538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x12E (17x12E.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 0.0998 0.0436 0.005 0.310 0.263 3.662 0.035 1.168 32.515 0.07 26654. 0.5767
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0.47 0.0295 0.0658 0.0988 0.0444 0.005 0.315 0.260 3.727 0.036 1.156 31.638 0.07 26675. 0.5584
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0.95 0.0591 0.1279 0.0977 0.0452 0.005 0.321 0.257 3.792 0.036 1.144 30.753 0.07 26698. 0.5398
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1.42 0.0886 0.1863 0.0965 0.0459 0.005 0.326 0.254 3.856 0.037 1.129 29.867 0.07 26724. 0.5210
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1.90 0.1182 0.2411 0.0952 0.0467 0.005 0.331 0.250 3.918 0.037 1.114 28.983 0.07 26752. 0.5020
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2.37 0.1477 0.2922 0.0937 0.0474 0.005 0.336 0.246 3.976 0.038 1.096 28.106 0.07 26783. 0.4830
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2.85 0.1773 0.3398 0.0920 0.0480 0.005 0.341 0.242 4.030 0.038 1.076 27.239 0.07 26817. 0.4639
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3.32 0.2068 0.3840 0.0901 0.0485 0.005 0.345 0.237 4.076 0.039 1.055 26.386 0.07 26854. 0.4448
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3.79 0.2364 0.4250 0.0881 0.0490 0.006 0.348 0.232 4.114 0.039 1.031 25.548 0.07 26894. 0.4257
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4.27 0.2659 0.4627 0.0858 0.0493 0.006 0.350 0.226 4.141 0.040 1.004 24.727 0.07 26937. 0.4067
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4.74 0.2955 0.4974 0.0833 0.0495 0.006 0.351 0.219 4.156 0.040 0.975 23.923 0.07 26984. 0.3877
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5.22 0.3250 0.5292 0.0806 0.0495 0.006 0.351 0.212 4.156 0.040 0.943 23.138 0.07 27033. 0.3688
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5.69 0.3546 0.5581 0.0776 0.0493 0.006 0.350 0.204 4.141 0.040 0.908 22.369 0.07 27086. 0.3499
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6.17 0.3841 0.5843 0.0744 0.0489 0.006 0.347 0.196 4.108 0.039 0.871 21.615 0.07 27143. 0.3311
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6.64 0.4137 0.6076 0.0710 0.0483 0.005 0.343 0.187 4.056 0.039 0.830 20.872 0.07 27203. 0.3122
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7.11 0.4432 0.6280 0.0672 0.0474 0.005 0.337 0.177 3.984 0.038 0.787 20.136 0.07 27266. 0.2931
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7.59 0.4728 0.6455 0.0632 0.0463 0.005 0.329 0.166 3.890 0.037 0.740 19.401 0.07 27332. 0.2739
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8.06 0.5023 0.6596 0.0590 0.0449 0.005 0.319 0.155 3.774 0.036 0.691 18.661 0.07 27402. 0.2545
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8.54 0.5319 0.6702 0.0546 0.0433 0.005 0.307 0.144 3.637 0.035 0.639 17.905 0.07 27475. 0.2348
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9.01 0.5614 0.6765 0.0499 0.0415 0.005 0.294 0.131 3.480 0.033 0.584 17.125 0.07 27551. 0.2149
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9.49 0.5910 0.6781 0.0452 0.0394 0.004 0.279 0.119 3.306 0.032 0.529 16.305 0.07 27631. 0.1946
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9.96 0.6205 0.6738 0.0403 0.0371 0.004 0.263 0.106 3.115 0.030 0.471 15.431 0.07 27714. 0.1739
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10.43 0.6501 0.6624 0.0353 0.0346 0.004 0.246 0.093 2.909 0.028 0.413 14.480 0.07 27800. 0.1528
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10.91 0.6796 0.6420 0.0302 0.0320 0.004 0.227 0.080 2.688 0.026 0.354 13.425 0.07 27890. 0.1311
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11.38 0.7092 0.6101 0.0251 0.0292 0.003 0.207 0.066 2.454 0.023 0.294 12.225 0.07 27982. 0.1088
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11.86 0.7387 0.5625 0.0200 0.0263 0.003 0.187 0.053 2.208 0.021 0.234 10.821 0.07 28078. 0.0860
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12.33 0.7683 0.4931 0.0149 0.0232 0.003 0.165 0.039 1.951 0.019 0.175 9.122 0.07 28178. 0.0626
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12.81 0.7978 0.3917 0.0099 0.0201 0.002 0.143 0.026 1.686 0.016 0.115 6.976 0.07 28280. 0.0389
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13.28 0.8274 0.2399 0.0049 0.0169 0.002 0.120 0.013 1.415 0.014 0.057 4.121 0.07 28385. 0.0162
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13.75 0.8569 0.0022 0.0000 0.0136 0.002 0.096 0.000 1.139 0.011 0.000 0.037 0.07 28494. 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 0.1001 0.0404 0.036 1.146 1.054 27.128 0.130 4.686 17.615 0.13 53308. 0.6259
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0.95 0.0297 0.0715 0.0992 0.0412 0.037 1.170 1.043 27.678 0.132 4.641 17.099 0.13 53350. 0.6046
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1.91 0.0594 0.1386 0.0981 0.0420 0.038 1.193 1.032 28.232 0.135 4.591 16.582 0.13 53396. 0.5831
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2.86 0.0891 0.2015 0.0969 0.0428 0.039 1.216 1.019 28.780 0.137 4.534 16.066 0.13 53448. 0.5615
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3.81 0.1188 0.2601 0.0955 0.0436 0.039 1.239 1.005 29.312 0.140 4.471 15.555 0.13 53505. 0.5399
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4.77 0.1485 0.3146 0.0940 0.0444 0.040 1.260 0.989 29.816 0.142 4.401 15.050 0.13 53568. 0.5182
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5.72 0.1782 0.3651 0.0923 0.0451 0.041 1.280 0.972 30.281 0.145 4.322 14.555 0.13 53636. 0.4967
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6.67 0.2079 0.4117 0.0905 0.0457 0.041 1.297 0.952 30.691 0.147 4.235 14.070 0.13 53711. 0.4753
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7.63 0.2376 0.4547 0.0884 0.0462 0.042 1.311 0.930 31.033 0.148 4.138 13.598 0.13 53791. 0.4540
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8.58 0.2673 0.4943 0.0861 0.0466 0.042 1.322 0.906 31.291 0.149 4.032 13.138 0.13 53879. 0.4330
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9.54 0.2970 0.5306 0.0836 0.0468 0.042 1.329 0.880 31.448 0.150 3.914 12.692 0.14 53972. 0.4122
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10.49 0.3267 0.5637 0.0809 0.0469 0.042 1.331 0.851 31.489 0.150 3.786 12.260 0.14 54072. 0.3915
