612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
13x10 (13x10.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 0.1224 0.0656 0.002 0.121 0.110 1.433 0.014 0.488 34.728 0.05 21807. 0.5212
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0.39 0.0321 0.0585 0.1213 0.0666 0.002 0.123 0.109 1.456 0.014 0.483 33.848 0.05 21828. 0.5056
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0.79 0.0643 0.1138 0.1199 0.0677 0.002 0.125 0.107 1.479 0.014 0.478 32.957 0.05 21850. 0.4896
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1.18 0.0964 0.1661 0.1185 0.0687 0.002 0.127 0.106 1.502 0.014 0.472 32.061 0.05 21876. 0.4734
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1.58 0.1285 0.2153 0.1168 0.0697 0.002 0.129 0.105 1.524 0.015 0.466 31.166 0.05 21904. 0.4569
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1.97 0.1606 0.2614 0.1150 0.0707 0.002 0.131 0.103 1.544 0.015 0.458 30.273 0.05 21934. 0.4404
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2.36 0.1928 0.3045 0.1129 0.0715 0.002 0.132 0.101 1.562 0.015 0.450 29.387 0.05 21968. 0.4236
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2.76 0.2249 0.3447 0.1107 0.0722 0.002 0.133 0.099 1.578 0.015 0.441 28.511 0.05 22004. 0.4068
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3.15 0.2570 0.3820 0.1081 0.0728 0.002 0.134 0.097 1.590 0.015 0.431 27.644 0.05 22044. 0.3899
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3.55 0.2891 0.4164 0.1053 0.0731 0.002 0.135 0.094 1.598 0.015 0.420 26.790 0.05 22087. 0.3730
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3.94 0.3213 0.4481 0.1023 0.0733 0.002 0.135 0.092 1.602 0.015 0.408 25.946 0.05 22132. 0.3559
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4.33 0.3534 0.4771 0.0989 0.0733 0.002 0.135 0.089 1.601 0.015 0.394 25.113 0.05 22182. 0.3387
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4.73 0.3855 0.5034 0.0952 0.0729 0.002 0.135 0.085 1.593 0.015 0.380 24.288 0.05 22234. 0.3215
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5.12 0.4177 0.5270 0.0912 0.0723 0.002 0.134 0.082 1.580 0.015 0.364 23.470 0.05 22289. 0.3040
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5.52 0.4498 0.5478 0.0869 0.0713 0.002 0.132 0.078 1.559 0.015 0.346 22.654 0.05 22348. 0.2864
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5.91 0.4819 0.5658 0.0822 0.0700 0.002 0.129 0.074 1.530 0.015 0.328 21.838 0.05 22410. 0.2686
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6.30 0.5140 0.5808 0.0773 0.0684 0.002 0.126 0.069 1.495 0.014 0.308 21.016 0.05 22475. 0.2506
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6.70 0.5462 0.5925 0.0721 0.0665 0.002 0.123 0.065 1.452 0.014 0.287 20.181 0.05 22543. 0.2325
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7.09 0.5783 0.6008 0.0667 0.0642 0.002 0.119 0.060 1.403 0.013 0.266 19.325 0.05 22614. 0.2141
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7.49 0.6104 0.6051 0.0612 0.0617 0.002 0.114 0.055 1.348 0.013 0.244 18.439 0.05 22689. 0.1956
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7.88 0.6425 0.6048 0.0554 0.0589 0.002 0.109 0.050 1.287 0.012 0.221 17.510 0.05 22766. 0.1768
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8.27 0.6747 0.5993 0.0496 0.0558 0.002 0.103 0.044 1.220 0.012 0.198 16.523 0.05 22847. 0.1578
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8.67 0.7068 0.5873 0.0436 0.0525 0.002 0.097 0.039 1.147 0.011 0.174 15.456 0.05 22931. 0.1384
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9.06 0.7389 0.5673 0.0375 0.0489 0.001 0.090 0.034 1.069 0.010 0.150 14.281 0.05 23017. 0.1187
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9.46 0.7710 0.5371 0.0314 0.0451 0.001 0.083 0.028 0.985 0.009 0.125 12.958 0.05 23107. 0.0985
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9.85 0.8032 0.4933 0.0252 0.0410 0.001 0.076 0.023 0.896 0.009 0.100 11.425 0.05 23200. 0.0778
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10.24 0.8353 0.4307 0.0189 0.0367 0.001 0.068 0.017 0.802 0.008 0.075 9.591 0.05 23296. 0.0566
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10.64 0.8674 0.3406 0.0126 0.0322 0.001 0.059 0.011 0.703 0.007 0.050 7.304 0.05 23395. 0.0352
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11.03 0.8996 0.2080 0.0063 0.0275 0.001 0.051 0.006 0.600 0.006 0.025 4.302 0.05 23497. 0.0147
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11.43 0.9317 0.0039 0.0001 0.0225 0.001 0.042 0.000 0.493 0.005 0.000 0.077 0.05 23601. 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 0.1230 0.0585 0.014 0.432 0.441 10.231 0.049 1.961 19.546 0.10 43614. 0.5880
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0.79 0.0324 0.0661 0.1218 0.0597 0.014 0.441 0.437 10.430 0.050 1.943 18.994 0.10 43655. 0.5688
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1.59 0.0648 0.1284 0.1206 0.0608 0.014 0.449 0.432 10.630 0.051 1.922 18.440 0.10 43701. 0.5493
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2.38 0.0971 0.1868 0.1191 0.0619 0.015 0.458 0.427 10.827 0.052 1.899 17.887 0.10 43752. 0.5296
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3.18 0.1295 0.2415 0.1175 0.0630 0.015 0.466 0.421 11.017 0.053 1.873 17.338 0.10 43809. 0.5098
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3.97 0.1619 0.2924 0.1156 0.0640 0.015 0.473 0.415 11.195 0.053 1.844 16.796 0.10 43871. 0.4900
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4.76 0.1943 0.3397 0.1136 0.0650 0.015 0.480 0.407 11.357 0.054 1.811 16.263 0.10 43938. 0.4702
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5.56 0.2267 0.3836 0.1113 0.0658 0.015 0.486 0.399 11.499 0.055 1.775 15.740 0.10 44012. 0.4505
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6.35 0.2590 0.4241 0.1088 0.0664 0.016 0.491 0.390 11.614 0.055 1.734 15.228 0.10 44093. 0.4309
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7.15 0.2914 0.4615 0.1060 0.0669 0.016 0.494 0.380 11.698 0.056 1.690 14.728 0.10 44179. 0.4113
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7.94 0.3238 0.4958 0.1029 0.0672 0.016 0.496 0.369 11.745 0.056 1.640 14.241 0.10 44272. 0.3918
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8.74 0.3562 0.5271 0.0995 0.0672 0.016 0.497 0.357 11.749 0.056 1.586 13.765 0.10 44372. 0.3724
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9.53 0.3886 0.5556 0.0957 0.0670 0.016 0.495 0.343 11.705 0.056 1.527 13.300 0.10 44478. 0.3530
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10.32 0.4209 0.5813 0.0917 0.0664 0.016 0.490 0.329 11.606 0.055 1.462 12.844 0.10 44590. 0.3337
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11.12 0.4533 0.6043 0.0873 0.0655 0.015 0.484 0.313 11.449 0.055 1.392 12.397 0.10 44709. 0.3142
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11.91 0.4857 0.6244 0.0826 0.0642 0.015 0.475 0.296 11.230 0.054 1.317 11.957 0.10 44834. 0.2948
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12.71 0.5181 0.6417 0.0776 0.0626 0.015 0.463 0.278 10.951 0.052 1.237 11.520 0.10 44966. 0.2753
