501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x5.5MR (18x55MR.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 0.0720 0.0249 0.004 0.239 0.241 2.825 0.027 1.072 38.696 0.07 36929. 0.6193
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0.27 0.0156 0.0441 0.0704 0.0249 0.004 0.239 0.235 2.824 0.027 1.047 37.828 0.07 36945. 0.5984
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0.53 0.0312 0.0862 0.0687 0.0249 0.004 0.238 0.230 2.820 0.027 1.022 36.945 0.07 36962. 0.5772
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0.80 0.0468 0.1261 0.0668 0.0248 0.004 0.238 0.224 2.813 0.027 0.995 36.051 0.07 36980. 0.5557
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1.06 0.0624 0.1639 0.0650 0.0247 0.004 0.237 0.217 2.805 0.027 0.967 35.145 0.07 36998. 0.5341
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1.33 0.0780 0.1995 0.0630 0.0246 0.004 0.236 0.211 2.794 0.027 0.938 34.222 0.07 37018. 0.5122
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1.60 0.0936 0.2329 0.0610 0.0245 0.004 0.235 0.204 2.780 0.027 0.907 33.285 0.07 37038. 0.4901
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1.86 0.1092 0.2639 0.0589 0.0244 0.004 0.234 0.197 2.763 0.026 0.876 32.328 0.07 37059. 0.4677
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2.13 0.1248 0.2925 0.0567 0.0242 0.004 0.232 0.190 2.744 0.026 0.844 31.352 0.07 37081. 0.4451
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2.39 0.1404 0.3185 0.0544 0.0240 0.004 0.230 0.182 2.721 0.026 0.810 30.350 0.07 37104. 0.4221
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2.66 0.1560 0.3419 0.0521 0.0238 0.004 0.228 0.174 2.695 0.026 0.775 29.322 0.07 37128. 0.3989
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2.93 0.1717 0.3626 0.0497 0.0235 0.004 0.225 0.166 2.666 0.025 0.739 28.265 0.07 37153. 0.3755
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3.19 0.1873 0.3803 0.0472 0.0232 0.004 0.223 0.158 2.633 0.025 0.702 27.176 0.07 37179. 0.3519
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3.46 0.2029 0.3949 0.0446 0.0229 0.003 0.220 0.149 2.598 0.025 0.664 26.052 0.07 37205. 0.3281
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3.72 0.2185 0.4063 0.0420 0.0226 0.003 0.216 0.140 2.559 0.024 0.625 24.889 0.07 37233. 0.3040
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3.99 0.2341 0.4142 0.0393 0.0222 0.003 0.213 0.131 2.517 0.024 0.585 23.682 0.07 37262. 0.2799
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4.26 0.2497 0.4184 0.0365 0.0218 0.003 0.209 0.122 2.472 0.024 0.544 22.426 0.07 37291. 0.2556
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4.52 0.2653 0.4186 0.0337 0.0214 0.003 0.205 0.113 2.423 0.023 0.502 21.114 0.07 37322. 0.2311
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4.79 0.2809 0.4143 0.0308 0.0209 0.003 0.200 0.103 2.370 0.023 0.459 19.740 0.07 37354. 0.2067
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5.05 0.2965 0.4054 0.0279 0.0204 0.003 0.196 0.093 2.314 0.022 0.415 18.296 0.07 37387. 0.1822
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5.32 0.3121 0.3912 0.0249 0.0199 0.003 0.191 0.083 2.254 0.022 0.371 16.772 0.07 37421. 0.1579
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5.59 0.3277 0.3712 0.0219 0.0193 0.003 0.185 0.073 2.191 0.021 0.326 15.157 0.07 37456. 0.1337
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5.85 0.3433 0.3448 0.0188 0.0187 0.003 0.180 0.063 2.124 0.020 0.280 13.440 0.07 37493. 0.1099
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6.12 0.3589 0.3113 0.0157 0.0181 0.003 0.174 0.053 2.053 0.020 0.234 11.607 0.07 37530. 0.0867
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6.38 0.3745 0.2698 0.0126 0.0174 0.003 0.167 0.042 1.978 0.019 0.187 9.642 0.07 37569. 0.0645
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6.65 0.3901 0.2195 0.0094 0.0168 0.003 0.161 0.032 1.901 0.018 0.140 7.531 0.07 37608. 0.0436
