612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
14x8 (14x8.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 0.1047 0.0497 0.002 0.136 0.128 1.605 0.015 0.570 36.214 0.06 25281. 0.5433
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0.34 0.0254 0.0522 0.1031 0.0502 0.002 0.137 0.126 1.619 0.015 0.561 35.349 0.06 25300. 0.5263
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0.67 0.0508 0.1019 0.1014 0.0506 0.002 0.138 0.124 1.632 0.016 0.552 34.477 0.06 25320. 0.5090
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1.01 0.0763 0.1490 0.0995 0.0509 0.002 0.139 0.122 1.644 0.016 0.542 33.603 0.06 25342. 0.4916
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1.35 0.1017 0.1934 0.0975 0.0513 0.002 0.140 0.119 1.654 0.016 0.531 32.728 0.06 25366. 0.4739
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1.69 0.1271 0.2353 0.0954 0.0515 0.002 0.141 0.117 1.663 0.016 0.519 31.853 0.06 25392. 0.4562
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2.02 0.1525 0.2746 0.0931 0.0517 0.002 0.141 0.114 1.668 0.016 0.507 30.978 0.06 25420. 0.4383
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2.36 0.1780 0.3114 0.0906 0.0518 0.002 0.141 0.111 1.671 0.016 0.493 30.106 0.06 25450. 0.4203
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2.70 0.2034 0.3456 0.0880 0.0518 0.002 0.141 0.108 1.671 0.016 0.479 29.234 0.06 25481. 0.4021
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3.03 0.2288 0.3772 0.0852 0.0517 0.002 0.141 0.104 1.668 0.016 0.464 28.364 0.06 25515. 0.3839
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3.37 0.2542 0.4063 0.0822 0.0514 0.002 0.140 0.101 1.660 0.016 0.448 27.495 0.06 25551. 0.3656
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3.71 0.2796 0.4327 0.0790 0.0511 0.002 0.139 0.097 1.648 0.016 0.430 26.624 0.06 25589. 0.3471
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4.04 0.3051 0.4566 0.0757 0.0506 0.002 0.138 0.093 1.632 0.016 0.412 25.749 0.06 25629. 0.3285
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4.38 0.3305 0.4777 0.0721 0.0499 0.002 0.136 0.088 1.610 0.015 0.393 24.869 0.06 25672. 0.3097
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4.72 0.3559 0.4960 0.0684 0.0491 0.002 0.134 0.084 1.583 0.015 0.372 23.980 0.06 25716. 0.2908
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5.06 0.3813 0.5115 0.0645 0.0481 0.002 0.131 0.079 1.552 0.015 0.351 23.077 0.06 25763. 0.2718
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5.39 0.4068 0.5238 0.0604 0.0469 0.002 0.128 0.074 1.515 0.014 0.329 22.156 0.06 25812. 0.2526
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5.73 0.4322 0.5328 0.0563 0.0456 0.002 0.125 0.069 1.473 0.014 0.306 21.211 0.06 25864. 0.2333
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6.07 0.4576 0.5381 0.0520 0.0442 0.002 0.121 0.064 1.426 0.014 0.283 20.233 0.06 25917. 0.2139
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6.40 0.4830 0.5394 0.0476 0.0426 0.002 0.116 0.058 1.375 0.013 0.259 19.213 0.06 25973. 0.1944
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6.74 0.5084 0.5361 0.0431 0.0409 0.002 0.111 0.053 1.319 0.013 0.235 18.140 0.06 26031. 0.1746
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7.08 0.5339 0.5274 0.0385 0.0390 0.002 0.106 0.047 1.258 0.012 0.210 16.997 0.06 26091. 0.1547
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7.41 0.5593 0.5124 0.0338 0.0369 0.002 0.101 0.041 1.192 0.011 0.184 15.763 0.06 26154. 0.1345
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7.75 0.5847 0.4898 0.0291 0.0348 0.002 0.095 0.036 1.122 0.011 0.159 14.414 0.06 26219. 0.1141
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8.09 0.6101 0.4578 0.0243 0.0324 0.001 0.088 0.030 1.047 0.010 0.133 12.910 0.06 26286. 0.0934
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8.43 0.6356 0.4137 0.0195 0.0300 0.001 0.082 0.024 0.967 0.009 0.106 11.199 0.06 26356. 0.0725
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8.76 0.6610 0.3537 0.0146 0.0274 0.001 0.075 0.018 0.883 0.008 0.080 9.208 0.06 26428. 0.0517
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9.10 0.6864 0.2721 0.0098 0.0246 0.001 0.067 0.012 0.795 0.008 0.053 6.822 0.06 26502. 0.0313
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9.44 0.7118 0.1597 0.0049 0.0218 0.001 0.059 0.006 0.702 0.007 0.027 3.861 0.06 26578. 0.0125
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9.77 0.7372 0.0008 0.0000 0.0188 0.001 0.051 0.000 0.606 0.006 0.000 0.019 0.06 26656. 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 0.1052 0.0440 0.015 0.480 0.515 11.356 0.054 2.291 20.570 0.11 50561. 0.6187
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0.68 0.0256 0.0596 0.1036 0.0445 0.015 0.485 0.507 11.487 0.055 2.256 20.029 0.11 50599. 0.5979
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1.36 0.0512 0.1160 0.1019 0.0450 0.016 0.491 0.499 11.609 0.055 2.219 19.490 0.11 50640. 0.5769
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2.04 0.0768 0.1693 0.1000 0.0454 0.016 0.495 0.490 11.721 0.056 2.179 18.953 0.11 50685. 0.5559
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2.72 0.1024 0.2193 0.0980 0.0458 0.016 0.499 0.480 11.819 0.056 2.135 18.421 0.11 50734. 0.5349
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3.39 0.1280 0.2663 0.0959 0.0461 0.016 0.503 0.469 11.901 0.057 2.088 17.893 0.11 50786. 0.5139
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4.07 0.1536 0.3103 0.0936 0.0463 0.016 0.506 0.458 11.963 0.057 2.038 17.372 0.11 50842. 0.4928
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4.75 0.1792 0.3512 0.0911 0.0465 0.016 0.507 0.446 12.004 0.057 1.984 16.856 0.11 50902. 0.4719
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5.43 0.2049 0.3893 0.0885 0.0465 0.016 0.508 0.433 12.018 0.057 1.927 16.347 0.11 50966. 0.4509
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6.11 0.2305 0.4245 0.0856 0.0465 0.016 0.507 0.419 12.004 0.057 1.865 15.844 0.11 51035. 0.4300
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6.79 0.2561 0.4568 0.0826 0.0463 0.016 0.505 0.405 11.957 0.057 1.800 15.348 0.11 51107. 0.4092
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7.47 0.2817 0.4864 0.0794 0.0460 0.016 0.502 0.389 11.874 0.057 1.730 14.856 0.11 51184. 0.3883
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8.15 0.3073 0.5133 0.0760 0.0455 0.016 0.497 0.372 11.752 0.056 1.656 14.369 0.11 51266. 0.3675
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8.83 0.3329 0.5373 0.0724 0.0449 0.016 0.490 0.355 11.587 0.055 1.578 13.885 0.11 51352. 0.3466
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9.51 0.3585 0.5585 0.0687 0.0441 0.015 0.481 0.336 11.379 0.054 1.496 13.403 0.11 51442. 0.3257
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10.18 0.3841 0.5769 0.0647 0.0431 0.015 0.470 0.317 11.128 0.053 1.410 12.921 0.11 51537. 0.3049
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10.86 0.4097 0.5922 0.0607 0.0420 0.015 0.458 0.297 10.834 0.052 1.321 12.435 0.11 51636. 0.2840
