
32.58 0.1771 0.4307 0.0822 0.0338 3.343 14.048 16.575 2493.044 1.587 73.726 3.016 0.77 251553. 0.5563
|
|
36.65 0.1993 0.4711 0.0796 0.0337 3.329 13.988 16.047 2482.331 1.580 71.376 2.932 0.77 251826. 0.5322
|
|
40.72 0.2214 0.5088 0.0768 0.0334 3.305 13.885 15.484 2464.214 1.569 68.874 2.850 0.77 252114. 0.5082
|
|
44.80 0.2435 0.5439 0.0738 0.0331 3.269 13.738 14.887 2438.015 1.552 66.219 2.770 0.77 252418. 0.4842
|
|
48.87 0.2657 0.5765 0.0707 0.0326 3.223 13.541 14.256 2403.099 1.530 63.410 2.691 0.77 252738. 0.4603
|
|
52.94 0.2878 0.6065 0.0674 0.0320 3.163 13.292 13.590 2358.863 1.502 60.447 2.613 0.77 253075. 0.4365
|
|
57.01 0.3100 0.6340 0.0639 0.0313 3.091 12.987 12.889 2304.799 1.467 57.331 2.537 0.77 253427. 0.4126
|
|
61.09 0.3321 0.6590 0.0603 0.0304 3.005 12.625 12.155 2240.475 1.426 54.065 2.461 0.77 253796. 0.3887
|
|
65.16 0.3542 0.6813 0.0565 0.0294 2.904 12.203 11.388 2165.630 1.379 50.653 2.385 0.78 254181. 0.3647
|
|
69.23 0.3764 0.7008 0.0525 0.0282 2.790 11.723 10.592 2080.444 1.324 47.113 2.309 0.78 254583. 0.3405
|
|
73.30 0.3985 0.7174 0.0485 0.0269 2.662 11.186 9.770 1985.241 1.264 43.459 2.232 0.78 255001. 0.3162
|
|
77.38 0.4206 0.7304 0.0443 0.0255 2.522 10.595 8.927 1880.318 1.197 39.706 2.153 0.78 255436. 0.2915
|
|
81.45 0.4428 0.7395 0.0400 0.0239 2.368 9.951 8.064 1765.973 1.124 35.868 2.071 0.78 255887. 0.2665
|
|
85.52 0.4649 0.7438 0.0356 0.0223 2.203 9.255 7.185 1642.552 1.046 31.957 1.984 0.78 256356. 0.2410
|
|
89.59 0.4871 0.7421 0.0312 0.0205 2.026 8.511 6.292 1510.469 0.962 27.986 1.889 0.78 256841. 0.2147
|
|
93.66 0.5092 0.7324 0.0267 0.0186 1.838 7.721 5.389 1370.254 0.872 23.969 1.784 0.78 257343. 0.1876
|
|
97.74 0.5313 0.7120 0.0222 0.0166 1.640 6.889 4.479 1222.582 0.778 19.923 1.662 0.78 257863. 0.1594
|
|
101.81 0.5535 0.6759 0.0177 0.0145 1.433 6.020 3.567 1068.312 0.680 15.866 1.514 0.78 258399. 0.1296
|
|
105.88 0.5756 0.6157 0.0132 0.0123 1.218 5.119 2.657 908.525 0.578 11.819 1.327 0.78 258953. 0.0980
|
|
109.95 0.5978 0.5153 0.0087 0.0101 0.998 4.195 1.755 744.544 0.474 7.806 1.069 0.78 259524. 0.0642
|
|
114.03 0.6199 0.3400 0.0043 0.0078 0.775 3.256 0.866 577.897 0.368 3.854 0.680 0.79 260111. 0.0287
|
|
118.10 0.6420 -0.0045 0.0000 0.0055 0.548 2.304 -0.008 408.799 0.260 -0.035 -0.009 0.79 260696. 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 0.0991 0.0344 4.132 16.278 22.728 3081.326 1.839 101.093 3.346 0.82 266522. 0.7227
|
|
4.34 0.0221 0.0623 0.0976 0.0346 4.158 16.380 22.396 3100.778 1.851 99.620 3.276 0.82 266694. 0.7025
|
|
8.68 0.0442 0.1220 0.0961 0.0348 4.181 16.469 22.036 3117.560 1.861 98.018 3.206 0.82 266879. 0.6819
|
|
13.02 0.0664 0.1790 0.0944 0.0350 4.199 16.540 21.646 3131.046 1.869 96.283 3.136 0.82 267078. 0.6611
|
|
17.36 0.0885 0.2333 0.0925 0.0351 4.212 16.591 21.224 3140.586 1.874 94.405 3.065 0.82 267292. 0.6399
|
|
21.70 0.1106 0.2849 0.0905 0.0351 4.218 16.617 20.768 3145.500 1.877 92.377 2.995 0.82 267520. 0.6184
|
|
26.04 0.1327 0.3339 0.0884 0.0351 4.218 16.614 20.277 3145.055 1.877 90.192 2.924 0.82 267764. 0.5967
|
|
30.38 0.1549 0.3802 0.0861 0.0351 4.209 16.580 19.749 3138.503 1.873 87.843 2.854 0.82 268024. 0.5747
|
|
34.72 0.1770 0.4238 0.0836 0.0349 4.191 16.509 19.183 3125.071 1.865 85.324 2.784 0.82 268299. 0.5525
|
|