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6.92 0.4057 0.1594 0.0063 0.0160 0.002 0.154 0.021 1.820 0.017 0.094 5.256 0.07 37649. 0.0249
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7.18 0.4213 0.0873 0.0032 0.0153 0.002 0.147 0.011 1.735 0.017 0.047 2.774 0.07 37691. 0.0093
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7.45 0.4369 0.0004 0.0000 0.0145 0.002 0.139 0.000 1.646 0.016 0.000 0.012 0.07 37732. 0.0000
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7.71 0.4525
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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 0.0723 0.0229 0.028 0.877 0.967 20.751 0.099 4.303 21.144 0.14 73857. 0.6779
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0.52 0.0151 0.0468 0.0707 0.0229 0.028 0.876 0.946 20.738 0.099 4.207 20.687 0.14 73889. 0.6558
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1.03 0.0303 0.0915 0.0690 0.0228 0.028 0.875 0.923 20.709 0.099 4.107 20.224 0.14 73922. 0.6335
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1.55 0.0454 0.1341 0.0672 0.0228 0.028 0.873 0.900 20.656 0.099 4.002 19.759 0.14 73956. 0.6110
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2.06 0.0606 0.1746 0.0654 0.0227 0.028 0.870 0.876 20.587 0.098 3.895 19.291 0.14 73992. 0.5884
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2.58 0.0757 0.2129 0.0635 0.0226 0.027 0.866 0.850 20.496 0.098 3.782 18.817 0.14 74029. 0.5656
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3.10 0.0908 0.2489 0.0616 0.0225 0.027 0.861 0.824 20.382 0.097 3.665 18.339 0.14 74068. 0.5427
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3.61 0.1060 0.2828 0.0596 0.0223 0.027 0.856 0.797 20.246 0.097 3.545 17.854 0.14 74109. 0.5196
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4.13 0.1211 0.3143 0.0575 0.0221 0.027 0.849 0.769 20.083 0.096 3.420 17.363 0.14 74151. 0.4963
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4.64 0.1362 0.3434 0.0553 0.0219 0.027 0.841 0.740 19.895 0.095 3.290 16.863 0.14 74195. 0.4728
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5.16 0.1514 0.3700 0.0530 0.0217 0.026 0.832 0.709 19.678 0.094 3.156 16.353 0.14 74241. 0.4490
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5.68 0.1665 0.3940 0.0507 0.0214 0.026 0.821 0.678 19.434 0.093 3.017 15.832 0.14 74289. 0.4251
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6.19 0.1817 0.4153 0.0483 0.0211 0.026 0.810 0.646 19.163 0.091 2.875 15.298 0.14 74338. 0.4009
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6.71 0.1968 0.4338 0.0458 0.0208 0.025 0.797 0.613 18.864 0.090 2.729 14.750 0.14 74389. 0.3766
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7.23 0.2119 0.4493 0.0433 0.0204 0.025 0.783 0.580 18.537 0.089 2.579 14.186 0.14 74442. 0.3521
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7.74 0.2271 0.4616 0.0407 0.0200 0.024 0.768 0.545 18.180 0.087 2.425 13.603 0.14 74497. 0.3274
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8.26 0.2422 0.4705 0.0381 0.0196 0.024 0.752 0.510 17.794 0.085 2.268 12.998 0.14 74554. 0.3026
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8.77 0.2574 0.4757 0.0354 0.0192 0.023 0.734 0.474 17.376 0.083 2.107 12.367 0.14 74613. 0.2775
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9.29 0.2725 0.4768 0.0327 0.0187 0.023 0.715 0.437 16.928 0.081 1.944 11.708 0.14 74673. 0.2523
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9.81 0.2876 0.4735 0.0298 0.0181 0.022 0.695 0.399 16.448 0.079 1.777 11.014 0.14 74736. 0.2269
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10.32 0.3028 0.4652 0.0270 0.0176 0.021 0.673 0.361 15.935 0.076 1.607 10.281 0.14 74801. 0.2014
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10.84 0.3179 0.4514 0.0241 0.0170 0.021 0.650 0.322 15.389 0.073 1.434 9.501 0.14 74868. 0.1758