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11.54 0.4353 0.6044 0.0564 0.0407 0.014 0.444 0.276 10.497 0.050 1.229 11.943 0.11 51740. 0.2632
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12.22 0.4609 0.6130 0.0521 0.0392 0.014 0.428 0.255 10.118 0.048 1.135 11.441 0.11 51849. 0.2423
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12.90 0.4865 0.6178 0.0477 0.0376 0.013 0.410 0.234 9.697 0.046 1.039 10.923 0.11 51962. 0.2212
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13.58 0.5121 0.6181 0.0432 0.0358 0.012 0.390 0.211 9.233 0.044 0.940 10.383 0.11 52079. 0.2001
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14.26 0.5377 0.6133 0.0386 0.0338 0.012 0.369 0.189 8.727 0.042 0.840 9.811 0.11 52202. 0.1787
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14.94 0.5634 0.6023 0.0339 0.0317 0.011 0.346 0.166 8.180 0.039 0.738 9.197 0.11 52329. 0.1570
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15.62 0.5890 0.5834 0.0291 0.0294 0.010 0.321 0.143 7.590 0.036 0.634 8.522 0.11 52460. 0.1349
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16.30 0.6146 0.5545 0.0243 0.0270 0.009 0.294 0.119 6.959 0.033 0.530 7.762 0.11 52597. 0.1123
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16.97 0.6402 0.5120 0.0195 0.0244 0.008 0.266 0.095 6.288 0.030 0.424 6.881 0.11 52738. 0.0891
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17.65 0.6658 0.4503 0.0146 0.0216 0.007 0.236 0.072 5.578 0.027 0.318 5.819 0.11 52883. 0.0652
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18.33 0.6914 0.3598 0.0097 0.0187 0.006 0.204 0.048 4.831 0.023 0.212 4.477 0.11 53033. 0.0410
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19.01 0.7170 0.2226 0.0049 0.0157 0.005 0.171 0.024 4.048 0.019 0.106 2.671 0.11 53188. 0.0173
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19.69 0.7426 0.0012 0.0000 0.0125 0.004 0.137 0.000 3.232 0.015 0.000 0.013 0.11 53345. 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 0.1055 0.0417 0.049 1.023 1.163 36.307 0.116 5.172 14.526 0.17 75840. 0.6565
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1.02 0.0257 0.0633 0.1040 0.0422 0.049 1.036 1.145 36.772 0.117 5.095 14.128 0.17 75897. 0.6337
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2.04 0.0514 0.1230 0.1022 0.0427 0.050 1.048 1.126 37.209 0.118 5.011 13.732 0.17 75959. 0.6108
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3.06 0.0770 0.1792 0.1004 0.0432 0.050 1.060 1.106 37.611 0.120 4.920 13.339 0.17 76027. 0.5880
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4.09 0.1027 0.2320 0.0984 0.0436 0.051 1.070 1.084 37.967 0.121 4.822 12.951 0.17 76100. 0.5652
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5.11 0.1284 0.2814 0.0962 0.0439 0.051 1.078 1.060 38.268 0.122 4.717 12.569 0.17 76179. 0.5424
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6.13 0.1541 0.3276 0.0939 0.0442 0.052 1.085 1.035 38.503 0.123 4.603 12.192 0.17 76263. 0.5198
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7.15 0.1798 0.3706 0.0915 0.0444 0.052 1.089 1.008 38.662 0.123 4.482 11.822 0.17 76354. 0.4974
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8.17 0.2055 0.4105 0.0888 0.0445 0.052 1.091 0.978 38.733 0.123 4.352 11.458 0.17 76451. 0.4750
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9.19 0.2311 0.4473 0.0860 0.0444 0.052 1.090 0.947 38.705 0.123 4.213 11.100 0.17 76554. 0.4528
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10.21 0.2568 0.4813 0.0829 0.0443 0.052 1.087 0.914 38.565 0.123 4.065 10.749 0.17 76664. 0.4307
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11.24 0.2825 0.5124 0.0797 0.0440 0.051 1.079 0.878 38.301 0.122 3.908 10.403 0.17 76780. 0.4087
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12.26 0.3082 0.5408 0.0763 0.0435 0.051 1.068 0.841 37.900 0.121 3.740 10.063 0.17 76903. 0.3868
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13.28 0.3339 0.5663 0.0727 0.0429 0.050 1.052 0.801 37.355 0.119 3.564 9.728 0.17 77032. 0.3649
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14.30 0.3595 0.5890 0.0689 0.0421 0.049 1.033 0.759 36.660 0.117 3.378 9.396 0.17 77168. 0.3432
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15.32 0.3852 0.6089 0.0650 0.0411 0.048 1.009 0.716 35.814 0.114 3.184 9.066 0.17 77311. 0.3215
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16.34 0.4109 0.6259 0.0609 0.0400 0.047 0.981 0.671 34.818 0.111 2.983 8.737 0.17 77461. 0.2999
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17.36 0.4366 0.6399 0.0566 0.0386 0.045 0.949 0.624 33.674 0.107 2.776 8.406 0.17 77618. 0.2783
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18.39 0.4623 0.6505 0.0523 0.0372 0.043 0.912 0.576 32.381 0.103 2.563 8.070 0.17 77781. 0.2567
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19.41 0.4880 0.6574 0.0478 0.0355 0.041 0.872 0.527 30.940 0.098 2.344 7.727 0.17 77952. 0.2351
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20.43 0.5136 0.6602 0.0433 0.0337 0.039 0.827 0.477 29.351 0.093 2.122 7.371 0.17 78129. 0.2134
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21.45 0.5393 0.6580 0.0387 0.0317 0.037 0.778 0.426 27.613 0.088 1.895 6.997 0.17 78314. 0.1914
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22.47 0.5650 0.6499 0.0340 0.0295 0.035 0.725 0.374 25.728 0.082 1.664 6.597 0.17 78505. 0.1691
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23.49 0.5907 0.6342 0.0292 0.0272 0.032 0.668 0.322 23.696 0.075 1.431 6.158 0.17 78704. 0.1464
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24.51 0.6164 0.6086 0.0244 0.0247 0.029 0.606 0.269 21.518 0.068 1.195 5.663 0.17 78909. 0.1230
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25.54 0.6420 0.5691 0.0195 0.0220 0.026 0.541 0.215 19.199 0.061 0.957 5.083 0.17 79122. 0.0988
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26.56 0.6677 0.5092 0.0147 0.0192 0.022 0.472 0.161 16.742 0.053 0.718 4.374 0.17 79342. 0.0737
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27.58 0.6934 0.4169 0.0098 0.0162 0.019 0.399 0.108 14.155 0.045 0.479 3.449 0.17 79568. 0.0474
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28.60 0.7191 0.2680 0.0049 0.0131 0.015 0.322 0.054 11.445 0.036 0.240 2.137 0.17 79801. 0.0208
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29.62 0.7448 0.0031 0.0000 0.0099 0.012 0.243 0.000 8.616 0.027 0.002 0.024 0.17 80036. 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 0.1059 0.0404 0.112 1.764 2.075 83.504 0.199 9.228 11.269 0.22 101117. 0.6803
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1.36 0.0257 0.0655 0.1043 0.0410 0.114 1.789 2.044 84.642 0.202 9.091 10.952 0.22 101194. 0.6562
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2.73 0.0515 0.1273 0.1026 0.0415 0.115 1.811 2.010 85.716 0.205 8.942 10.637 0.22 101277. 0.6321
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4.09 0.0772 0.1854 0.1008 0.0420 0.116 1.832 1.974 86.704 0.207 8.780 10.326 0.22 101367. 0.6081
