427 lines
76 KiB
Plaintext
427 lines
76 KiB
Plaintext
20.5x10.5PN (205x105PN.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 0.0911 0.0356 0.010 0.654 0.513 7.734 0.074 2.280 30.059 0.08 45241. 0.6159
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0.46 0.0235 0.0585 0.0896 0.0360 0.010 0.661 0.504 7.821 0.075 2.244 29.254 0.08 45270. 0.5947
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0.91 0.0470 0.1138 0.0881 0.0364 0.011 0.668 0.496 7.902 0.075 2.205 28.451 0.08 45301. 0.5734
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1.37 0.0705 0.1659 0.0864 0.0367 0.011 0.674 0.486 7.975 0.076 2.163 27.654 0.08 45336. 0.5519
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1.82 0.0940 0.2148 0.0846 0.0370 0.011 0.679 0.476 8.038 0.077 2.117 26.862 0.08 45372. 0.5305
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2.28 0.1175 0.2607 0.0826 0.0372 0.011 0.684 0.465 8.089 0.077 2.069 26.078 0.08 45412. 0.5090
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2.74 0.1410 0.3036 0.0805 0.0374 0.011 0.687 0.453 8.125 0.078 2.016 25.303 0.08 45455. 0.4876
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3.19 0.1645 0.3434 0.0783 0.0375 0.011 0.688 0.441 8.145 0.078 1.960 24.535 0.08 45500. 0.4662
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3.65 0.1880 0.3803 0.0759 0.0375 0.011 0.689 0.427 8.146 0.078 1.899 23.777 0.08 45549. 0.4447
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4.10 0.2114 0.4144 0.0733 0.0374 0.011 0.687 0.413 8.126 0.078 1.835 23.027 0.08 45600. 0.4233
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4.56 0.2349 0.4456 0.0706 0.0372 0.011 0.683 0.397 8.083 0.077 1.766 22.285 0.08 45655. 0.4020
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5.02 0.2584 0.4740 0.0677 0.0369 0.011 0.678 0.381 8.016 0.077 1.694 21.549 0.08 45713. 0.3806
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5.47 0.2819 0.4995 0.0646 0.0365 0.011 0.670 0.364 7.925 0.076 1.618 20.819 0.08 45774. 0.3594
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5.93 0.3054 0.5222 0.0615 0.0359 0.010 0.660 0.346 7.809 0.075 1.539 20.091 0.08 45839. 0.3382
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6.39 0.3289 0.5420 0.0582 0.0353 0.010 0.648 0.327 7.669 0.073 1.456 19.363 0.08 45907. 0.3171
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6.84 0.3524 0.5588 0.0548 0.0345 0.010 0.634 0.308 7.502 0.072 1.371 18.632 0.08 45978. 0.2960
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7.30 0.3759 0.5724 0.0512 0.0336 0.010 0.618 0.288 7.310 0.070 1.283 17.893 0.08 46053. 0.2750
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7.75 0.3994 0.5827 0.0476 0.0326 0.010 0.599 0.268 7.092 0.068 1.192 17.143 0.08 46131. 0.2540
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8.21 0.4229 0.5893 0.0439 0.0315 0.009 0.579 0.247 6.848 0.065 1.100 16.374 0.08 46212. 0.2330
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8.67 0.4464 0.5919 0.0401 0.0303 0.009 0.556 0.226 6.577 0.063 1.005 15.580 0.08 46297. 0.2120
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9.12 0.4699 0.5898 0.0363 0.0289 0.008 0.531 0.204 6.279 0.060 0.908 14.750 0.08 46386. 0.1908
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9.58 0.4934 0.5824 0.0324 0.0274 0.008 0.503 0.182 5.954 0.057 0.810 13.871 0.08 46478. 0.1694
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10.03 0.5169 0.5686 0.0284 0.0258 0.008 0.473 0.160 5.602 0.053 0.710 12.927 0.08 46574. 0.1478
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10.49 0.5404 0.5469 0.0243 0.0240 0.007 0.441 0.137 5.223 0.050 0.609 11.893 0.08 46673. 0.1260
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10.95 0.5639 0.5152 0.0203 0.0222 0.006 0.407 0.114 4.818 0.046 0.507 10.737 0.08 46776. 0.1038
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11.40 0.5874 0.4703 0.0162 0.0202 0.006 0.371 0.091 4.387 0.042 0.405 9.408 0.08 46882. 0.0812
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11.86 0.6108 0.4072 0.0121 0.0181 0.005 0.332 0.068 3.932 0.038 0.302 7.834 0.08 46992. 0.0584
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12.31 0.6343 0.3181 0.0080 0.0159 0.005 0.292 0.045 3.454 0.033 0.200 5.891 0.08 47105. 0.0357
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12.77 0.6578 0.1887 0.0039 0.0136 0.004 0.250 0.022 2.954 0.028 0.098 3.370 0.08 47221. 0.0143
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13.23 0.6813 -0.0107 -0.0002 0.0112 0.003 0.205 -0.001 2.429 0.023 -0.004 -0.185 0.08 47332. 0.0000
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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 0.0915 0.0323 0.075 2.370 2.060 56.075 0.268 9.165 16.666 0.16 90480. 0.6847
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0.93 0.0240 0.0660 0.0901 0.0327 0.076 2.403 2.028 56.855 0.271 9.019 16.176 0.16 90539. 0.6593
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1.86 0.0480 0.1281 0.0885 0.0331 0.077 2.434 1.992 57.583 0.275 8.861 15.691 0.16 90604. 0.6339