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13.50 0.5505 0.6561 0.0724 0.0607 0.014 0.449 0.259 10.613 0.051 1.154 11.084 0.10 45104. 0.2558
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14.29 0.5828 0.6671 0.0669 0.0585 0.014 0.432 0.240 10.219 0.049 1.067 10.645 0.10 45249. 0.2362
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15.09 0.6152 0.6746 0.0613 0.0559 0.013 0.413 0.220 9.770 0.047 0.977 10.198 0.10 45400. 0.2166
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15.88 0.6476 0.6780 0.0555 0.0530 0.012 0.392 0.199 9.270 0.044 0.885 9.737 0.10 45557. 0.1968
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16.68 0.6800 0.6765 0.0496 0.0499 0.012 0.368 0.178 8.718 0.042 0.791 9.253 0.11 45721. 0.1768
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17.47 0.7124 0.6691 0.0436 0.0464 0.011 0.343 0.156 8.116 0.039 0.695 8.735 0.11 45891. 0.1565
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18.27 0.7448 0.6540 0.0375 0.0427 0.010 0.316 0.134 7.466 0.036 0.598 8.168 0.11 46067. 0.1357
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19.06 0.7771 0.6290 0.0313 0.0387 0.009 0.286 0.112 6.768 0.032 0.500 7.527 0.11 46249. 0.1143
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19.85 0.8095 0.5898 0.0251 0.0345 0.008 0.255 0.090 6.023 0.029 0.400 6.776 0.11 46438. 0.0921
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20.65 0.8419 0.5296 0.0188 0.0299 0.007 0.221 0.068 5.235 0.025 0.300 5.851 0.11 46632. 0.0689
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21.44 0.8743 0.4358 0.0126 0.0252 0.006 0.186 0.045 4.405 0.021 0.200 4.636 0.11 46833. 0.0446
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22.24 0.9067 0.2822 0.0063 0.0202 0.005 0.149 0.023 3.536 0.017 0.100 2.895 0.11 47039. 0.0197
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23.03 0.9390 0.0045 0.0001 0.0151 0.004 0.111 0.000 2.633 0.013 0.001 0.045 0.11 47250. 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 0.1233 0.0557 0.044 0.925 0.995 32.834 0.105 4.425 13.741 0.15 65421. 0.6210
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1.20 0.0325 0.0699 0.1222 0.0568 0.045 0.945 0.986 33.528 0.107 4.384 13.334 0.15 65482. 0.5998
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2.39 0.0650 0.1355 0.1209 0.0580 0.046 0.964 0.975 34.225 0.109 4.338 12.926 0.15 65551. 0.5784
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3.59 0.0975 0.1969 0.1195 0.0592 0.047 0.984 0.964 34.913 0.111 4.287 12.520 0.15 65628. 0.5569
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4.78 0.1300 0.2541 0.1179 0.0603 0.048 1.002 0.951 35.578 0.113 4.229 12.120 0.15 65713. 0.5354
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5.98 0.1625 0.3073 0.1160 0.0614 0.049 1.020 0.936 36.207 0.115 4.163 11.725 0.15 65807. 0.5140
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7.17 0.1950 0.3566 0.1140 0.0623 0.049 1.036 0.919 36.782 0.117 4.090 11.339 0.15 65909. 0.4927
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8.37 0.2275 0.4022 0.1117 0.0632 0.050 1.051 0.901 37.286 0.119 4.008 10.961 0.15 66021. 0.4715
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9.56 0.2600 0.4442 0.1092 0.0639 0.051 1.062 0.881 37.702 0.120 3.917 10.594 0.15 66142. 0.4505
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10.76 0.2925 0.4829 0.1064 0.0644 0.051 1.071 0.858 38.011 0.121 3.816 10.237 0.15 66273. 0.4296
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11.96 0.3250 0.5184 0.1033 0.0647 0.051 1.076 0.833 38.193 0.122 3.704 9.890 0.15 66413. 0.4090
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13.15 0.3575 0.5508 0.0998 0.0648 0.051 1.077 0.805 38.229 0.122 3.582 9.554 0.16 66563. 0.3885
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14.35 0.3900 0.5804 0.0961 0.0646 0.051 1.073 0.775 38.098 0.121 3.447 9.227 0.16 66723. 0.3681
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15.54 0.4225 0.6071 0.0920 0.0640 0.051 1.064 0.742 37.781 0.120 3.301 8.909 0.16 66893. 0.3478
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16.74 0.4550 0.6310 0.0876 0.0632 0.050 1.050 0.706 37.262 0.119 3.142 8.599 0.16 67072. 0.3275
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17.93 0.4875 0.6523 0.0828 0.0619 0.049 1.029 0.668 36.532 0.116 2.972 8.296 0.16 67262. 0.3073
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19.13 0.5200 0.6708 0.0778 0.0603 0.048 1.003 0.628 35.592 0.113 2.792 7.998 0.16 67461. 0.2871
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20.33 0.5525 0.6864 0.0725 0.0584 0.046 0.971 0.585 34.449 0.110 2.602 7.704 0.16 67670. 0.2670
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21.52 0.5850 0.6991 0.0671 0.0561 0.044 0.933 0.541 33.109 0.105 2.406 7.409 0.16 67888. 0.2469
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22.72 0.6175 0.7083 0.0614 0.0535 0.042 0.890 0.495 31.582 0.101 2.203 7.113 0.16 68116. 0.2268
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23.91 0.6500 0.7138 0.0556 0.0506 0.040 0.842 0.448 29.870 0.095 1.995 6.809 0.16 68354. 0.2066
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25.11 0.6825 0.7148 0.0497 0.0474 0.038 0.788 0.401 27.980 0.089 1.782 6.494 0.16 68601. 0.1862
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26.30 0.7150 0.7103 0.0436 0.0439 0.035 0.730 0.352 25.914 0.082 1.565 6.160 0.16 68857. 0.1656
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27.50 0.7475 0.6987 0.0375 0.0401 0.032 0.667 0.303 23.676 0.075 1.346 5.795 0.16 69123. 0.1444
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28.69 0.7800 0.6774 0.0313 0.0361 0.029 0.599 0.253 21.271 0.068 1.123 5.385 0.16 69398. 0.1226
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29.89 0.8125 0.6424 0.0251 0.0317 0.025 0.527 0.202 18.704 0.060 0.899 4.902 0.16 69683. 0.0999
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31.09 0.8450 0.5860 0.0188 0.0271 0.021 0.450 0.152 15.981 0.051 0.674 4.300 0.16 69976. 0.0758
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32.28 0.8775 0.4935 0.0125 0.0222 0.018 0.369 0.101 13.112 0.042 0.448 3.487 0.16 70279. 0.0502
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33.48 0.9100 0.3309 0.0062 0.0171 0.014 0.285 0.050 10.109 0.032 0.224 2.255 0.16 70590. 0.0229
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34.67 0.9425 0.0006 0.0000 0.0118 0.009 0.197 0.000 6.983 0.022 0.000 0.004 0.16 70907. 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 0.1236 0.0541 0.101 1.598 1.773 75.637 0.181 7.886 10.631 0.21 87226. 0.6414
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1.60 0.0326 0.0722 0.1225 0.0553 0.104 1.634 1.757 77.314 0.185 7.815 10.307 0.21 87308. 0.6190
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3.20 0.0651 0.1398 0.1213 0.0565 0.106 1.669 1.739 79.003 0.189 7.734 9.983 0.21 87400. 0.5965
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4.79 0.0977 0.2030 0.1198 0.0577 0.108 1.705 1.718 80.672 0.193 7.643 9.661 0.21 87503. 0.5738