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5.46 0.1029 0.2398 0.0988 0.0424 0.117 1.851 1.935 87.584 0.209 8.606 10.020 0.22 101465. 0.5841
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6.82 0.1287 0.2907 0.0966 0.0428 0.118 1.867 1.893 88.332 0.211 8.418 9.718 0.22 101571. 0.5604
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8.19 0.1544 0.3383 0.0943 0.0431 0.119 1.879 1.847 88.924 0.212 8.217 9.422 0.22 101684. 0.5367
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9.55 0.1802 0.3825 0.0918 0.0432 0.120 1.888 1.799 89.332 0.213 8.000 9.132 0.22 101805. 0.5133
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10.92 0.2059 0.4235 0.0892 0.0433 0.120 1.892 1.747 89.530 0.214 7.769 8.848 0.22 101935. 0.4901
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12.28 0.2316 0.4615 0.0863 0.0433 0.120 1.891 1.691 89.488 0.214 7.521 8.570 0.22 102073. 0.4670
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13.65 0.2574 0.4965 0.0833 0.0432 0.120 1.884 1.631 89.178 0.213 7.256 8.297 0.22 102220. 0.4442
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15.01 0.2831 0.5285 0.0801 0.0429 0.119 1.871 1.568 88.568 0.211 6.975 8.030 0.22 102375. 0.4215
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16.38 0.3088 0.5578 0.0766 0.0424 0.118 1.852 1.501 87.630 0.209 6.676 7.769 0.22 102540. 0.3989
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17.74 0.3346 0.5843 0.0730 0.0418 0.116 1.824 1.430 86.343 0.206 6.360 7.511 0.22 102713. 0.3764
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19.11 0.3603 0.6080 0.0692 0.0410 0.114 1.790 1.355 84.694 0.202 6.028 7.258 0.22 102896. 0.3541
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20.47 0.3860 0.6289 0.0652 0.0400 0.111 1.747 1.277 82.681 0.197 5.682 7.007 0.22 103087. 0.3319
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21.84 0.4118 0.6470 0.0611 0.0389 0.108 1.697 1.197 80.306 0.192 5.323 6.759 0.22 103288. 0.3099
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23.20 0.4375 0.6622 0.0568 0.0376 0.104 1.639 1.113 77.570 0.185 4.952 6.510 0.22 103497. 0.2879
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24.57 0.4633 0.6741 0.0525 0.0361 0.100 1.574 1.028 74.473 0.178 4.571 6.259 0.22 103716. 0.2659
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25.93 0.4890 0.6825 0.0480 0.0344 0.095 1.501 0.940 71.016 0.170 4.181 6.004 0.22 103945. 0.2440
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27.30 0.5147 0.6870 0.0434 0.0325 0.090 1.420 0.851 67.198 0.160 3.783 5.741 0.23 104182. 0.2219
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28.66 0.5405 0.6868 0.0388 0.0305 0.085 1.332 0.759 63.020 0.150 3.378 5.466 0.23 104429. 0.1996
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30.03 0.5662 0.6808 0.0340 0.0283 0.078 1.236 0.667 58.482 0.140 2.966 5.172 0.23 104686. 0.1770
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31.39 0.5919 0.6676 0.0293 0.0259 0.072 1.132 0.573 53.586 0.128 2.549 4.851 0.23 104952. 0.1539
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32.76 0.6177 0.6446 0.0244 0.0234 0.065 1.021 0.478 48.337 0.115 2.128 4.489 0.23 105227. 0.1301
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34.12 0.6434 0.6078 0.0195 0.0207 0.057 0.903 0.383 42.743 0.102 1.703 4.063 0.23 105511. 0.1054
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35.49 0.6692 0.5501 0.0147 0.0178 0.049 0.778 0.287 36.815 0.088 1.277 3.536 0.23 105805. 0.0794
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36.85 0.6949 0.4578 0.0098 0.0148 0.041 0.646 0.191 30.570 0.073 0.849 2.834 0.23 106109. 0.0519
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38.22 0.7206 0.3012 0.0049 0.0116 0.032 0.508 0.095 24.028 0.057 0.424 1.798 0.23 106420. 0.0233
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39.58 0.7464 -0.0009 0.0000 0.0083 0.023 0.363 0.000 17.188 0.041 -0.001 -0.005 0.23 106733. 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 0.1064 0.0397 0.215 2.708 3.255 160.189 0.306 14.480 9.217 0.28 126392. 0.6970
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1.71 0.0258 0.0671 0.1048 0.0403 0.218 2.746 3.207 162.466 0.310 14.265 8.953 0.28 126488. 0.6720
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3.42 0.0515 0.1302 0.1031 0.0408 0.221 2.783 3.155 164.618 0.314 14.032 8.692 0.28 126593. 0.6470
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5.13 0.0773 0.1895 0.1012 0.0413 0.223 2.816 3.098 166.601 0.318 13.780 8.434 0.28 126706. 0.6222
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6.83 0.1031 0.2451 0.0992 0.0417 0.226 2.846 3.037 168.371 0.322 13.508 8.181 0.28 126828. 0.5975
|
|
8.54 0.1289 0.2970 0.0971 0.0421 0.228 2.872 2.971 169.881 0.324 13.214 7.932 0.28 126961. 0.5730
|
|
10.25 0.1546 0.3455 0.0947 0.0424 0.229 2.892 2.900 171.081 0.327 12.898 7.688 0.28 127103. 0.5487
|
|
11.96 0.1804 0.3905 0.0923 0.0426 0.231 2.906 2.824 171.920 0.328 12.560 7.449 0.28 127255. 0.5246
|
|
13.67 0.2062 0.4324 0.0896 0.0427 0.231 2.913 2.742 172.343 0.329 12.196 7.216 0.28 127418. 0.5008
|
|
15.38 0.2319 0.4710 0.0867 0.0427 0.231 2.913 2.655 172.293 0.329 11.808 6.988 0.28 127591. 0.4772
|
|
17.08 0.2577 0.5067 0.0837 0.0426 0.230 2.903 2.561 171.710 0.328 11.393 6.766 0.28 127775. 0.4538
|
|
18.79 0.2835 0.5395 0.0804 0.0423 0.229 2.883 2.462 170.535 0.326 10.951 6.548 0.28 127970. 0.4306
|
|
20.50 0.3093 0.5694 0.0770 0.0418 0.226 2.852 2.357 168.712 0.322 10.482 6.336 0.28 128176. 0.4076
|
|
22.21 0.3350 0.5965 0.0734 0.0412 0.223 2.809 2.245 166.195 0.317 9.986 6.127 0.28 128394. 0.3848
|
|
23.92 0.3608 0.6210 0.0695 0.0404 0.219 2.755 2.128 162.962 0.311 9.465 5.923 0.28 128622. 0.3621
|
|
25.63 0.3866 0.6427 0.0655 0.0394 0.213 2.688 2.006 159.007 0.304 8.921 5.721 0.28 128862. 0.3396
|
|
27.33 0.4123 0.6616 0.0614 0.0383 0.207 2.609 1.879 154.332 0.295 8.357 5.521 0.28 129114. 0.3172
|
|
29.04 0.4381 0.6777 0.0571 0.0369 0.200 2.518 1.748 148.938 0.284 7.774 5.323 0.28 129377. 0.2949
|
|
30.75 0.4639 0.6907 0.0527 0.0354 0.192 2.414 1.613 142.828 0.273 7.176 5.123 0.28 129651. 0.2727
|
|
32.46 0.4897 0.7003 0.0482 0.0337 0.182 2.299 1.476 136.001 0.260 6.563 4.921 0.28 129938. 0.2505
|
|
34.17 0.5154 0.7060 0.0436 0.0318 0.172 2.171 1.335 128.456 0.245 5.938 4.714 0.28 130236. 0.2283
|
|
35.88 0.5412 0.7074 0.0389 0.0298 0.161 2.032 1.192 120.193 0.230 5.301 4.498 0.28 130545. 0.2058
|
|
37.58 0.5670 0.7032 0.0342 0.0276 0.149 1.880 1.046 111.214 0.212 4.655 4.268 0.28 130867. 0.1830
|
|
39.29 0.5927 0.6920 0.0294 0.0252 0.136 1.716 0.899 101.522 0.194 4.000 4.017 0.28 131200. 0.1597
|
|
41.00 0.6185 0.6713 0.0245 0.0226 0.122 1.540 0.750 91.128 0.174 3.338 3.735 0.28 131545. 0.1356
|
|
42.71 0.6443 0.6371 0.0196 0.0198 0.107 1.353 0.600 80.045 0.153 2.671 3.402 0.28 131901. 0.1105
|
|
44.42 0.6701 0.5817 0.0147 0.0169 0.092 1.155 0.450 68.299 0.130 2.001 2.988 0.28 132270. 0.0840
|
|
46.13 0.6958 0.4906 0.0098 0.0139 0.075 0.945 0.299 55.921 0.107 1.330 2.426 0.28 132650. 0.0556
|
|