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2.79 0.0719 0.1863 0.0868 0.0335 0.078 2.461 1.953 58.243 0.278 8.689 15.213 0.16 90674. 0.6086
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3.72 0.0959 0.2407 0.0849 0.0338 0.079 2.486 1.912 58.820 0.281 8.504 14.742 0.16 90750. 0.5834
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4.66 0.1199 0.2915 0.0829 0.0341 0.080 2.506 1.867 59.294 0.283 8.304 14.280 0.16 90831. 0.5585
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5.59 0.1439 0.3387 0.0808 0.0343 0.080 2.521 1.818 59.647 0.285 8.088 13.827 0.16 90919. 0.5337
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6.52 0.1679 0.3824 0.0785 0.0344 0.080 2.530 1.766 59.859 0.286 7.856 13.383 0.16 91013. 0.5091
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7.45 0.1919 0.4229 0.0760 0.0345 0.080 2.532 1.710 59.909 0.286 7.607 12.948 0.16 91113. 0.4847
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8.38 0.2158 0.4601 0.0733 0.0344 0.080 2.526 1.650 59.778 0.285 7.341 12.523 0.16 91219. 0.4605
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9.31 0.2398 0.4942 0.0705 0.0342 0.080 2.513 1.587 59.452 0.284 7.058 12.106 0.16 91333. 0.4365
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10.24 0.2638 0.5253 0.0675 0.0339 0.079 2.490 1.520 58.922 0.281 6.759 11.698 0.16 91453. 0.4127
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11.17 0.2878 0.5534 0.0644 0.0335 0.078 2.459 1.449 58.180 0.278 6.445 11.297 0.16 91579. 0.3892
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12.11 0.3118 0.5785 0.0611 0.0329 0.077 2.418 1.375 57.224 0.273 6.118 10.901 0.16 91713. 0.3659
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13.04 0.3358 0.6007 0.0577 0.0322 0.075 2.369 1.299 56.049 0.268 5.777 10.511 0.16 91854. 0.3429
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13.97 0.3597 0.6198 0.0542 0.0314 0.073 2.310 1.220 54.652 0.261 5.425 10.122 0.16 92001. 0.3200
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14.90 0.3837 0.6358 0.0506 0.0305 0.071 2.241 1.138 53.029 0.253 5.062 9.735 0.16 92156. 0.2973
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15.83 0.4077 0.6485 0.0468 0.0294 0.069 2.163 1.054 51.176 0.244 4.690 9.345 0.16 92318. 0.2746
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16.76 0.4317 0.6576 0.0430 0.0282 0.066 2.075 0.969 49.089 0.234 4.308 8.949 0.16 92487. 0.2521
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17.69 0.4557 0.6626 0.0391 0.0269 0.063 1.976 0.881 46.767 0.223 3.918 8.543 0.16 92664. 0.2295
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18.62 0.4797 0.6631 0.0352 0.0254 0.059 1.868 0.792 44.206 0.211 3.521 8.122 0.16 92848. 0.2068
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19.55 0.5036 0.6581 0.0311 0.0238 0.056 1.750 0.701 41.406 0.198 3.117 7.677 0.16 93039. 0.1840
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20.49 0.5276 0.6464 0.0270 0.0221 0.051 1.621 0.609 38.366 0.183 2.708 7.198 0.16 93238. 0.1607
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21.42 0.5516 0.6260 0.0229 0.0202 0.047 1.483 0.516 35.091 0.168 2.294 6.668 0.17 93444. 0.1371
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22.35 0.5756 0.5940 0.0188 0.0182 0.042 1.335 0.422 31.585 0.151 1.878 6.063 0.17 93657. 0.1127
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23.28 0.5996 0.5453 0.0146 0.0160 0.037 1.177 0.328 27.857 0.133 1.460 5.343 0.17 93878. 0.0876
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24.21 0.6236 0.4713 0.0104 0.0138 0.032 1.011 0.234 23.919 0.114 1.042 4.441 0.17 94106. 0.0615
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25.14 0.6475 0.3554 0.0062 0.0114 0.027 0.836 0.141 19.788 0.094 0.626 3.225 0.17 94341. 0.0346
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26.07 0.6715 0.1603 0.0021 0.0089 0.021 0.654 0.048 15.469 0.074 0.213 1.402 0.17 94577. 0.0088
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27.00 0.6955
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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 0.0920 0.0310 0.244 5.126 4.662 181.957 0.579 20.735 11.620 0.24 135715. 0.7181
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1.38 0.0237 0.0681 0.0906 0.0315 0.248 5.203 4.589 184.660 0.588 20.412 11.272 0.24 135803. 0.6911
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2.76 0.0473 0.1321 0.0890 0.0319 0.251 5.274 4.510 187.196 0.596 20.062 10.928 0.24 135899. 0.6643
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4.13 0.0710 0.1920 0.0874 0.0323 0.254 5.339 4.425 189.511 0.603 19.683 10.591 0.24 136002. 0.6377
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5.51 0.0947 0.2480 0.0855 0.0327 0.257 5.397 4.333 191.553 0.610 19.273 10.260 0.24 136114. 0.6113
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6.89 0.1183 0.3002 0.0836 0.0329 0.259 5.445 4.234 193.261 0.615 18.832 9.936 0.24 136235. 0.5852
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8.27 0.1420 0.3487 0.0815 0.0332 0.261 5.482 4.127 194.572 0.619 18.355 9.620 0.24 136364. 0.5593