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11.44 0.3564 0.5940 0.0779 0.0467 0.042 1.327 0.820 31.399 0.150 3.646 11.841 0.14 54179. 0.3711
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12.40 0.3861 0.6213 0.0747 0.0464 0.042 1.317 0.786 31.163 0.149 3.494 11.434 0.14 54293. 0.3508
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13.35 0.4158 0.6459 0.0711 0.0458 0.041 1.300 0.749 30.768 0.147 3.330 11.037 0.14 54414. 0.3306
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14.30 0.4455 0.6677 0.0674 0.0450 0.041 1.276 0.709 30.203 0.144 3.154 10.649 0.14 54541. 0.3104
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15.26 0.4752 0.6866 0.0634 0.0438 0.039 1.245 0.667 29.454 0.141 2.965 10.266 0.14 54675. 0.2902
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16.21 0.5049 0.7025 0.0591 0.0425 0.038 1.205 0.622 28.522 0.136 2.765 9.886 0.14 54816. 0.2698
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17.16 0.5346 0.7152 0.0546 0.0408 0.037 1.159 0.574 27.415 0.131 2.555 9.505 0.14 54964. 0.2494
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18.12 0.5643 0.7240 0.0499 0.0389 0.035 1.105 0.525 26.142 0.125 2.337 9.116 0.14 55118. 0.2287
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19.07 0.5940 0.7286 0.0451 0.0368 0.033 1.044 0.475 24.715 0.118 2.112 8.715 0.14 55279. 0.2079
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20.02 0.6237 0.7279 0.0402 0.0345 0.031 0.978 0.423 23.142 0.110 1.882 8.292 0.14 55446. 0.1867
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20.98 0.6534 0.7207 0.0352 0.0319 0.029 0.906 0.370 21.433 0.102 1.647 7.837 0.14 55621. 0.1651
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21.93 0.6831 0.7052 0.0301 0.0292 0.026 0.828 0.317 19.596 0.094 1.410 7.335 0.14 55801. 0.1429
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22.88 0.7128 0.6786 0.0250 0.0263 0.024 0.746 0.263 17.642 0.084 1.170 6.764 0.14 55988. 0.1201
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23.84 0.7425 0.6363 0.0199 0.0232 0.021 0.659 0.209 15.584 0.074 0.931 6.089 0.14 56182. 0.0964
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24.79 0.7722 0.5709 0.0148 0.0200 0.018 0.568 0.156 13.433 0.064 0.692 5.253 0.14 56382. 0.0717
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25.74 0.8019 0.4684 0.0097 0.0167 0.015 0.474 0.103 11.207 0.054 0.456 4.150 0.14 56589. 0.0460
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26.70 0.8316 0.3006 0.0048 0.0133 0.012 0.377 0.051 8.924 0.043 0.225 2.568 0.14 56802. 0.0200
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27.65 0.8614 -0.0008 0.0000 0.0098 0.009 0.279 0.000 6.604 0.032 0.000 -0.006 0.14 57021. 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 0.1004 0.0390 0.119 2.494 2.377 88.509 0.282 10.574 12.183 0.20 79960. 0.6503
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1.43 0.0298 0.0742 0.0995 0.0399 0.121 2.547 2.355 90.417 0.288 10.474 11.813 0.20 80023. 0.6275
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2.87 0.0595 0.1438 0.0984 0.0407 0.124 2.602 2.330 92.341 0.294 10.362 11.442 0.20 80094. 0.6045
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4.30 0.0893 0.2087 0.0972 0.0416 0.126 2.655 2.301 94.250 0.300 10.236 11.074 0.20 80172. 0.5815
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5.73 0.1190 0.2692 0.0958 0.0424 0.129 2.708 2.269 96.108 0.306 10.094 10.710 0.20 80257. 0.5585
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7.17 0.1488 0.3252 0.0943 0.0432 0.131 2.758 2.234 97.877 0.312 9.936 10.352 0.20 80352. 0.5356
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8.60 0.1786 0.3770 0.0927 0.0439 0.133 2.804 2.194 99.511 0.317 9.760 10.001 0.20 80455. 0.5128
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10.03 0.2083 0.4248 0.0908 0.0445 0.135 2.845 2.150 100.964 0.321 9.564 9.659 0.20 80567. 0.4903
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11.47 0.2381 0.4688 0.0887 0.0451 0.137 2.879 2.101 102.184 0.325 9.346 9.327 0.20 80688. 0.4680
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12.90 0.2679 0.5092 0.0865 0.0455 0.138 2.905 2.047 103.117 0.328 9.106 9.005 0.20 80819. 0.4460
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14.33 0.2976 0.5462 0.0840 0.0457 0.139 2.922 1.988 103.709 0.330 8.841 8.693 0.20 80960. 0.4243
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15.77 0.3274 0.5800 0.0812 0.0458 0.139 2.927 1.923 103.905 0.331 8.552 8.393 0.20 81111. 0.4028
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17.20 0.3571 0.6109 0.0782 0.0457 0.139 2.920 1.852 103.650 0.330 8.235 8.102 0.20 81272. 0.3816
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18.63 0.3869 0.6388 0.0749 0.0454 0.138 2.899 1.774 102.894 0.328 7.892 7.821 0.20 81444. 0.3607
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20.06 0.4167 0.6641 0.0714 0.0448 0.136 2.862 1.691 101.593 0.323 7.521 7.549 0.20 81625. 0.3398
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21.50 0.4464 0.6866 0.0676 0.0440 0.134 2.809 1.601 99.702 0.317 7.123 7.285 0.20 81817. 0.3191
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22.93 0.4762 0.7063 0.0636 0.0429 0.130 2.738 1.505 97.180 0.309 6.696 7.026 0.20 82019. 0.2984
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24.36 0.5060 0.7232 0.0593 0.0415 0.126 2.649 1.403 94.021 0.299 6.243 6.770 0.20 82231. 0.2777
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25.80 0.5357 0.7369 0.0548 0.0398 0.121 2.543 1.297 90.253 0.287 5.767 6.516 0.20 82453. 0.2569
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27.23 0.5655 0.7473 0.0501 0.0379 0.115 2.420 1.186 85.910 0.273 5.274 6.260 0.20 82686. 0.2359
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28.66 0.5952 0.7535 0.0452 0.0357 0.109 2.283 1.071 81.025 0.258 4.765 5.997 0.21 82928. 0.2148
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30.10 0.6250 0.7550 0.0403 0.0334 0.101 2.131 0.954 75.628 0.241 4.244 5.722 0.21 83180. 0.1935
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31.53 0.6548 0.7504 0.0353 0.0308 0.094 1.965 0.835 69.749 0.222 3.713 5.429 0.21 83443. 0.1717
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32.96 0.6845 0.7381 0.0302 0.0280 0.085 1.787 0.714 63.422 0.202 3.177 5.107 0.21 83715. 0.1494