47.83 0.7216 0.3295 0.0049 0.0106 0.058 0.726 0.149 42.955 0.082 0.662 1.572 0.28 133041. 0.0254
|
|
49.54 0.7474 -0.0037 0.0000 0.0073 0.039 0.497 -0.001 29.382 0.056 -0.005 -0.017 0.29 133430. 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 0.1069 0.0393 0.367 3.859 4.711 273.941 0.436 20.953 7.799 0.33 151664. 0.7095
|
|
2.05 0.0258 0.0681 0.1053 0.0399 0.373 3.916 4.641 277.958 0.442 20.644 7.573 0.33 151780. 0.6838
|
|
4.10 0.0516 0.1322 0.1036 0.0404 0.378 3.969 4.566 281.757 0.448 20.309 7.350 0.33 151905. 0.6583
|
|
6.16 0.0774 0.1924 0.1017 0.0409 0.383 4.018 4.484 285.261 0.454 19.946 7.130 0.33 152042. 0.6328
|
|
8.21 0.1032 0.2488 0.0997 0.0414 0.387 4.063 4.396 288.393 0.459 19.554 6.914 0.33 152189. 0.6076
|
|
10.26 0.1290 0.3015 0.0976 0.0418 0.390 4.100 4.301 291.070 0.463 19.131 6.702 0.33 152348. 0.5826
|
|
12.31 0.1548 0.3506 0.0953 0.0421 0.393 4.130 4.199 293.206 0.467 18.676 6.495 0.33 152519. 0.5578
|
|
14.36 0.1806 0.3963 0.0928 0.0423 0.395 4.152 4.089 294.709 0.469 18.186 6.293 0.33 152703. 0.5333
|
|
16.42 0.2064 0.4386 0.0901 0.0424 0.396 4.163 3.971 295.484 0.470 17.662 6.095 0.33 152898. 0.5090
|
|
18.47 0.2322 0.4779 0.0872 0.0424 0.396 4.162 3.844 295.432 0.470 17.100 5.902 0.33 153107. 0.4850
|
|
20.52 0.2580 0.5141 0.0842 0.0422 0.395 4.148 3.710 294.447 0.469 16.501 5.714 0.33 153328. 0.4613
|
|
22.57 0.2838 0.5473 0.0809 0.0419 0.392 4.119 3.566 292.427 0.465 15.862 5.531 0.33 153563. 0.4378
|
|
24.62 0.3096 0.5778 0.0774 0.0415 0.388 4.075 3.413 289.271 0.460 15.183 5.352 0.33 153811. 0.4144
|
|
26.68 0.3354 0.6055 0.0738 0.0409 0.382 4.013 3.252 284.901 0.453 14.465 5.177 0.34 154073. 0.3913
|
|
28.73 0.3612 0.6305 0.0699 0.0401 0.375 3.934 3.082 279.275 0.444 13.710 5.006 0.34 154348. 0.3683
|
|
30.78 0.3870 0.6528 0.0659 0.0391 0.365 3.837 2.905 272.384 0.434 12.922 4.838 0.34 154637. 0.3456
|
|
32.83 0.4128 0.6724 0.0617 0.0379 0.354 3.722 2.721 264.229 0.421 12.105 4.671 0.34 154939. 0.3230
|
|
34.88 0.4385 0.6892 0.0574 0.0366 0.342 3.590 2.532 254.814 0.406 11.261 4.507 0.34 155256. 0.3005
|
|
36.94 0.4643 0.7030 0.0530 0.0350 0.327 3.439 2.337 244.141 0.389 10.394 4.341 0.34 155586. 0.2782
|
|
38.99 0.4901 0.7136 0.0485 0.0333 0.311 3.271 2.137 232.210 0.370 9.507 4.175 0.34 155931. 0.2558
|
|
41.04 0.5159 0.7205 0.0439 0.0314 0.294 3.085 1.934 219.017 0.349 8.601 4.004 0.34 156289. 0.2334
|
|
43.09 0.5417 0.7230 0.0392 0.0293 0.274 2.882 1.726 204.564 0.326 7.678 3.827 0.34 156661. 0.2108
|
|
45.14 0.5675 0.7204 0.0344 0.0271 0.253 2.660 1.516 188.852 0.301 6.741 3.640 0.34 157048. 0.1878
|
|
47.20 0.5933 0.7109 0.0295 0.0247 0.231 2.421 1.302 171.889 0.274 5.792 3.436 0.34 157448. 0.1643
|
|
49.25 0.6191 0.6923 0.0247 0.0220 0.206 2.165 1.087 153.692 0.245 4.833 3.207 0.34 157863. 0.1401
|
|
51.30 0.6449 0.6604 0.0197 0.0193 0.180 1.892 0.869 134.287 0.214 3.867 2.936 0.34 158292. 0.1147
|
|
53.35 0.6707 0.6074 0.0148 0.0163 0.152 1.602 0.651 113.716 0.181 2.896 2.597 0.34 158735. 0.0878
|
|
55.40 0.6965 0.5180 0.0098 0.0132 0.123 1.297 0.433 92.038 0.146 1.925 2.132 0.34 159192. 0.0588
|
|
57.46 0.7223 0.3543 0.0049 0.0099 0.093 0.977 0.215 69.327 0.110 0.956 1.407 0.34 159662. 0.0273
|
|
59.51 0.7481 -0.0062 -0.0001 0.0065 0.061 0.641 -0.002 45.528 0.072 -0.011 -0.024 0.34 160127. 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 0.1075 0.0391 0.580 5.226 6.448 432.824 0.590 28.681 6.757 0.39 176933. 0.7191
|
|
2.40 0.0258 0.0689 0.1059 0.0397 0.589 5.305 6.354 439.329 0.599 28.262 6.560 0.39 177067. 0.6930
|
|
4.79 0.0516 0.1337 0.1042 0.0402 0.597 5.379 6.252 445.484 0.608 27.807 6.365 0.39 177214. 0.6670
|
|
7.19 0.0775 0.1945 0.1024 0.0408 0.605 5.448 6.141 451.163 0.615 27.314 6.173 0.39 177374. 0.6412
|
|
9.58 0.1033 0.2515 0.1004 0.0412 0.612 5.509 6.021 456.243 0.622 26.780 5.985 0.39 177547. 0.6155
|
|
11.98 0.1291 0.3047 0.0982 0.0416 0.618 5.561 5.891 460.590 0.628 26.203 5.801 0.39 177733. 0.5901
|
|
14.38 0.1549 0.3543 0.0959 0.0419 0.622 5.603 5.751 464.064 0.633 25.582 5.621 0.39 177933. 0.5650
|
|
16.77 0.1807 0.4004 0.0934 0.0421 0.626 5.633 5.601 466.520 0.636 24.915 5.446 0.39 178148. 0.5402
|
|
19.17 0.2065 0.4432 0.0907 0.0423 0.627 5.649 5.440 467.804 0.638 24.198 5.275 0.39 178377. 0.5156
|
|
21.56 0.2324 0.4829 0.0878 0.0423 0.627 5.648 5.268 467.754 0.638 23.431 5.108 0.39 178621. 0.4914
|
|
23.96 0.2582 0.5195 0.0847 0.0421 0.625 5.629 5.084 466.206 0.636 22.612 4.946 0.39 178880. 0.4674
|
|
26.35 0.2840 0.5532 0.0815 0.0418 0.621 5.590 4.887 462.991 0.632 21.738 4.788 0.39 179155. 0.4436
|
|
28.75 0.3098 0.5840 0.0780 0.0414 0.614 5.530 4.678 457.948 0.625 20.809 4.634 0.39 179445. 0.4200
|
|
31.15 0.3356 0.6121 0.0743 0.0407 0.605 5.445 4.457 450.951 0.615 19.826 4.483 0.39 179751. 0.3967
|
|
33.54 0.3614 0.6376 0.0704 0.0399 0.593 5.336 4.225 441.932 0.603 18.792 4.336 0.39 180073. 0.3735
|
|
35.94 0.3873 0.6605 0.0664 0.0389 0.578 5.203 3.982 430.873 0.588 17.713 4.192 0.39 180411. 0.3506
|
|
38.33 0.4131 0.6806 0.0622 0.0377 0.560 5.045 3.730 417.779 0.570 16.593 4.050 0.39 180764. 0.3279
|
|
40.73 0.4389 0.6981 0.0579 0.0364 0.540 4.862 3.471 402.655 0.549 15.437 3.909 0.39 181134. 0.3052
|
|
43.13 0.4647 0.7126 0.0534 0.0348 0.517 4.655 3.203 385.503 0.526 14.249 3.769 0.39 181521. 0.2827
|
|
45.52 0.4905 0.7240 0.0488 0.0331 0.491 4.423 2.930 366.322 0.500 13.032 3.628 0.39 181923. 0.2603
|
|
47.92 0.5163 0.7318 0.0442 0.0312 0.463 4.167 2.651 345.110 0.471 11.790 3.484 0.39 182342. 0.2377
|
|
50.31 0.5422 0.7355 0.0394 0.0291 0.432 3.886 2.366 321.864 0.439 10.525 3.335 0.39 182777. 0.2150
|
|
52.71 0.5680 0.7341 0.0346 0.0268 0.398 3.581 2.078 296.591 0.405 9.241 3.177 0.40 183229. 0.1919
|
|
55.11 0.5938 0.7263 0.0298 0.0243 0.361 3.252 1.785 269.301 0.367 7.939 3.006 0.40 183697. 0.1683
|
|
57.50 0.6196 0.7094 0.0248 0.0217 0.322 2.898 1.489 240.021 0.327 6.624 2.814 0.40 184182. 0.1439
|
|
59.90 0.6454 0.6796 0.0199 0.0189 0.280 2.521 1.191 208.795 0.285 5.299 2.588 0.40 184683. 0.1184
|
|
62.29 0.6712 0.6290 0.0149 0.0159 0.236 2.121 0.892 175.690 0.240 3.969 2.303 0.40 185201. 0.0912
|
|
64.69 0.6971 0.5415 0.0099 0.0127 0.189 1.700 0.593 140.802 0.192 2.636 1.909 0.40 185735. 0.0616
|
|
67.08 0.7229 0.3764 0.0049 0.0094 0.140 1.259 0.294 104.252 0.142 1.309 1.280 0.40 186284. 0.0291
|
|
69.48 0.7487 -0.0088 -0.0001 0.0060 0.088 0.796 -0.004 65.910 0.090 -0.019 -0.029 0.40 186823. 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 0.1082 0.0391 0.866 6.820 8.477 645.551 0.771 37.706 5.956 0.44 202196. 0.7268
|
|
2.74 0.0258 0.0694 0.1066 0.0397 0.879 6.925 8.355 655.456 0.782 37.162 5.781 0.44 202351. 0.7004
|
|
5.48 0.0517 0.1347 0.1049 0.0402 0.892 7.024 8.221 664.828 0.794 36.569 5.609 0.44 202519. 0.6740
|
|
8.22 0.0775 0.1960 0.1031 0.0408 0.903 7.116 8.077 673.480 0.804 35.925 5.439 0.44 202702. 0.6479
|
|
10.96 0.1033 0.2534 0.1011 0.0412 0.914 7.197 7.920 681.218 0.813 35.228 5.273 0.44 202900. 0.6220
|
|
13.70 0.1292 0.3069 0.0989 0.0416 0.922 7.267 7.751 687.845 0.821 34.475 5.111 0.44 203114. 0.5963