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9.65 0.1657 0.3938 0.0792 0.0333 0.262 5.506 4.012 195.419 0.622 17.843 9.311 0.24 136502. 0.5338
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11.03 0.1893 0.4355 0.0768 0.0334 0.262 5.515 3.888 195.736 0.623 17.294 9.010 0.24 136650. 0.5085
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12.40 0.2130 0.4740 0.0742 0.0333 0.262 5.507 3.756 195.458 0.622 16.707 8.716 0.24 136806. 0.4835
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13.78 0.2366 0.5093 0.0714 0.0332 0.261 5.481 3.616 194.535 0.619 16.082 8.430 0.24 136973. 0.4588
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15.16 0.2603 0.5417 0.0684 0.0329 0.259 5.436 3.467 192.931 0.614 15.421 8.151 0.24 137149. 0.4344
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16.54 0.2840 0.5712 0.0654 0.0325 0.256 5.371 3.311 190.624 0.607 14.727 7.878 0.24 137336. 0.4103
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17.92 0.3076 0.5978 0.0621 0.0320 0.252 5.285 3.148 187.599 0.597 14.002 7.611 0.25 137532. 0.3865
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19.29 0.3313 0.6216 0.0588 0.0313 0.247 5.180 2.978 183.841 0.585 13.248 7.348 0.25 137738. 0.3630
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20.67 0.3550 0.6425 0.0553 0.0306 0.240 5.053 2.803 179.338 0.571 12.469 7.090 0.25 137955. 0.3398
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22.05 0.3786 0.6606 0.0518 0.0297 0.233 4.904 2.623 174.075 0.554 11.665 6.833 0.25 138182. 0.3167
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23.43 0.4023 0.6756 0.0481 0.0286 0.225 4.734 2.437 168.041 0.535 10.839 6.578 0.25 138420. 0.2939
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24.81 0.4260 0.6874 0.0444 0.0275 0.216 4.542 2.247 161.222 0.513 9.993 6.321 0.25 138668. 0.2712
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26.19 0.4496 0.6957 0.0405 0.0262 0.206 4.328 2.052 153.608 0.489 9.129 6.060 0.25 138927. 0.2485
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27.56 0.4733 0.7000 0.0366 0.0248 0.195 4.091 1.854 145.191 0.462 8.248 5.793 0.25 139196. 0.2258
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28.94 0.4970 0.6996 0.0326 0.0232 0.182 3.831 1.653 135.965 0.433 7.352 5.514 0.25 139477. 0.2029
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30.32 0.5206 0.6936 0.0286 0.0215 0.169 3.548 1.449 125.931 0.401 6.444 5.218 0.25 139768. 0.1798
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31.70 0.5443 0.6802 0.0245 0.0196 0.154 3.243 1.242 115.096 0.366 5.525 4.895 0.25 140070. 0.1561
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33.08 0.5680 0.6571 0.0204 0.0176 0.139 2.915 1.034 103.473 0.329 4.598 4.532 0.25 140382. 0.1319
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34.45 0.5916 0.6202 0.0163 0.0155 0.122 2.566 0.825 91.089 0.290 3.668 4.106 0.25 140706. 0.1067
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35.83 0.6153 0.5620 0.0121 0.0133 0.105 2.197 0.615 77.981 0.248 2.736 3.578 0.25 141040. 0.0803
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37.21 0.6389 0.4684 0.0080 0.0109 0.086 1.809 0.406 64.200 0.204 1.808 2.872 0.25 141384. 0.0524
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38.59 0.6626 0.3071 0.0039 0.0085 0.067 1.403 0.199 49.790 0.158 0.886 1.815 0.25 141734. 0.0232
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39.97 0.6863 -0.0306 -0.0003 0.0058 0.046 0.964 -0.013 34.219 0.109 -0.059 -0.174 0.25 142013. 0.0000
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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 0.0927 0.0305 0.568 8.954 8.345 423.747 1.012 37.121 8.933 0.33 180944. 0.7386
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1.85 0.0239 0.0703 0.0912 0.0310 0.577 9.095 8.216 430.398 1.027 36.544 8.658 0.33 181063. 0.7103
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3.71 0.0477 0.1363 0.0897 0.0314 0.586 9.227 8.075 436.644 1.042 35.918 8.388 0.33 181192. 0.6823
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5.56 0.0716 0.1980 0.0880 0.0318 0.593 9.347 7.922 442.352 1.056 35.238 8.123 0.33 181332. 0.6544
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7.41 0.0955 0.2555 0.0861 0.0322 0.600 9.454 7.757 447.388 1.068 34.503 7.864 0.33 181483. 0.6269
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9.27 0.1193 0.3092 0.0842 0.0325 0.606 9.543 7.578 451.606 1.078 33.708 7.611 0.33 181646. 0.5997
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11.12 0.1432 0.3590 0.0820 0.0327 0.610 9.611 7.385 454.850 1.086 32.850 7.365 0.33 181820. 0.5729
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12.97 0.1670 0.4052 0.0797 0.0329 0.613 9.656 7.178 456.953 1.091 31.927 7.125 0.33 182007. 0.5464
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14.82 0.1909 0.4479 0.0772 0.0329 0.614 9.673 6.955 457.752 1.093 30.935 6.891 0.33 182207. 0.5202
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16.68 0.2148 0.4873 0.0746 0.0329 0.613 9.659 6.716 457.087 1.091 29.874 6.665 0.33 182419. 0.4944
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18.53 0.2386 0.5235 0.0718 0.0327 0.610 9.611 6.462 454.834 1.086 28.744 6.444 0.33 182645. 0.4689