39.07 0.1991 0.4649 0.0810 0.0347 4.162 16.397 18.577 3103.971 1.853 82.631 2.715 0.82 268591. 0.5302
|
|
43.41 0.2212 0.5034 0.0782 0.0343 4.123 16.241 17.932 3074.426 1.835 79.761 2.645 0.82 268900. 0.5076
|
|
47.75 0.2434 0.5394 0.0752 0.0339 4.071 16.036 17.246 3035.652 1.812 76.710 2.577 0.82 269226. 0.4849
|
|
52.09 0.2655 0.5728 0.0720 0.0334 4.005 15.779 16.519 2986.897 1.783 73.478 2.509 0.82 269568. 0.4620
|
|
56.43 0.2876 0.6037 0.0687 0.0327 3.926 15.465 15.752 2927.440 1.747 70.064 2.441 0.83 269928. 0.4389
|
|
60.77 0.3097 0.6321 0.0651 0.0319 3.831 15.091 14.944 2856.687 1.705 66.472 2.373 0.83 270305. 0.4156
|
|
65.11 0.3318 0.6578 0.0614 0.0310 3.721 14.657 14.097 2774.553 1.656 62.703 2.304 0.83 270699. 0.3920
|
|
69.45 0.3540 0.6806 0.0576 0.0299 3.595 14.161 13.211 2680.585 1.600 58.763 2.235 0.83 271111. 0.3682
|
|
73.79 0.3761 0.7004 0.0536 0.0288 3.453 13.602 12.291 2574.854 1.537 54.670 2.165 0.83 271540. 0.3439
|
|
78.13 0.3982 0.7168 0.0494 0.0275 3.296 12.984 11.341 2457.803 1.467 50.443 2.093 0.83 271987. 0.3193
|
|
82.47 0.4203 0.7296 0.0452 0.0260 3.124 12.306 10.364 2329.535 1.390 46.099 2.018 0.83 272452. 0.2944
|
|
86.81 0.4425 0.7380 0.0408 0.0245 2.937 11.571 9.364 2190.438 1.307 41.653 1.939 0.83 272934. 0.2689
|
|
91.15 0.4646 0.7411 0.0364 0.0228 2.737 10.783 8.345 2041.153 1.218 37.120 1.854 0.83 273434. 0.2427
|
|
95.49 0.4867 0.7374 0.0319 0.0210 2.524 9.944 7.310 1882.452 1.124 32.516 1.761 0.83 273952. 0.2158
|
|
99.83 0.5088 0.7248 0.0273 0.0192 2.300 9.061 6.262 1715.313 1.024 27.855 1.656 0.83 274487. 0.1878
|
|
104.17 0.5309 0.7000 0.0227 0.0172 2.066 8.140 5.206 1540.819 0.920 23.158 1.533 0.83 275041. 0.1585
|
|
108.52 0.5531 0.6578 0.0181 0.0152 1.824 7.186 4.147 1360.304 0.812 18.446 1.383 0.83 275613. 0.1276
|
|
112.86 0.5752 0.5899 0.0135 0.0131 1.576 6.209 3.090 1175.364 0.701 13.743 1.192 0.84 276204. 0.0950
|
|
117.20 0.5973 0.4814 0.0089 0.0110 1.325 5.219 2.041 987.875 0.590 9.076 0.937 0.84 276812. 0.0606
|
|
121.54 0.6194 0.3042 0.0044 0.0089 1.073 4.226 1.007 799.899 0.477 4.478 0.571 0.84 277438. 0.0260
|
|
125.88 0.6416 -0.0044 0.0000 0.0068 0.820 3.230 -0.011 611.479 0.365 -0.048 -0.008 0.84 278064. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1005 0.0381 5.488 20.347 26.018 4092.359 2.299 115.728 2.884 0.87 283143. 0.6665
|
|
4.62 0.0222 0.0575 0.0990 0.0382 5.496 20.378 25.652 4098.715 2.302 114.099 2.839 0.87 283326. 0.6515
|
|
9.24 0.0443 0.1132 0.0975 0.0382 5.500 20.390 25.252 4100.987 2.304 112.322 2.793 0.87 283524. 0.6359
|
|
13.86 0.0665 0.1669 0.0958 0.0382 5.496 20.378 24.818 4098.562 2.302 110.389 2.746 0.87 283737. 0.6200
|
|
18.48 0.0887 0.2187 0.0940 0.0381 5.486 20.339 24.346 4090.795 2.298 108.290 2.699 0.87 283966. 0.6035
|
|
23.11 0.1108 0.2686 0.0920 0.0380 5.467 20.270 23.834 4076.998 2.290 106.014 2.652 0.87 284210. 0.5866
|
|
27.73 0.1330 0.3164 0.0899 0.0378 5.440 20.168 23.281 4056.436 2.279 103.554 2.603 0.87 284471. 0.5691
|
|
32.35 0.1552 0.3622 0.0876 0.0375 5.402 20.029 22.684 4028.362 2.263 100.900 2.554 0.87 284749. 0.5512
|
|
36.97 0.1773 0.4059 0.0851 0.0372 5.353 19.848 22.043 3992.023 2.242 98.046 2.504 0.87 285045. 0.5328
|
|
41.59 0.1995 0.4475 0.0825 0.0368 5.293 19.622 21.355 3946.665 2.217 94.987 2.454 0.88 285358. 0.5139
|
|
46.21 0.2217 0.4869 0.0796 0.0362 5.219 19.348 20.620 3891.556 2.186 91.717 2.403 0.88 285688. 0.4945