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11.35 0.3330 0.4313 0.0211 0.0163 0.020 0.626 0.283 14.811 0.071 1.259 8.666 0.14 74937. 0.1503
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11.87 0.3482 0.4041 0.0182 0.0157 0.019 0.600 0.243 14.199 0.068 1.081 7.765 0.14 75008. 0.1248
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12.39 0.3633 0.3686 0.0152 0.0149 0.018 0.573 0.203 13.555 0.065 0.902 6.788 0.14 75082. 0.0997
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12.90 0.3785 0.3235 0.0121 0.0142 0.017 0.544 0.162 12.879 0.061 0.722 5.719 0.14 75157. 0.0751
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13.42 0.3936 0.2673 0.0091 0.0134 0.016 0.514 0.122 12.174 0.058 0.542 4.543 0.14 75235. 0.0517
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13.93 0.4087 0.1976 0.0061 0.0126 0.015 0.484 0.082 11.442 0.055 0.363 3.235 0.14 75315. 0.0301
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14.45 0.4239 0.1110 0.0031 0.0118 0.014 0.451 0.041 10.679 0.051 0.184 1.753 0.14 75396. 0.0116
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14.97 0.4390 0.0010 0.0000 0.0109 0.013 0.417 0.000 9.874 0.047 0.001 0.015 0.14 75472. 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 0.0726 0.0220 0.090 1.899 2.185 67.390 0.215 9.719 14.706 0.21 110784. 0.7086
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0.78 0.0152 0.0489 0.0710 0.0220 0.090 1.897 2.136 67.343 0.214 9.503 14.389 0.21 110831. 0.6856
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1.55 0.0303 0.0957 0.0693 0.0220 0.090 1.894 2.086 67.237 0.214 9.277 14.069 0.21 110881. 0.6623
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2.33 0.0455 0.1403 0.0675 0.0219 0.090 1.889 2.032 67.047 0.213 9.040 13.749 0.21 110933. 0.6389
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3.10 0.0607 0.1827 0.0657 0.0218 0.090 1.882 1.977 66.801 0.213 8.796 13.427 0.21 110987. 0.6155
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3.88 0.0759 0.2228 0.0638 0.0217 0.089 1.873 1.920 66.478 0.212 8.542 13.102 0.21 111043. 0.5919
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4.65 0.0910 0.2607 0.0618 0.0216 0.089 1.861 1.861 66.069 0.210 8.278 12.776 0.21 111102. 0.5681
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5.43 0.1062 0.2963 0.0598 0.0214 0.088 1.848 1.800 65.583 0.209 8.005 12.446 0.21 111163. 0.5443
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6.21 0.1214 0.3296 0.0577 0.0212 0.087 1.831 1.736 65.002 0.207 7.722 12.113 0.21 111227. 0.5203
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6.98 0.1365 0.3604 0.0555 0.0210 0.086 1.812 1.670 64.328 0.205 7.428 11.775 0.21 111294. 0.4961
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7.76 0.1517 0.3888 0.0532 0.0208 0.085 1.791 1.602 63.552 0.202 7.125 11.432 0.21 111362. 0.4716
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8.53 0.1669 0.4146 0.0509 0.0205 0.084 1.766 1.531 62.679 0.200 6.811 11.081 0.21 111434. 0.4470
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9.31 0.1820 0.4377 0.0485 0.0202 0.083 1.739 1.459 61.708 0.196 6.489 10.724 0.21 111508. 0.4222
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10.09 0.1972 0.4579 0.0460 0.0198 0.081 1.708 1.385 60.635 0.193 6.159 10.358 0.21 111585. 0.3973
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10.86 0.2124 0.4752 0.0435 0.0194 0.080 1.675 1.308 59.460 0.189 5.820 9.981 0.21 111665. 0.3722
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11.64 0.2276 0.4894 0.0409 0.0190 0.078 1.639 1.230 58.178 0.185 5.473 9.593 0.21 111748. 0.3469
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12.41 0.2427 0.5001 0.0382 0.0185 0.076 1.600 1.151 56.787 0.181 5.118 9.190 0.21 111833. 0.3213