|
|
16.44 0.1550 0.3569 0.0966 0.0419 0.930 7.323 7.568 693.145 0.827 33.662 4.952 0.44 203343. 0.5710
|
|
19.18 0.1808 0.4034 0.0941 0.0422 0.935 7.363 7.371 696.901 0.832 32.788 4.798 0.45 203589. 0.5459
|
|
21.92 0.2067 0.4465 0.0914 0.0423 0.937 7.384 7.160 698.879 0.834 31.849 4.647 0.45 203852. 0.5212
|
|
24.66 0.2325 0.4865 0.0885 0.0423 0.937 7.383 6.934 698.838 0.834 30.843 4.501 0.45 204132. 0.4967
|
|
27.40 0.2583 0.5235 0.0854 0.0422 0.934 7.359 6.692 696.526 0.831 29.767 4.358 0.45 204429. 0.4725
|
|
30.14 0.2842 0.5575 0.0821 0.0419 0.928 7.308 6.434 691.690 0.826 28.620 4.219 0.45 204744. 0.4486
|
|
32.88 0.3100 0.5887 0.0786 0.0414 0.917 7.228 6.160 684.087 0.817 27.400 4.084 0.45 205076. 0.4249
|
|
35.62 0.3358 0.6172 0.0749 0.0408 0.903 7.116 5.870 673.524 0.804 26.108 3.953 0.45 205427. 0.4014
|
|
38.36 0.3617 0.6431 0.0710 0.0399 0.885 6.972 5.564 659.898 0.788 24.748 3.824 0.45 205796. 0.3781
|
|
41.10 0.3875 0.6664 0.0669 0.0389 0.863 6.795 5.245 643.181 0.768 23.329 3.699 0.45 206183. 0.3550
|
|
43.84 0.4133 0.6870 0.0627 0.0377 0.836 6.586 4.913 623.378 0.744 21.855 3.575 0.45 206588. 0.3321
|
|
46.58 0.4392 0.7050 0.0583 0.0363 0.805 6.344 4.571 600.501 0.717 20.333 3.453 0.45 207012. 0.3094
|
|
49.32 0.4650 0.7202 0.0539 0.0348 0.770 6.070 4.220 574.552 0.686 18.769 3.331 0.45 207454. 0.2868
|
|
52.06 0.4908 0.7323 0.0493 0.0330 0.732 5.764 3.860 545.531 0.651 17.167 3.209 0.45 207915. 0.2642
|
|
54.80 0.5167 0.7410 0.0446 0.0311 0.689 5.425 3.492 513.433 0.613 15.531 3.085 0.45 208395. 0.2416
|
|
57.54 0.5425 0.7457 0.0398 0.0289 0.641 5.053 3.117 478.255 0.571 13.865 2.956 0.45 208893. 0.2188
|
|
60.28 0.5683 0.7455 0.0349 0.0266 0.590 4.649 2.737 440.005 0.525 12.173 2.821 0.45 209411. 0.1956
|
|
63.02 0.5942 0.7390 0.0300 0.0241 0.535 4.212 2.351 398.702 0.476 10.459 2.675 0.45 209947. 0.1719
|
|
65.76 0.6200 0.7239 0.0250 0.0214 0.475 3.744 1.962 354.385 0.423 8.727 2.511 0.45 210502. 0.1474
|
|
68.50 0.6458 0.6960 0.0200 0.0186 0.412 3.245 1.569 307.121 0.367 6.981 2.318 0.45 211075. 0.1217
|
|
71.24 0.6717 0.6476 0.0150 0.0156 0.345 2.715 1.175 257.012 0.307 5.227 2.074 0.45 211668. 0.0942
|
|
73.98 0.6975 0.5622 0.0100 0.0124 0.274 2.157 0.780 204.203 0.244 3.472 1.734 0.46 212278. 0.0642
|
|
76.72 0.7233 0.3966 0.0049 0.0090 0.200 1.573 0.387 148.881 0.178 1.722 1.179 0.46 212907. 0.0307
|
|
79.46 0.7492 -0.0115 -0.0001 0.0055 0.122 0.959 -0.007 90.783 0.108 -0.029 -0.033 0.46 213520. 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 0.1090 0.0392 1.236 8.656 10.809 921.685 0.978 48.080 5.319 0.50 227454. 0.7330
|
|
3.08 0.0258 0.0698 0.1075 0.0398 1.255 8.791 10.655 936.091 0.993 47.395 5.163 0.50 227628. 0.7063
|
|
6.17 0.0517 0.1354 0.1058 0.0404 1.274 8.919 10.487 949.722 1.008 46.648 5.009 0.50 227819. 0.6798
|
|
9.25 0.0775 0.1970 0.1039 0.0409 1.290 9.037 10.305 962.305 1.021 45.835 4.857 0.50 228025. 0.6535
|
|
12.34 0.1034 0.2546 0.1019 0.0414 1.306 9.143 10.107 973.560 1.033 44.954 4.709 0.50 228249. 0.6274
|
|
15.42 0.1292 0.3085 0.0998 0.0418 1.318 9.234 9.892 983.197 1.043 44.000 4.563 0.50 228490. 0.6016
|
|
18.50 0.1551 0.3587 0.0974 0.0421 1.329 9.306 9.661 990.907 1.051 42.970 4.422 0.50 228749. 0.5760
|
|
21.59 0.1809 0.4054 0.0949 0.0423 1.336 9.357 9.411 996.374 1.057 41.860 4.284 0.50 229026. 0.5508
|
|
24.67 0.2068 0.4489 0.0922 0.0425 1.340 9.384 9.143 999.265 1.060 40.668 4.150 0.50 229323. 0.5259
|
|
27.76 0.2326 0.4891 0.0893 0.0425 1.340 9.384 8.855 999.231 1.060 39.389 4.020 0.50 229639. 0.5013
|
|
30.84 0.2585 0.5263 0.0862 0.0423 1.336 9.353 8.548 995.911 1.057 38.020 3.893 0.50 229974. 0.4770
|
|
33.92 0.2843 0.5606 0.0829 0.0420 1.326 9.288 8.219 988.939 1.049 36.559 3.770 0.50 230330. 0.4530
|
|
37.01 0.3102 0.5922 0.0794 0.0416 1.311 9.184 7.870 977.967 1.038 35.005 3.650 0.50 230705. 0.4291
|
|
40.09 0.3360 0.6210 0.0756 0.0409 1.291 9.041 7.499 962.713 1.021 33.358 3.533 0.50 231101. 0.4055
|
|
43.18 0.3619 0.6473 0.0717 0.0401 1.265 8.856 7.110 943.026 1.001 31.624 3.420 0.50 231517. 0.3822
|
|
46.26 0.3877 0.6710 0.0676 0.0391 1.232 8.629 6.702 918.866 0.975 29.812 3.308 0.50 231954. 0.3590
|
|
49.34 0.4135 0.6921 0.0633 0.0378 1.194 8.361 6.280 890.243 0.945 27.931 3.199 0.50 232411. 0.3360
|
|
52.43 0.4394 0.7106 0.0589 0.0364 1.149 8.050 5.843 857.172 0.909 25.989 3.092 0.50 232889. 0.3132
|
|
55.51 0.4652 0.7263 0.0544 0.0348 1.099 7.698 5.394 819.661 0.870 23.991 2.985 0.51 233387. 0.2905
|
|
58.60 0.4911 0.7391 0.0498 0.0331 1.043 7.304 4.934 777.709 0.825 21.945 2.877 0.51 233907. 0.2679
|
|
61.68 0.5169 0.7486 0.0450 0.0311 0.981 6.868 4.464 731.309 0.776 19.855 2.768 0.51 234448. 0.2451
|
|
64.76 0.5428 0.7542 0.0402 0.0289 0.913 6.390 3.985 680.461 0.722 17.726 2.656 0.51 235009. 0.2222
|
|
67.85 0.5686 0.7551 0.0353 0.0266 0.838 5.871 3.499 625.174 0.663 15.563 2.539 0.51 235592. 0.1990
|
|
70.93 0.5945 0.7498 0.0303 0.0240 0.758 5.311 3.006 565.474 0.600 13.372 2.411 0.51 236196. 0.1752
|
|
74.02 0.6203 0.7362 0.0253 0.0213 0.672 4.709 2.508 501.418 0.532 11.157 2.269 0.51 236821. 0.1506
|
|
77.10 0.6462 0.7102 0.0202 0.0184 0.581 4.067 2.006 433.105 0.460 8.925 2.101 0.51 237468. 0.1247
|
|
80.18 0.6720 0.6641 0.0151 0.0153 0.484 3.387 1.502 360.681 0.383 6.682 1.889 0.51 238135. 0.0970
|
|
83.27 0.6979 0.5808 0.0101 0.0121 0.381 2.671 0.997 284.358 0.302 4.437 1.591 0.51 238823. 0.0666
|
|
86.35 0.7237 0.4152 0.0050 0.0087 0.274 1.920 0.494 204.407 0.217 2.198 1.097 0.51 239530. 0.0323
|
|
89.44 0.7496 -0.0145 -0.0001 0.0051 0.161 1.130 -0.010 120.350 0.128 -0.044 -0.037 0.51 240216. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1099 0.0394 1.706 10.750 13.459 1271.895 1.215 59.865 4.800 0.56 252705. 0.7380
|
|
3.43 0.0259 0.0700 0.1084 0.0400 1.733 10.921 13.270 1292.129 1.234 59.026 4.658 0.56 252900. 0.7112
|
|
6.86 0.0517 0.1358 0.1067 0.0406 1.758 11.083 13.064 1311.276 1.252 58.109 4.519 0.56 253112. 0.6845
|
|
10.28 0.0776 0.1976 0.1049 0.0412 1.782 11.233 12.839 1328.943 1.269 57.109 4.382 0.56 253342. 0.6581
|
|
13.71 0.1034 0.2554 0.1029 0.0417 1.803 11.366 12.595 1344.744 1.284 56.023 4.248 0.56 253591. 0.6319
|
|
17.14 0.1293 0.3094 0.1007 0.0421 1.821 11.480 12.330 1358.265 1.297 54.846 4.118 0.56 253860. 0.6060
|
|
20.57 0.1552 0.3598 0.0984 0.0424 1.836 11.572 12.044 1369.084 1.307 53.572 3.990 0.56 254149. 0.5804
|
|
24.00 0.1810 0.4067 0.0959 0.0427 1.846 11.637 11.735 1376.755 1.315 52.199 3.866 0.56 254459. 0.5551
|
|
27.43 0.2069 0.4504 0.0931 0.0428 1.852 11.671 11.403 1380.815 1.319 50.721 3.746 0.56 254790. 0.5301
|
|
30.85 0.2327 0.4908 0.0902 0.0428 1.852 11.671 11.046 1380.783 1.319 49.134 3.629 0.56 255142. 0.5055
|
|
34.28 0.2586 0.5283 0.0871 0.0426 1.845 11.632 10.664 1376.161 1.314 47.435 3.515 0.56 255516. 0.4811
|
|
37.71 0.2844 0.5628 0.0838 0.0423 1.832 11.549 10.256 1366.438 1.305 45.620 3.404 0.56 255912. 0.4570
|
|
41.14 0.3103 0.5946 0.0802 0.0419 1.812 11.420 9.822 1351.130 1.290 43.686 3.297 0.56 256331. 0.4331