|
|
50.83 0.2438 0.5241 0.0766 0.0356 5.131 19.022 19.837 3825.979 2.149 88.235 2.352 0.88 286037. 0.4746
|
|
55.45 0.2660 0.5590 0.0734 0.0349 5.028 18.641 19.006 3749.198 2.106 84.539 2.299 0.88 286404. 0.4542
|
|
60.07 0.2882 0.5916 0.0700 0.0341 4.909 18.200 18.127 3660.481 2.056 80.630 2.246 0.88 286790. 0.4333
|
|
64.70 0.3103 0.6217 0.0664 0.0332 4.773 17.696 17.201 3559.154 1.999 76.511 2.192 0.88 287193. 0.4119
|
|
69.32 0.3325 0.6492 0.0627 0.0321 4.620 17.129 16.228 3445.239 1.935 72.184 2.136 0.88 287616. 0.3900
|
|
73.94 0.3547 0.6735 0.0587 0.0309 4.453 16.509 15.210 3320.480 1.865 67.656 2.078 0.88 288056. 0.3672
|
|
78.56 0.3768 0.6942 0.0546 0.0297 4.270 15.833 14.152 3184.427 1.789 62.948 2.016 0.88 288516. 0.3436
|
|
83.18 0.3990 0.7107 0.0504 0.0283 4.075 15.109 13.058 3038.834 1.707 58.082 1.949 0.88 288993. 0.3191
|
|
87.80 0.4212 0.7219 0.0461 0.0269 3.870 14.349 11.933 2885.924 1.621 53.077 1.875 0.88 289490. 0.2935
|
|
92.42 0.4433 0.7274 0.0416 0.0254 3.652 13.542 10.780 2723.606 1.530 47.951 1.795 0.88 290005. 0.2671
|
|
97.04 0.4655 0.7265 0.0371 0.0238 3.421 12.684 9.605 2551.061 1.433 42.723 1.708 0.88 290540. 0.2398
|
|
101.66 0.4877 0.7175 0.0325 0.0221 3.178 11.781 8.411 2369.607 1.331 37.411 1.610 0.88 291093. 0.2116
|
|
106.29 0.5098 0.6979 0.0278 0.0203 2.925 10.843 7.202 2180.856 1.225 32.035 1.498 0.88 291665. 0.1821
|
|
110.91 0.5320 0.6643 0.0231 0.0185 2.664 9.877 5.984 1986.593 1.116 26.617 1.366 0.89 292256. 0.1514
|
|
115.53 0.5542 0.6116 0.0184 0.0167 2.399 8.893 4.762 1788.632 1.005 21.183 1.208 0.89 292867. 0.1194
|
|
120.15 0.5763 0.5327 0.0137 0.0148 2.131 7.901 3.544 1589.174 0.893 15.762 1.011 0.89 293497. 0.0863
|
|
124.77 0.5985 0.4168 0.0090 0.0130 1.865 6.914 2.336 1390.698 0.781 10.391 0.762 0.89 294146. 0.0528
|
|
129.39 0.6207 0.2470 0.0044 0.0111 1.603 5.945 1.148 1195.659 0.672 5.106 0.435 0.89 294814. 0.0211
|
|
134.01 0.6428 -0.0056 -0.0001 0.0093 1.344 4.984 -0.021 1002.423 0.563 -0.094 -0.010 0.89 295485. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 18000
|
|
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1012 0.0433 7.399 25.909 29.382 5517.661 2.927 130.691 2.415 0.92 299777. 0.5932
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5.02 0.0227 0.0525 0.0998 0.0433 7.394 25.892 28.990 5514.061 2.925 128.949 2.385 0.92 299974. 0.5818
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10.04 0.0455 0.1036 0.0984 0.0432 7.379 25.836 28.558 5502.156 2.919 127.025 2.354 0.92 300188. 0.5700
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15.06 0.0682 0.1534 0.0967 0.0430 7.350 25.738 28.082 5481.156 2.908 124.907 2.324 0.92 300419. 0.5580
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20.08 0.0910 0.2019 0.0949 0.0428 7.309 25.593 27.559 5450.325 2.891 122.583 2.293 0.93 300668. 0.5455
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25.10 0.1137 0.2490 0.0929 0.0424 7.254 25.399 26.987 5409.020 2.870 120.038 2.263 0.93 300935. 0.5327
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30.12 0.1365 0.2948 0.0908 0.0420 7.183 25.153 26.363 5356.629 2.842 117.263 2.232 0.93 301221. 0.5193
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35.14 0.1592 0.3391 0.0885 0.0415 7.098 24.852 25.685 5292.611 2.808 114.247 2.201 0.93 301527. 0.5055