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6.39 0.1303 0.2618 0.1182 0.0588 0.110 1.739 1.695 82.290 0.196 7.541 9.344 0.21 87617. 0.5513
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7.99 0.1628 0.3163 0.1164 0.0599 0.112 1.771 1.669 83.821 0.200 7.425 9.033 0.21 87742. 0.5288
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9.59 0.1954 0.3668 0.1144 0.0609 0.114 1.801 1.640 85.226 0.203 7.295 8.729 0.21 87879. 0.5065
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11.18 0.2280 0.4134 0.1121 0.0618 0.116 1.827 1.607 86.463 0.206 7.150 8.432 0.21 88029. 0.4844
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12.78 0.2605 0.4563 0.1096 0.0626 0.117 1.849 1.571 87.489 0.209 6.988 8.145 0.21 88191. 0.4626
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14.38 0.2931 0.4958 0.1068 0.0631 0.118 1.865 1.531 88.260 0.211 6.808 7.866 0.21 88365. 0.4410
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15.98 0.3257 0.5320 0.1036 0.0634 0.119 1.875 1.486 88.728 0.212 6.610 7.596 0.21 88553. 0.4196
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17.57 0.3582 0.5651 0.1002 0.0635 0.119 1.877 1.437 88.845 0.212 6.391 7.335 0.21 88754. 0.3984
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19.17 0.3908 0.5952 0.0965 0.0633 0.119 1.871 1.383 88.563 0.211 6.151 7.083 0.21 88968. 0.3774
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20.77 0.4234 0.6226 0.0924 0.0628 0.118 1.856 1.324 87.833 0.210 5.890 6.838 0.21 89196. 0.3566
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22.37 0.4560 0.6472 0.0879 0.0619 0.116 1.830 1.261 86.617 0.207 5.607 6.601 0.21 89436. 0.3358
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23.96 0.4885 0.6691 0.0831 0.0607 0.114 1.794 1.192 84.893 0.203 5.303 6.370 0.21 89690. 0.3151
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25.56 0.5211 0.6884 0.0781 0.0591 0.111 1.747 1.120 82.663 0.197 4.980 6.144 0.21 89956. 0.2946
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27.16 0.5537 0.7050 0.0728 0.0572 0.107 1.689 1.044 79.942 0.191 4.642 5.921 0.21 90236. 0.2741
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28.76 0.5862 0.7187 0.0673 0.0549 0.103 1.622 0.965 76.748 0.183 4.291 5.701 0.21 90528. 0.2537
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30.35 0.6188 0.7292 0.0616 0.0523 0.098 1.545 0.883 73.096 0.175 3.928 5.480 0.21 90834. 0.2333
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31.95 0.6514 0.7361 0.0558 0.0493 0.093 1.458 0.799 69.000 0.165 3.556 5.255 0.21 91152. 0.2129
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33.55 0.6839 0.7389 0.0498 0.0461 0.086 1.362 0.714 64.468 0.154 3.176 5.024 0.21 91482. 0.1924
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35.15 0.7165 0.7364 0.0437 0.0426 0.080 1.257 0.627 59.510 0.142 2.789 4.780 0.21 91826. 0.1715
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36.74 0.7491 0.7273 0.0376 0.0387 0.073 1.144 0.539 54.135 0.129 2.397 4.515 0.21 92182. 0.1502
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38.34 0.7816 0.7091 0.0314 0.0346 0.065 1.022 0.450 48.352 0.115 2.000 4.219 0.21 92550. 0.1282
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39.94 0.8142 0.6776 0.0251 0.0302 0.057 0.891 0.360 42.174 0.101 1.601 3.870 0.21 92931. 0.1052
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41.54 0.8468 0.6249 0.0188 0.0255 0.048 0.753 0.269 35.619 0.085 1.199 3.432 0.21 93324. 0.0807
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43.13 0.8793 0.5350 0.0125 0.0205 0.038 0.607 0.179 28.709 0.069 0.797 2.829 0.21 93729. 0.0543
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44.73 0.9119 0.3686 0.0062 0.0154 0.029 0.454 0.089 21.473 0.051 0.396 1.880 0.21 94146. 0.0254
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46.33 0.9445 -0.0030 0.0000 0.0100 0.019 0.295 0.000 13.937 0.033 -0.002 -0.015 0.21 94568. 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 0.1240 0.0531 0.195 2.453 2.777 145.129 0.277 12.354 8.680 0.26 109029. 0.6555
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2.00 0.0326 0.0737 0.1229 0.0544 0.199 2.510 2.753 148.459 0.284 12.244 8.410 0.26 109133. 0.6323
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4.00 0.0652 0.1427 0.1216 0.0556 0.204 2.566 2.725 151.815 0.290 12.120 8.141 0.26 109248. 0.6089
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6.00 0.0978 0.2071 0.1202 0.0568 0.208 2.623 2.693 155.137 0.296 11.980 7.874 0.26 109377. 0.5855
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8.00 0.1304 0.2669 0.1186 0.0580 0.212 2.677 2.658 158.361 0.302 11.821 7.612 0.26 109519. 0.5622
|
|
10.00 0.1630 0.3223 0.1168 0.0591 0.216 2.729 2.617 161.417 0.308 11.641 7.354 0.26 109676. 0.5391
|
|
12.00 0.1957 0.3736 0.1148 0.0601 0.220 2.776 2.572 164.227 0.314 11.440 7.103 0.26 109848. 0.5162
|
|
14.00 0.2283 0.4209 0.1125 0.0610 0.224 2.818 2.521 166.709 0.318 11.214 6.859 0.26 110035. 0.4935
|
|
16.00 0.2609 0.4644 0.1100 0.0618 0.226 2.853 2.464 168.777 0.322 10.961 6.623 0.26 110238. 0.4711
|
|
17.99 0.2935 0.5044 0.1072 0.0624 0.228 2.880 2.401 170.341 0.325 10.681 6.394 0.26 110457. 0.4489
|
|
19.99 0.3261 0.5411 0.1041 0.0627 0.230 2.896 2.331 171.309 0.327 10.370 6.173 0.26 110692. 0.4271
|
|
21.99 0.3587 0.5746 0.1006 0.0628 0.230 2.901 2.255 171.585 0.328 10.028 5.960 0.26 110944. 0.4055
|
|
23.99 0.3913 0.6052 0.0969 0.0626 0.229 2.892 2.170 171.072 0.327 9.653 5.754 0.26 111213. 0.3841
|
|
25.99 0.4239 0.6330 0.0928 0.0621 0.228 2.868 2.078 169.676 0.324 9.243 5.555 0.26 111498. 0.3629
|
|
27.99 0.4565 0.6581 0.0883 0.0613 0.224 2.828 1.978 167.318 0.320 8.799 5.363 0.26 111799. 0.3418
|
|
29.99 0.4891 0.6805 0.0835 0.0600 0.220 2.772 1.871 163.955 0.313 8.322 5.176 0.26 112117. 0.3208
|
|
31.99 0.5217 0.7004 0.0784 0.0584 0.214 2.698 1.757 159.590 0.305 7.816 4.994 0.26 112451. 0.3000
|
|
33.99 0.5544 0.7176 0.0731 0.0565 0.207 2.608 1.638 154.252 0.295 7.285 4.816 0.26 112801. 0.2793
|
|
35.99 0.5870 0.7321 0.0676 0.0542 0.198 2.501 1.514 147.974 0.283 6.734 4.640 0.26 113168. 0.2587
|
|
37.99 0.6196 0.7436 0.0619 0.0515 0.189 2.380 1.386 140.788 0.269 6.164 4.465 0.26 113551. 0.2382
|
|
39.99 0.6522 0.7516 0.0560 0.0486 0.178 2.244 1.255 132.717 0.253 5.580 4.288 0.26 113949. 0.2176
|
|
41.99 0.6848 0.7557 0.0500 0.0453 0.166 2.092 1.120 123.780 0.236 4.984 4.106 0.26 114364. 0.1969
|
|
43.99 0.7174 0.7550 0.0439 0.0417 0.153 1.927 0.984 113.995 0.218 4.377 3.915 0.26 114794. 0.1760
|
|
45.99 0.7500 0.7479 0.0377 0.0378 0.139 1.748 0.846 103.380 0.197 3.761 3.710 0.26 115240. 0.1546
|
|
47.99 0.7826 0.7321 0.0315 0.0337 0.123 1.554 0.706 91.953 0.176 3.138 3.480 0.26 115701. 0.1325
|
|
49.99 0.8152 0.7036 0.0252 0.0292 0.107 1.348 0.564 79.740 0.152 2.511 3.211 0.27 116178. 0.1093
|
|
51.98 0.8478 0.6543 0.0189 0.0244 0.090 1.129 0.423 66.776 0.128 1.880 2.871 0.27 116671. 0.0846
|
|
53.98 0.8805 0.5677 0.0125 0.0194 0.071 0.898 0.281 53.106 0.101 1.249 2.399 0.27 117179. 0.0576
|
|
55.98 0.9131 0.4005 0.0062 0.0142 0.052 0.656 0.140 38.789 0.074 0.621 1.632 0.27 117701. 0.0276