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20.38 0.2625 0.5567 0.0688 0.0324 0.605 9.528 6.193 450.908 1.076 27.548 6.230 0.33 182884. 0.4438
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22.24 0.2864 0.5870 0.0656 0.0320 0.597 9.408 5.911 445.253 1.063 26.291 6.021 0.33 183136. 0.4190
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24.09 0.3102 0.6144 0.0624 0.0315 0.587 9.252 5.616 437.829 1.045 24.979 5.818 0.33 183402. 0.3946
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25.94 0.3341 0.6390 0.0590 0.0308 0.575 9.057 5.309 428.603 1.023 23.615 5.618 0.33 183681. 0.3705
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27.80 0.3580 0.6608 0.0554 0.0300 0.560 8.823 4.992 417.542 0.997 22.203 5.422 0.33 183975. 0.3468
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29.65 0.3818 0.6797 0.0518 0.0291 0.543 8.550 4.665 404.610 0.966 20.748 5.229 0.33 184282. 0.3233
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31.50 0.4057 0.6956 0.0481 0.0280 0.523 8.236 4.329 389.777 0.931 19.253 5.037 0.33 184604. 0.3000
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33.36 0.4296 0.7084 0.0442 0.0268 0.500 7.882 3.984 373.012 0.891 17.722 4.845 0.33 184940. 0.2768
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35.21 0.4534 0.7178 0.0403 0.0255 0.475 7.486 3.633 354.288 0.846 16.157 4.650 0.33 185291. 0.2537
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37.06 0.4773 0.7233 0.0364 0.0240 0.447 7.049 3.274 333.586 0.796 14.563 4.452 0.33 185656. 0.2306
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38.91 0.5011 0.7242 0.0323 0.0224 0.417 6.569 2.910 310.894 0.742 12.942 4.245 0.33 186035. 0.2073
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40.77 0.5250 0.7195 0.0282 0.0206 0.384 6.048 2.540 286.215 0.683 11.299 4.026 0.33 186429. 0.1836
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42.62 0.5489 0.7074 0.0241 0.0187 0.348 5.485 2.167 259.568 0.620 9.638 3.786 0.33 186838. 0.1595
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44.47 0.5727 0.6854 0.0199 0.0166 0.310 4.881 1.790 230.994 0.551 7.963 3.515 0.33 187262. 0.1346
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46.33 0.5966 0.6487 0.0157 0.0144 0.269 4.238 1.412 200.561 0.479 6.282 3.194 0.33 187700. 0.1087
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48.18 0.6205 0.5886 0.0115 0.0121 0.226 3.558 1.035 168.372 0.402 4.602 2.787 0.33 188152. 0.0811
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50.03 0.6443 0.4868 0.0073 0.0097 0.180 2.843 0.658 134.554 0.321 2.928 2.219 0.33 188617. 0.0515
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51.89 0.6682 0.2963 0.0032 0.0071 0.133 2.096 0.285 99.187 0.237 1.267 1.303 0.33 189089. 0.0199
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53.74 0.6921
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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 0.0935 0.0303 1.104 13.913 13.156 823.015 1.572 58.517 7.250 0.41 226165. 0.7527
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2.30 0.0237 0.0709 0.0921 0.0308 1.121 14.137 12.956 836.290 1.597 57.626 7.027 0.41 226313. 0.7239
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4.61 0.0474 0.1374 0.0905 0.0313 1.138 14.348 12.738 848.772 1.621 56.657 6.807 0.41 226474. 0.6953
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6.91 0.0712 0.1996 0.0888 0.0317 1.154 14.541 12.501 860.202 1.643 55.605 6.592 0.41 226648. 0.6671
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9.21 0.0949 0.2577 0.0870 0.0320 1.167 14.712 12.245 870.316 1.662 54.464 6.381 0.41 226836. 0.6391
|
|
11.51 0.1186 0.3117 0.0851 0.0324 1.179 14.856 11.967 878.831 1.678 53.231 6.176 0.41 227039. 0.6116
|
|
13.82 0.1423 0.3620 0.0829 0.0326 1.187 14.968 11.668 885.444 1.691 51.900 5.977 0.41 227256. 0.5844
|
|
16.12 0.1661 0.4087 0.0806 0.0328 1.193 15.042 11.346 889.830 1.699 50.466 5.783 0.41 227488. 0.5576
|
|
18.42 0.1898 0.4518 0.0782 0.0328 1.196 15.073 10.999 891.666 1.703 48.925 5.595 0.41 227736. 0.5311
|
|
20.72 0.2135 0.4917 0.0755 0.0328 1.194 15.056 10.628 890.644 1.701 47.274 5.412 0.41 228000. 0.5050
|
|
23.03 0.2372 0.5285 0.0727 0.0326 1.189 14.986 10.233 886.510 1.693 45.514 5.235 0.41 228280. 0.4793
|
|
25.33 0.2609 0.5622 0.0697 0.0324 1.179 14.861 9.814 879.091 1.679 43.651 5.063 0.41 228576. 0.4540
|
|
27.63 0.2847 0.5931 0.0666 0.0320 1.164 14.678 9.373 868.276 1.658 41.692 4.896 0.41 228889. 0.4291
|
|
29.93 0.3084 0.6212 0.0633 0.0314 1.145 14.436 8.913 853.986 1.631 39.645 4.734 0.41 229219. 0.4045
|
|
32.24 0.3321 0.6466 0.0599 0.0308 1.121 14.135 8.434 836.154 1.597 37.515 4.575 0.41 229566. 0.3803
|
|
34.54 0.3558 0.6692 0.0564 0.0300 1.093 13.772 7.939 814.716 1.556 35.311 4.420 0.41 229930. 0.3564
|
|
36.84 0.3796 0.6891 0.0528 0.0291 1.059 13.348 7.428 789.608 1.508 33.038 4.267 0.41 230311. 0.3328
|
|
39.14 0.4033 0.7062 0.0491 0.0280 1.020 12.860 6.902 760.766 1.453 30.702 4.115 0.41 230709. 0.3095
|
|