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13.19 0.2579 0.5071 0.0355 0.0181 0.074 1.558 1.069 55.285 0.176 4.755 8.770 0.21 111922. 0.2956
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13.96 0.2731 0.5100 0.0327 0.0175 0.072 1.512 0.986 53.669 0.171 4.385 8.331 0.22 112013. 0.2696
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14.74 0.2882 0.5084 0.0299 0.0170 0.070 1.463 0.901 51.936 0.165 4.007 7.868 0.22 112108. 0.2435
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15.52 0.3034 0.5018 0.0271 0.0164 0.067 1.411 0.815 50.085 0.159 3.624 7.377 0.22 112206. 0.2171
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16.29 0.3186 0.4894 0.0241 0.0157 0.065 1.356 0.727 48.115 0.153 3.234 6.853 0.22 112306. 0.1905
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17.07 0.3338 0.4705 0.0212 0.0150 0.062 1.297 0.638 46.024 0.146 2.838 6.288 0.22 112410. 0.1637
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17.84 0.3489 0.4439 0.0182 0.0143 0.059 1.234 0.548 43.814 0.139 2.438 5.674 0.22 112518. 0.1369
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18.62 0.3641 0.4082 0.0152 0.0136 0.056 1.169 0.457 41.484 0.132 2.034 5.001 0.22 112628. 0.1102
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19.39 0.3793 0.3617 0.0122 0.0128 0.052 1.100 0.366 39.041 0.124 1.629 4.254 0.22 112742. 0.0839
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20.17 0.3944 0.3023 0.0091 0.0119 0.049 1.028 0.275 36.494 0.116 1.223 3.418 0.22 112859. 0.0584
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20.95 0.4096 0.2266 0.0061 0.0111 0.045 0.954 0.184 33.847 0.108 0.819 2.467 0.22 112979. 0.0345
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21.72 0.4248 0.1296 0.0031 0.0102 0.042 0.876 0.093 31.091 0.099 0.415 1.361 0.22 113101. 0.0135
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22.50 0.4399 0.0011 0.0000 0.0092 0.038 0.794 0.001 28.170 0.090 0.003 0.011 0.22 113213. 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 0.0729 0.0216 0.210 3.306 3.904 156.462 0.374 17.366 11.318 0.29 147709. 0.7290
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1.03 0.0152 0.0502 0.0713 0.0215 0.210 3.303 3.817 156.332 0.373 16.979 11.075 0.29 147772. 0.7054
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2.07 0.0304 0.0983 0.0696 0.0215 0.209 3.298 3.726 156.062 0.373 16.575 10.830 0.29 147838. 0.6815
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3.10 0.0455 0.1441 0.0678 0.0214 0.209 3.288 3.631 155.587 0.371 16.152 10.586 0.29 147907. 0.6576
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4.14 0.0607 0.1876 0.0660 0.0214 0.208 3.275 3.533 154.970 0.370 15.716 10.341 0.29 147980. 0.6337
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5.17 0.0759 0.2290 0.0641 0.0212 0.207 3.258 3.431 154.168 0.368 15.262 10.095 0.29 148055. 0.6096
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6.21 0.0911 0.2680 0.0621 0.0211 0.205 3.236 3.325 153.153 0.366 14.790 9.848 0.29 148134. 0.5854
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7.24 0.1062 0.3048 0.0601 0.0209 0.204 3.211 3.216 151.951 0.363 14.303 9.598 0.29 148216. 0.5611
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8.28 0.1214 0.3392 0.0579 0.0207 0.202 3.180 3.102 150.513 0.359 13.797 9.347 0.29 148301. 0.5366
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9.31 0.1366 0.3712 0.0557 0.0205 0.200 3.145 2.984 148.848 0.355 13.273 9.093 0.29 148390. 0.5120
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10.35 0.1518 0.4008 0.0535 0.0202 0.197 3.105 2.862 146.932 0.351 12.730 8.835 0.29 148482. 0.4872
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11.38 0.1669 0.4277 0.0511 0.0200 0.194 3.059 2.736 144.777 0.346 12.171 8.572 0.29 148578. 0.4622
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12.42 0.1821 0.4521 0.0487 0.0196 0.191 3.009 2.607 142.378 0.340 11.596 8.305 0.29 148677. 0.4371