|
|
44.57 0.3362 0.6238 0.0765 0.0412 1.783 11.240 9.361 1329.846 1.270 41.636 3.193 0.56 256772. 0.4094
|
|
48.00 0.3620 0.6504 0.0725 0.0404 1.747 11.008 8.875 1302.369 1.244 39.478 3.091 0.56 257236. 0.3859
|
|
51.42 0.3879 0.6745 0.0684 0.0393 1.701 10.723 8.368 1268.647 1.211 37.220 2.992 0.56 257722. 0.3627
|
|
54.85 0.4137 0.6960 0.0640 0.0381 1.648 10.385 7.841 1228.694 1.173 34.875 2.894 0.56 258231. 0.3397
|
|
58.28 0.4396 0.7150 0.0596 0.0366 1.586 9.995 7.296 1182.538 1.129 32.453 2.798 0.56 258764. 0.3168
|
|
61.71 0.4655 0.7313 0.0550 0.0350 1.516 9.553 6.736 1130.191 1.079 29.961 2.703 0.56 259319. 0.2940
|
|
65.14 0.4913 0.7447 0.0503 0.0332 1.437 9.058 6.162 1071.653 1.023 27.408 2.608 0.56 259898. 0.2713
|
|
68.57 0.5172 0.7549 0.0455 0.0312 1.350 8.511 5.575 1006.920 0.962 24.799 2.511 0.56 260500. 0.2485
|
|
71.99 0.5430 0.7614 0.0407 0.0290 1.255 7.911 4.978 935.989 0.894 22.142 2.412 0.56 261125. 0.2256
|
|
75.42 0.5689 0.7632 0.0357 0.0266 1.152 7.259 4.371 858.871 0.820 19.442 2.308 0.56 261774. 0.2023
|
|
78.85 0.5948 0.7592 0.0307 0.0240 1.040 6.556 3.756 775.607 0.741 16.705 2.196 0.57 262446. 0.1784
|
|
82.28 0.6206 0.7471 0.0256 0.0213 0.920 5.801 3.134 686.275 0.655 13.939 2.071 0.57 263142. 0.1537
|
|
85.71 0.6465 0.7228 0.0205 0.0183 0.793 4.995 2.507 591.011 0.564 11.150 1.924 0.57 263861. 0.1277
|
|
89.13 0.6723 0.6788 0.0153 0.0152 0.657 4.142 1.877 490.021 0.468 8.348 1.737 0.57 264603. 0.0997
|
|
92.56 0.6982 0.5978 0.0102 0.0119 0.514 3.242 1.246 383.601 0.366 5.542 1.473 0.57 265368. 0.0689
|
|
95.99 0.7240 0.4327 0.0050 0.0084 0.365 2.300 0.617 272.132 0.260 2.744 1.028 0.57 266155. 0.0338
|
|
99.42 0.7499 -0.0179 -0.0001 0.0048 0.208 1.308 -0.014 154.799 0.148 -0.062 -0.041 0.57 266911. 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 0.1110 0.0398 2.291 13.127 16.443 1708.375 1.483 73.137 4.365 0.61 277948. 0.7419
|
|
3.77 0.0259 0.0701 0.1095 0.0404 2.328 13.339 16.217 1736.042 1.507 72.132 4.237 0.61 278163. 0.7151
|
|
7.55 0.0517 0.1360 0.1078 0.0410 2.363 13.541 15.969 1762.216 1.530 71.031 4.110 0.61 278397. 0.6884
|
|
11.32 0.0776 0.1978 0.1060 0.0416 2.396 13.726 15.699 1786.359 1.551 69.829 3.986 0.61 278651. 0.6619
|
|
15.09 0.1035 0.2557 0.1040 0.0421 2.424 13.892 15.404 1807.943 1.570 68.519 3.865 0.61 278926. 0.6357
|
|
18.86 0.1294 0.3098 0.1018 0.0425 2.449 14.034 15.084 1826.405 1.586 67.096 3.746 0.61 279223. 0.6098
|
|
22.64 0.1552 0.3603 0.0995 0.0429 2.469 14.147 14.738 1841.165 1.598 65.553 3.631 0.61 279542. 0.5842
|
|
26.41 0.1811 0.4073 0.0970 0.0431 2.483 14.228 14.363 1851.621 1.607 63.887 3.518 0.61 279885. 0.5589
|
|
30.18 0.2070 0.4511 0.0942 0.0432 2.490 14.270 13.960 1857.154 1.612 62.092 3.409 0.61 280250. 0.5339
|
|
33.95 0.2328 0.4917 0.0913 0.0432 2.490 14.270 13.526 1857.113 1.612 60.162 3.303 0.61 280639. 0.5092
|
|
37.73 0.2587 0.5294 0.0882 0.0431 2.482 14.221 13.061 1850.828 1.607 58.093 3.201 0.61 281053. 0.4848
|
|
41.50 0.2846 0.5642 0.0848 0.0428 2.464 14.120 12.563 1837.618 1.595 55.881 3.101 0.61 281490. 0.4606
|
|
45.27 0.3104 0.5962 0.0812 0.0423 2.436 13.960 12.033 1816.825 1.577 53.522 3.004 0.61 281952. 0.4367
|
|
49.05 0.3363 0.6257 0.0774 0.0416 2.398 13.738 11.470 1787.917 1.552 51.020 2.910 0.61 282439. 0.4130
|
|
52.82 0.3622 0.6526 0.0734 0.0408 2.348 13.451 10.877 1750.601 1.520 48.382 2.818 0.61 282951. 0.3896
|
|
56.59 0.3881 0.6770 0.0692 0.0397 2.286 13.099 10.257 1704.804 1.480 45.622 2.729 0.62 283488. 0.3663
|
|
60.36 0.4139 0.6990 0.0649 0.0384 2.213 12.683 9.612 1650.554 1.433 42.753 2.641 0.62 284050. 0.3432
|
|
64.14 0.4398 0.7184 0.0604 0.0370 2.129 12.201 8.945 1587.890 1.378 39.788 2.555 0.62 284637. 0.3203
|
|
67.91 0.4657 0.7353 0.0558 0.0353 2.034 11.655 8.259 1516.839 1.317 36.737 2.470 0.62 285249. 0.2975
|
|
71.68 0.4915 0.7493 0.0510 0.0335 1.928 11.045 7.556 1437.407 1.248 33.610 2.384 0.62 285887. 0.2747
|
|
75.45 0.5174 0.7602 0.0462 0.0314 1.810 10.370 6.838 1349.587 1.172 30.415 2.298 0.62 286551. 0.2519
|
|
79.23 0.5433 0.7674 0.0412 0.0292 1.681 9.631 6.106 1253.378 1.088 27.159 2.210 0.62 287240. 0.2288
|
|
83.00 0.5691 0.7703 0.0362 0.0267 1.541 8.827 5.362 1148.797 0.997 23.849 2.117 0.62 287955. 0.2054
|
|
86.77 0.5950 0.7674 0.0311 0.0241 1.389 7.960 4.607 1035.899 0.899 20.494 2.017 0.62 288696. 0.1815
|
|
90.55 0.6209 0.7567 0.0260 0.0213 1.227 7.029 3.845 914.788 0.794 17.101 1.906 0.62 289462. 0.1567
|
|
94.32 0.6468 0.7342 0.0208 0.0183 1.054 6.037 3.075 785.649 0.682 13.680 1.776 0.62 290254. 0.1305
|
|
98.09 0.6726 0.6922 0.0155 0.0151 0.870 4.985 2.302 648.760 0.563 10.241 1.610 0.62 291072. 0.1024
|
|
101.86 0.6985 0.6135 0.0103 0.0117 0.677 3.877 1.528 504.527 0.438 6.798 1.374 0.63 291915. 0.0712
|
|
105.64 0.7244 0.4493 0.0051 0.0082 0.474 2.716 0.756 353.465 0.307 3.363 0.970 0.63 292781. 0.0354
|
|
109.41 0.7502 -0.0219 -0.0001 0.0045 0.260 1.493 -0.020 194.247 0.169 -0.087 -0.046 0.63 293605. 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 0.1122 0.0403 3.014 15.831 19.781 2247.635 1.789 87.985 3.992 0.67 303182. 0.7441
|
|
4.12 0.0259 0.0700 0.1107 0.0410 3.063 16.089 19.516 2284.152 1.818 86.807 3.875 0.67 303416. 0.7175
|
|
8.23 0.0518 0.1358 0.1091 0.0416 3.110 16.332 19.225 2318.757 1.845 85.512 3.761 0.67 303672. 0.6911
|
|
12.35 0.0776 0.1975 0.1072 0.0422 3.152 16.557 18.906 2350.716 1.871 84.093 3.648 0.67 303950. 0.6648
|
|
16.47 0.1035 0.2554 0.1053 0.0427 3.191 16.759 18.557 2379.310 1.893 82.543 3.538 0.67 304252. 0.6387
|
|
20.59 0.1294 0.3096 0.1031 0.0431 3.224 16.931 18.177 2403.785 1.913 80.853 3.430 0.67 304577. 0.6129
|
|
24.70 0.1553 0.3601 0.1008 0.0435 3.250 17.069 17.765 2423.358 1.928 79.019 3.325 0.67 304927. 0.5874
|
|
28.82 0.1812 0.4072 0.0982 0.0437 3.268 17.167 17.318 2437.218 1.939 77.032 3.223 0.67 305302. 0.5621
|
|
32.94 0.2071 0.4511 0.0955 0.0438 3.278 17.218 16.836 2444.530 1.945 74.887 3.124 0.67 305703. 0.5372
|
|
37.06 0.2329 0.4919 0.0926 0.0438 3.278 17.217 16.317 2444.424 1.945 72.578 3.028 0.67 306130. 0.5126
|
|
41.17 0.2588 0.5297 0.0894 0.0437 3.267 17.158 15.760 2436.015 1.939 70.099 2.934 0.67 306583. 0.4882
|
|
45.29 0.2847 0.5647 0.0860 0.0434 3.243 17.034 15.163 2418.406 1.925 67.445 2.844 0.67 307062. 0.4641
|
|
49.41 0.3106 0.5970 0.0824 0.0429 3.206 16.839 14.526 2390.739 1.902 64.613 2.756 0.67 307568. 0.4402
|
|
53.53 0.3365 0.6267 0.0786 0.0422 3.154 16.569 13.850 2352.301 1.872 61.605 2.671 0.67 308102. 0.4165
|
|
57.64 0.3623 0.6539 0.0745 0.0413 3.088 16.219 13.136 2302.693 1.832 58.431 2.588 0.67 308662. 0.3931
|
|
61.76 0.3882 0.6787 0.0703 0.0402 3.006 15.790 12.389 2241.827 1.784 55.107 2.507 0.67 309250. 0.3698
|
|
65.88 0.4141 0.7011 0.0659 0.0389 2.910 15.283 11.612 2169.744 1.727 51.650 2.427 0.67 309865. 0.3467
|
|
70.00 0.4400 0.7210 0.0613 0.0374 2.798 14.696 10.808 2086.514 1.660 48.076 2.350 0.67 310508. 0.3237
|
|
74.11 0.4659 0.7384 0.0566 0.0357 2.672 14.032 9.981 1992.178 1.585 44.396 2.272 0.67 311178. 0.3009