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34.40 0.7143 0.7152 0.0250 0.0250 0.076 1.597 0.593 56.682 0.180 2.636 4.743 0.21 83996. 0.1264
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35.83 0.7441 0.6771 0.0199 0.0219 0.066 1.397 0.471 49.570 0.158 2.096 4.311 0.21 84288. 0.1024
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37.26 0.7738 0.6158 0.0148 0.0186 0.057 1.187 0.350 42.134 0.134 1.558 3.770 0.21 84590. 0.0772
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38.70 0.8036 0.5156 0.0097 0.0152 0.046 0.970 0.231 34.431 0.110 1.026 3.040 0.21 84901. 0.0505
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40.13 0.8333 0.3419 0.0048 0.0117 0.036 0.747 0.114 26.527 0.084 0.506 1.944 0.21 85222. 0.0227
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41.56 0.8631 -0.0006 0.0000 0.0082 0.025 0.521 0.000 18.493 0.059 -0.001 -0.003 0.21 85550. 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 0.1007 0.0383 0.276 4.353 4.240 206.024 0.492 18.861 9.335 0.27 106611. 0.6654
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1.91 0.0298 0.0759 0.0998 0.0392 0.282 4.451 4.201 210.636 0.503 18.685 9.046 0.27 106696. 0.6418
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3.83 0.0596 0.1469 0.0987 0.0401 0.289 4.549 4.156 215.294 0.514 18.487 8.756 0.27 106789. 0.6179
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5.74 0.0894 0.2131 0.0976 0.0409 0.295 4.647 4.106 219.922 0.525 18.265 8.469 0.27 106893. 0.5941
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7.65 0.1192 0.2746 0.0962 0.0418 0.301 4.742 4.050 224.435 0.536 18.016 8.185 0.27 107008. 0.5702
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9.57 0.1490 0.3316 0.0947 0.0426 0.307 4.833 3.987 228.739 0.546 17.736 7.907 0.27 107134. 0.5466
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11.48 0.1788 0.3842 0.0931 0.0433 0.312 4.918 3.917 232.728 0.556 17.424 7.635 0.27 107271. 0.5231
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13.39 0.2086 0.4327 0.0912 0.0440 0.317 4.993 3.839 236.285 0.564 17.077 7.370 0.27 107421. 0.4999
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15.30 0.2384 0.4772 0.0891 0.0445 0.321 5.056 3.752 239.288 0.571 16.691 7.113 0.27 107584. 0.4769
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17.22 0.2682 0.5181 0.0869 0.0450 0.324 5.105 3.656 241.607 0.577 16.263 6.864 0.27 107759. 0.4543
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19.13 0.2980 0.5556 0.0844 0.0452 0.326 5.137 3.551 243.109 0.580 15.793 6.624 0.27 107947. 0.4321
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21.04 0.3278 0.5898 0.0816 0.0453 0.327 5.149 3.434 243.660 0.582 15.277 6.393 0.27 108149. 0.4101
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22.96 0.3576 0.6211 0.0786 0.0452 0.326 5.137 3.308 243.129 0.580 14.713 6.171 0.27 108365. 0.3885
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24.87 0.3874 0.6494 0.0753 0.0449 0.324 5.101 3.170 241.395 0.576 14.100 5.956 0.27 108594. 0.3671
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26.78 0.4172 0.6751 0.0718 0.0444 0.320 5.036 3.021 238.345 0.569 13.438 5.749 0.27 108836. 0.3459
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28.70 0.4469 0.6980 0.0680 0.0435 0.314 4.942 2.861 233.874 0.558 12.726 5.549 0.27 109093. 0.3249
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30.61 0.4767 0.7183 0.0639 0.0424 0.306 4.815 2.689 227.881 0.544 11.963 5.353 0.27 109363. 0.3039
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32.52 0.5065 0.7359 0.0596 0.0410 0.295 4.656 2.507 220.348 0.526 11.152 5.161 0.27 109646. 0.2829
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34.44 0.5363 0.7505 0.0550 0.0393 0.283 4.466 2.316 211.338 0.505 10.303 4.971 0.27 109943. 0.2619
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36.35 0.5661 0.7618 0.0503 0.0374 0.269 4.246 2.118 200.932 0.480 9.420 4.780 0.27 110254. 0.2408
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38.26 0.5959 0.7693 0.0455 0.0352 0.254 3.998 1.913 189.205 0.452 8.510 4.586 0.27 110578. 0.2196
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40.18 0.6257 0.7723 0.0405 0.0328 0.236 3.724 1.704 176.230 0.421 7.578 4.385 0.27 110915. 0.1981
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42.09 0.6555 0.7696 0.0354 0.0302 0.217 3.425 1.490 162.082 0.387 6.629 4.171 0.27 111266. 0.1763
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44.00 0.6853 0.7595 0.0303 0.0273 0.197 3.103 1.275 146.836 0.351 5.670 3.937 0.28 111629. 0.1539
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45.91 0.7151 0.7394 0.0251 0.0243 0.175 2.759 1.058 130.581 0.312 4.704 3.673 0.28 112006. 0.1308
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47.83 0.7449 0.7046 0.0200 0.0211 0.152 2.397 0.840 113.416 0.271 3.738 3.360 0.28 112396. 0.1066
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49.74 0.7747 0.6468 0.0148 0.0178 0.128 2.017 0.624 95.458 0.228 2.777 2.966 0.28 112798. 0.0811
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51.65 0.8045 0.5493 0.0098 0.0143 0.103 1.624 0.411 76.848 0.183 1.828 2.426 0.28 113214. 0.0538
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53.57 0.8343 0.3728 0.0048 0.0107 0.077 1.220 0.202 57.751 0.138 0.899 1.588 0.28 113643. 0.0247
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55.48 0.8641 -0.0023 0.0000 0.0071 0.051 0.810 -0.001 38.334 0.092 -0.004 -0.010 0.28 114082. 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 0.1011 0.0380 0.534 6.736 6.651 398.487 0.761 29.586 7.571 0.34 133260. 0.6759
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2.39 0.0298 0.0769 0.1002 0.0388 0.547 6.891 6.591 407.649 0.779 29.315 7.333 0.34 133366. 0.6517
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4.78 0.0596 0.1488 0.0992 0.0397 0.559 7.048 6.522 416.912 0.796 29.011 7.096 0.34 133483. 0.6273
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7.18 0.0894 0.2158 0.0980 0.0406 0.571 7.203 6.445 426.126 0.814 28.668 6.860 0.34 133613. 0.6029
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|
9.57 0.1192 0.2780 0.0967 0.0415 0.584 7.356 6.359 435.127 0.831 28.283 6.628 0.34 133756. 0.5786
|
|
11.96 0.1490 0.3356 0.0952 0.0423 0.595 7.501 6.261 443.725 0.847 27.850 6.400 0.34 133914. 0.5544
|
|