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13.45 0.1973 0.4736 0.0462 0.0193 0.187 2.953 2.474 139.730 0.334 11.005 8.031 0.29 148780. 0.4118
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14.49 0.2125 0.4922 0.0437 0.0189 0.183 2.891 2.338 136.826 0.327 10.400 7.751 0.29 148886. 0.3863
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15.52 0.2276 0.5077 0.0411 0.0184 0.179 2.824 2.199 133.658 0.319 9.780 7.462 0.29 148997. 0.3607
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16.56 0.2428 0.5198 0.0384 0.0179 0.175 2.752 2.056 130.222 0.311 9.146 7.162 0.29 149111. 0.3348
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17.59 0.2580 0.5283 0.0357 0.0174 0.170 2.673 1.911 126.508 0.302 8.499 6.850 0.29 149229. 0.3087
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18.63 0.2732 0.5327 0.0329 0.0169 0.164 2.589 1.762 122.513 0.292 7.838 6.524 0.29 149351. 0.2823
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19.66 0.2883 0.5326 0.0301 0.0163 0.159 2.498 1.611 118.229 0.282 7.164 6.179 0.29 149478. 0.2556
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20.69 0.3035 0.5274 0.0272 0.0157 0.152 2.402 1.457 113.652 0.271 6.479 5.813 0.29 149608. 0.2287
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21.73 0.3187 0.5165 0.0243 0.0150 0.146 2.299 1.300 108.779 0.260 5.784 5.422 0.29 149743. 0.2015
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22.76 0.3339 0.4988 0.0213 0.0143 0.139 2.189 1.142 103.609 0.247 5.078 4.998 0.29 149881. 0.1741
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23.80 0.3491 0.4731 0.0183 0.0135 0.132 2.074 0.981 98.142 0.234 4.365 4.535 0.29 150025. 0.1464
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24.83 0.3642 0.4380 0.0153 0.0127 0.124 1.952 0.819 92.382 0.221 3.645 4.023 0.29 150172. 0.1187
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25.87 0.3794 0.3913 0.0123 0.0119 0.116 1.824 0.657 86.340 0.206 2.921 3.450 0.29 150324. 0.0911
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26.90 0.3946 0.3304 0.0092 0.0110 0.107 1.691 0.494 80.043 0.191 2.199 2.801 0.29 150480. 0.0642
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27.94 0.4098 0.2511 0.0062 0.0101 0.099 1.553 0.332 73.497 0.175 1.478 2.050 0.29 150640. 0.0385
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28.97 0.4249 0.1471 0.0032 0.0092 0.089 1.409 0.170 66.685 0.159 0.758 1.159 0.29 150803. 0.0156
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30.01 0.4401 0.0051 0.0001 0.0082 0.080 1.256 0.005 59.456 0.142 0.023 0.039 0.29 150950. 0.0001
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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 0.0734 0.0213 0.405 5.110 6.139 302.289 0.577 27.308 9.212 0.36 184630. 0.7440
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1.32 0.0155 0.0522 0.0717 0.0213 0.405 5.105 5.999 301.976 0.577 26.685 9.011 0.36 184711. 0.7195
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2.64 0.0310 0.1021 0.0700 0.0213 0.404 5.095 5.853 301.377 0.576 26.036 8.809 0.36 184796. 0.6948
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3.97 0.0466 0.1497 0.0682 0.0212 0.403 5.077 5.700 300.349 0.574 25.354 8.608 0.36 184885. 0.6699
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5.29 0.0621 0.1949 0.0663 0.0211 0.401 5.055 5.542 299.024 0.571 24.651 8.406 0.36 184978. 0.6451
|
|
6.61 0.0776 0.2378 0.0643 0.0210 0.399 5.026 5.377 297.294 0.568 23.918 8.204 0.36 185076. 0.6201
|
|
7.93 0.0931 0.2783 0.0622 0.0208 0.396 4.989 5.206 295.133 0.564 23.156 8.001 0.36 185177. 0.5951
|
|
9.26 0.1086 0.3164 0.0601 0.0206 0.392 4.946 5.029 292.559 0.559 22.368 7.796 0.36 185283. 0.5699
|
|
10.58 0.1241 0.3521 0.0579 0.0204 0.388 4.894 4.845 289.504 0.553 21.551 7.591 0.36 185393. 0.5447
|
|
11.90 0.1397 0.3852 0.0556 0.0202 0.383 4.834 4.654 285.947 0.546 20.702 7.383 0.36 185507. 0.5192