41.45 0.4270 0.7203 0.0452 0.0268 0.976 12.309 6.364 728.131 1.391 28.308 3.964 0.41 231126. 0.2863
|
|
43.75 0.4507 0.7313 0.0413 0.0255 0.928 11.692 5.814 691.650 1.321 25.861 3.813 0.41 231560. 0.2631
|
|
46.05 0.4745 0.7386 0.0373 0.0240 0.873 11.010 5.253 651.283 1.244 23.366 3.658 0.41 232012. 0.2400
|
|
48.35 0.4982 0.7418 0.0333 0.0224 0.814 10.261 4.683 607.006 1.159 20.830 3.499 0.41 232482. 0.2167
|
|
50.66 0.5219 0.7399 0.0292 0.0206 0.749 9.447 4.105 558.819 1.067 18.257 3.332 0.41 232970. 0.1932
|
|
52.96 0.5456 0.7314 0.0250 0.0187 0.680 8.566 3.520 506.754 0.968 15.655 3.150 0.41 233476. 0.1692
|
|
55.26 0.5693 0.7140 0.0208 0.0166 0.605 7.622 2.930 450.884 0.861 13.031 2.947 0.41 233999. 0.1444
|
|
57.57 0.5931 0.6836 0.0166 0.0144 0.525 6.615 2.337 391.335 0.747 10.395 2.709 0.41 234541. 0.1185
|
|
59.87 0.6168 0.6324 0.0124 0.0121 0.440 5.550 1.744 328.295 0.627 7.757 2.409 0.41 235101. 0.0911
|
|
62.17 0.6405 0.5440 0.0082 0.0096 0.351 4.429 1.153 262.011 0.500 5.128 1.996 0.41 235677. 0.0613
|
|
64.47 0.6642 0.3768 0.0040 0.0071 0.258 3.257 0.566 192.691 0.368 2.519 1.333 0.42 236263. 0.0287
|
|
66.78 0.6880
|
|
|
|
|
|
|
|
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 0.0945 0.0304 1.913 20.094 19.152 1426.406 2.270 85.190 6.090 0.49 271375. 0.7629
|
|
2.76 0.0237 0.0714 0.0931 0.0309 1.945 20.427 18.866 1450.020 2.308 83.918 5.901 0.49 271553. 0.7337
|
|
5.52 0.0474 0.1384 0.0916 0.0314 1.974 20.739 18.554 1472.233 2.343 82.530 5.716 0.49 271747. 0.7048
|
|
8.28 0.0711 0.2010 0.0899 0.0318 2.002 21.026 18.215 1492.584 2.376 81.021 5.535 0.49 271956. 0.6762
|
|
11.04 0.0948 0.2595 0.0881 0.0322 2.026 21.280 17.847 1510.611 2.404 79.382 5.359 0.49 272183. 0.6479
|
|
13.81 0.1185 0.3139 0.0861 0.0325 2.046 21.494 17.448 1525.816 2.428 77.607 5.187 0.49 272426. 0.6201
|
|
16.57 0.1422 0.3646 0.0840 0.0328 2.062 21.661 17.016 1537.660 2.447 75.688 5.019 0.49 272688. 0.5926
|
|
19.33 0.1659 0.4116 0.0817 0.0329 2.073 21.773 16.551 1545.582 2.460 73.618 4.857 0.49 272967. 0.5656
|
|
22.09 0.1896 0.4551 0.0792 0.0330 2.077 21.821 16.050 1549.010 2.465 71.391 4.700 0.49 273266. 0.5389
|
|
24.85 0.2134 0.4954 0.0766 0.0330 2.075 21.798 15.513 1547.400 2.463 69.002 4.547 0.49 273583. 0.5126
|
|
27.61 0.2371 0.5325 0.0737 0.0328 2.066 21.698 14.940 1540.299 2.451 66.453 4.399 0.49 273920. 0.4867
|
|
30.37 0.2608 0.5667 0.0707 0.0325 2.048 21.517 14.333 1527.397 2.431 63.752 4.256 0.49 274276. 0.4612
|
|
33.13 0.2845 0.5981 0.0676 0.0321 2.023 21.250 13.694 1508.502 2.401 60.910 4.117 0.49 274652. 0.4361
|
|
35.90 0.3082 0.6267 0.0643 0.0316 1.989 20.898 13.025 1483.474 2.361 57.936 3.982 0.49 275048. 0.4114
|
|
38.66 0.3319 0.6526 0.0609 0.0309 1.947 20.457 12.330 1452.202 2.311 54.842 3.851 0.49 275465. 0.3870
|
|
41.42 0.3556 0.6759 0.0573 0.0301 1.897 19.927 11.609 1414.576 2.251 51.637 3.722 0.49 275902. 0.3630
|
|
44.18 0.3793 0.6965 0.0536 0.0292 1.838 19.306 10.866 1370.489 2.181 48.332 3.596 0.49 276360. 0.3393
|
|
46.94 0.4030 0.7144 0.0499 0.0281 1.770 18.593 10.102 1319.830 2.101 44.933 3.472 0.49 276839. 0.3158
|
|
49.70 0.4267 0.7294 0.0460 0.0269 1.693 17.785 9.319 1262.499 2.009 41.449 3.348 0.49 277339. 0.2925
|
|
52.46 0.4504 0.7415 0.0420 0.0255 1.607 16.882 8.518 1198.403 1.907 37.887 3.224 0.49 277860. 0.2693
|
|
55.22 0.4741 0.7501 0.0380 0.0240 1.512 15.883 7.701 1127.475 1.794 34.255 3.098 0.49 278402. 0.2461
|
|
57.98 0.4978 0.7547 0.0339 0.0224 1.408 14.787 6.871 1049.666 1.671 30.561 2.969 0.49 278966. 0.2227
|
|
60.75 0.5215 0.7546 0.0298 0.0206 1.294 13.594 6.028 964.982 1.536 26.813 2.833 0.49 279551. 0.1991
|
|
63.51 0.5452 0.7483 0.0255 0.0186 1.171 12.305 5.176 873.473 1.390 23.021 2.688 0.50 280158. 0.1750
|
|
66.27 0.5689 0.7336 0.0213 0.0165 1.040 10.921 4.316 775.266 1.234 19.197 2.525 0.50 280786. 0.1501
|
|
69.03 0.5926 0.7065 0.0170 0.0143 0.899 9.446 3.452 670.579 1.067 15.353 2.335 0.50 281436. 0.1241
|
|
71.79 0.6163 0.6596 0.0128 0.0119 0.751 7.885 2.587 559.742 0.891 11.505 2.096 0.50 282107. 0.0965
|
|
74.55 0.6401 0.5768 0.0085 0.0094 0.594 6.243 1.724 443.189 0.705 7.670 1.765 0.50 282797. 0.0663
|
|
77.31 0.6638 0.4155 0.0043 0.0068 0.431 4.526 0.868 321.298 0.511 3.863 1.226 0.50 283501. 0.0327
|
|
80.07 0.6875 -0.0164 -0.0001 0.0040 0.252 2.649 -0.019 188.015 0.299 -0.086 -0.047 0.50 283996. 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 0.0958 0.0307 3.068 27.628 26.417 2288.093 3.121 117.501 5.237 0.57 316570. 0.7704
|
|
3.23 0.0238 0.0719 0.0944 0.0312 3.121 28.098 26.030 2327.053 3.175 115.783 5.074 0.57 316779. 0.7409
|
|
6.46 0.0476 0.1392 0.0929 0.0317 3.170 28.541 25.608 2363.692 3.225 113.903 4.914 0.57 317007. 0.7117
|
|
9.69 0.0713 0.2022 0.0912 0.0322 3.215 28.946 25.147 2397.251 3.270 111.852 4.758 0.57 317253. 0.6829
|
|
12.92 0.0951 0.2609 0.0894 0.0326 3.255 29.305 24.645 2426.966 3.311 109.619 4.606 0.57 317519. 0.6544
|
|
16.15 0.1189 0.3157 0.0874 0.0329 3.288 29.607 24.099 2452.020 3.345 107.194 4.458 0.57 317806. 0.6264
|
|
19.39 0.1427 0.3667 0.0852 0.0332 3.314 29.843 23.509 2471.531 3.372 104.567 4.314 0.57 318114. 0.5987