|
|
78.23 0.4917 0.7530 0.0518 0.0338 2.530 13.289 9.133 1886.755 1.501 40.622 2.195 0.67 311876. 0.2781
|
|
82.35 0.5176 0.7646 0.0469 0.0317 2.374 12.469 8.265 1770.242 1.409 36.765 2.118 0.68 312601. 0.2552
|
|
86.47 0.5435 0.7726 0.0419 0.0295 2.203 11.570 7.382 1642.639 1.307 32.833 2.038 0.68 313355. 0.2321
|
|
90.58 0.5694 0.7764 0.0368 0.0270 2.017 10.593 6.483 1503.964 1.197 28.835 1.955 0.68 314136. 0.2086
|
|
94.70 0.5953 0.7747 0.0316 0.0243 1.816 9.539 5.571 1354.292 1.078 24.781 1.866 0.68 314946. 0.1846
|
|
98.82 0.6212 0.7653 0.0264 0.0214 1.601 8.408 4.649 1193.763 0.950 20.680 1.767 0.68 315783. 0.1596
|
|
102.94 0.6470 0.7445 0.0211 0.0183 1.371 7.203 3.719 1022.618 0.814 16.544 1.650 0.68 316649. 0.1333
|
|
107.05 0.6729 0.7046 0.0158 0.0151 1.128 5.925 2.784 841.229 0.669 12.385 1.501 0.68 317542. 0.1050
|
|
111.17 0.6988 0.6283 0.0105 0.0117 0.872 4.579 1.848 650.131 0.517 8.220 1.289 0.68 318462. 0.0735
|
|
115.29 0.7247 0.4654 0.0052 0.0081 0.603 3.170 0.914 450.020 0.358 4.064 0.921 0.68 319408. 0.0369
|
|
119.41 0.7506 -0.0267 -0.0002 0.0043 0.320 1.682 -0.027 238.828 0.190 -0.119 -0.051 0.69 320298. 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 0.1136 0.0413 3.929 19.050 23.495 2930.004 2.152 104.507 3.637 0.72 328403. 0.7389
|
|
4.46 0.0259 0.0692 0.1121 0.0420 3.989 19.341 23.191 2974.772 2.185 103.155 3.536 0.72 328658. 0.7137
|
|
8.92 0.0518 0.1344 0.1105 0.0426 4.046 19.616 22.856 3017.062 2.216 101.662 3.436 0.72 328936. 0.6885
|
|
13.39 0.0777 0.1959 0.1087 0.0431 4.098 19.869 22.486 3055.986 2.245 100.019 3.337 0.72 329238. 0.6633
|
|
17.85 0.1036 0.2536 0.1067 0.0436 4.145 20.095 22.081 3090.655 2.270 98.216 3.241 0.72 329566. 0.6382
|
|
22.31 0.1295 0.3077 0.1046 0.0440 4.184 20.286 21.638 3120.118 2.292 96.246 3.145 0.72 329921. 0.6132
|
|
26.77 0.1553 0.3583 0.1022 0.0443 4.215 20.437 21.155 3143.391 2.309 94.098 3.053 0.72 330302. 0.5884
|
|
31.24 0.1812 0.4056 0.0997 0.0446 4.237 20.542 20.631 3159.446 2.321 91.766 2.962 0.72 330710. 0.5638
|
|
35.70 0.2071 0.4497 0.0970 0.0447 4.247 20.592 20.063 3167.226 2.327 89.241 2.873 0.72 331147. 0.5394
|
|
40.16 0.2330 0.4907 0.0940 0.0446 4.245 20.582 19.451 3165.624 2.325 86.518 2.787 0.72 331611. 0.5151
|
|
44.62 0.2589 0.5288 0.0908 0.0445 4.229 20.503 18.792 3153.483 2.316 83.588 2.703 0.72 332104. 0.4911
|
|
49.09 0.2848 0.5640 0.0874 0.0441 4.197 20.348 18.086 3129.621 2.299 80.447 2.621 0.72 332627. 0.4672
|
|
53.55 0.3107 0.5967 0.0838 0.0436 4.148 20.109 17.331 3092.887 2.272 77.090 2.542 0.73 333178. 0.4435
|
|
58.01 0.3366 0.6267 0.0799 0.0429 4.080 19.780 16.529 3042.297 2.235 73.521 2.464 0.73 333758. 0.4199
|
|
62.47 0.3625 0.6543 0.0758 0.0420 3.993 19.357 15.681 2977.278 2.187 69.750 2.389 0.73 334368. 0.3965
|
|
66.93 0.3884 0.6795 0.0715 0.0409 3.886 18.840 14.793 2897.650 2.129 65.797 2.315 0.73 335007. 0.3732
|
|
71.40 0.4143 0.7023 0.0670 0.0395 3.759 18.227 13.867 2803.451 2.059 61.683 2.244 0.73 335676. 0.3502
|
|
75.86 0.4402 0.7227 0.0624 0.0380 3.614 17.521 12.910 2694.765 1.979 57.425 2.173 0.73 336374. 0.3272
|
|
80.32 0.4660 0.7406 0.0576 0.0363 3.449 16.720 11.924 2571.662 1.889 53.039 2.103 0.73 337103. 0.3044
|
|
84.78 0.4919 0.7558 0.0527 0.0343 3.264 15.826 10.913 2434.175 1.788 48.540 2.033 0.73 337861. 0.2815
|
|
89.25 0.5178 0.7681 0.0477 0.0322 3.061 14.839 9.878 2282.310 1.676 43.939 1.963 0.73 338649. 0.2586
|
|
93.71 0.5437 0.7770 0.0426 0.0298 2.838 13.758 8.824 2116.068 1.554 39.247 1.891 0.73 339468. 0.2355
|
|
98.17 0.5696 0.7817 0.0375 0.0273 2.596 12.584 7.751 1935.474 1.422 34.475 1.816 0.73 340316. 0.2119
|
|
102.63 0.5955 0.7811 0.0322 0.0245 2.334 11.317 6.662 1740.612 1.279 29.633 1.736 0.73 341195. 0.1878
|
|
107.10 0.6214 0.7731 0.0269 0.0216 2.054 9.959 5.561 1531.680 1.125 24.734 1.647 0.74 342104. 0.1627
|
|
111.56 0.6473 0.7539 0.0215 0.0185 1.755 8.511 4.449 1309.057 0.962 19.790 1.542 0.74 343043. 0.1363
|
|
116.02 0.6732 0.7160 0.0161 0.0151 1.439 6.979 3.331 1073.370 0.788 14.817 1.408 0.74 344012. 0.1077
|
|
120.48 0.6991 0.6415 0.0107 0.0116 1.107 5.368 2.211 825.567 0.606 9.833 1.215 0.74 345010. 0.0757
|
|
124.94 0.7250 0.4787 0.0053 0.0080 0.760 3.686 1.092 566.894 0.416 4.859 0.874 0.74 346036. 0.0383
|
|
129.41 0.7508 -0.0313 -0.0002 0.0042 0.395 1.914 -0.036 294.457 0.216 -0.159 -0.055 0.74 346989. 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 0.1150 0.0435 5.170 23.275 27.606 3855.205 2.630 122.794 3.248 0.78 353610. 0.7152
|
|
4.81 0.0259 0.0667 0.1136 0.0441 5.236 23.571 27.266 3904.224 2.663 121.277 3.168 0.78 353884. 0.6932
|
|
9.61 0.0518 0.1301 0.1120 0.0446 5.296 23.845 26.887 3949.581 2.694 119.592 3.088 0.78 354184. 0.6710
|
|
14.42 0.0777 0.1902 0.1103 0.0451 5.351 24.090 26.467 3990.265 2.722 117.727 3.009 0.78 354511. 0.6487
|
|
19.23 0.1036 0.2470 0.1084 0.0455 5.398 24.302 26.005 4025.312 2.746 115.670 2.930 0.78 354866. 0.6263
|
|
24.03 0.1295 0.3006 0.1063 0.0458 5.436 24.473 25.497 4053.635 2.765 113.411 2.853 0.78 355249. 0.6038
|
|
28.84 0.1554 0.3511 0.1039 0.0460 5.463 24.597 24.941 4074.129 2.779 110.938 2.777 0.78 355662. 0.5812
|
|
33.65 0.1813 0.3985 0.1014 0.0461 5.479 24.666 24.335 4085.627 2.787 108.243 2.702 0.78 356104. 0.5586
|
|
38.45 0.2072 0.4430 0.0987 0.0461 5.481 24.674 23.677 4086.904 2.788 105.315 2.628 0.78 356577. 0.5359
|
|
43.26 0.2331 0.4845 0.0957 0.0460 5.467 24.612 22.964 4076.697 2.781 102.146 2.555 0.78 357080. 0.5132
|
|
48.07 0.2590 0.5233 0.0925 0.0458 5.436 24.473 22.196 4053.661 2.765 98.729 2.484 0.78 357614. 0.4904
|
|
52.87 0.2849 0.5594 0.0891 0.0454 5.386 24.248 21.371 4016.392 2.740 95.057 2.413 0.78 358180. 0.4676
|
|
57.68 0.3108 0.5928 0.0854 0.0448 5.315 23.929 20.487 3963.483 2.703 91.126 2.344 0.78 358776. 0.4448
|
|
62.48 0.3367 0.6237 0.0815 0.0440 5.222 23.507 19.546 3893.698 2.656 86.939 2.277 0.78 359405. 0.4219
|
|
67.29 0.3625 0.6521 0.0773 0.0430 5.104 22.980 18.550 3806.250 2.596 82.509 2.210 0.78 360064. 0.3990
|
|
72.10 0.3884 0.6781 0.0729 0.0418 4.963 22.343 17.504 3700.834 2.524 77.859 2.145 0.78 360756. 0.3762
|
|
76.90 0.4143 0.7017 0.0684 0.0404 4.797 21.598 16.415 3577.416 2.440 73.013 2.081 0.78 361479. 0.3534
|
|
81.71 0.4402 0.7228 0.0637 0.0388 4.608 20.744 15.286 3436.023 2.344 67.993 2.018 0.79 362234. 0.3307
|
|
86.52 0.4661 0.7415 0.0589 0.0370 4.394 19.782 14.123 3276.647 2.235 62.819 1.955 0.79 363021. 0.3079
|
|
91.32 0.4920 0.7575 0.0539 0.0350 4.156 18.711 12.929 3099.251 2.114 57.507 1.892 0.79 363840. 0.2851
|
|
96.13 0.5179 0.7706 0.0488 0.0328 3.894 17.531 11.707 2903.756 1.981 52.071 1.829 0.79 364692. 0.2622
|
|
100.94 0.5438 0.7804 0.0436 0.0304 3.608 16.242 10.460 2690.206 1.835 46.526 1.764 0.79 365575. 0.2390
|
|
105.74 0.5697 0.7860 0.0383 0.0278 3.297 14.844 9.191 2458.708 1.677 40.882 1.696 0.79 366491. 0.2154
|
|
110.55 0.5956 0.7862 0.0329 0.0250 2.963 13.340 7.903 2209.597 1.507 35.153 1.622 0.79 367439. 0.1911
|
|