|
|
57.98 0.9457 -0.0036 0.0000 0.0087 0.032 0.404 -0.001 23.872 0.046 -0.003 -0.014 0.27 118228. 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 0.1243 0.0525 0.333 3.493 4.011 247.982 0.395 17.841 7.336 0.31 130831. 0.6658
|
|
2.40 0.0326 0.0748 0.1233 0.0538 0.340 3.576 3.976 253.823 0.404 17.686 7.105 0.31 130955. 0.6420
|
|
4.80 0.0653 0.1447 0.1220 0.0550 0.348 3.659 3.937 259.716 0.413 17.511 6.875 0.31 131094. 0.6181
|
|
7.20 0.0979 0.2099 0.1206 0.0563 0.356 3.741 3.892 265.556 0.423 17.311 6.647 0.31 131248. 0.5942
|
|
9.60 0.1305 0.2705 0.1191 0.0575 0.364 3.821 3.841 271.231 0.432 17.085 6.423 0.31 131419. 0.5704
|
|
12.01 0.1632 0.3265 0.1173 0.0586 0.371 3.897 3.783 276.616 0.440 16.829 6.204 0.31 131608. 0.5468
|
|
14.41 0.1958 0.3783 0.1153 0.0597 0.378 3.967 3.719 281.577 0.448 16.540 5.990 0.31 131814. 0.5234
|
|
16.81 0.2284 0.4261 0.1130 0.0606 0.383 4.028 3.646 285.968 0.455 16.216 5.782 0.31 132039. 0.5003
|
|
19.21 0.2611 0.4701 0.1105 0.0614 0.388 4.080 3.564 289.639 0.461 15.854 5.582 0.31 132283. 0.4775
|
|
21.61 0.2937 0.5104 0.1077 0.0620 0.392 4.120 3.474 292.433 0.465 15.451 5.388 0.31 132547. 0.4550
|
|
24.01 0.3264 0.5475 0.1046 0.0623 0.395 4.144 3.373 294.187 0.468 15.004 5.201 0.31 132830. 0.4328
|
|
26.41 0.3590 0.5814 0.1011 0.0624 0.395 4.152 3.262 294.733 0.469 14.511 5.021 0.31 133133. 0.4109
|
|
28.81 0.3916 0.6123 0.0974 0.0623 0.394 4.140 3.141 293.901 0.468 13.970 4.847 0.31 133456. 0.3892
|
|
31.22 0.4243 0.6404 0.0932 0.0618 0.391 4.107 3.008 291.527 0.464 13.379 4.680 0.31 133798. 0.3678
|
|
33.62 0.4569 0.6659 0.0888 0.0609 0.386 4.050 2.864 287.472 0.458 12.737 4.518 0.31 134161. 0.3464
|
|
36.02 0.4895 0.6887 0.0840 0.0597 0.378 3.968 2.709 281.659 0.448 12.048 4.362 0.31 134543. 0.3253
|
|
38.42 0.5222 0.7091 0.0789 0.0581 0.368 3.861 2.544 274.090 0.436 11.316 4.210 0.31 134945. 0.3043
|
|
40.82 0.5548 0.7269 0.0735 0.0561 0.355 3.730 2.371 264.816 0.421 10.548 4.062 0.31 135366. 0.2834
|
|
43.22 0.5874 0.7420 0.0679 0.0538 0.340 3.577 2.192 253.895 0.404 9.750 3.916 0.31 135807. 0.2627
|
|
45.62 0.6201 0.7542 0.0622 0.0511 0.324 3.400 2.007 241.381 0.384 8.926 3.771 0.31 136267. 0.2420
|
|
48.02 0.6527 0.7632 0.0563 0.0482 0.305 3.202 1.817 227.313 0.362 8.081 3.625 0.31 136746. 0.2214
|
|
50.43 0.6853 0.7684 0.0503 0.0449 0.284 2.983 1.623 211.727 0.337 7.217 3.476 0.32 137244. 0.2006
|
|
52.83 0.7180 0.7690 0.0442 0.0412 0.261 2.742 1.425 194.651 0.310 6.338 3.320 0.32 137761. 0.1796
|
|
55.23 0.7506 0.7636 0.0380 0.0373 0.236 2.481 1.225 176.116 0.280 5.447 3.154 0.32 138297. 0.1581
|
|
57.63 0.7832 0.7499 0.0317 0.0331 0.209 2.200 1.022 156.157 0.249 4.546 2.968 0.32 138852. 0.1360
|
|
60.03 0.8159 0.7240 0.0253 0.0286 0.181 1.899 0.818 134.819 0.215 3.637 2.751 0.32 139426. 0.1127
|
|
62.43 0.8485 0.6779 0.0190 0.0238 0.150 1.580 0.612 112.161 0.179 2.724 2.477 0.32 140017. 0.0878
|
|
64.83 0.8812 0.5947 0.0126 0.0187 0.118 1.243 0.407 88.264 0.140 1.811 2.092 0.32 140628. 0.0605
|
|
67.23 0.9138 0.4284 0.0063 0.0134 0.085 0.891 0.203 63.233 0.101 0.901 1.454 0.32 141255. 0.0296
|
|
69.64 0.9464 -0.0017 0.0000 0.0079 0.050 0.523 0.000 37.142 0.059 -0.002 -0.005 0.32 141888. 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 0.1247 0.0522 0.525 4.723 5.477 391.127 0.534 24.363 6.352 0.36 152631. 0.6736
|
|
2.80 0.0327 0.0756 0.1237 0.0534 0.537 4.836 5.431 400.545 0.546 24.157 6.150 0.36 152775. 0.6494
|
|
5.61 0.0653 0.1462 0.1225 0.0547 0.550 4.951 5.378 410.056 0.559 23.922 5.949 0.36 152937. 0.6251
|
|
8.41 0.0980 0.2120 0.1211 0.0560 0.563 5.065 5.318 419.494 0.572 23.654 5.750 0.36 153118. 0.6008
|
|
11.22 0.1307 0.2731 0.1195 0.0572 0.575 5.176 5.250 428.675 0.585 23.350 5.554 0.36 153318. 0.5766
|
|
14.02 0.1633 0.3296 0.1178 0.0584 0.587 5.281 5.172 437.397 0.597 23.005 5.363 0.36 153538. 0.5527
|
|
16.82 0.1960 0.3818 0.1158 0.0594 0.597 5.379 5.084 445.442 0.608 22.616 5.177 0.36 153779. 0.5290
|
|
19.63 0.2287 0.4300 0.1135 0.0604 0.607 5.465 4.986 452.577 0.617 22.178 4.997 0.36 154042. 0.5056
|
|
22.43 0.2613 0.4742 0.1110 0.0612 0.615 5.537 4.876 458.557 0.626 21.687 4.823 0.36 154327. 0.4825
|
|
25.24 0.2940 0.5149 0.1082 0.0618 0.621 5.592 4.753 463.130 0.632 21.139 4.654 0.36 154636. 0.4598
|
|
28.04 0.3266 0.5522 0.1051 0.0622 0.625 5.627 4.616 466.032 0.636 20.532 4.493 0.36 154967. 0.4374
|
|
30.84 0.3593 0.5864 0.1017 0.0623 0.626 5.639 4.465 466.993 0.637 19.861 4.337 0.36 155321. 0.4152
|
|
33.65 0.3920 0.6176 0.0979 0.0621 0.625 5.624 4.299 465.740 0.635 19.123 4.187 0.36 155698. 0.3934
|
|
36.45 0.4246 0.6460 0.0938 0.0616 0.620 5.579 4.118 462.006 0.630 18.316 4.043 0.36 156099. 0.3717
|
|
39.25 0.4573 0.6717 0.0893 0.0608 0.611 5.501 3.921 455.569 0.621 17.439 3.903 0.36 156523. 0.3502
|
|
42.06 0.4900 0.6950 0.0845 0.0595 0.599 5.389 3.709 446.302 0.609 16.496 3.769 0.36 156970. 0.3289
|
|
44.86 0.5226 0.7157 0.0793 0.0579 0.582 5.243 3.484 434.207 0.592 15.495 3.639 0.36 157440. 0.3077
|
|
47.67 0.5553 0.7339 0.0740 0.0560 0.562 5.064 3.247 419.364 0.572 14.444 3.512 0.37 157932. 0.2868
|
|
50.47 0.5880 0.7496 0.0684 0.0536 0.539 4.852 3.002 401.868 0.548 13.351 3.388 0.37 158448. 0.2659
|
|
53.27 0.6206 0.7624 0.0626 0.0509 0.512 4.610 2.748 381.802 0.521 12.223 3.264 0.37 158985. 0.2452
|
|
56.08 0.6533 0.7722 0.0567 0.0479 0.482 4.338 2.488 359.233 0.490 11.065 3.141 0.37 159546. 0.2245
|
|
58.88 0.6860 0.7783 0.0506 0.0446 0.448 4.036 2.222 334.216 0.456 9.882 3.015 0.37 160128. 0.2036
|
|
61.69 0.7186 0.7800 0.0444 0.0409 0.411 3.704 1.951 306.797 0.419 8.678 2.884 0.37 160733. 0.1826
|
|
64.49 0.7513 0.7760 0.0382 0.0370 0.371 3.345 1.676 277.026 0.378 7.457 2.745 0.37 161359. 0.1610
|
|
67.29 0.7839 0.7641 0.0319 0.0327 0.328 2.958 1.399 244.958 0.334 6.222 2.590 0.37 162008. 0.1388
|
|
70.10 0.8166 0.7403 0.0255 0.0281 0.283 2.544 1.119 210.667 0.287 4.977 2.409 0.37 162678. 0.1155
|
|
72.90 0.8493 0.6969 0.0191 0.0232 0.234 2.104 0.838 174.248 0.238 3.726 2.181 0.37 163370. 0.0904
|
|
75.71 0.8819 0.6166 0.0127 0.0181 0.182 1.640 0.556 135.832 0.185 2.475 1.858 0.37 164083. 0.0628
|
|
78.51 0.9146 0.4509 0.0063 0.0128 0.128 1.154 0.276 95.591 0.130 1.228 1.310 0.37 164816. 0.0312
|
|
81.31 0.9473 -0.0069 -0.0001 0.0072 0.072 0.648 -0.002 53.625 0.073 -0.010 -0.019 0.38 165552. 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 0.1252 0.0520 0.780 6.147 7.180 581.829 0.695 31.936 5.597 0.41 174428. 0.6796
|
|
3.21 0.0327 0.0761 0.1242 0.0533 0.799 6.298 7.121 596.108 0.712 31.674 5.418 0.41 174593. 0.6551
|
|
6.41 0.0653 0.1473 0.1230 0.0546 0.819 6.451 7.054 610.544 0.729 31.374 5.240 0.41 174778. 0.6306
|
|
9.62 0.0980 0.2135 0.1216 0.0559 0.838 6.602 6.977 624.885 0.746 31.032 5.064 0.41 174984. 0.6061
|
|
12.82 0.1307 0.2749 0.1201 0.0571 0.857 6.750 6.889 638.852 0.763 30.641 4.891 0.41 175213. 0.5817
|
|
16.03 0.1634 0.3317 0.1184 0.0583 0.875 6.890 6.789 652.139 0.778 30.197 4.722 0.41 175464. 0.5575
|
|