14.35 0.1788 0.3887 0.0935 0.0430 0.606 7.636 6.152 451.710 0.863 27.366 6.178 0.34 134086. 0.5304
|
|
16.75 0.2086 0.4377 0.0917 0.0437 0.615 7.757 6.031 458.852 0.876 26.826 5.962 0.34 134274. 0.5068
|
|
19.14 0.2385 0.4826 0.0896 0.0443 0.623 7.859 5.896 464.906 0.888 26.225 5.752 0.34 134477. 0.4835
|
|
21.53 0.2683 0.5238 0.0874 0.0447 0.630 7.939 5.746 469.613 0.897 25.559 5.550 0.34 134696. 0.4605
|
|
23.92 0.2981 0.5616 0.0849 0.0450 0.634 7.991 5.581 472.710 0.903 24.824 5.355 0.34 134932. 0.4379
|
|
26.31 0.3279 0.5961 0.0821 0.0452 0.636 8.011 5.400 473.927 0.905 24.017 5.168 0.34 135185. 0.4157
|
|
28.71 0.3577 0.6277 0.0791 0.0451 0.634 7.996 5.201 473.008 0.903 23.135 4.987 0.34 135454. 0.3937
|
|
31.10 0.3875 0.6563 0.0758 0.0448 0.630 7.940 4.985 469.705 0.897 22.175 4.814 0.34 135741. 0.3721
|
|
33.49 0.4173 0.6823 0.0723 0.0442 0.622 7.840 4.752 463.797 0.886 21.137 4.647 0.34 136045. 0.3507
|
|
35.88 0.4471 0.7057 0.0684 0.0434 0.610 7.693 4.501 455.073 0.869 20.019 4.486 0.34 136366. 0.3294
|
|
38.28 0.4769 0.7264 0.0643 0.0422 0.595 7.494 4.231 443.328 0.847 18.821 4.329 0.34 136704. 0.3083
|
|
40.67 0.5067 0.7445 0.0600 0.0408 0.575 7.244 3.945 428.520 0.818 17.548 4.176 0.34 137059. 0.2871
|
|
43.06 0.5365 0.7597 0.0554 0.0391 0.551 6.944 3.645 410.771 0.785 16.212 4.025 0.34 137430. 0.2660
|
|
45.45 0.5663 0.7718 0.0507 0.0372 0.523 6.597 3.333 390.234 0.745 14.824 3.874 0.34 137819. 0.2448
|
|
47.84 0.5961 0.7804 0.0458 0.0350 0.492 6.205 3.011 367.059 0.701 13.392 3.720 0.34 138224. 0.2235
|
|
50.24 0.6259 0.7846 0.0408 0.0325 0.458 5.771 2.681 341.389 0.652 11.926 3.562 0.34 138646. 0.2019
|
|
52.63 0.6558 0.7834 0.0357 0.0299 0.420 5.297 2.346 313.368 0.598 10.434 3.395 0.34 139085. 0.1800
|
|
55.02 0.6856 0.7752 0.0305 0.0270 0.380 4.787 2.006 283.151 0.541 8.924 3.214 0.34 139540. 0.1576
|
|
57.41 0.7154 0.7575 0.0253 0.0239 0.336 4.242 1.665 250.910 0.479 7.405 3.009 0.34 140011. 0.1344
|
|
59.81 0.7452 0.7255 0.0201 0.0207 0.291 3.666 1.323 216.845 0.414 5.885 2.767 0.35 140499. 0.1102
|
|
62.20 0.7750 0.6711 0.0149 0.0173 0.243 3.063 0.983 181.192 0.346 4.373 2.461 0.35 141002. 0.0845
|
|
64.59 0.8048 0.5768 0.0098 0.0137 0.193 2.438 0.648 144.231 0.275 2.881 2.037 0.35 141523. 0.0568
|
|
66.98 0.8346 0.4001 0.0049 0.0101 0.143 1.797 0.319 106.296 0.203 1.420 1.363 0.35 142059. 0.0267
|
|
69.37 0.8644 0.0006 0.0000 0.0065 0.091 1.145 0.000 67.721 0.129 0.001 0.002 0.35 142607. 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 0.1016 0.0378 0.920 9.660 9.622 685.700 1.091 42.801 6.365 0.40 159906. 0.6835
|
|
2.87 0.0298 0.0776 0.1007 0.0387 0.941 9.886 9.537 701.798 1.117 42.420 6.164 0.40 160033. 0.6589
|
|
5.74 0.0596 0.1501 0.0997 0.0396 0.963 10.116 9.440 718.096 1.143 41.990 5.963 0.40 160174. 0.6342
|
|
8.62 0.0895 0.2177 0.0985 0.0405 0.985 10.345 9.331 734.330 1.169 41.504 5.763 0.40 160330. 0.6094
|
|
11.49 0.1193 0.2804 0.0972 0.0414 1.006 10.568 9.208 750.210 1.194 40.957 5.567 0.40 160502. 0.5848
|
|
14.36 0.1491 0.3383 0.0958 0.0422 1.026 10.782 9.070 765.404 1.218 40.342 5.375 0.40 160691. 0.5603
|
|
17.23 0.1789 0.3918 0.0941 0.0430 1.045 10.981 8.914 779.540 1.241 39.651 5.187 0.40 160898. 0.5361
|
|
20.10 0.2087 0.4410 0.0923 0.0437 1.062 11.160 8.741 792.213 1.261 38.878 5.004 0.40 161124. 0.5121
|
|
22.98 0.2386 0.4863 0.0902 0.0443 1.077 11.312 8.547 802.989 1.278 38.016 4.828 0.40 161368. 0.4886
|
|
25.85 0.2684 0.5277 0.0880 0.0447 1.088 11.430 8.332 811.415 1.291 37.060 4.657 0.40 161632. 0.4654
|
|
28.72 0.2982 0.5658 0.0855 0.0450 1.096 11.509 8.094 817.021 1.300 36.003 4.493 0.41 161915. 0.4425
|
|
31.59 0.3280 0.6005 0.0827 0.0452 1.099 11.542 7.833 819.338 1.304 34.840 4.336 0.41 162219. 0.4201
|
|
34.46 0.3578 0.6323 0.0797 0.0451 1.097 11.522 7.546 817.906 1.302 33.567 4.185 0.41 162543. 0.3980
|
|
37.34 0.3877 0.6612 0.0764 0.0448 1.089 11.443 7.235 812.292 1.293 32.180 4.040 0.41 162888. 0.3761
|
|
40.21 0.4175 0.6875 0.0728 0.0442 1.076 11.299 6.897 802.103 1.277 30.678 3.900 0.41 163253. 0.3546
|
|
43.08 0.4473 0.7111 0.0690 0.0434 1.055 11.086 6.533 786.966 1.252 29.060 3.765 0.41 163639. 0.3332
|
|
45.95 0.4771 0.7322 0.0649 0.0423 1.028 10.798 6.143 766.519 1.220 27.324 3.635 0.41 164045. 0.3119
|
|
48.82 0.5069 0.7508 0.0605 0.0408 0.993 10.434 5.728 740.677 1.179 25.478 3.508 0.41 164472. 0.2906
|
|
51.69 0.5368 0.7666 0.0559 0.0391 0.952 9.997 5.292 709.645 1.129 23.540 3.383 0.41 164918. 0.2694
|
|
54.57 0.5666 0.7794 0.0511 0.0371 0.903 9.490 4.839 673.691 1.072 21.524 3.258 0.41 165386. 0.2481
|
|
57.44 0.5964 0.7887 0.0462 0.0349 0.849 8.918 4.372 633.074 1.008 19.445 3.132 0.41 165873. 0.2267
|
|
60.31 0.6262 0.7939 0.0411 0.0324 0.789 8.284 3.893 588.046 0.936 17.316 3.003 0.41 166380. 0.2051
|
|
63.18 0.6560 0.7940 0.0360 0.0297 0.723 7.591 3.406 538.860 0.858 15.148 2.866 0.41 166906. 0.1831
|
|
66.05 0.6859 0.7874 0.0307 0.0268 0.651 6.843 2.912 485.788 0.773 12.953 2.719 0.41 167453. 0.1606
|
|
68.93 0.7157 0.7715 0.0255 0.0237 0.575 6.045 2.416 429.132 0.683 10.745 2.553 0.41 168019. 0.1374
|
|
71.80 0.7455 0.7419 0.0203 0.0204 0.495 5.202 1.919 369.248 0.588 8.535 2.357 0.41 168605. 0.1130
|
|
74.67 0.7753 0.6901 0.0150 0.0169 0.411 4.318 1.425 306.556 0.488 6.338 2.108 0.42 169210. 0.0871
|
|
77.54 0.8051 0.5984 0.0099 0.0133 0.324 3.403 0.937 241.555 0.384 4.170 1.760 0.42 169835. 0.0590
|
|
80.41 0.8350 0.4208 0.0049 0.0096 0.234 2.463 0.460 174.837 0.278 2.047 1.194 0.42 170478. 0.0280
|
|
83.29 0.8648 -0.0053 0.0000 0.0059 0.143 1.507 -0.003 106.991 0.170 -0.015 -0.014 0.42 171137. 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 0.1022 0.0378 1.460 13.148 13.168 1088.861 1.485 58.572 5.485 0.47 186549. 0.6890
|
|
3.35 0.0298 0.0780 0.1013 0.0387 1.495 13.462 13.055 1114.872 1.521 58.068 5.311 0.47 186696. 0.6643
|
|
6.70 0.0596 0.1509 0.1003 0.0396 1.530 13.780 12.926 1141.241 1.557 57.497 5.137 0.47 186861. 0.6394
|
|
10.05 0.0895 0.2188 0.0992 0.0405 1.566 14.098 12.781 1167.547 1.593 56.851 4.965 0.47 187043. 0.6145
|
|
13.40 0.1193 0.2818 0.0979 0.0414 1.600 14.409 12.617 1193.318 1.628 56.120 4.796 0.47 187244. 0.5897
|
|
16.75 0.1491 0.3400 0.0964 0.0423 1.633 14.707 12.431 1218.016 1.662 55.295 4.629 0.47 187465. 0.5650
|
|
20.10 0.1789 0.3937 0.0948 0.0431 1.664 14.985 12.223 1241.038 1.693 54.367 4.467 0.47 187707. 0.5406