|
|
22.62 0.1664 0.4140 0.0829 0.0333 3.332 30.000 22.870 2484.583 3.389 101.726 4.175 0.57 318443. 0.5715
|
|
25.85 0.1902 0.4578 0.0804 0.0334 3.339 30.069 22.182 2490.228 3.397 98.664 4.040 0.57 318794. 0.5446
|
|
29.08 0.2140 0.4984 0.0777 0.0334 3.336 30.037 21.442 2487.579 3.394 95.375 3.910 0.57 319168. 0.5182
|
|
32.31 0.2378 0.5359 0.0749 0.0332 3.320 29.896 20.652 2475.896 3.378 91.860 3.783 0.57 319564. 0.4921
|
|
35.54 0.2615 0.5704 0.0718 0.0329 3.292 29.639 19.814 2454.670 3.349 88.131 3.661 0.57 319983. 0.4665
|
|
38.77 0.2853 0.6022 0.0686 0.0325 3.250 29.264 18.930 2423.589 3.306 84.201 3.543 0.57 320426. 0.4412
|
|
42.00 0.3091 0.6312 0.0653 0.0320 3.195 28.767 18.005 2382.436 3.250 80.087 3.428 0.57 320892. 0.4163
|
|
45.23 0.3329 0.6576 0.0618 0.0313 3.126 28.146 17.042 2331.043 3.180 75.803 3.316 0.57 321382. 0.3918
|
|
48.46 0.3566 0.6813 0.0582 0.0305 3.043 27.400 16.044 2269.236 3.096 71.364 3.207 0.57 321896. 0.3677
|
|
51.70 0.3804 0.7025 0.0544 0.0295 2.946 26.526 15.014 2196.854 2.997 66.783 3.100 0.57 322435. 0.3438
|
|
54.93 0.4042 0.7211 0.0506 0.0284 2.835 25.523 13.955 2113.730 2.884 62.072 2.994 0.57 322997. 0.3202
|
|
58.16 0.4280 0.7368 0.0467 0.0271 2.708 24.387 12.869 2019.705 2.755 57.240 2.890 0.57 323585. 0.2967
|
|
61.39 0.4517 0.7496 0.0426 0.0257 2.568 23.119 11.758 1914.634 2.612 52.300 2.785 0.58 324197. 0.2734
|
|
64.62 0.4755 0.7591 0.0385 0.0241 2.412 21.715 10.625 1798.404 2.453 47.260 2.680 0.58 324834. 0.2500
|
|
67.85 0.4993 0.7648 0.0343 0.0224 2.241 20.176 9.472 1670.953 2.279 42.134 2.571 0.58 325497. 0.2265
|
|
71.08 0.5231 0.7659 0.0301 0.0206 2.055 18.502 8.303 1532.280 2.090 36.931 2.458 0.58 326184. 0.2027
|
|
74.31 0.5469 0.7609 0.0258 0.0186 1.854 16.693 7.119 1382.481 1.886 31.667 2.336 0.58 326897. 0.1784
|
|
77.54 0.5706 0.7478 0.0215 0.0164 1.638 14.752 5.925 1221.772 1.667 26.356 2.200 0.58 327634. 0.1533
|
|
80.77 0.5944 0.7225 0.0171 0.0141 1.409 12.685 4.725 1050.516 1.433 21.018 2.040 0.58 328397. 0.1269
|
|
84.00 0.6182 0.6772 0.0128 0.0117 1.166 10.496 3.524 869.268 1.186 15.675 1.839 0.58 329184. 0.0988
|
|
87.24 0.6420 0.5947 0.0084 0.0091 0.910 8.196 2.327 678.747 0.926 10.350 1.555 0.58 329994. 0.0679
|
|
90.47 0.6657 0.4269 0.0041 0.0064 0.643 5.790 1.138 479.540 0.654 5.062 1.076 0.58 330819. 0.0329
|
|
93.70 0.6895
|
|
|
|
|
|
|
|
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 0.0973 0.0312 4.660 36.710 35.055 3474.602 4.147 155.923 4.576 0.65 361746. 0.7755
|
|
3.73 0.0240 0.0724 0.0959 0.0318 4.741 37.355 34.555 3535.588 4.220 153.699 4.433 0.65 361988. 0.7459
|
|
7.45 0.0480 0.1402 0.0944 0.0323 4.818 37.961 34.004 3592.973 4.289 151.252 4.293 0.65 362252. 0.7165
|
|
11.18 0.0720 0.2037 0.0927 0.0328 4.889 38.516 33.401 3645.524 4.352 148.568 4.156 0.65 362538. 0.6874
|
|
14.91 0.0960 0.2628 0.0909 0.0332 4.951 39.007 32.742 3692.006 4.407 145.634 4.022 0.65 362847. 0.6588
|
|
18.63 0.1200 0.3180 0.0889 0.0335 5.003 39.420 32.022 3731.101 4.454 142.435 3.893 0.65 363181. 0.6305
|
|
22.36 0.1440 0.3692 0.0867 0.0338 5.044 39.740 31.240 3761.407 4.490 138.956 3.767 0.65 363539. 0.6027
|
|
26.08 0.1680 0.4169 0.0844 0.0340 5.071 39.952 30.392 3781.452 4.514 135.184 3.645 0.65 363922. 0.5752
|
|
29.81 0.1919 0.4610 0.0818 0.0341 5.082 40.040 29.475 3789.750 4.524 131.105 3.528 0.65 364331. 0.5482
|
|
33.54 0.2159 0.5019 0.0791 0.0340 5.076 39.989 28.487 3784.893 4.518 126.712 3.414 0.65 364766. 0.5215
|
|
37.26 0.2399 0.5397 0.0762 0.0339 5.050 39.786 27.430 3765.733 4.495 122.009 3.304 0.65 365228. 0.4953
|
|
40.99 0.2639 0.5746 0.0730 0.0335 5.004 39.424 26.306 3731.488 4.454 117.009 3.198 0.65 365717. 0.4694
|
|
44.72 0.2879 0.6067 0.0697 0.0331 4.937 38.898 25.120 3681.698 4.395 111.734 3.095 0.65 366232. 0.4440
|
|
48.44 0.3119 0.6360 0.0663 0.0325 4.849 38.205 23.877 3616.052 4.316 106.205 2.995 0.65 366776. 0.4189
|
|
52.17 0.3359 0.6628 0.0627 0.0318 4.740 37.341 22.582 3534.311 4.219 100.445 2.898 0.65 367347. 0.3942
|
|
55.89 0.3599 0.6870 0.0590 0.0309 4.608 36.305 21.239 3436.243 4.102 94.473 2.804 0.65 367945. 0.3698
|
|
59.62 0.3839 0.7086 0.0551 0.0299 4.454 35.094 19.853 3321.609 3.965 88.307 2.711 0.66 368572. 0.3457
|
|
63.35 0.4079 0.7276 0.0512 0.0287 4.278 33.705 18.427 3190.174 3.808 81.962 2.620 0.66 369228. 0.3219
|
|
67.07 0.4319 0.7438 0.0471 0.0273 4.079 32.136 16.964 3041.698 3.631 75.454 2.530 0.66 369912. 0.2982
|
|
70.80 0.4559 0.7571 0.0429 0.0259 3.857 30.386 15.467 2875.983 3.433 68.797 2.439 0.66 370624. 0.2746
|
|
74.53 0.4799 0.7671 0.0387 0.0242 3.611 28.451 13.940 2692.864 3.214 62.007 2.348 0.66 371366. 0.2509
|
|
78.25 0.5039 0.7734 0.0344 0.0224 3.342 26.331 12.387 2492.254 2.975 55.097 2.254 0.66 372137. 0.2271
|
|
81.98 0.5279 0.7749 0.0300 0.0204 3.050 24.027 10.811 2274.186 2.715 48.085 2.156 0.66 372937. 0.2029
|
|
85.70 0.5519 0.7703 0.0256 0.0183 2.734 21.541 9.215 2038.835 2.434 40.990 2.050 0.66 373766. 0.1781
|
|
89.43 0.5758 0.7571 0.0211 0.0161 2.396 18.876 7.607 1786.581 2.133 33.834 1.931 0.66 374624. 0.1524