19.23 0.1960 0.3842 0.1164 0.0594 0.891 7.020 6.676 664.412 0.793 29.694 4.557 0.41 175740. 0.5336
|
|
22.44 0.2287 0.4326 0.1142 0.0604 0.906 7.135 6.548 675.315 0.806 29.127 4.398 0.41 176041. 0.5100
|
|
25.64 0.2614 0.4771 0.1117 0.0612 0.918 7.232 6.405 684.480 0.817 28.490 4.244 0.41 176368. 0.4867
|
|
28.85 0.2940 0.5180 0.1089 0.0618 0.927 7.306 6.245 691.520 0.825 27.778 4.096 0.41 176720. 0.4638
|
|
32.05 0.3267 0.5555 0.1058 0.0622 0.933 7.354 6.067 696.040 0.831 26.986 3.954 0.41 177099. 0.4413
|
|
35.26 0.3594 0.5899 0.1023 0.0624 0.936 7.371 5.870 697.630 0.833 26.111 3.817 0.41 177504. 0.4190
|
|
38.46 0.3921 0.6213 0.0986 0.0622 0.933 7.352 5.653 695.874 0.831 25.146 3.685 0.41 177937. 0.3970
|
|
41.67 0.4247 0.6500 0.0944 0.0617 0.926 7.294 5.416 690.373 0.824 24.090 3.558 0.41 178395. 0.3752
|
|
44.87 0.4574 0.6760 0.0899 0.0608 0.913 7.193 5.158 680.786 0.813 22.942 3.436 0.42 178880. 0.3536
|
|
48.08 0.4901 0.6995 0.0851 0.0596 0.894 7.046 4.880 666.916 0.796 21.706 3.319 0.42 179392. 0.3322
|
|
51.28 0.5227 0.7206 0.0799 0.0580 0.870 6.854 4.585 648.766 0.774 20.392 3.205 0.42 179930. 0.3110
|
|
54.49 0.5554 0.7393 0.0745 0.0560 0.840 6.619 4.274 626.453 0.748 19.012 3.095 0.42 180493. 0.2899
|
|
57.69 0.5881 0.7554 0.0689 0.0536 0.805 6.340 3.952 600.121 0.716 17.577 2.987 0.42 181083. 0.2690
|
|
60.90 0.6208 0.7688 0.0631 0.0509 0.764 6.021 3.618 569.898 0.680 16.094 2.880 0.42 181698. 0.2482
|
|
64.10 0.6534 0.7793 0.0571 0.0479 0.719 5.662 3.276 535.885 0.640 14.573 2.773 0.42 182339. 0.2274
|
|
67.31 0.6861 0.7863 0.0510 0.0445 0.668 5.263 2.927 498.165 0.595 13.017 2.665 0.42 183005. 0.2065
|
|
70.51 0.7188 0.7890 0.0448 0.0408 0.613 4.826 2.571 456.810 0.545 11.434 2.552 0.42 183697. 0.1854
|
|
73.72 0.7514 0.7863 0.0385 0.0368 0.552 4.352 2.210 411.892 0.492 9.828 2.433 0.42 184414. 0.1639
|
|
76.92 0.7841 0.7760 0.0322 0.0325 0.487 3.840 1.844 363.498 0.434 8.203 2.301 0.42 185155. 0.1416
|
|
80.13 0.8168 0.7544 0.0257 0.0279 0.418 3.294 1.476 311.734 0.372 6.565 2.147 0.42 185922. 0.1182
|
|
83.34 0.8495 0.7138 0.0193 0.0229 0.344 2.713 1.106 256.749 0.306 4.919 1.954 0.43 186713. 0.0931
|
|
86.54 0.8821 0.6370 0.0128 0.0178 0.267 2.100 0.736 198.740 0.237 3.272 1.679 0.43 187528. 0.0652
|
|
89.75 0.9148 0.4744 0.0064 0.0123 0.185 1.458 0.367 137.966 0.165 1.631 1.206 0.43 188366. 0.0331
|
|
92.95 0.9475 0.0007 0.0000 0.0067 0.100 0.788 0.000 74.574 0.089 0.001 0.002 0.43 189207. 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 0.1257 0.0520 1.110 7.774 9.124 827.776 0.878 40.582 4.999 0.46 196222. 0.6842
|
|
3.61 0.0327 0.0765 0.1247 0.0533 1.138 7.968 9.051 848.460 0.900 40.260 4.839 0.46 196407. 0.6596
|
|
7.22 0.0654 0.1480 0.1236 0.0546 1.166 8.165 8.968 869.400 0.922 39.891 4.679 0.46 196615. 0.6349
|
|
10.82 0.0981 0.2145 0.1222 0.0559 1.194 8.360 8.873 890.228 0.945 39.468 4.521 0.46 196847. 0.6102
|
|
14.43 0.1308 0.2762 0.1207 0.0572 1.221 8.551 8.764 910.538 0.966 38.984 4.366 0.46 197105. 0.5856
|
|
18.04 0.1635 0.3333 0.1190 0.0584 1.247 8.733 8.640 929.883 0.987 38.431 4.214 0.46 197388. 0.5613
|
|
21.65 0.1962 0.3860 0.1171 0.0595 1.271 8.901 8.499 947.775 1.006 37.803 4.067 0.46 197699. 0.5373
|
|
25.26 0.2289 0.4346 0.1149 0.0605 1.292 9.050 8.339 963.698 1.023 37.091 3.925 0.46 198038. 0.5135
|
|
28.87 0.2615 0.4793 0.1124 0.0613 1.310 9.176 8.159 977.112 1.037 36.291 3.787 0.46 198406. 0.4902
|
|
32.47 0.2942 0.5203 0.1096 0.0620 1.324 9.274 7.957 987.457 1.048 35.394 3.655 0.46 198804. 0.4672
|
|
36.08 0.3269 0.5580 0.1065 0.0624 1.333 9.337 7.732 994.160 1.055 34.394 3.528 0.46 199231. 0.4445
|
|
39.69 0.3596 0.5926 0.1031 0.0626 1.337 9.360 7.483 996.630 1.057 33.286 3.406 0.47 199688. 0.4221
|
|
43.30 0.3923 0.6242 0.0993 0.0624 1.333 9.338 7.209 994.265 1.055 32.064 3.288 0.47 200175. 0.4001
|
|
46.91 0.4250 0.6531 0.0952 0.0619 1.323 9.264 6.907 986.486 1.047 30.724 3.176 0.47 200692. 0.3782
|
|
50.51 0.4577 0.6793 0.0906 0.0611 1.305 9.136 6.579 972.798 1.032 29.265 3.068 0.47 201239. 0.3565
|
|
54.12 0.4904 0.7031 0.0858 0.0598 1.278 8.949 6.226 952.916 1.011 27.693 2.963 0.47 201816. 0.3350
|
|
57.73 0.5231 0.7245 0.0806 0.0582 1.243 8.704 5.850 926.836 0.983 26.020 2.863 0.47 202422. 0.3137
|
|
61.34 0.5558 0.7436 0.0751 0.0562 1.200 8.403 5.455 894.729 0.949 24.262 2.765 0.47 203058. 0.2926
|
|
64.95 0.5885 0.7601 0.0695 0.0538 1.149 8.047 5.043 856.807 0.909 22.432 2.670 0.47 203723. 0.2717
|
|
68.56 0.6212 0.7741 0.0636 0.0511 1.091 7.638 4.618 813.256 0.863 20.541 2.576 0.47 204416. 0.2508
|
|
72.16 0.6539 0.7851 0.0576 0.0480 1.025 7.177 4.182 764.224 0.811 18.599 2.482 0.47 205139. 0.2299
|
|
75.77 0.6866 0.7929 0.0515 0.0446 0.952 6.666 3.735 709.831 0.753 16.615 2.387 0.47 205890. 0.2090
|
|
79.38 0.7192 0.7965 0.0452 0.0408 0.872 6.106 3.281 650.181 0.690 14.594 2.289 0.47 206669. 0.1879
|
|
82.99 0.7519 0.7949 0.0388 0.0367 0.785 5.498 2.820 585.381 0.621 12.543 2.185 0.48 207476. 0.1662
|
|
86.60 0.7846 0.7860 0.0324 0.0324 0.691 4.842 2.353 515.553 0.547 10.468 2.070 0.48 208312. 0.1439
|
|
90.21 0.8173 0.7661 0.0259 0.0277 0.591 4.140 1.883 440.854 0.468 8.375 1.937 0.48 209176. 0.1205
|
|
93.81 0.8500 0.7277 0.0194 0.0227 0.485 3.395 1.410 361.497 0.384 6.273 1.769 0.48 210067. 0.0952
|
|
97.42 0.8827 0.6536 0.0129 0.0174 0.372 2.609 0.937 277.768 0.295 4.168 1.530 0.48 210985. 0.0671
|
|
101.03 0.9154 0.4924 0.0064 0.0119 0.255 1.785 0.466 190.046 0.202 2.072 1.112 0.48 211929. 0.0344
|
|
104.64 0.9481 -0.0059 0.0000 0.0062 0.132 0.925 -0.003 98.501 0.105 -0.012 -0.013 0.48 212872. 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 0.1262 0.0520 1.525 9.612 11.313 1137.165 1.086 50.322 4.512 0.51 218012. 0.6877
|
|
4.01 0.0327 0.0768 0.1253 0.0534 1.564 9.856 11.228 1166.069 1.114 49.941 4.367 0.51 218218. 0.6631
|
|
8.02 0.0654 0.1485 0.1242 0.0547 1.603 10.104 11.129 1195.382 1.142 49.501 4.223 0.51 218449. 0.6383
|
|
12.03 0.0981 0.2152 0.1229 0.0560 1.642 10.350 11.015 1224.579 1.169 48.994 4.080 0.51 218707. 0.6135
|
|
16.04 0.1308 0.2771 0.1214 0.0573 1.680 10.591 10.884 1253.094 1.197 48.411 3.939 0.51 218992. 0.5889
|
|
20.05 0.1635 0.3343 0.1198 0.0586 1.717 10.821 10.733 1280.292 1.223 47.742 3.803 0.51 219308. 0.5645
|
|
24.06 0.1962 0.3871 0.1179 0.0597 1.751 11.034 10.562 1305.484 1.247 46.979 3.670 0.51 219654. 0.5404
|
|
28.08 0.2289 0.4358 0.1157 0.0608 1.781 11.224 10.367 1327.943 1.268 46.112 3.541 0.52 220031. 0.5166
|
|
32.09 0.2617 0.4806 0.1132 0.0616 1.806 11.384 10.147 1346.909 1.286 45.132 3.417 0.52 220441. 0.4932
|
|
36.10 0.2944 0.5218 0.1105 0.0623 1.826 11.509 9.899 1361.598 1.300 44.032 3.298 0.52 220883. 0.4701
|
|
40.11 0.3271 0.5597 0.1074 0.0628 1.839 11.590 9.623 1371.210 1.309 42.802 3.183 0.52 221359. 0.4474
|
|
44.12 0.3598 0.5944 0.1040 0.0629 1.844 11.621 9.316 1374.917 1.313 41.436 3.073 0.52 221868. 0.4250
|
|
48.13 0.3925 0.6262 0.1002 0.0628 1.840 11.595 8.976 1371.884 1.310 39.927 2.968 0.52 222410. 0.4029
|
|