115.36 0.6215 0.7788 0.0275 0.0219 2.606 11.734 6.599 1943.540 1.326 29.352 1.540 0.79 368420. 0.1658
|
|
120.16 0.6474 0.7596 0.0220 0.0188 2.228 10.031 5.282 1661.512 1.133 23.494 1.442 0.79 369432. 0.1389
|
|
124.97 0.6733 0.7202 0.0165 0.0154 1.830 8.240 3.956 1364.888 0.931 17.596 1.315 0.80 370477. 0.1096
|
|
129.78 0.6992 0.6420 0.0109 0.0119 1.415 6.372 2.626 1055.431 0.720 11.680 1.128 0.80 371554. 0.0766
|
|
134.58 0.7251 0.4720 0.0054 0.0083 0.986 4.439 1.297 735.307 0.502 5.769 0.800 0.80 372660. 0.0382
|
|
139.39 0.7510 -0.0315 -0.0002 0.0045 0.537 2.419 -0.045 400.642 0.273 -0.202 -0.051 0.80 373684. 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 0.1166 0.0479 7.002 29.422 32.119 5221.472 3.324 142.865 2.790 0.83 378800. 0.6627
|
|
5.19 0.0261 0.0622 0.1152 0.0484 7.064 29.684 31.744 5267.877 3.354 141.196 2.733 0.83 379095. 0.6454
|
|
10.39 0.0522 0.1219 0.1137 0.0487 7.118 29.907 31.323 5307.615 3.379 139.323 2.677 0.83 379420. 0.6279
|
|
15.58 0.0783 0.1790 0.1120 0.0490 7.160 30.087 30.852 5339.554 3.399 137.231 2.621 0.83 379775. 0.6101
|
|
20.77 0.1045 0.2336 0.1101 0.0492 7.191 30.218 30.330 5362.691 3.414 134.907 2.565 0.83 380160. 0.5921
|
|
25.97 0.1306 0.2857 0.1080 0.0494 7.209 30.293 29.752 5376.026 3.422 132.336 2.510 0.83 380577. 0.5738
|
|
31.16 0.1567 0.3354 0.1057 0.0494 7.213 30.307 29.115 5378.536 3.424 129.504 2.455 0.83 381027. 0.5553
|
|
36.35 0.1828 0.3826 0.1032 0.0493 7.200 30.254 28.417 5369.105 3.418 126.399 2.401 0.83 381509. 0.5364
|
|
41.55 0.2089 0.4273 0.1004 0.0491 7.170 30.126 27.655 5346.463 3.404 123.011 2.346 0.83 382025. 0.5171
|
|
46.74 0.2350 0.4696 0.0974 0.0487 7.120 29.917 26.827 5309.270 3.380 119.327 2.292 0.84 382574. 0.4975
|
|
51.93 0.2611 0.5094 0.0941 0.0483 7.049 29.617 25.930 5256.105 3.346 115.339 2.238 0.84 383158. 0.4776
|
|
57.12 0.2873 0.5468 0.0906 0.0476 6.954 29.219 24.964 5185.499 3.301 111.038 2.184 0.84 383776. 0.4572
|
|
62.32 0.3134 0.5818 0.0869 0.0468 6.834 28.715 23.925 5095.972 3.244 106.420 2.129 0.84 384427. 0.4366
|
|
67.51 0.3395 0.6143 0.0828 0.0458 6.687 28.097 22.817 4986.235 3.174 101.490 2.076 0.84 385114. 0.4155
|
|
72.70 0.3656 0.6444 0.0786 0.0446 6.511 27.360 21.643 4855.546 3.091 96.267 2.022 0.84 385834. 0.3942
|
|
77.90 0.3917 0.6721 0.0741 0.0432 6.308 26.505 20.408 4703.698 2.994 90.777 1.968 0.84 386589. 0.3726
|
|
83.09 0.4178 0.6973 0.0694 0.0416 6.076 25.529 19.121 4530.657 2.884 85.051 1.914 0.84 387379. 0.3508
|
|
88.28 0.4439 0.7201 0.0646 0.0398 5.815 24.434 17.786 4336.303 2.761 79.114 1.860 0.84 388203. 0.3288
|
|
93.48 0.4701 0.7402 0.0596 0.0378 5.526 23.218 16.410 4120.513 2.623 72.990 1.806 0.84 389062. 0.3067
|
|
98.67 0.4962 0.7576 0.0544 0.0357 5.207 21.881 14.995 3883.160 2.472 66.698 1.751 0.84 389955. 0.2843
|
|
103.86 0.5223 0.7720 0.0492 0.0333 4.860 20.421 13.547 3624.068 2.307 60.256 1.695 0.84 390883. 0.2615
|
|
109.06 0.5484 0.7824 0.0438 0.0307 4.486 18.848 12.068 3344.991 2.129 53.680 1.636 0.85 391847. 0.2383
|
|
114.25 0.5745 0.7867 0.0383 0.0280 4.090 17.187 10.562 3050.207 1.942 46.981 1.571 0.85 392845. 0.2139
|
|
119.44 0.6006 0.7839 0.0328 0.0251 3.670 15.420 9.033 2736.624 1.742 40.177 1.497 0.85 393878. 0.1886
|
|
124.64 0.6267 0.7709 0.0272 0.0221 3.226 13.556 7.483 2405.674 1.531 33.284 1.411 0.85 394946. 0.1618
|
|
129.83 0.6529 0.7418 0.0215 0.0189 2.762 11.604 5.917 2059.349 1.311 26.320 1.303 0.85 396049. 0.1329
|
|
135.02 0.6790 0.6853 0.0158 0.0156 2.280 9.581 4.341 1700.403 1.083 19.307 1.158 0.85 397186. 0.1011
|
|
140.22 0.7051 0.5774 0.0100 0.0122 1.786 7.505 2.759 1331.967 0.848 12.270 0.939 0.85 398358. 0.0654
|
|
145.41 0.7312 0.3557 0.0043 0.0088 1.284 5.396 1.178 957.622 0.610 5.241 0.558 0.86 399559. 0.0254
|
|
150.60 0.7573
|
|
|
|
|
|
|
|
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 0.1174 0.0541 9.583 37.751 36.784 7146.255 4.265 163.615 2.335 0.89 404013. 0.5935
|
|
5.50 0.0259 0.0554 0.1161 0.0544 9.649 38.010 36.401 7195.164 4.294 161.913 2.295 0.89 404321. 0.5803
|
|
11.01 0.0519 0.1088 0.1148 0.0547 9.701 38.215 35.969 7234.088 4.318 159.990 2.255 0.89 404660. 0.5669
|
|
16.51 0.0778 0.1604 0.1132 0.0549 9.737 38.356 35.482 7260.833 4.333 157.823 2.216 0.89 405032. 0.5534
|
|
22.01 0.1038 0.2102 0.1115 0.0550 9.754 38.422 34.934 7273.203 4.341 155.388 2.179 0.89 405436. 0.5397
|
|
27.52 0.1297 0.2583 0.1095 0.0550 9.749 38.402 34.322 7269.536 4.339 152.663 2.141 0.89 405875. 0.5258
|
|
33.02 0.1557 0.3047 0.1073 0.0548 9.721 38.292 33.640 7248.612 4.326 149.631 2.105 0.89 406349. 0.5117
|
|
38.52 0.1816 0.3494 0.1049 0.0545 9.668 38.084 32.886 7209.239 4.303 146.275 2.069 0.89 406858. 0.4973
|
|
44.03 0.2076 0.3925 0.1023 0.0541 9.589 37.773 32.055 7150.377 4.268 142.579 2.033 0.89 407404. 0.4825
|
|
49.53 0.2335 0.4338 0.0994 0.0535 9.482 37.354 31.144 7071.065 4.220 138.531 1.998 0.89 407986. 0.4673
|
|
55.03 0.2594 0.4734 0.0962 0.0527 9.347 36.822 30.152 6970.370 4.160 134.118 1.962 0.89 408604. 0.4516
|
|
60.54 0.2854 0.5112 0.0928 0.0518 9.182 36.172 29.076 6847.356 4.087 129.332 1.926 0.89 409258. 0.4353
|
|
66.04 0.3113 0.5471 0.0891 0.0507 8.986 35.399 27.915 6700.995 3.999 124.167 1.889 0.89 409950. 0.4184
|
|
71.54 0.3373 0.5810 0.0851 0.0494 8.757 34.497 26.670 6530.282 3.897 118.627 1.852 0.89 410677. 0.4009
|
|
77.05 0.3632 0.6129 0.0809 0.0479 8.495 33.464 25.344 6334.612 3.781 112.729 1.815 0.89 411442. 0.3829
|
|
82.55 0.3892 0.6428 0.0764 0.0463 8.199 32.298 23.944 6114.015 3.649 106.503 1.776 0.90 412242. 0.3643
|
|
88.06 0.4151 0.6706 0.0717 0.0444 7.870 31.004 22.479 5869.025 3.503 99.987 1.737 0.90 413079. 0.3452
|
|
93.56 0.4411 0.6961 0.0669 0.0424 7.510 29.584 20.956 5600.252 3.342 93.212 1.697 0.90 413952. 0.3256
|
|
99.06 0.4670 0.7192 0.0618 0.0402 7.118 28.041 19.381 5308.065 3.168 86.209 1.656 0.90 414862. 0.3056
|
|
104.57 0.4930 0.7397 0.0567 0.0378 6.695 26.373 17.761 4992.465 2.980 79.002 1.614 0.90 415808. 0.2850
|
|
110.07 0.5189 0.7573 0.0514 0.0352 6.240 24.581 16.100 4653.209 2.777 71.611 1.569 0.90 416791. 0.2639
|
|
115.57 0.5448 0.7708 0.0459 0.0325 5.758 22.681 14.401 4293.541 2.563 64.054 1.521 0.90 417810. 0.2420
|
|
121.08 0.5708 0.7750 0.0404 0.0298 5.276 20.782 12.664 3934.027 2.348 56.330 1.460 0.90 418865. 0.2178
|
|
126.58 0.5967 0.7675 0.0348 0.0270 4.791 18.874 10.895 3572.811 2.132 48.462 1.383 0.90 419957. 0.1913
|
|
132.08 0.6227 0.7473 0.0290 0.0242 4.289 16.897 9.101 3198.522 1.909 40.481 1.291 0.91 421086. 0.1632
|
|
137.59 0.6486 0.7083 0.0232 0.0213 3.774 14.868 7.287 2814.498 1.680 32.410 1.174 0.91 422250. 0.1328
|
|
143.09 0.6746 0.6407 0.0174 0.0183 3.251 12.805 5.458 2423.915 1.447 24.277 1.021 0.91 423452. 0.1000
|
|
148.59 0.7005 0.5269 0.0116 0.0154 2.724 10.732 3.623 2031.638 1.213 16.114 0.809 0.91 424688. 0.0645
|
|
154.10 0.7265 0.3340 0.0057 0.0124 2.202 8.674 1.790 1641.976 0.980 7.961 0.494 0.91 425958. 0.0277
|
|
159.60 0.7524 -0.0125 -0.0002 0.0094 1.675 6.598 -0.049 1249.002 0.745 -0.219 -0.018 0.91 427201. 0.0000
|
|
|
|
|
|
|