|
|
13.22 0.1552 0.4158 0.0533 0.0199 0.378 4.765 4.457 281.876 0.538 19.824 7.171 0.36 185626. 0.4935
|
|
14.55 0.1707 0.4437 0.0509 0.0196 0.372 4.688 4.253 277.298 0.530 18.919 6.957 0.36 185750. 0.4677
|
|
15.87 0.1862 0.4688 0.0484 0.0192 0.365 4.601 4.044 272.204 0.520 17.988 6.739 0.36 185878. 0.4417
|
|
17.19 0.2017 0.4910 0.0458 0.0188 0.357 4.506 3.829 266.582 0.509 17.032 6.515 0.36 186011. 0.4156
|
|
18.51 0.2172 0.5102 0.0432 0.0184 0.349 4.402 3.609 260.416 0.497 16.053 6.286 0.36 186149. 0.3893
|
|
19.84 0.2328 0.5260 0.0405 0.0179 0.340 4.289 3.383 253.692 0.485 15.049 6.049 0.36 186292. 0.3627
|
|
21.16 0.2483 0.5383 0.0377 0.0174 0.330 4.165 3.153 246.395 0.471 14.023 5.803 0.36 186440. 0.3359
|
|
22.48 0.2638 0.5467 0.0349 0.0168 0.320 4.032 2.917 238.512 0.456 12.975 5.547 0.36 186593. 0.3088
|
|
23.80 0.2793 0.5507 0.0320 0.0162 0.308 3.888 2.676 230.027 0.439 11.905 5.278 0.36 186751. 0.2815
|
|
25.13 0.2948 0.5499 0.0291 0.0156 0.296 3.735 2.432 220.932 0.422 10.816 4.992 0.36 186915. 0.2537
|
|
26.45 0.3103 0.5434 0.0261 0.0149 0.283 3.571 2.182 211.218 0.403 9.708 4.687 0.36 187084. 0.2257
|
|
27.77 0.3259 0.5305 0.0231 0.0142 0.269 3.396 1.930 200.878 0.384 8.583 4.357 0.36 187259. 0.1973
|
|
29.09 0.3414 0.5098 0.0200 0.0134 0.255 3.210 1.673 189.911 0.363 7.444 3.997 0.36 187439. 0.1685
|
|
30.42 0.3569 0.4798 0.0169 0.0126 0.239 3.014 1.415 178.323 0.341 6.292 3.598 0.36 187625. 0.1395
|
|
31.74 0.3724 0.4384 0.0138 0.0117 0.223 2.808 1.154 166.129 0.317 5.133 3.151 0.36 187816. 0.1103
|
|
33.06 0.3879 0.3827 0.0107 0.0108 0.206 2.593 0.893 153.368 0.293 3.971 2.640 0.36 188014. 0.0813
|
|
34.38 0.4034 0.3087 0.0076 0.0099 0.188 2.368 0.633 140.096 0.268 2.814 2.048 0.36 188216. 0.0531
|
|
35.71 0.4190 0.2095 0.0045 0.0089 0.169 2.135 0.373 126.275 0.241 1.657 1.338 0.36 188423. 0.0266
|
|
37.03 0.4345 0.0735 0.0013 0.0079 0.150 1.890 0.112 111.825 0.214 0.496 0.453 0.36 188628. 0.0049
|
|
38.35 0.4500
|
|
|
|
|
|
|
|
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 0.0740 0.0212 0.698 7.329 8.911 520.247 0.828 39.636 7.769 0.43 221547. 0.7560
|
|
1.59 0.0155 0.0530 0.0723 0.0212 0.697 7.319 8.707 519.590 0.827 38.729 7.601 0.43 221645. 0.7311
|
|
3.18 0.0311 0.1036 0.0705 0.0212 0.695 7.303 8.495 518.452 0.825 37.785 7.432 0.43 221748. 0.7061
|
|
4.77 0.0466 0.1519 0.0687 0.0211 0.693 7.277 8.272 516.546 0.822 36.792 7.263 0.43 221856. 0.6809
|
|
6.36 0.0622 0.1979 0.0668 0.0210 0.689 7.242 8.041 514.093 0.818 35.769 7.095 0.43 221968. 0.6558
|
|
7.95 0.0777 0.2414 0.0648 0.0209 0.685 7.198 7.802 510.941 0.813 34.702 6.926 0.43 222086. 0.6306
|
|
9.54 0.0933 0.2826 0.0627 0.0207 0.680 7.142 7.553 507.007 0.807 33.594 6.757 0.43 222208. 0.6053
|
|
11.13 0.1088 0.3214 0.0606 0.0205 0.674 7.077 7.295 502.345 0.800 32.447 6.586 0.43 222336. 0.5799
|
|
12.72 0.1244 0.3578 0.0583 0.0203 0.666 6.999 7.027 496.824 0.791 31.257 6.415 0.43 222469. 0.5544
|
|
14.31 0.1399 0.3917 0.0560 0.0200 0.658 6.908 6.749 490.413 0.781 30.022 6.242 0.43 222607. 0.5287
|
|
15.90 0.1555 0.4230 0.0537 0.0197 0.648 6.805 6.462 483.085 0.769 28.743 6.067 0.43 222750. 0.5028
|
|
17.49 0.1710 0.4517 0.0512 0.0194 0.637 6.689 6.166 474.855 0.756 27.426 5.890 0.43 222899. 0.4767
|
|
19.08 0.1866 0.4776 0.0487 0.0190 0.625 6.560 5.861 465.706 0.741 26.072 5.709 0.43 223054. 0.4505
|
|
20.67 0.2021 0.5007 0.0461 0.0186 0.611 6.418 5.549 455.616 0.725 24.681 5.524 0.43 223215. 0.4242
|
|
22.26 0.2177 0.5207 0.0434 0.0182 0.596 6.263 5.228 444.557 0.708 23.255 5.334 0.43 223381. 0.3976
|
|
23.85 0.2332 0.5374 0.0407 0.0177 0.580 6.093 4.900 432.502 0.688 21.795 5.139 0.43 223554. 0.3708
|
|
25.45 0.2488 0.5506 0.0379 0.0171 0.562 5.909 4.564 419.428 0.668 20.302 4.936 0.43 223732. 0.3437
|
|
27.04 0.2643 0.5599 0.0351 0.0165 0.544 5.710 4.221 405.308 0.645 18.776 4.724 0.43 223917. 0.3164