52.14 0.4252 0.6553 0.0960 0.0623 1.826 11.506 8.604 1361.303 1.300 38.269 2.867 0.52 222986. 0.3810
|
|
56.15 0.4579 0.6817 0.0915 0.0614 1.800 11.347 8.197 1342.481 1.282 36.460 2.769 0.52 223595. 0.3593
|
|
60.16 0.4906 0.7058 0.0866 0.0602 1.763 11.115 7.758 1315.012 1.256 34.509 2.676 0.52 224237. 0.3377
|
|
64.17 0.5233 0.7275 0.0814 0.0585 1.715 10.809 7.291 1278.885 1.221 32.431 2.586 0.52 224912. 0.3164
|
|
68.18 0.5560 0.7469 0.0759 0.0565 1.655 10.433 6.800 1234.341 1.179 30.245 2.499 0.52 225620. 0.2952
|
|
72.19 0.5887 0.7638 0.0702 0.0541 1.585 9.988 6.288 1181.677 1.128 27.967 2.413 0.52 226360. 0.2742
|
|
76.21 0.6214 0.7783 0.0643 0.0513 1.504 9.476 5.758 1121.161 1.071 25.613 2.330 0.52 227132. 0.2533
|
|
80.22 0.6541 0.7899 0.0582 0.0482 1.412 8.900 5.215 1053.002 1.006 23.195 2.246 0.52 227936. 0.2324
|
|
84.23 0.6868 0.7983 0.0520 0.0447 1.311 8.261 4.659 977.371 0.933 20.722 2.162 0.53 228771. 0.2114
|
|
88.24 0.7196 0.8028 0.0457 0.0409 1.199 7.560 4.092 894.413 0.854 18.203 2.075 0.53 229638. 0.1902
|
|
92.25 0.7523 0.8023 0.0393 0.0368 1.079 6.798 3.518 804.276 0.768 15.646 1.984 0.53 230537. 0.1686
|
|
96.26 0.7850 0.7947 0.0328 0.0324 0.948 5.977 2.936 707.130 0.675 13.058 1.883 0.53 231466. 0.1462
|
|
100.27 0.8177 0.7764 0.0262 0.0276 0.809 5.098 2.349 603.194 0.576 10.448 1.766 0.53 232427. 0.1227
|
|
104.28 0.8504 0.7403 0.0196 0.0226 0.661 4.165 1.759 492.763 0.471 7.825 1.619 0.53 233418. 0.0973
|
|
108.29 0.8831 0.6689 0.0130 0.0172 0.505 3.180 1.169 376.240 0.359 5.198 1.409 0.53 234440. 0.0690
|
|
112.30 0.9158 0.5099 0.0065 0.0116 0.341 2.148 0.580 254.153 0.243 2.581 1.036 0.54 235490. 0.0357
|
|
116.31 0.9485 -0.0090 -0.0001 0.0058 0.170 1.071 -0.005 126.692 0.121 -0.022 -0.018 0.54 236535. 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 0.1269 0.0522 2.037 11.670 13.755 1518.808 1.319 61.183 4.108 0.57 239799. 0.6903
|
|
4.41 0.0327 0.0769 0.1259 0.0536 2.089 11.972 13.656 1558.082 1.353 60.743 3.975 0.57 240025. 0.6657
|
|
8.83 0.0654 0.1488 0.1249 0.0549 2.143 12.279 13.542 1597.987 1.387 60.233 3.844 0.57 240278. 0.6409
|
|
13.24 0.0982 0.2156 0.1237 0.0563 2.196 12.585 13.409 1637.810 1.422 59.642 3.713 0.57 240562. 0.6161
|
|
17.66 0.1309 0.2775 0.1222 0.0577 2.249 12.884 13.255 1676.768 1.456 58.958 3.586 0.57 240876. 0.5915
|
|
22.07 0.1636 0.3348 0.1206 0.0589 2.298 13.170 13.078 1713.989 1.488 58.170 3.461 0.57 241223. 0.5671
|
|
26.48 0.1963 0.3878 0.1187 0.0601 2.345 13.435 12.874 1748.524 1.518 57.265 3.340 0.57 241604. 0.5430
|
|
30.90 0.2291 0.4365 0.1166 0.0612 2.386 13.672 12.642 1779.367 1.545 56.232 3.223 0.57 242019. 0.5192
|
|
35.31 0.2618 0.4814 0.1142 0.0621 2.421 13.873 12.379 1805.483 1.567 55.061 3.110 0.57 242471. 0.4958
|
|
39.73 0.2945 0.5227 0.1114 0.0628 2.448 14.029 12.082 1825.797 1.585 53.739 3.001 0.57 242959. 0.4727
|
|
44.14 0.3272 0.5607 0.1083 0.0632 2.466 14.132 11.749 1839.218 1.597 52.259 2.897 0.57 243483. 0.4500
|
|
48.55 0.3600 0.5955 0.1049 0.0634 2.474 14.174 11.378 1844.629 1.601 50.609 2.798 0.57 244044. 0.4276
|
|
52.97 0.3927 0.6275 0.1011 0.0633 2.469 14.145 10.967 1840.899 1.598 48.782 2.702 0.57 244643. 0.4055
|
|
57.38 0.4254 0.6567 0.0970 0.0628 2.450 14.038 10.515 1826.929 1.586 46.770 2.611 0.57 245278. 0.3836
|
|
61.80 0.4581 0.6834 0.0924 0.0619 2.416 13.845 10.021 1801.782 1.564 44.573 2.523 0.57 245949. 0.3618
|
|
66.21 0.4908 0.7077 0.0875 0.0607 2.367 13.561 9.487 1764.890 1.532 42.199 2.438 0.57 246657. 0.3403
|
|
70.62 0.5236 0.7297 0.0822 0.0590 2.302 13.187 8.918 1716.240 1.490 39.666 2.357 0.57 247402. 0.3189
|
|
75.04 0.5563 0.7494 0.0767 0.0569 2.221 12.726 8.318 1656.155 1.438 36.999 2.278 0.57 248182. 0.2977
|
|
79.45 0.5890 0.7668 0.0709 0.0545 2.126 12.179 7.693 1585.051 1.376 34.218 2.201 0.57 248997. 0.2767
|
|
83.87 0.6217 0.7817 0.0650 0.0517 2.016 11.551 7.046 1503.297 1.305 31.342 2.126 0.58 249848. 0.2557
|
|
88.28 0.6545 0.7938 0.0589 0.0485 1.892 10.843 6.382 1411.189 1.225 28.386 2.051 0.58 250734. 0.2348
|
|
92.70 0.6872 0.8029 0.0526 0.0450 1.755 10.058 5.702 1308.958 1.136 25.362 1.976 0.58 251655. 0.2138
|
|
97.11 0.7199 0.8082 0.0462 0.0411 1.605 9.196 5.009 1196.803 1.039 22.281 1.898 0.58 252610. 0.1925
|
|
101.52 0.7526 0.8086 0.0397 0.0370 1.441 8.260 4.306 1074.926 0.933 19.151 1.817 0.58 253600. 0.1708
|
|
105.94 0.7854 0.8022 0.0331 0.0324 1.265 7.250 3.593 943.556 0.819 15.983 1.727 0.58 254624. 0.1484
|
|
110.35 0.8181 0.7856 0.0265 0.0276 1.077 6.170 2.875 802.990 0.697 12.787 1.624 0.58 255682. 0.1248
|
|
114.77 0.8508 0.7514 0.0198 0.0225 0.877 5.022 2.152 653.628 0.567 9.573 1.493 0.59 256773. 0.0993
|
|
119.18 0.8835 0.6826 0.0132 0.0171 0.665 3.811 1.429 496.012 0.431 6.355 1.306 0.59 257898. 0.0708
|
|
123.59 0.9162 0.5255 0.0065 0.0114 0.444 2.542 0.707 330.865 0.287 3.147 0.970 0.59 259054. 0.0370
|
|
128.01 0.9490 -0.0167 -0.0001 0.0054 0.212 1.217 -0.010 158.352 0.137 -0.046 -0.030 0.59 260199. 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 0.1275 0.0525 2.659 13.964 16.455 1982.488 1.578 73.190 3.765 0.62 261581. 0.6919
|
|
4.81 0.0327 0.0769 0.1267 0.0539 2.728 14.330 16.344 2034.532 1.619 72.697 3.644 0.62 261826. 0.6674
|
|
9.63 0.0654 0.1487 0.1256 0.0553 2.799 14.704 16.215 2087.566 1.661 72.123 3.523 0.62 262102. 0.6428
|
|
14.44 0.0981 0.2155 0.1245 0.0567 2.871 15.078 16.064 2140.629 1.703 71.452 3.404 0.62 262410. 0.6181
|
|
19.25 0.1308 0.2774 0.1231 0.0581 2.940 15.444 15.888 2192.668 1.745 70.672 3.287 0.62 262753. 0.5936
|
|
24.06 0.1635 0.3347 0.1215 0.0594 3.007 15.795 15.685 2242.497 1.785 69.765 3.172 0.62 263131. 0.5693
|
|
28.88 0.1962 0.3876 0.1197 0.0606 3.069 16.122 15.449 2288.839 1.821 68.718 3.062 0.62 263546. 0.5452
|
|
33.69 0.2289 0.4364 0.1176 0.0617 3.125 16.414 15.179 2330.334 1.854 67.516 2.954 0.62 263999. 0.5215
|
|
38.50 0.2617 0.4813 0.1152 0.0626 3.172 16.662 14.871 2365.588 1.882 66.144 2.851 0.62 264492. 0.4982
|
|
43.32 0.2944 0.5226 0.1125 0.0634 3.209 16.856 14.521 2393.169 1.904 64.591 2.752 0.62 265024. 0.4752
|
|
48.13 0.3271 0.5607 0.1095 0.0639 3.234 16.986 14.128 2411.627 1.919 62.843 2.657 0.62 265597. 0.4526
|
|
52.94 0.3598 0.5956 0.1061 0.0641 3.245 17.042 13.689 2419.485 1.925 60.890 2.566 0.62 266210. 0.4302
|
|
57.76 0.3925 0.6277 0.1023 0.0640 3.239 17.012 13.202 2415.254 1.922 58.720 2.479 0.62 266863. 0.4082
|
|
62.57 0.4252 0.6571 0.0981 0.0635 3.215 16.887 12.663 2397.484 1.908 56.326 2.396 0.62 267556. 0.3863
|
|
67.38 0.4579 0.6841 0.0936 0.0626 3.171 16.657 12.074 2364.922 1.882 53.706 2.316 0.62 268290. 0.3646
|
|
72.19 0.4906 0.7086 0.0886 0.0614 3.107 16.318 11.436 2316.804 1.844 50.868 2.239 0.62 269063. 0.3431
|
|
77.01 0.5233 0.7309 0.0833 0.0597 3.021 15.870 10.754 2253.087 1.793 47.836 2.165 0.62 269876. 0.3217
|
|
81.82 0.5560 0.7509 0.0778 0.0576 2.916 15.314 10.035 2174.207 1.730 44.638 2.094 0.63 270727. 0.3005
|
|
86.63 0.5887 0.7687 0.0720 0.0551 2.790 14.656 9.285 2080.724 1.656 41.300 2.024 0.63 271617. 0.2795
|
|