|
|
23.45 0.2087 0.4431 0.0930 0.0438 1.692 15.235 11.989 1261.726 1.721 53.325 4.310 0.47 187970. 0.5166
|
|
26.80 0.2386 0.4885 0.0910 0.0444 1.716 15.448 11.727 1279.376 1.745 52.161 4.157 0.47 188255. 0.4928
|
|
30.15 0.2684 0.5302 0.0887 0.0449 1.734 15.616 11.436 1293.249 1.764 50.865 4.011 0.47 188563. 0.4695
|
|
33.50 0.2982 0.5684 0.0862 0.0452 1.747 15.728 11.113 1302.585 1.777 49.430 3.870 0.47 188895. 0.4465
|
|
36.86 0.3280 0.6033 0.0834 0.0454 1.752 15.777 10.757 1306.620 1.782 47.848 3.734 0.47 189249. 0.4240
|
|
40.21 0.3578 0.6353 0.0804 0.0453 1.750 15.753 10.367 1304.607 1.780 46.113 3.604 0.47 189628. 0.4017
|
|
43.56 0.3876 0.6645 0.0771 0.0450 1.738 15.647 9.942 1295.842 1.768 44.220 3.480 0.47 190030. 0.3798
|
|
46.91 0.4175 0.6910 0.0735 0.0444 1.716 15.452 9.480 1279.687 1.746 42.168 3.360 0.47 190457. 0.3581
|
|
50.26 0.4473 0.7149 0.0697 0.0436 1.684 15.160 8.982 1255.538 1.713 39.953 3.245 0.48 190907. 0.3366
|
|
53.61 0.4771 0.7364 0.0655 0.0425 1.640 14.765 8.447 1222.807 1.668 37.574 3.133 0.48 191382. 0.3153
|
|
56.96 0.5069 0.7553 0.0611 0.0410 1.584 14.264 7.879 1181.333 1.612 35.044 3.025 0.48 191880. 0.2939
|
|
60.31 0.5367 0.7717 0.0565 0.0393 1.517 13.662 7.280 1131.432 1.543 32.383 2.919 0.48 192402. 0.2726
|
|
63.66 0.5666 0.7851 0.0517 0.0373 1.440 12.963 6.658 1073.536 1.465 29.615 2.813 0.48 192947. 0.2513
|
|
67.01 0.5964 0.7951 0.0467 0.0350 1.352 12.172 6.016 1008.062 1.375 26.758 2.707 0.48 193516. 0.2298
|
|
70.36 0.6262 0.8013 0.0416 0.0325 1.254 11.295 5.357 935.418 1.276 23.830 2.598 0.48 194108. 0.2081
|
|
73.71 0.6560 0.8025 0.0364 0.0297 1.148 10.336 4.687 856.012 1.168 20.847 2.483 0.48 194723. 0.1861
|
|
77.06 0.6858 0.7973 0.0311 0.0267 1.033 9.301 4.008 770.287 1.051 17.828 2.360 0.48 195360. 0.1636
|
|
80.41 0.7157 0.7832 0.0258 0.0236 0.910 8.195 3.325 678.732 0.926 14.788 2.222 0.48 196021. 0.1402
|
|
83.76 0.7455 0.7558 0.0205 0.0202 0.780 7.027 2.641 581.926 0.794 11.745 2.058 0.48 196705. 0.1158
|
|
87.11 0.7753 0.7067 0.0152 0.0167 0.644 5.802 1.960 480.552 0.656 8.720 1.850 0.48 197411. 0.0897
|
|
90.46 0.8051 0.6177 0.0100 0.0130 0.503 4.533 1.289 375.427 0.512 5.734 1.558 0.49 198140. 0.0612
|
|
93.81 0.8349 0.4407 0.0049 0.0093 0.359 3.230 0.632 267.519 0.365 2.811 1.071 0.49 198891. 0.0295
|
|
97.16 0.8648 -0.0077 0.0000 0.0055 0.212 1.905 -0.006 157.779 0.215 -0.028 -0.018 0.49 199658. 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 0.1028 0.0379 2.187 17.233 17.307 1631.066 1.947 76.979 4.813 0.54 213187. 0.6931
|
|
3.83 0.0298 0.0782 0.1019 0.0389 2.240 17.651 17.164 1670.616 1.994 76.345 4.660 0.54 213356. 0.6683
|
|
7.65 0.0596 0.1512 0.1010 0.0398 2.294 18.075 17.002 1710.776 2.042 75.624 4.508 0.54 213543. 0.6434
|
|
11.48 0.0894 0.2192 0.0999 0.0407 2.348 18.499 16.817 1750.907 2.090 74.804 4.357 0.54 213751. 0.6185
|
|
15.31 0.1192 0.2823 0.0986 0.0416 2.401 18.915 16.608 1790.295 2.137 73.874 4.208 0.54 213981. 0.5936
|
|
19.13 0.1490 0.3407 0.0972 0.0425 2.452 19.315 16.371 1828.118 2.182 72.819 4.062 0.54 214234. 0.5689
|
|
22.96 0.1788 0.3945 0.0956 0.0433 2.499 19.688 16.103 1863.452 2.224 71.628 3.920 0.54 214510. 0.5445
|
|
26.78 0.2086 0.4440 0.0939 0.0441 2.542 20.024 15.802 1895.289 2.262 70.286 3.782 0.54 214811. 0.5204
|
|
30.61 0.2384 0.4896 0.0918 0.0447 2.578 20.312 15.464 1922.553 2.295 68.782 3.648 0.54 215137. 0.4966
|
|
34.44 0.2682 0.5314 0.0896 0.0452 2.607 20.540 15.086 1944.110 2.321 67.102 3.520 0.54 215489. 0.4732
|
|
38.26 0.2980 0.5697 0.0871 0.0456 2.627 20.695 14.667 1958.798 2.338 65.237 3.396 0.54 215868. 0.4502
|
|
42.09 0.3278 0.6048 0.0844 0.0457 2.636 20.766 14.203 1965.448 2.346 63.176 3.278 0.54 216273. 0.4276
|
|
45.92 0.3576 0.6369 0.0813 0.0457 2.632 20.739 13.694 1962.918 2.343 60.910 3.164 0.54 216706. 0.4053
|
|
49.74 0.3874 0.6663 0.0780 0.0454 2.615 20.604 13.137 1950.132 2.328 58.434 3.055 0.54 217166. 0.3834
|
|
53.57 0.4172 0.6931 0.0744 0.0448 2.583 20.350 12.532 1926.112 2.299 55.744 2.951 0.54 217654. 0.3617
|
|
57.40 0.4470 0.7173 0.0706 0.0440 2.534 19.968 11.879 1889.944 2.256 52.837 2.851 0.54 218169. 0.3401
|
|
61.22 0.4768 0.7391 0.0664 0.0428 2.468 19.448 11.176 1840.728 2.197 49.712 2.754 0.54 218711. 0.3187
|
|
65.05 0.5066 0.7585 0.0619 0.0414 2.385 18.787 10.427 1778.170 2.123 46.381 2.660 0.54 219280. 0.2973
|
|
68.88 0.5364 0.7753 0.0573 0.0396 2.283 17.990 9.639 1702.730 2.032 42.876 2.568 0.55 219877. 0.2760
|
|
72.70 0.5662 0.7893 0.0524 0.0376 2.166 17.064 8.818 1615.057 1.928 39.224 2.477 0.55 220500. 0.2546
|
|
76.53 0.5960 0.8002 0.0473 0.0353 2.033 16.015 7.970 1515.792 1.809 35.452 2.385 0.55 221149. 0.2331
|
|
80.35 0.6258 0.8072 0.0422 0.0327 1.885 14.850 7.101 1405.555 1.678 31.584 2.291 0.55 221825. 0.2114
|
|
84.18 0.6556 0.8095 0.0369 0.0299 1.723 13.576 6.214 1284.972 1.534 27.642 2.194 0.55 222528. 0.1893
|
|
88.01 0.6854 0.8057 0.0316 0.0269 1.548 12.200 5.317 1154.711 1.378 23.648 2.088 0.55 223256. 0.1667
|
|
91.83 0.7152 0.7934 0.0262 0.0236 1.362 10.729 4.412 1015.526 1.212 19.625 1.971 0.55 224010. 0.1433
|
|
95.66 0.7449 0.7682 0.0208 0.0202 1.164 9.174 3.507 868.294 1.036 15.598 1.832 0.55 224791. 0.1187
|
|
99.49 0.7747 0.7220 0.0155 0.0166 0.958 7.544 2.606 714.061 0.852 11.591 1.655 0.55 225597. 0.0925
|
|
103.31 0.8045 0.6365 0.0102 0.0129 0.743 5.854 1.717 554.081 0.661 7.636 1.405 0.56 226429. 0.0637
|
|
107.14 0.8343 0.4623 0.0050 0.0091 0.523 4.119 0.846 389.837 0.465 3.762 0.984 0.56 227286. 0.0313
|
|
110.97 0.8641 0.0001 0.0000 0.0052 0.299 2.354 0.000 222.805 0.266 0.000 0.000 0.56 228162. 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 0.1035 0.0382 3.135 21.957 22.059 2337.974 2.481 98.118 4.279 0.61 239820. 0.6958
|
|
4.30 0.0298 0.0782 0.1027 0.0391 3.212 22.497 21.887 2395.485 2.542 97.353 4.144 0.61 240010. 0.6711
|
|
8.61 0.0596 0.1512 0.1018 0.0401 3.291 23.046 21.690 2454.004 2.604 96.478 4.009 0.61 240221. 0.6463
|
|
12.91 0.0894 0.2193 0.1007 0.0410 3.369 23.597 21.466 2512.605 2.666 95.479 3.875 0.61 240455. 0.6215
|
|
17.21 0.1191 0.2824 0.0995 0.0420 3.447 24.138 21.209 2570.247 2.727 94.339 3.743 0.61 240713. 0.5967
|
|
21.51 0.1489 0.3408 0.0982 0.0429 3.521 24.659 20.917 2625.719 2.786 93.041 3.613 0.61 240997. 0.5721