|
|
28.63 0.2799 0.5649 0.0321 0.0159 0.523 5.496 3.871 390.120 0.621 17.220 4.501 0.43 224108. 0.2887
|
|
30.22 0.2954 0.5649 0.0292 0.0153 0.501 5.266 3.515 373.843 0.595 15.636 4.265 0.43 224305. 0.2607
|
|
31.81 0.3110 0.5594 0.0262 0.0146 0.478 5.022 3.153 356.464 0.567 14.024 4.012 0.43 224509. 0.2322
|
|
33.40 0.3265 0.5472 0.0231 0.0138 0.453 4.761 2.785 337.973 0.538 12.388 3.738 0.43 224719. 0.2033
|
|
34.99 0.3421 0.5272 0.0200 0.0130 0.427 4.485 2.413 318.368 0.507 10.731 3.437 0.43 224937. 0.1740
|
|
36.58 0.3576 0.4976 0.0169 0.0122 0.399 4.193 2.036 297.660 0.474 9.058 3.103 0.43 225161. 0.1443
|
|
38.17 0.3732 0.4560 0.0138 0.0113 0.370 3.886 1.657 275.878 0.439 7.372 2.725 0.43 225391. 0.1144
|
|
39.76 0.3887 0.3992 0.0106 0.0103 0.339 3.565 1.278 253.095 0.403 5.684 2.290 0.43 225629. 0.0844
|
|
41.35 0.4043 0.3225 0.0075 0.0094 0.308 3.232 0.900 229.407 0.365 4.002 1.779 0.43 225873. 0.0550
|
|
42.94 0.4198 0.2177 0.0043 0.0084 0.275 2.884 0.522 204.743 0.326 2.322 1.156 0.43 226122. 0.0272
|
|
44.53 0.4354 0.0704 0.0012 0.0073 0.240 2.521 0.142 178.927 0.285 0.633 0.361 0.43 226367. 0.0044
|
|
46.12 0.4509
|
|
|
|
|
|
|
|
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 0.0747 0.0213 1.109 9.990 12.247 827.318 1.129 54.473 6.714 0.50 258458. 0.7659
|
|
1.84 0.0154 0.0530 0.0730 0.0212 1.108 9.974 11.968 826.057 1.127 53.234 6.571 0.50 258573. 0.7411
|
|
3.68 0.0308 0.1037 0.0712 0.0212 1.105 9.951 11.679 824.092 1.124 51.949 6.428 0.50 258692. 0.7161
|
|
5.52 0.0463 0.1521 0.0694 0.0211 1.101 9.912 11.375 820.880 1.120 50.597 6.285 0.50 258818. 0.6910
|
|
7.36 0.0617 0.1982 0.0675 0.0210 1.095 9.862 11.061 816.749 1.114 49.201 6.143 0.50 258948. 0.6660
|
|
9.20 0.0771 0.2420 0.0655 0.0209 1.088 9.799 10.735 811.569 1.107 47.751 6.000 0.50 259085. 0.6408
|
|
11.04 0.0925 0.2834 0.0634 0.0207 1.080 9.721 10.396 805.092 1.098 46.241 5.857 0.50 259227. 0.6156
|
|
12.88 0.1079 0.3226 0.0613 0.0205 1.069 9.629 10.045 797.488 1.088 44.682 5.713 0.50 259374. 0.5903
|
|
14.72 0.1233 0.3593 0.0591 0.0203 1.057 9.521 9.681 788.482 1.076 43.062 5.569 0.50 259529. 0.5649
|
|
16.56 0.1388 0.3937 0.0568 0.0200 1.043 9.395 9.304 778.097 1.061 41.384 5.424 0.50 259689. 0.5393
|
|
18.40 0.1542 0.4255 0.0544 0.0197 1.028 9.252 8.913 766.226 1.045 39.646 5.276 0.50 259855. 0.5135
|
|
20.24 0.1696 0.4549 0.0519 0.0194 1.010 9.091 8.511 752.914 1.027 37.855 5.127 0.50 260027. 0.4876
|
|
22.08 0.1850 0.4815 0.0494 0.0190 0.990 8.913 8.097 738.138 1.007 36.014 4.975 0.50 260206. 0.4615
|
|
23.92 0.2004 0.5054 0.0468 0.0186 0.968 8.716 7.672 721.861 0.985 34.124 4.820 0.50 260392. 0.4352
|
|
25.76 0.2159 0.5264 0.0441 0.0181 0.944 8.501 7.236 704.040 0.960 32.186 4.662 0.50 260584. 0.4088
|
|
27.60 0.2313 0.5442 0.0414 0.0176 0.918 8.267 6.790 684.636 0.934 30.202 4.498 0.50 260783. 0.3821
|
|
29.44 0.2467 0.5586 0.0386 0.0171 0.890 8.013 6.334 663.608 0.905 28.173 4.329 0.50 260989. 0.3552
|
|
31.28 0.2621 0.5694 0.0358 0.0165 0.859 7.739 5.868 640.917 0.874 26.101 4.153 0.50 261202. 0.3279
|
|
33.12 0.2775 0.5760 0.0329 0.0159 0.827 7.444 5.393 616.526 0.841 23.987 3.967 0.50 261423. 0.3003
|
|
34.95 0.2930 0.5779 0.0299 0.0152 0.792 7.129 4.909 590.403 0.805 21.834 3.771 0.50 261650. 0.2723
|
|
36.79 0.3084 0.5744 0.0269 0.0145 0.754 6.792 4.416 562.526 0.767 19.644 3.561 0.50 261885. 0.2439
|
|
38.63 0.3238 0.5646 0.0239 0.0137 0.715 6.434 3.917 532.877 0.727 17.421 3.334 0.50 262127. 0.2151
|
|
40.47 0.3392 0.5473 0.0208 0.0129 0.672 6.055 3.410 501.452 0.684 15.169 3.085 0.50 262378. 0.1857
|
|
42.31 0.3546 0.5208 0.0177 0.0120 0.628 5.654 2.899 468.265 0.639 12.893 2.808 0.50 262635. 0.1558
|
|
44.15 0.3700 0.4828 0.0145 0.0111 0.581 5.233 2.383 433.355 0.591 10.600 2.494 0.50 262901. 0.1255
|
|