91.45 0.6214 0.7841 0.0659 0.0523 2.646 13.898 8.508 1973.142 1.570 37.846 1.956 0.63 272546. 0.2585
|
|
96.26 0.6541 0.7968 0.0597 0.0490 2.483 13.044 7.710 1851.871 1.474 34.292 1.888 0.63 273513. 0.2376
|
|
101.07 0.6868 0.8066 0.0534 0.0455 2.303 12.095 6.892 1717.224 1.367 30.655 1.820 0.63 274517. 0.2165
|
|
105.88 0.7195 0.8127 0.0469 0.0416 2.105 11.055 6.058 1569.465 1.249 26.947 1.751 0.63 275560. 0.1953
|
|
110.70 0.7523 0.8142 0.0404 0.0373 1.889 9.923 5.211 1408.861 1.121 23.179 1.678 0.63 276639. 0.1735
|
|
115.51 0.7850 0.8091 0.0337 0.0327 1.657 8.704 4.353 1235.714 0.983 19.363 1.598 0.64 277756. 0.1511
|
|
120.32 0.8177 0.7943 0.0270 0.0278 1.409 7.399 3.487 1050.409 0.836 15.511 1.506 0.64 278910. 0.1274
|
|
125.14 0.8504 0.7627 0.0203 0.0226 1.145 6.011 2.616 853.470 0.679 11.635 1.390 0.64 280100. 0.1019
|
|
129.95 0.8831 0.6976 0.0135 0.0171 0.866 4.547 1.743 645.609 0.514 7.753 1.225 0.64 281326. 0.0733
|
|
134.76 0.9158 0.5466 0.0068 0.0113 0.574 3.013 0.873 427.778 0.340 3.882 0.925 0.64 282587. 0.0392
|
|
139.58 0.9485 0.0087 0.0000 0.0053 0.269 1.411 0.006 200.318 0.159 0.028 0.014 0.64 283839. 0.0001
|
|
|
|
|
|
|
|
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 0.1282 0.0530 3.413 16.550 19.417 2545.415 1.870 86.366 3.460 0.67 283358. 0.6908
|
|
5.22 0.0327 0.0766 0.1274 0.0544 3.503 16.984 19.296 2612.199 1.919 85.831 3.351 0.67 283623. 0.6669
|
|
10.43 0.0654 0.1483 0.1265 0.0558 3.595 17.428 19.155 2680.473 1.969 85.201 3.241 0.67 283921. 0.6428
|
|
15.65 0.0982 0.2150 0.1254 0.0573 3.686 17.873 18.989 2749.020 2.019 84.461 3.133 0.67 284254. 0.6186
|
|
20.87 0.1309 0.2769 0.1241 0.0587 3.777 18.312 18.793 2816.489 2.069 83.590 3.026 0.67 284624. 0.5945
|
|
26.08 0.1636 0.3342 0.1226 0.0600 3.864 18.734 18.564 2881.339 2.117 82.571 2.922 0.67 285034. 0.5705
|
|
31.30 0.1963 0.3871 0.1208 0.0613 3.945 19.127 18.297 2941.895 2.161 81.383 2.821 0.67 285484. 0.5467
|
|
36.52 0.2291 0.4359 0.1188 0.0624 4.018 19.482 17.987 2996.373 2.201 80.008 2.723 0.67 285976. 0.5233
|
|
41.74 0.2618 0.4809 0.1164 0.0634 4.081 19.784 17.633 3042.899 2.235 78.430 2.628 0.67 286510. 0.5001
|
|
46.95 0.2945 0.5223 0.1138 0.0641 4.130 20.022 17.228 3079.562 2.262 76.631 2.537 0.67 287089. 0.4772
|
|
52.17 0.3272 0.5604 0.1107 0.0647 4.163 20.184 16.771 3104.410 2.280 74.597 2.450 0.67 287710. 0.4547
|
|
57.39 0.3600 0.5955 0.1073 0.0649 4.178 20.256 16.258 3115.466 2.289 72.315 2.367 0.67 288376. 0.4324
|
|
62.60 0.3927 0.6277 0.1036 0.0648 4.172 20.225 15.686 3110.773 2.285 69.771 2.287 0.67 289086. 0.4104
|
|
67.82 0.4254 0.6573 0.0994 0.0643 4.142 20.080 15.053 3088.438 2.269 66.956 2.211 0.67 289840. 0.3886
|
|
73.04 0.4581 0.6844 0.0948 0.0635 4.086 19.810 14.358 3046.824 2.238 63.866 2.137 0.67 290637. 0.3670
|
|
78.25 0.4909 0.7092 0.0898 0.0622 4.003 19.407 13.604 2984.914 2.193 60.513 2.067 0.68 291477. 0.3455
|
|
83.47 0.5236 0.7318 0.0845 0.0605 3.892 18.872 12.797 2902.636 2.132 56.923 2.000 0.68 292360. 0.3241
|
|
88.69 0.5563 0.7522 0.0789 0.0583 3.756 18.209 11.945 2800.570 2.057 53.130 1.935 0.68 293285. 0.3030
|
|
93.90 0.5890 0.7703 0.0730 0.0558 3.593 17.421 11.054 2679.475 1.968 49.168 1.871 0.68 294252. 0.2819
|
|
99.12 0.6218 0.7861 0.0669 0.0529 3.406 16.515 10.131 2540.038 1.866 45.064 1.809 0.68 295261. 0.2609
|
|
104.34 0.6545 0.7994 0.0606 0.0496 3.195 15.492 9.181 2382.805 1.750 40.839 1.748 0.68 296310. 0.2400
|
|
109.55 0.6872 0.8098 0.0542 0.0460 2.961 14.357 8.209 2208.201 1.622 36.512 1.686 0.68 297401. 0.2189
|
|
114.77 0.7199 0.8166 0.0476 0.0420 2.704 13.111 7.216 2016.572 1.481 32.097 1.623 0.69 298532. 0.1976
|
|
119.99 0.7527 0.8190 0.0410 0.0377 2.425 11.757 6.207 1808.259 1.328 27.609 1.557 0.69 299704. 0.1758
|
|
125.21 0.7854 0.8151 0.0342 0.0330 2.124 10.297 5.185 1583.657 1.163 23.062 1.485 0.69 300916. 0.1532
|
|
130.42 0.8181 0.8016 0.0274 0.0280 1.801 8.734 4.152 1343.268 0.987 18.469 1.402 0.69 302168. 0.1294
|
|
135.64 0.8508 0.7718 0.0206 0.0227 1.459 7.073 3.113 1087.796 0.799 13.846 1.298 0.69 303459. 0.1038
|
|
140.86 0.8836 0.7089 0.0137 0.0170 1.097 5.320 2.071 818.251 0.601 9.212 1.148 0.69 304790. 0.0749
|
|
146.07 0.9163 0.5591 0.0068 0.0112 0.719 3.485 1.032 536.020 0.394 4.590 0.873 0.70 306157. 0.0402
|
|
151.29 0.9490 -0.0047 0.0000 0.0050 0.324 1.571 -0.004 241.595 0.177 -0.017 -0.007 0.70 307506. 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 0.1289 0.0542 4.361 19.633 22.643 3252.005 2.218 100.718 3.158 0.72 305130. 0.6809
|
|
5.62 0.0327 0.0754 0.1282 0.0556 4.472 20.132 22.517 3334.512 2.274 100.156 3.063 0.72 305414. 0.6585
|
|
11.24 0.0655 0.1462 0.1273 0.0570 4.585 20.641 22.367 3418.884 2.332 99.489 2.967 0.72 305733. 0.6359
|
|
16.86 0.0982 0.2123 0.1263 0.0584 4.698 21.152 22.189 3503.590 2.390 98.696 2.873 0.72 306090. 0.6131
|
|
22.48 0.1309 0.2738 0.1251 0.0598 4.810 21.655 21.977 3586.928 2.447 97.754 2.779 0.72 306488. 0.5903
|
|
28.09 0.1636 0.3310 0.1237 0.0612 4.917 22.139 21.726 3666.973 2.501 96.638 2.687 0.72 306929. 0.5676
|
|
33.71 0.1964 0.3840 0.1220 0.0624 5.018 22.589 21.431 3741.639 2.552 95.324 2.598 0.72 307413. 0.5449
|
|
39.33 0.2291 0.4330 0.1200 0.0635 5.108 22.994 21.085 3808.725 2.598 93.788 2.511 0.72 307943. 0.5224
|
|
44.95 0.2618 0.4783 0.1178 0.0645 5.184 23.340 20.685 3865.942 2.637 92.008 2.427 0.72 308519. 0.5001
|
|
50.57 0.2946 0.5200 0.1151 0.0652 5.245 23.612 20.226 3910.964 2.668 89.964 2.346 0.72 309143. 0.4780
|
|
56.19 0.3273 0.5585 0.1122 0.0657 5.285 23.795 19.703 3941.386 2.688 87.637 2.267 0.72 309814. 0.4560
|
|
61.81 0.3600 0.5939 0.1088 0.0660 5.303 23.876 19.112 3954.754 2.698 85.011 2.192 0.72 310533. 0.4342
|
|
67.43 0.3927 0.6265 0.1050 0.0659 5.295 23.839 18.451 3948.551 2.693 82.071 2.119 0.72 311299. 0.4125
|
|
73.05 0.4255 0.6564 0.1009 0.0654 5.257 23.668 17.717 3920.295 2.674 78.806 2.050 0.73 312113. 0.3910
|
|
78.66 0.4582 0.6838 0.0963 0.0645 5.187 23.351 16.909 3867.738 2.638 75.210 1.983 0.73 312974. 0.3695
|
|
84.28 0.4909 0.7089 0.0913 0.0632 5.082 22.878 16.029 3789.380 2.585 71.297 1.919 0.73 313881. 0.3481
|
|
89.90 0.5237 0.7318 0.0859 0.0615 4.942 22.247 15.085 3684.947 2.513 67.097 1.857 0.73 314834. 0.3268
|
|
95.52 0.5564 0.7525 0.0802 0.0593 4.767 21.463 14.086 3555.105 2.425 62.652 1.797 0.73 315833. 0.3056
|
|
101.14 0.5891 0.7711 0.0742 0.0567 4.561 20.532 13.040 3400.844 2.320 58.002 1.739 0.73 316876. 0.2846
|
|
106.76 0.6218 0.7874 0.0681 0.0538 4.322 19.459 11.956 3223.078 2.198 53.178 1.682 0.73 317965. 0.2636
|
|
112.38 0.6546 0.8013 0.0617 0.0504 4.053 18.248 10.838 3022.552 2.062 48.209 1.626 0.73 319097. 0.2426
|
|
118.00 0.6873 0.8123 0.0552 0.0467 3.755 16.903 9.693 2799.830 1.910 43.115 1.570 0.74 320274. 0.2215
|
|
123.62 0.7200 0.8199 0.0485 0.0426 3.427 15.428 8.524 2555.371 1.743 37.915 1.513 0.74 321494. 0.2002
|
|
129.23 0.7528 0.8232 0.0418 0.0382 3.070 13.823 7.335 2289.657 1.562 32.625 1.453 0.74 322758. 0.1783
|
|
134.85 0.7855 0.8203 0.0349 0.0334 2.686 12.095 6.129 2003.308 1.366 27.260 1.388 0.74 324064. 0.1557