|
|
25.82 0.1787 0.3947 0.0966 0.0437 3.591 25.147 20.586 2677.674 2.841 91.567 3.487 0.61 241308. 0.5477
|
|
30.12 0.2085 0.4443 0.0948 0.0445 3.654 25.588 20.211 2724.625 2.891 89.899 3.365 0.61 241646. 0.5236
|
|
34.42 0.2383 0.4899 0.0929 0.0452 3.708 25.967 19.789 2764.982 2.934 88.021 3.246 0.61 242014. 0.4999
|
|
38.73 0.2681 0.5318 0.0906 0.0457 3.751 26.269 19.316 2797.087 2.968 85.916 3.132 0.61 242410. 0.4765
|
|
43.03 0.2979 0.5702 0.0882 0.0461 3.781 26.476 18.788 2819.226 2.991 83.569 3.023 0.61 242837. 0.4535
|
|
47.33 0.3276 0.6054 0.0854 0.0462 3.795 26.575 18.203 2829.684 3.002 80.968 2.918 0.61 243293. 0.4309
|
|
51.63 0.3574 0.6377 0.0824 0.0462 3.791 26.547 17.559 2826.789 2.999 78.101 2.817 0.61 243781. 0.4087
|
|
55.94 0.3872 0.6673 0.0791 0.0459 3.767 26.380 16.852 2808.964 2.980 74.960 2.721 0.61 244299. 0.3867
|
|
60.24 0.4170 0.6943 0.0755 0.0453 3.721 26.059 16.084 2774.769 2.944 71.540 2.629 0.61 244848. 0.3650
|
|
64.54 0.4468 0.7188 0.0716 0.0445 3.651 25.572 15.251 2722.890 2.889 67.838 2.541 0.61 245428. 0.3434
|
|
68.85 0.4766 0.7410 0.0674 0.0433 3.556 24.906 14.355 2652.009 2.814 63.851 2.455 0.61 246038. 0.3220
|
|
73.15 0.5063 0.7608 0.0629 0.0418 3.435 24.057 13.398 2561.633 2.718 59.595 2.372 0.61 246679. 0.3006
|
|
77.45 0.5361 0.7781 0.0581 0.0401 3.289 23.031 12.390 2452.398 2.602 55.109 2.291 0.61 247351. 0.2792
|
|
81.75 0.5659 0.7926 0.0532 0.0380 3.118 21.837 11.338 2325.248 2.467 50.430 2.212 0.61 248052. 0.2578
|
|
86.06 0.5957 0.8042 0.0481 0.0356 2.925 20.484 10.250 2181.120 2.314 45.592 2.132 0.62 248783. 0.2362
|
|
90.36 0.6255 0.8120 0.0429 0.0330 2.710 18.979 9.134 2020.930 2.144 40.626 2.050 0.62 249544. 0.2145
|
|
94.66 0.6553 0.8154 0.0375 0.0302 2.475 17.333 7.995 1845.589 1.958 35.562 1.965 0.62 250334. 0.1923
|
|
98.97 0.6851 0.8129 0.0321 0.0271 2.221 15.553 6.841 1656.079 1.757 30.428 1.874 0.62 251153. 0.1696
|
|
103.27 0.7148 0.8021 0.0266 0.0237 1.949 13.650 5.677 1453.501 1.542 25.253 1.772 0.62 252002. 0.1461
|
|
107.57 0.7446 0.7789 0.0212 0.0202 1.662 11.637 4.512 1239.139 1.315 20.070 1.652 0.62 252879. 0.1214
|
|
111.87 0.7744 0.7351 0.0157 0.0166 1.361 9.528 3.352 1014.526 1.076 14.911 1.499 0.62 253786. 0.0950
|
|
116.18 0.8042 0.6524 0.0104 0.0128 1.048 7.339 2.207 781.504 0.829 9.817 1.281 0.62 254722. 0.0659
|
|
120.48 0.8340 0.4794 0.0051 0.0089 0.727 5.093 1.085 542.265 0.575 4.827 0.908 0.63 255685. 0.0327
|
|
124.78 0.8638 -0.0038 0.0000 0.0049 0.401 2.808 -0.005 298.968 0.317 -0.020 -0.007 0.63 256670. 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 0.1043 0.0386 4.349 27.409 27.450 3242.839 3.097 122.096 3.839 0.67 266448. 0.6963
|
|
4.78 0.0298 0.0779 0.1036 0.0396 4.456 28.085 27.250 3322.730 3.173 121.209 3.720 0.67 266657. 0.6722
|
|
9.56 0.0595 0.1508 0.1027 0.0405 4.565 28.774 27.021 3404.341 3.251 120.189 3.600 0.67 266891. 0.6478
|
|
14.33 0.0893 0.2187 0.1017 0.0415 4.675 29.468 26.757 3486.393 3.329 119.017 3.481 0.67 267151. 0.6233
|
|
19.11 0.1191 0.2818 0.1006 0.0425 4.784 30.153 26.455 3567.449 3.407 117.671 3.363 0.67 267438. 0.5989
|
|
23.89 0.1488 0.3401 0.0992 0.0434 4.889 30.815 26.108 3645.807 3.481 116.127 3.248 0.67 267753. 0.5745
|
|
28.67 0.1786 0.3940 0.0977 0.0443 4.988 31.438 25.711 3719.537 3.552 114.363 3.135 0.67 268098. 0.5503
|
|
33.44 0.2083 0.4436 0.0960 0.0451 5.078 32.004 25.260 3786.502 3.616 112.355 3.026 0.67 268475. 0.5264
|
|
38.22 0.2381 0.4892 0.0941 0.0458 5.155 32.494 24.748 3844.395 3.671 110.080 2.920 0.67 268883. 0.5028
|
|
43.00 0.2679 0.5312 0.0919 0.0463 5.218 32.886 24.172 3890.798 3.715 107.518 2.818 0.67 269324. 0.4796
|
|
47.78 0.2976 0.5697 0.0894 0.0467 5.261 33.160 23.527 3923.235 3.746 104.648 2.720 0.68 269798. 0.4567
|
|
52.55 0.3274 0.6051 0.0867 0.0469 5.283 33.296 22.809 3939.268 3.762 101.453 2.626 0.68 270306. 0.4342
|
|
57.33 0.3572 0.6375 0.0837 0.0469 5.279 33.272 22.014 3936.512 3.759 97.920 2.537 0.68 270848. 0.4120
|
|
62.11 0.3869 0.6673 0.0804 0.0466 5.247 33.071 21.141 3912.735 3.736 94.036 2.451 0.68 271424. 0.3901
|
|
66.89 0.4167 0.6945 0.0767 0.0460 5.184 32.676 20.188 3865.905 3.692 89.796 2.369 0.68 272035. 0.3684
|
|
71.66 0.4465 0.7194 0.0728 0.0452 5.088 32.069 19.154 3794.169 3.623 85.195 2.290 0.68 272679. 0.3469
|
|
76.44 0.4762 0.7418 0.0686 0.0440 4.956 31.237 18.037 3695.692 3.529 80.230 2.214 0.68 273358. 0.3255
|
|
81.22 0.5060 0.7620 0.0640 0.0425 4.787 30.172 16.844 3569.661 3.409 74.920 2.140 0.68 274071. 0.3041
|
|
86.00 0.5358 0.7798 0.0592 0.0407 4.582 28.881 15.583 3416.916 3.263 69.311 2.068 0.68 274817. 0.2827
|
|
90.77 0.5655 0.7950 0.0542 0.0386 4.343 27.375 14.265 3238.794 3.093 63.452 1.998 0.68 275597. 0.2612
|
|
95.55 0.5953 0.8072 0.0490 0.0362 4.072 25.666 12.902 3036.626 2.900 57.386 1.927 0.68 276409. 0.2396
|
|
100.33 0.6250 0.8160 0.0437 0.0335 3.771 23.765 11.500 2811.709 2.685 51.153 1.855 0.69 277254. 0.2178
|
|
105.11 0.6548 0.8204 0.0383 0.0306 3.440 21.683 10.070 2565.346 2.450 44.790 1.780 0.69 278132. 0.1956
|
|
109.88 0.6846 0.8191 0.0328 0.0274 3.083 19.431 8.618 2298.923 2.195 38.333 1.700 0.69 279042. 0.1728
|
|
114.66 0.7143 0.8099 0.0272 0.0240 2.701 17.023 7.154 2013.996 1.923 31.821 1.611 0.69 279984. 0.1492
|
|
119.44 0.7441 0.7886 0.0216 0.0204 2.296 14.474 5.686 1712.393 1.635 25.292 1.506 0.69 280959. 0.1243
|
|
124.22 0.7739 0.7473 0.0161 0.0166 1.873 11.802 4.225 1396.338 1.333 18.792 1.372 0.69 281965. 0.0976
|
|
128.99 0.8036 0.6674 0.0106 0.0127 1.433 9.032 2.780 1068.547 1.020 12.367 1.180 0.69 283004. 0.0681
|
|
133.77 0.8334 0.4959 0.0052 0.0087 0.982 6.190 1.365 732.316 0.699 6.073 0.846 0.70 284073. 0.0342
|
|
138.55 0.8632 -0.0070 0.0000 0.0047 0.524 3.305 -0.010 390.976 0.373 -0.044 -0.011 0.70 285165. 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 0.1052 0.0398 5.969 34.201 33.498 4451.083 3.864 149.001 3.414 0.74 293068. 0.6839
|
|
5.25 0.0297 0.0763 0.1045 0.0407 6.106 34.989 33.277 4553.582 3.953 148.018 3.315 0.74 293298. 0.6619
|
|
10.50 0.0595 0.1480 0.1037 0.0417 6.247 35.794 33.021 4658.377 4.044 146.878 3.215 0.74 293554. 0.6396
|
|
15.75 0.0892 0.2151 0.1028 0.0426 6.388 36.605 32.724 4763.829 4.136 145.558 3.116 0.74 293839. 0.6170
|
|