|
|
93.16 0.5998 0.7309 0.0166 0.0136 2.036 16.039 5.990 1518.056 1.812 26.644 1.790 0.66 375511. 0.1254
|
|
96.88 0.6238 0.6825 0.0121 0.0111 1.655 13.040 4.373 1234.197 1.473 19.450 1.607 0.66 376426. 0.0962
|
|
100.61 0.6478 0.5903 0.0077 0.0084 1.255 9.891 2.762 936.175 1.117 12.286 1.338 0.66 377367. 0.0637
|
|
104.34 0.6718 0.3860 0.0032 0.0056 0.838 6.598 1.162 624.533 0.745 5.168 0.844 0.67 378316. 0.0260
|
|
108.06 0.6958
|
|
|
|
|
|
|
|
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 0.0991 0.0325 6.904 48.346 45.197 5147.955 5.462 201.036 3.982 0.73 406897. 0.7663
|
|
4.19 0.0240 0.0710 0.0978 0.0330 7.014 49.117 44.585 5230.049 5.549 198.316 3.867 0.73 407170. 0.7390
|
|
8.37 0.0479 0.1378 0.0963 0.0335 7.117 49.839 43.908 5306.854 5.631 195.301 3.753 0.73 407467. 0.7117
|
|
12.56 0.0719 0.2005 0.0947 0.0339 7.210 50.495 43.160 5376.712 5.705 191.974 3.641 0.73 407790. 0.6846
|
|
16.75 0.0959 0.2593 0.0929 0.0343 7.292 51.070 42.337 5437.961 5.770 188.315 3.531 0.73 408140. 0.6577
|
|
20.94 0.1198 0.3143 0.0909 0.0347 7.361 51.548 41.436 5488.836 5.824 184.305 3.424 0.73 408516. 0.6309
|
|
25.12 0.1438 0.3656 0.0887 0.0349 7.412 51.910 40.451 5527.414 5.865 179.924 3.319 0.73 408921. 0.6043
|
|
29.31 0.1678 0.4134 0.0864 0.0351 7.445 52.138 39.378 5551.658 5.890 175.155 3.217 0.73 409354. 0.5779
|
|
33.50 0.1917 0.4579 0.0838 0.0351 7.455 52.211 38.215 5559.441 5.899 169.980 3.118 0.73 409817. 0.5517
|
|
37.69 0.2157 0.4991 0.0811 0.0350 7.441 52.110 36.958 5548.718 5.887 164.389 3.021 0.73 410309. 0.5257
|
|
41.87 0.2397 0.5373 0.0781 0.0348 7.399 51.819 35.608 5517.714 5.854 158.386 2.927 0.73 410831. 0.4999
|
|
46.06 0.2636 0.5727 0.0750 0.0345 7.329 51.326 34.170 5465.179 5.799 151.988 2.836 0.73 411383. 0.4745
|
|
50.25 0.2876 0.6052 0.0716 0.0340 7.229 50.623 32.649 5390.317 5.719 145.222 2.747 0.73 411965. 0.4493
|
|
54.44 0.3116 0.6351 0.0681 0.0334 7.097 49.705 31.052 5292.590 5.616 138.118 2.661 0.74 412579. 0.4244
|
|
58.62 0.3355 0.6624 0.0645 0.0327 6.935 48.568 29.385 5171.555 5.487 130.705 2.577 0.74 413223. 0.3999
|
|
62.81 0.3595 0.6871 0.0607 0.0317 6.741 47.209 27.655 5026.795 5.334 123.009 2.495 0.74 413899. 0.3756
|
|
67.00 0.3835 0.7094 0.0567 0.0307 6.515 45.622 25.867 4857.875 5.154 115.055 2.415 0.74 414606. 0.3516
|
|
71.19 0.4074 0.7291 0.0527 0.0295 6.255 43.805 24.025 4664.399 4.949 106.865 2.336 0.74 415345. 0.3278
|
|
75.37 0.4314 0.7462 0.0486 0.0281 5.962 41.754 22.135 4446.004 4.717 98.457 2.258 0.74 416115. 0.3041
|
|
79.56 0.4554 0.7605 0.0443 0.0265 5.636 39.466 20.201 4202.409 4.459 89.853 2.180 0.74 416918. 0.2805
|
|
83.75 0.4793 0.7716 0.0400 0.0248 5.275 36.940 18.226 3933.391 4.173 81.069 2.102 0.74 417754. 0.2568
|
|
87.94 0.5033 0.7792 0.0356 0.0230 4.880 34.174 16.215 3638.829 3.861 72.126 2.021 0.74 418621. 0.2330
|
|
92.12 0.5273 0.7823 0.0311 0.0210 4.450 31.168 14.174 3318.737 3.521 63.045 1.937 0.74 419521. 0.2087
|
|
96.31 0.5512 0.7798 0.0266 0.0188 3.987 27.924 12.107 2973.389 3.155 53.850 1.847 0.74 420454. 0.1839
|
|
100.50 0.5752 0.7691 0.0220 0.0164 3.491 24.449 10.020 2603.391 2.762 44.570 1.746 0.74 421419. 0.1582
|
|
104.69 0.5992 0.7463 0.0174 0.0140 2.963 20.753 7.922 2209.761 2.345 35.238 1.626 0.75 422416. 0.1310
|
|
108.87 0.6232 0.7025 0.0128 0.0113 2.406 16.848 5.822 1794.029 1.904 25.895 1.472 0.75 423445. 0.1016
|
|
113.06 0.6471 0.6171 0.0082 0.0086 1.821 12.755 3.728 1358.211 1.441 16.584 1.245 0.75 424503. 0.0688
|
|
117.25 0.6711 0.4250 0.0036 0.0057 1.212 8.487 1.647 903.721 0.959 7.327 0.827 0.75 425573. 0.0304
|
|
121.44 0.6951
|
|
|
|
|
|
|
|
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 0.1012 0.0365 10.627 66.979 56.962 7924.369 7.567 253.367 3.260 0.81 452016. 0.7043
|
|
4.62 0.0238 0.0645 0.1000 0.0369 10.742 67.705 56.256 8010.308 7.649 250.229 3.185 0.81 452316. 0.6839
|
|
9.24 0.0476 0.1260 0.0986 0.0372 10.843 68.344 55.467 8085.867 7.721 246.716 3.111 0.81 452644. 0.6632
|
|
13.86 0.0714 0.1846 0.0970 0.0375 10.928 68.877 54.587 8148.957 7.782 242.803 3.038 0.81 453001. 0.6425
|
|
18.48 0.0952 0.2403 0.0953 0.0377 10.993 69.289 53.611 8197.669 7.828 238.462 2.966 0.81 453387. 0.6217
|
|
23.10 0.1190 0.2932 0.0933 0.0379 11.037 69.563 52.533 8230.087 7.859 233.667 2.895 0.81 453804. 0.6006
|
|
27.72 0.1428 0.3433 0.0912 0.0379 11.056 69.682 51.347 8244.212 7.873 228.393 2.825 0.81 454252. 0.5794
|
|
32.34 0.1666 0.3906 0.0889 0.0379 11.047 69.629 50.048 8237.935 7.867 222.615 2.756 0.81 454732. 0.5580
|
|
36.96 0.1904 0.4353 0.0864 0.0378 11.009 69.385 48.631 8209.090 7.839 216.313 2.687 0.81 455245. 0.5363
|
|
41.58 0.2142 0.4774 0.0837 0.0375 10.937 68.932 47.093 8155.517 7.788 209.471 2.619 0.82 455790. 0.5145
|
|
46.20 0.2380 0.5168 0.0807 0.0372 10.829 68.255 45.435 8075.364 7.711 202.093 2.552 0.82 456368. 0.4923
|
|
50.81 0.2618 0.5537 0.0776 0.0367 10.684 67.342 43.659 7967.388 7.608 194.197 2.485 0.82 456979. 0.4701
|
|
55.43 0.2856 0.5880 0.0742 0.0360 10.501 66.188 41.776 7830.839 7.478 185.818 2.420 0.82 457624. 0.4476