|
|
140.47 0.8182 0.8080 0.0280 0.0283 2.276 10.246 4.910 1697.179 1.158 21.838 1.312 0.74 325414. 0.1317
|
|
146.09 0.8509 0.7793 0.0210 0.0229 1.841 8.286 3.682 1372.476 0.936 16.377 1.217 0.75 326806. 0.1058
|
|
151.71 0.8837 0.7170 0.0139 0.0172 1.382 6.224 2.450 1030.900 0.703 10.898 1.078 0.75 328239. 0.0765
|
|
157.33 0.9164 0.5656 0.0069 0.0113 0.905 4.074 1.220 674.737 0.460 5.426 0.820 0.75 329712. 0.0410
|
|
162.95 0.9491 -0.0081 0.0000 0.0051 0.409 1.842 -0.008 305.117 0.208 -0.034 -0.011 0.75 331161. 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 0.1296 0.0568 5.621 23.619 26.130 4191.541 2.668 116.226 2.828 0.77 326897. 0.6549
|
|
6.02 0.0327 0.0725 0.1290 0.0582 5.754 24.176 26.002 4290.547 2.731 115.656 2.749 0.77 327198. 0.6351
|
|
12.04 0.0654 0.1409 0.1282 0.0595 5.889 24.745 25.848 4391.417 2.796 114.974 2.670 0.77 327538. 0.6150
|
|
18.06 0.0982 0.2051 0.1273 0.0609 6.024 25.312 25.664 4492.116 2.860 114.155 2.591 0.77 327919. 0.5948
|
|
24.08 0.1309 0.2653 0.1262 0.0622 6.156 25.866 25.443 4590.416 2.922 113.168 2.514 0.77 328343. 0.5746
|
|
30.10 0.1636 0.3217 0.1249 0.0635 6.281 26.393 25.176 4683.833 2.982 111.985 2.438 0.77 328813. 0.5543
|
|
36.11 0.1963 0.3743 0.1233 0.0647 6.396 26.877 24.859 4769.757 3.037 110.571 2.364 0.77 329331. 0.5340
|
|
42.13 0.2291 0.4233 0.1214 0.0657 6.498 27.304 24.483 4845.492 3.085 108.899 2.292 0.77 329898. 0.5138
|
|
48.15 0.2618 0.4690 0.1192 0.0666 6.582 27.658 24.042 4908.361 3.125 106.937 2.222 0.77 330516. 0.4936
|
|
54.17 0.2945 0.5114 0.1167 0.0672 6.646 27.925 23.530 4955.712 3.155 104.662 2.154 0.77 331185. 0.4733
|
|
60.19 0.3272 0.5508 0.1138 0.0676 6.685 28.089 22.943 4984.901 3.173 102.048 2.088 0.77 331905. 0.4531
|
|
66.21 0.3599 0.5873 0.1105 0.0677 6.696 28.136 22.275 4993.191 3.179 99.077 2.023 0.78 332677. 0.4327
|
|
72.23 0.3927 0.6210 0.1067 0.0675 6.675 28.049 21.522 4977.747 3.169 95.730 1.961 0.78 333500. 0.4122
|
|
78.25 0.4254 0.6520 0.1026 0.0669 6.619 27.812 20.682 4935.710 3.142 91.993 1.901 0.78 334374. 0.3916
|
|
84.27 0.4581 0.6804 0.0980 0.0660 6.523 27.410 19.753 4864.417 3.097 87.862 1.842 0.78 335299. 0.3709
|
|
90.29 0.4908 0.7064 0.0929 0.0646 6.386 26.833 18.738 4761.957 3.032 83.348 1.785 0.78 336273. 0.3501
|
|
96.30 0.5236 0.7302 0.0875 0.0628 6.206 26.077 17.646 4627.813 2.946 78.489 1.729 0.78 337297. 0.3292
|
|
102.32 0.5563 0.7517 0.0818 0.0605 5.984 25.146 16.486 4462.635 2.841 73.331 1.676 0.78 338369. 0.3083
|
|
108.34 0.5890 0.7709 0.0757 0.0579 5.723 24.046 15.271 4267.451 2.717 67.925 1.623 0.78 339490. 0.2874
|
|
114.36 0.6217 0.7879 0.0695 0.0548 5.422 22.783 14.008 4043.172 2.574 62.308 1.571 0.79 340658. 0.2665
|
|
120.38 0.6544 0.8023 0.0630 0.0514 5.083 21.360 12.705 3790.647 2.413 56.514 1.520 0.79 341873. 0.2455
|
|
126.40 0.6872 0.8139 0.0564 0.0476 4.708 19.781 11.369 3510.563 2.235 50.569 1.469 0.79 343136. 0.2244
|
|
132.42 0.7199 0.8222 0.0496 0.0434 4.296 18.052 10.003 3203.608 2.039 44.494 1.416 0.79 344445. 0.2030
|
|
138.44 0.7526 0.8259 0.0427 0.0389 3.850 16.176 8.613 2870.728 1.828 38.309 1.361 0.79 345800. 0.1809
|
|
144.46 0.7853 0.8230 0.0357 0.0341 3.370 14.161 7.201 2513.161 1.600 32.030 1.300 0.79 347201. 0.1580
|
|
150.48 0.8181 0.8099 0.0286 0.0289 2.860 12.017 5.772 2132.651 1.358 25.676 1.228 0.80 348647. 0.1337
|
|
156.49 0.8508 0.7785 0.0215 0.0235 2.322 9.756 4.332 1731.454 1.102 19.268 1.135 0.80 350139. 0.1070
|
|
162.51 0.8835 0.7101 0.0143 0.0178 1.760 7.396 2.884 1312.580 0.836 12.830 0.997 0.80 351675. 0.0767
|
|
168.53 0.9162 0.5473 0.0071 0.0119 1.180 4.958 1.437 879.823 0.560 6.391 0.741 0.80 353253. 0.0402
|
|
174.55 0.9489 -0.0078 0.0000 0.0059 0.584 2.455 -0.010 435.696 0.277 -0.044 -0.010 0.80 354809. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1302 0.0616 7.397 29.138 29.860 5515.782 3.292 132.817 2.455 0.82 348657. 0.6080
|
|
6.42 0.0327 0.0674 0.1296 0.0629 7.554 29.758 29.735 5633.225 3.362 132.259 2.394 0.82 348976. 0.5915
|
|
12.84 0.0655 0.1313 0.1290 0.0643 7.714 30.387 29.584 5752.207 3.433 131.589 2.333 0.82 349336. 0.5749
|
|
19.26 0.0982 0.1919 0.1282 0.0656 7.871 31.008 29.401 5869.750 3.503 130.775 2.272 0.82 349739. 0.5582
|
|
25.69 0.1309 0.2491 0.1272 0.0668 8.023 31.604 29.177 5982.604 3.571 129.781 2.212 0.82 350189. 0.5414
|
|
32.11 0.1636 0.3032 0.1260 0.0680 8.163 32.157 28.905 6087.269 3.633 128.569 2.154 0.82 350688. 0.5247
|
|
38.53 0.1964 0.3542 0.1246 0.0690 8.288 32.648 28.574 6180.179 3.689 127.098 2.097 0.82 351239. 0.5079
|
|
44.95 0.2291 0.4024 0.1228 0.0699 8.392 33.058 28.176 6257.854 3.735 125.328 2.042 0.82 351843. 0.4912
|
|
51.37 0.2618 0.4480 0.1208 0.0706 8.471 33.371 27.702 6317.018 3.770 123.220 1.989 0.82 352502. 0.4744
|
|
57.79 0.2946 0.4909 0.1183 0.0710 8.522 33.570 27.145 6354.761 3.793 120.742 1.937 0.83 353216. 0.4574
|
|
64.21 0.3273 0.5313 0.1155 0.0712 8.540 33.642 26.498 6368.432 3.801 117.863 1.887 0.83 353986. 0.4402
|
|
70.64 0.3600 0.5692 0.1123 0.0710 8.523 33.574 25.755 6355.428 3.793 114.558 1.838 0.83 354811. 0.4227
|
|
77.06 0.3927 0.6046 0.1086 0.0705 8.466 33.350 24.911 6313.040 3.768 110.803 1.790 0.83 355692. 0.4048
|
|
83.48 0.4255 0.6376 0.1044 0.0697 8.366 32.956 23.962 6238.489 3.723 106.582 1.742 0.83 356628. 0.3864
|
|
89.90 0.4582 0.6681 0.0998 0.0685 8.219 32.378 22.907 6129.132 3.658 101.890 1.695 0.83 357618. 0.3676
|
|
96.32 0.4909 0.6962 0.0948 0.0668 8.023 31.607 21.749 5983.113 3.571 96.739 1.649 0.83 358661. 0.3484
|
|
102.74 0.5236 0.7220 0.0893 0.0648 7.778 30.640 20.498 5800.061 3.462 91.173 1.603 0.83 359757. 0.3288
|
|
109.16 0.5564 0.7454 0.0835 0.0624 7.484 29.481 19.165 5580.735 3.331 85.246 1.558 0.83 360905. 0.3090
|
|
115.59 0.5891 0.7665 0.0774 0.0595 7.143 28.137 17.764 5326.341 3.179 79.014 1.513 0.84 362104. 0.2889
|
|
122.01 0.6218 0.7852 0.0711 0.0563 6.756 26.614 16.305 5038.054 3.007 72.526 1.468 0.84 363354. 0.2686
|
|
128.43 0.6546 0.8011 0.0645 0.0527 6.326 24.921 14.798 4717.468 2.816 65.821 1.423 0.84 364654. 0.2480
|
|
134.85 0.6873 0.8135 0.0577 0.0488 5.856 23.068 13.249 4366.714 2.606 58.930 1.376 0.84 366003. 0.2270
|
|
141.27 0.7200 0.8216 0.0508 0.0446 5.348 21.067 11.663 3987.865 2.380 51.878 1.327 0.84 367403. 0.2053
|
|
147.69 0.7527 0.8239 0.0438 0.0400 4.802 18.917 10.047 3581.000 2.137 44.689 1.273 0.85 368851. 0.1828
|
|
154.11 0.7855 0.8183 0.0366 0.0352 4.221 16.627 8.404 3147.448 1.878 37.382 1.211 0.85 370348. 0.1591
|
|
160.54 0.8182 0.7997 0.0294 0.0301 3.608 14.213 6.740 2690.525 1.606 29.979 1.136 0.85 371893. 0.1337
|
|
166.96 0.8509 0.7585 0.0221 0.0247 2.970 11.698 5.059 2214.371 1.322 22.504 1.036 0.85 373486. 0.1056
|
|
173.38 0.8837 0.6738 0.0147 0.0193 2.312 9.107 3.369 1724.012 1.029 14.987 0.886 0.85 375126. 0.0737
|
|
179.80 0.9164 0.4895 0.0073 0.0137 1.643 6.473 1.678 1225.368 0.731 7.462 0.621 0.86 376811. 0.0364
|
|
186.22 0.9491 -0.0059 0.0000 0.0081 0.969 3.819 -0.011 722.839 0.431 -0.051 -0.007 0.86 378489. 0.0000
|
|
|
|
|
|
|