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40.16 0.1820 0.3820 0.0859 0.0409 6.995 24.495 24.951 5216.427 2.767 110.980 2.169 0.93 301852. 0.4910
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45.19 0.2047 0.4233 0.0832 0.0402 6.876 24.078 24.159 5127.605 2.720 107.457 2.137 0.93 302197. 0.4759
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50.21 0.2275 0.4630 0.0803 0.0394 6.740 23.599 23.308 5025.670 2.666 103.672 2.104 0.93 302563. 0.4602
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55.23 0.2502 0.5009 0.0771 0.0385 6.584 23.056 22.397 4910.024 2.605 99.622 2.069 0.93 302948. 0.4437
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60.25 0.2729 0.5370 0.0738 0.0375 6.410 22.446 21.426 4780.141 2.536 95.305 2.033 0.93 303354. 0.4264
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65.27 0.2957 0.5710 0.0702 0.0364 6.216 21.767 20.396 4635.565 2.459 90.723 1.996 0.93 303781. 0.4084
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70.29 0.3184 0.6029 0.0665 0.0351 6.002 21.017 19.308 4475.759 2.374 85.881 1.957 0.93 304229. 0.3896
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75.31 0.3412 0.6324 0.0626 0.0337 5.767 20.194 18.162 4300.511 2.281 80.783 1.915 0.93 304697. 0.3699
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80.33 0.3639 0.6583 0.0584 0.0323 5.519 19.325 16.961 4115.564 2.183 75.444 1.869 0.93 305185. 0.3488
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85.35 0.3867 0.6799 0.0541 0.0308 5.260 18.419 15.713 3922.449 2.081 69.893 1.817 0.93 305695. 0.3264
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90.37 0.4094 0.6961 0.0497 0.0292 4.994 17.485 14.424 3723.705 1.975 64.157 1.757 0.93 306225. 0.3023
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95.39 0.4322 0.7033 0.0451 0.0277 4.736 16.584 13.096 3531.832 1.874 58.252 1.682 0.93 306775. 0.2758
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100.41 0.4549 0.7002 0.0404 0.0263 4.488 15.714 11.736 3346.388 1.775 52.202 1.591 0.93 307347. 0.2469
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105.43 0.4776 0.6883 0.0357 0.0247 4.228 14.805 10.351 3152.884 1.673 46.042 1.489 0.94 307940. 0.2171
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110.45 0.5004 0.6653 0.0308 0.0232 3.961 13.869 8.947 2953.531 1.567 39.798 1.374 0.94 308553. 0.1862
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115.47 0.5231 0.6286 0.0259 0.0216 3.689 12.916 7.531 2750.707 1.459 33.497 1.242 0.94 309188. 0.1544
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120.49 0.5459 0.5746 0.0210 0.0200 3.416 11.962 6.109 2547.378 1.351 27.171 1.088 0.94 309844. 0.1218
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125.51 0.5686 0.4990 0.0162 0.0184 3.146 11.015 4.690 2345.823 1.244 20.862 0.907 0.94 310521. 0.0890
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130.54 0.5914 0.3969 0.0113 0.0169 2.881 10.090 3.285 2148.687 1.140 14.614 0.694 0.94 311220. 0.0570
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135.56 0.6141 0.2623 0.0066 0.0154 2.626 9.196 1.906 1958.434 1.039 8.477 0.441 0.94 311941. 0.0276
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140.58 0.6369 0.0882 0.0019 0.0139 2.381 8.337 0.560 1775.505 0.942 2.492 0.143 0.94 312683. 0.0049
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145.60 0.6596
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