|
|
60.05 0.3094 0.6199 0.0707 0.0353 10.279 64.788 39.792 7665.241 7.320 176.993 2.355 0.82 458302. 0.4251
|
|
64.67 0.3331 0.6493 0.0670 0.0344 10.018 63.140 37.716 7470.198 7.134 167.760 2.290 0.82 459015. 0.4025
|
|
69.29 0.3569 0.6762 0.0632 0.0333 9.716 61.239 35.556 7245.287 6.919 158.153 2.226 0.82 459761. 0.3799
|
|
73.91 0.3807 0.7006 0.0592 0.0322 9.374 59.081 33.320 6990.008 6.675 148.205 2.162 0.82 460542. 0.3572
|
|
78.53 0.4045 0.7224 0.0551 0.0309 8.990 56.662 31.013 6703.736 6.402 137.944 2.098 0.82 461357. 0.3345
|
|
83.15 0.4283 0.7416 0.0509 0.0294 8.563 53.974 28.642 6385.780 6.098 127.397 2.034 0.82 462207. 0.3116
|
|
87.77 0.4521 0.7580 0.0466 0.0278 8.094 51.012 26.212 6035.377 5.763 116.589 1.970 0.82 463092. 0.2887
|
|
92.39 0.4759 0.7713 0.0422 0.0260 7.579 47.771 23.729 5651.852 5.397 105.545 1.904 0.82 464013. 0.2655
|
|
97.01 0.4997 0.7809 0.0377 0.0241 7.022 44.257 21.197 5236.067 5.000 94.286 1.836 0.82 464968. 0.2420
|
|
101.63 0.5235 0.7861 0.0331 0.0220 6.421 40.469 18.624 4787.941 4.572 82.841 1.764 0.82 465959. 0.2179
|
|
106.25 0.5473 0.7853 0.0285 0.0198 5.778 36.417 16.015 4308.581 4.114 71.236 1.686 0.83 466985. 0.1931
|
|
110.87 0.5711 0.7765 0.0238 0.0175 5.093 32.101 13.378 3797.973 3.627 59.506 1.598 0.83 468046. 0.1673
|
|
115.49 0.5949 0.7556 0.0191 0.0150 4.370 27.541 10.722 3258.393 3.112 47.691 1.492 0.83 469142. 0.1399
|
|
120.11 0.6187 0.7145 0.0143 0.0124 3.612 22.764 8.057 2693.277 2.572 35.838 1.357 0.83 470273. 0.1102
|
|
124.73 0.6425 0.6351 0.0096 0.0097 2.826 17.810 5.396 2107.166 2.012 24.001 1.161 0.83 471436. 0.0772
|
|
129.35 0.6663 0.4698 0.0049 0.0069 2.017 12.713 2.748 1504.062 1.436 12.221 0.829 0.83 472620. 0.0393
|
|
133.97 0.6901 -0.0124 -0.0001 0.0038 1.121 7.063 -0.039 835.644 0.798 -0.173 -0.021 0.83 473331. 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 0.1025 0.0443 17.188 98.482 69.774 12816.737 11.126 310.356 2.469 0.89 497150. 0.5904
|
|
5.11 0.0239 0.0543 0.1014 0.0447 17.317 99.225 69.024 12913.494 11.210 307.017 2.424 0.89 497476. 0.5765
|
|
10.22 0.0479 0.1067 0.1001 0.0449 17.421 99.819 68.173 12990.759 11.278 303.232 2.380 0.89 497834. 0.5625
|
|
15.34 0.0718 0.1571 0.0987 0.0451 17.492 100.229 67.212 13044.085 11.324 298.959 2.337 0.89 498224. 0.5484
|
|
20.45 0.0958 0.2058 0.0971 0.0452 17.526 100.421 66.131 13069.107 11.346 294.150 2.295 0.89 498649. 0.5342
|
|
25.56 0.1197 0.2526 0.0953 0.0452 17.516 100.364 64.919 13061.678 11.339 288.758 2.254 0.90 499108. 0.5199
|
|
30.67 0.1436 0.2978 0.0933 0.0450 17.457 100.029 63.565 13018.024 11.301 282.737 2.215 0.90 499603. 0.5054
|
|
35.79 0.1676 0.3414 0.0911 0.0447 17.346 99.391 62.061 12935.031 11.229 276.046 2.176 0.90 500135. 0.4907
|
|
40.90 0.1915 0.3834 0.0887 0.0443 17.179 98.432 60.398 12810.289 11.121 268.652 2.139 0.90 500705. 0.4757
|
|
46.01 0.2155 0.4239 0.0860 0.0437 16.953 97.140 58.572 12642.083 10.975 260.530 2.101 0.90 501311. 0.4603
|
|
51.12 0.2394 0.4628 0.0831 0.0430 16.668 95.507 56.582 12429.518 10.790 251.678 2.065 0.90 501956. 0.4446
|
|
56.24 0.2634 0.5000 0.0799 0.0421 16.324 93.534 54.433 12172.761 10.567 242.120 2.028 0.90 502639. 0.4283
|
|
61.35 0.2873 0.5357 0.0766 0.0411 15.922 91.230 52.135 11872.947 10.307 231.899 1.992 0.90 503359. 0.4116
|
|
66.46 0.3112 0.5696 0.0730 0.0399 15.464 88.608 49.700 11531.739 10.011 221.067 1.955 0.90 504118. 0.3945
|
|
71.57 0.3352 0.6017 0.0692 0.0386 14.954 85.682 47.140 11150.915 9.680 209.679 1.917 0.90 504915. 0.3768
|
|
76.69 0.3591 0.6318 0.0653 0.0371 14.392 82.462 44.465 10731.848 9.317 197.781 1.879 0.90 505750. 0.3587
|
|
81.80 0.3831 0.6599 0.0612 0.0355 13.779 78.954 41.686 10275.368 8.920 185.418 1.840 0.90 506623. 0.3400
|
|
86.91 0.4070 0.6857 0.0570 0.0338 13.118 75.164 38.811 9782.082 8.492 172.632 1.800 0.90 507535. 0.3209
|
|
92.02 0.4309 0.7090 0.0526 0.0320 12.407 71.090 35.849 9251.848 8.032 159.458 1.758 0.90 508486. 0.3012
|
|
97.14 0.4549 0.7297 0.0482 0.0300 11.645 66.727 32.808 8684.026 7.539 145.929 1.714 0.90 509475. 0.2809
|
|
102.25 0.4788 0.7474 0.0436 0.0279 10.832 62.067 29.694 8077.642 7.012 132.078 1.667 0.90 510503. 0.2601
|
|
107.36 0.5028 0.7616 0.0389 0.0257 9.966 57.106 26.514 7431.924 6.452 117.935 1.618 0.91 511570. 0.2385
|
|
112.47 0.5267 0.7701 0.0342 0.0234 9.065 51.943 23.276 6760.046 5.869 103.532 1.562 0.91 512676. 0.2157
|
|
117.59 0.5507 0.7674 0.0293 0.0211 8.165 46.783 19.984 6088.493 5.286 88.887 1.489 0.91 513821. 0.1905
|
|
122.70 0.5746 0.7482 0.0244 0.0188 7.279 41.709 16.646 5428.142 4.712 74.042 1.391 0.91 515005. 0.1624
|
|
127.81 0.5985 0.7110 0.0195 0.0164 6.367 36.483 13.283 4747.995 4.122 59.081 1.269 0.91 516227. 0.1324
|
|
132.92 0.6225 0.6459 0.0145 0.0140 5.437 31.151 9.908 4054.100 3.519 44.069 1.108 0.91 517487. 0.0999
|
|
138.04 0.6464 0.5348 0.0096 0.0116 4.499 25.779 6.537 3354.992 2.913 29.076 0.884 0.91 518783. 0.0647
|
|
143.15 0.6704 0.3408 0.0047 0.0092 3.565 20.425 3.183 2658.178 2.308 14.156 0.543 0.91 520101. 0.0277
|
|
148.26 0.6943
|
|
|
|
|
|
|