20.99 0.1189 0.2777 0.1017 0.0436 6.528 37.406 32.380 4868.102 4.226 144.027 3.017 0.74 294154. 0.5943
|
|
26.24 0.1486 0.3359 0.1005 0.0445 6.664 38.181 31.983 4969.014 4.314 142.258 2.919 0.74 294500. 0.5715
|
|
31.49 0.1784 0.3898 0.0990 0.0453 6.791 38.912 31.524 5064.096 4.396 140.219 2.823 0.74 294879. 0.5488
|
|
36.74 0.2081 0.4397 0.0974 0.0461 6.907 39.576 30.998 5150.602 4.471 137.878 2.730 0.74 295293. 0.5261
|
|
41.99 0.2378 0.4857 0.0955 0.0468 7.008 40.152 30.397 5225.551 4.536 135.207 2.638 0.74 295742. 0.5036
|
|
47.24 0.2675 0.5281 0.0934 0.0473 7.088 40.615 29.716 5285.776 4.589 132.175 2.550 0.74 296226. 0.4812
|
|
52.49 0.2973 0.5670 0.0909 0.0477 7.145 40.940 28.947 5327.989 4.625 128.758 2.464 0.74 296748. 0.4590
|
|
57.74 0.3270 0.6028 0.0882 0.0479 7.173 41.100 28.087 5348.825 4.643 124.931 2.382 0.74 297307. 0.4369
|
|
62.98 0.3567 0.6357 0.0852 0.0478 7.168 41.070 27.131 5344.943 4.640 120.677 2.302 0.74 297903. 0.4151
|
|
68.23 0.3864 0.6658 0.0819 0.0475 7.125 40.825 26.075 5313.114 4.612 115.981 2.226 0.75 298537. 0.3935
|
|
73.48 0.4162 0.6934 0.0783 0.0470 7.041 40.343 24.918 5250.350 4.558 110.835 2.153 0.75 299209. 0.3720
|
|
78.73 0.4459 0.7186 0.0743 0.0461 6.911 39.602 23.659 5153.885 4.474 105.235 2.082 0.75 299918. 0.3506
|
|
83.98 0.4756 0.7415 0.0700 0.0449 6.733 38.581 22.297 5020.991 4.359 99.175 2.014 0.75 300665. 0.3292
|
|
89.23 0.5053 0.7622 0.0655 0.0434 6.504 37.268 20.836 4850.212 4.211 92.677 1.948 0.75 301449. 0.3079
|
|
94.48 0.5351 0.7805 0.0606 0.0415 6.226 35.673 19.289 4642.545 4.030 85.796 1.884 0.75 302270. 0.2865
|
|
99.72 0.5648 0.7963 0.0555 0.0394 5.900 33.808 17.669 4399.818 3.820 78.593 1.821 0.75 303127. 0.2650
|
|
104.97 0.5945 0.8093 0.0502 0.0369 5.530 31.688 15.990 4123.925 3.580 71.123 1.759 0.75 304020. 0.2434
|
|
110.22 0.6243 0.8189 0.0448 0.0342 5.118 29.327 14.261 3816.757 3.313 63.435 1.695 0.75 304949. 0.2216
|
|
115.47 0.6540 0.8243 0.0393 0.0311 4.667 26.742 12.495 3480.252 3.021 55.577 1.628 0.76 305914. 0.1993
|
|
120.72 0.6837 0.8241 0.0336 0.0279 4.179 23.947 10.700 3116.543 2.706 47.593 1.557 0.76 306914. 0.1763
|
|
125.97 0.7134 0.8160 0.0279 0.0244 3.658 20.962 8.887 2728.105 2.368 39.531 1.478 0.76 307949. 0.1525
|
|
131.22 0.7432 0.7956 0.0222 0.0207 3.108 17.811 7.068 2317.940 2.012 31.439 1.383 0.76 309019. 0.1273
|
|
136.47 0.7729 0.7545 0.0165 0.0169 2.534 14.521 5.255 1889.750 1.641 23.372 1.261 0.76 310124. 0.1001
|
|
141.71 0.8026 0.6733 0.0109 0.0130 1.942 11.127 3.460 1448.082 1.257 15.390 1.084 0.76 311264. 0.0698
|
|
146.96 0.8323 0.4974 0.0053 0.0089 1.339 7.672 1.699 998.395 0.867 7.559 0.772 0.77 312438. 0.0348
|
|
152.21 0.8621 -0.0075 0.0000 0.0049 0.732 4.197 -0.013 546.167 0.474 -0.060 -0.011 0.77 313637. 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 0.1061 0.0431 8.387 44.050 40.207 6253.940 4.977 178.843 2.916 0.81 319679. 0.6401
|
|
5.72 0.0297 0.0713 0.1055 0.0439 8.551 44.911 39.974 6376.221 5.074 177.804 2.844 0.81 319929. 0.6223
|
|
11.43 0.0594 0.1389 0.1048 0.0448 8.717 45.785 39.701 6500.262 5.173 176.589 2.770 0.81 320207. 0.6042
|
|
17.15 0.0890 0.2027 0.1040 0.0457 8.883 46.655 39.381 6623.823 5.271 175.167 2.697 0.81 320516. 0.5858
|
|
22.87 0.1187 0.2630 0.1030 0.0465 9.044 47.504 39.007 6744.387 5.367 173.502 2.623 0.81 320858. 0.5671
|
|
28.58 0.1484 0.3196 0.1018 0.0473 9.198 48.312 38.569 6859.078 5.458 171.554 2.550 0.81 321235. 0.5483
|
|
34.30 0.1781 0.3727 0.1005 0.0480 9.340 49.056 38.059 6964.714 5.542 169.285 2.479 0.81 321648. 0.5293
|
|
40.02 0.2078 0.4224 0.0989 0.0486 9.465 49.712 37.467 7057.841 5.616 166.652 2.408 0.81 322098. 0.5102
|
|
45.73 0.2374 0.4688 0.0971 0.0492 9.568 50.254 36.784 7134.824 5.678 163.616 2.338 0.81 322587. 0.4909
|
|
51.45 0.2671 0.5121 0.0950 0.0496 9.644 50.656 36.002 7191.878 5.723 160.137 2.271 0.81 323115. 0.4716
|
|
57.17 0.2968 0.5524 0.0927 0.0498 9.689 50.891 35.113 7225.145 5.750 156.181 2.204 0.81 323684. 0.4521
|
|
62.88 0.3265 0.5898 0.0900 0.0498 9.697 50.930 34.109 7230.730 5.754 151.717 2.140 0.81 324294. 0.4326
|
|
68.60 0.3561 0.6245 0.0871 0.0497 9.662 50.747 32.985 7204.803 5.733 146.717 2.077 0.81 324944. 0.4128
|
|
74.32 0.3858 0.6565 0.0838 0.0492 9.580 50.317 31.737 7143.668 5.685 141.164 2.015 0.81 325636. 0.3930
|
|
80.03 0.4155 0.6859 0.0801 0.0485 9.446 49.614 30.361 7043.844 5.605 135.046 1.955 0.81 326369. 0.3729
|
|
85.75 0.4452 0.7129 0.0762 0.0476 9.256 48.615 28.857 6902.045 5.492 128.357 1.896 0.81 327143. 0.3526
|
|
91.47 0.4749 0.7374 0.0719 0.0463 9.005 47.296 27.224 6714.801 5.343 121.091 1.839 0.82 327958. 0.3321
|
|
97.18 0.5045 0.7594 0.0672 0.0447 8.690 45.641 25.465 6479.796 5.156 113.269 1.782 0.82 328813. 0.3114
|
|
102.90 0.5342 0.7790 0.0623 0.0427 8.312 43.657 23.597 6198.181 4.932 104.958 1.727 0.82 329708. 0.2904
|
|
108.62 0.5639 0.7957 0.0571 0.0405 7.875 41.363 21.635 5872.521 4.673 96.232 1.671 0.82 330643. 0.2691
|
|
114.33 0.5936 0.8092 0.0517 0.0379 7.382 38.775 19.595 5505.022 4.381 87.159 1.614 0.82 331617. 0.2474
|
|
120.05 0.6233 0.8190 0.0462 0.0351 6.837 35.909 17.492 5098.122 4.057 77.804 1.556 0.82 332629. 0.2253
|
|
125.77 0.6529 0.8241 0.0405 0.0321 6.242 32.784 15.338 4654.532 3.704 68.223 1.495 0.82 333680. 0.2026
|
|
131.48 0.6826 0.8227 0.0347 0.0288 5.602 29.426 13.146 4177.710 3.325 58.472 1.427 0.83 334770. 0.1791
|
|
137.20 0.7123 0.8118 0.0288 0.0253 4.925 25.866 10.928 3672.313 2.922 48.609 1.350 0.83 335897. 0.1545
|
|
142.92 0.7420 0.7863 0.0230 0.0217 4.216 22.144 8.699 3143.945 2.502 38.692 1.255 0.83 337062. 0.1281
|
|
148.63 0.7716 0.7360 0.0171 0.0179 3.486 18.308 6.472 2599.192 2.068 28.789 1.129 0.83 338265. 0.0995
|
|
154.35 0.8013 0.6400 0.0113 0.0141 2.743 14.409 4.266 2045.665 1.628 18.973 0.946 0.83 339505. 0.0676
|
|
160.07 0.8310 0.4473 0.0055 0.0103 2.001 10.509 2.097 1491.986 1.187 9.326 0.637 0.83 340783. 0.0319
|
|
165.78 0.8607 -0.0059 0.0000 0.0065 1.269 6.665 -0.017 946.280 0.753 -0.075 -0.008 0.84 342089. 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 0.1067 0.0495 12.234 59.315 47.431 9122.933 6.701 210.975 2.358 0.87 346294. 0.5622
|
|
6.26 0.0300 0.0634 0.1062 0.0503 12.434 60.282 47.198 9271.754 6.811 209.936 2.309 0.87 346565. 0.5491
|
|
12.53 0.0600 0.1241 0.1055 0.0511 12.633 61.249 46.921 9420.411 6.920 208.707 2.259 0.87 346868. 0.5357
|
|
18.79 0.0901 0.1820 0.1048 0.0519 12.827 62.190 46.593 9565.147 7.026 207.246 2.209 0.87 347205. 0.5221
|
|
25.06 0.1201 0.2373 0.1039 0.0526 13.010 63.078 46.202 9701.744 7.127 205.507 2.160 0.87 347580. 0.5082
|
|
31.32 0.1501 0.2899 0.1029 0.0533 13.176 63.882 45.737 9825.430 7.217 203.438 2.111 0.88 347992. 0.4943
|
|
37.59 0.1801 0.3400 0.1016 0.0538 13.318 64.570 45.185 9931.136 7.295 200.983 2.064 0.88 348446. 0.4802
|
|
43.85 0.2101 0.3878 0.1002 0.0543 13.429 65.106 44.534 10013.708 7.356 198.086 2.017 0.88 348941. 0.4660
|
|
50.11 0.2402 0.4332 0.0984 0.0546 13.502 65.460 43.770 10068.118 7.396 194.690 1.972 0.88 349480. 0.4516
|
|
56.38 0.2702 0.4765 0.0965 0.0547 13.530 65.598 42.882 10089.293 7.411 190.739 1.928 0.88 350064. 0.4370
|
|
62.64 0.3002 0.5176 0.0941 0.0546 13.508 65.491 41.858 10072.924 7.399 186.185 1.885 0.88 350693. 0.4221
|
|
68.91 0.3302 0.5567 0.0915 0.0543 13.431 65.118 40.689 10015.456 7.357 180.987 1.843 0.88 351367. 0.4069
|
|
75.17 0.3602 0.5936 0.0885 0.0537 13.294 64.453 39.368 9913.236 7.282 175.108 1.801 0.88 352088. 0.3912
|
|
81.44 0.3903 0.6284 0.0852 0.0529 13.092 63.476 37.887 9762.889 7.171 168.523 1.760 0.88 352855. 0.3751
|
|
87.70 0.4203 0.6610 0.0815 0.0518 12.822 62.165 36.244 9561.295 7.023 161.213 1.719 0.88 353667. 0.3583
|
|
93.96 0.4503 0.6914 0.0775 0.0504 12.479 60.501 34.436 9305.447 6.835 153.171 1.678 0.88 354526. 0.3410
|
|
100.23 0.4803 0.7195 0.0730 0.0487 12.059 58.464 32.461 8992.025 6.605 144.388 1.637 0.88 355429. 0.3229
|
|
106.49 0.5103 0.7450 0.0682 0.0467 11.559 56.042 30.328 8619.631 6.332 134.898 1.596 0.89 356378. 0.3042
|
|
112.76 0.5404 0.7680 0.0631 0.0444 10.984 53.252 28.056 8190.452 6.016 124.792 1.554 0.89 357370. 0.2849
|
|
119.02 0.5704 0.7873 0.0577 0.0418 10.346 50.160 25.665 7714.925 5.667 114.157 1.509 0.89 358407. 0.2646
|
|
125.29 0.6004 0.8021 0.0521 0.0390 9.652 46.798 23.175 7197.745 5.287 103.083 1.460 0.89 359486. 0.2434
|
|
131.55 0.6304 0.8110 0.0463 0.0360 8.911 43.205 20.604 6645.236 4.881 91.647 1.406 0.89 360608. 0.2210
|
|
137.81 0.6604 0.8106 0.0404 0.0329 8.145 39.490 17.966 6073.748 4.462 79.912 1.342 0.89 361772. 0.1969
|
|
144.08 0.6905 0.7999 0.0344 0.0297 7.339 35.584 15.280 5472.996 4.020 67.966 1.266 0.89 362978. 0.1714
|
|
150.34 0.7205 0.7746 0.0283 0.0263 6.503 31.527 12.565 4849.014 3.562 55.889 1.175 0.90 364226. 0.1442
|
|
156.61 0.7505 0.7273 0.0221 0.0228 5.649 27.390 9.839 4212.740 3.095 43.766 1.059 0.90 365516. 0.1150
|
|
162.87 0.7805 0.6454 0.0160 0.0194 4.794 23.243 7.124 3574.914 2.626 31.688 0.904 0.90 366847. 0.0835
|
|
169.14 0.8105 0.5070 0.0100 0.0160 3.952 19.161 4.443 2947.140 2.165 19.763 0.684 0.90 368220. 0.0499
|
|
175.40 0.8406 0.2717 0.0041 0.0127 3.140 15.222 1.824 2341.169 1.720 8.111 0.353 0.90 369633. 0.0165
|
|
181.66 0.8706
|
|
|
|
|
|
|
|
PROP RPM = 14000
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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 0.1050 0.0554 17.132 77.128 54.155 12775.290 8.714 240.883 1.923 0.94 372987. 0.4898
|
|
6.74 0.0300 0.0557 0.1046 0.0563 17.403 78.351 53.949 12977.785 8.852 239.964 1.885 0.94 373272. 0.4794
|
|
13.49 0.0600 0.1092 0.1042 0.0572 17.681 79.601 53.704 13184.830 8.993 238.874 1.847 0.94 373592. 0.4687
|
|
20.23 0.0900 0.1604 0.1036 0.0581 17.958 80.849 53.411 13391.603 9.134 237.570 1.809 0.94 373948. 0.4577
|
|
26.97 0.1200 0.2094 0.1029 0.0590 18.227 82.060 53.058 13592.181 9.271 236.001 1.771 0.94 374343. 0.4464
|
|
33.72 0.1500 0.2561 0.1021 0.0598 18.478 83.187 52.631 13778.873 9.398 234.104 1.733 0.94 374779. 0.4351
|
|
40.46 0.1800 0.3007 0.1011 0.0605 18.697 84.173 52.115 13942.057 9.510 231.806 1.695 0.94 375259. 0.4237
|
|
47.20 0.2101 0.3434 0.0999 0.0611 18.874 84.969 51.493 14073.998 9.600 229.041 1.659 0.94 375784. 0.4122
|
|
53.95 0.2401 0.3843 0.0984 0.0615 18.995 85.516 50.749 14164.653 9.662 225.732 1.625 0.94 376357. 0.4007
|
|
60.69 0.2701 0.4237 0.0967 0.0616 19.048 85.754 49.865 14203.947 9.688 221.800 1.592 0.94 376978. 0.3892
|
|
67.43 0.3001 0.4616 0.0947 0.0616 19.019 85.624 48.823 14182.490 9.674 217.167 1.561 0.95 377649. 0.3777
|
|
74.18 0.3301 0.4983 0.0923 0.0612 18.898 85.079 47.608 14092.260 9.612 211.762 1.532 0.95 378370. 0.3660
|
|
80.92 0.3601 0.5338 0.0896 0.0604 18.677 84.082 46.206 13927.101 9.500 205.525 1.505 0.95 379142. 0.3541
|
|
87.67 0.3901 0.5683 0.0865 0.0594 18.349 82.607 44.606 13682.808 9.333 198.407 1.479 0.95 379965. 0.3419
|
|
94.41 0.4201 0.6015 0.0830 0.0580 17.912 80.641 42.800 13357.049 9.111 190.375 1.453 0.95 380838. 0.3291
|
|
101.15 0.4501 0.6335 0.0791 0.0562 17.365 78.178 40.786 12949.193 8.833 181.414 1.429 0.95 381762. 0.3158
|
|
107.90 0.4801 0.6640 0.0748 0.0541 16.708 75.220 38.559 12459.245 8.498 171.512 1.404 0.95 382736. 0.3017
|
|
114.64 0.5101 0.6927 0.0701 0.0516 15.944 71.780 36.129 11889.323 8.110 160.702 1.378 0.95 383758. 0.2868
|
|
121.38 0.5401 0.7194 0.0650 0.0488 15.081 67.897 33.519 11246.257 7.671 149.092 1.352 0.96 384828. 0.2709
|
|
128.13 0.5702 0.7435 0.0596 0.0457 14.133 63.626 30.755 10538.809 7.188 136.796 1.324 0.96 385946. 0.2541
|
|
134.87 0.6002 0.7626 0.0540 0.0425 13.138 59.149 27.859 9797.164 6.683 123.916 1.290 0.96 387110. 0.2357
|
|
141.61 0.6302 0.7750 0.0482 0.0392 12.111 54.524 24.855 9031.193 6.160 110.555 1.248 0.96 388319. 0.2154
|
|
148.36 0.6602 0.7749 0.0422 0.0360 11.109 50.013 21.760 8284.052 5.650 96.786 1.191 0.96 389574. 0.1924
|
|
155.10 0.6902 0.7525 0.0360 0.0331 10.215 45.990 18.586 7617.554 5.196 82.669 1.107 0.96 390875. 0.1651
|
|
161.84 0.7202 0.7127 0.0298 0.0301 9.313 41.927 15.379 6944.657 4.737 68.407 1.004 0.97 392219. 0.1364
|
|
168.59 0.7502 0.6499 0.0236 0.0272 8.418 37.899 12.171 6277.501 4.282 54.135 0.879 0.97 393608. 0.1062
|
|
175.33 0.7802 0.5570 0.0174 0.0244 7.549 33.986 8.995 5629.296 3.840 40.008 0.725 0.97 395042. 0.0752
|
|
182.07 0.8102 0.4254 0.0114 0.0218 6.721 30.260 5.890 5012.189 3.419 26.199 0.533 0.97 396521. 0.0448
|
|
188.82 0.8402 0.2453 0.0056 0.0192 5.946 26.770 2.897 4434.035 3.024 12.885 0.296 0.97 398048. 0.0175
|
|
195.56 0.8702 0.0023 0.0000 0.0169 5.214 23.472 0.023 3887.790 2.652 0.100 0.003 0.98 399654. 0.0000
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