45.99 0.3855 0.4301 0.0114 0.0102 0.532 4.791 1.866 396.819 0.541 8.300 2.133 0.50 263174. 0.0950
|
|
47.83 0.4009 0.3580 0.0082 0.0092 0.481 4.333 1.351 358.834 0.490 6.008 1.707 0.50 263455. 0.0647
|
|
49.67 0.4163 0.2586 0.0051 0.0082 0.428 3.856 0.836 319.319 0.436 3.718 1.187 0.50 263743. 0.0354
|
|
51.51 0.4317 0.1181 0.0020 0.0072 0.373 3.358 0.321 278.138 0.379 1.426 0.523 0.50 264030. 0.0096
|
|
53.35 0.4471
|
|
|
|
|
|
|
|
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 0.0756 0.0214 1.667 13.131 16.183 1242.853 1.484 71.982 5.906 0.57 295363. 0.7745
|
|
2.07 0.0152 0.0526 0.0739 0.0214 1.664 13.107 15.819 1240.599 1.481 70.364 5.784 0.57 295492. 0.7499
|
|
4.15 0.0304 0.1029 0.0721 0.0213 1.659 13.073 15.443 1237.384 1.477 68.692 5.661 0.57 295628. 0.7252
|
|
6.22 0.0456 0.1510 0.0703 0.0212 1.653 13.020 15.048 1232.311 1.471 66.933 5.539 0.57 295770. 0.7004
|
|
8.29 0.0608 0.1969 0.0684 0.0211 1.644 12.951 14.639 1225.781 1.463 65.113 5.417 0.57 295918. 0.6756
|
|
10.36 0.0760 0.2406 0.0664 0.0210 1.633 12.867 14.215 1217.816 1.454 63.230 5.294 0.57 296072. 0.6507
|
|
12.44 0.0912 0.2820 0.0643 0.0208 1.620 12.761 13.774 1207.848 1.442 61.266 5.172 0.57 296232. 0.6258
|
|
14.51 0.1064 0.3212 0.0622 0.0206 1.604 12.639 13.319 1196.259 1.428 59.241 5.050 0.57 296399. 0.6008
|
|
16.58 0.1216 0.3582 0.0600 0.0204 1.586 12.494 12.845 1182.536 1.412 57.135 4.927 0.57 296573. 0.5756
|
|
18.66 0.1368 0.3928 0.0577 0.0201 1.565 12.328 12.356 1166.855 1.393 54.960 4.803 0.57 296754. 0.5504
|
|
20.73 0.1520 0.4251 0.0553 0.0198 1.541 12.139 11.849 1148.933 1.371 52.704 4.678 0.57 296941. 0.5249
|
|
22.80 0.1672 0.4549 0.0529 0.0194 1.514 11.927 11.326 1128.873 1.347 50.380 4.551 0.57 297135. 0.4993
|
|
24.87 0.1824 0.4822 0.0504 0.0191 1.484 11.692 10.789 1106.643 1.321 47.991 4.422 0.57 297336. 0.4735
|
|
26.95 0.1976 0.5069 0.0478 0.0186 1.451 11.434 10.238 1082.196 1.292 45.539 4.291 0.57 297545. 0.4476
|
|
29.02 0.2128 0.5288 0.0452 0.0182 1.415 11.151 9.673 1055.473 1.260 43.025 4.157 0.57 297761. 0.4214
|
|
31.09 0.2280 0.5478 0.0425 0.0177 1.376 10.844 9.094 1026.416 1.225 40.452 4.019 0.57 297984. 0.3951
|
|
33.17 0.2432 0.5636 0.0397 0.0171 1.334 10.512 8.503 994.963 1.188 37.821 3.876 0.57 298215. 0.3684
|
|
35.24 0.2584 0.5759 0.0369 0.0166 1.289 10.154 7.899 961.060 1.147 35.133 3.728 0.57 298454. 0.3415
|
|
37.31 0.2736 0.5843 0.0340 0.0159 1.240 9.769 7.282 924.653 1.104 32.393 3.572 0.57 298701. 0.3143
|
|
39.38 0.2888 0.5884 0.0311 0.0153 1.188 9.358 6.655 885.695 1.057 29.601 3.408 0.57 298956. 0.2866
|
|
41.46 0.3040 0.5875 0.0281 0.0145 1.132 8.919 6.016 844.150 1.008 26.761 3.233 0.57 299218. 0.2585
|
|
43.53 0.3192 0.5808 0.0251 0.0138 1.073 8.452 5.368 799.989 0.955 23.877 3.044 0.57 299490. 0.2299
|
|
45.60 0.3344 0.5672 0.0220 0.0130 1.010 7.958 4.711 753.203 0.899 20.954 2.837 0.57 299769. 0.2007
|
|
47.68 0.3496 0.5451 0.0189 0.0121 0.944 7.436 4.046 703.803 0.840 17.999 2.608 0.57 300057. 0.1710
|
|
49.75 0.3648 0.5124 0.0158 0.0112 0.874 6.887 3.376 651.833 0.778 15.018 2.349 0.58 300354. 0.1407
|
|
51.82 0.3800 0.4662 0.0126 0.0103 0.801 6.312 2.703 597.400 0.713 12.023 2.052 0.58 300659. 0.1100
|
|
53.89 0.3952 0.4024 0.0095 0.0093 0.725 5.713 2.031 540.746 0.645 9.032 1.703 0.58 300973. 0.0791
|
|
55.97 0.4104 0.3140 0.0064 0.0083 0.646 5.092 1.360 481.915 0.575 6.049 1.280 0.58 301294. 0.0487
|
|
58.04 0.4256 0.1892 0.0032 0.0072 0.564 4.446 0.690 420.769 0.502 3.068 0.744 0.58 301620. 0.0201
|
|
60.11 0.4408 -0.0009 0.0000 0.0061 0.476 3.753 -0.003 355.180 0.424 -0.011 -0.003 0.58 301890. 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 0.0766 0.0217 2.400 16.808 20.770 1789.734 1.899 92.386 5.264 0.64 332258. 0.7820
|
|
2.37 0.0155 0.0536 0.0749 0.0216 2.395 16.771 20.293 1785.753 1.895 90.265 5.154 0.64 332408. 0.7569
|
|
4.75 0.0309 0.1050 0.0731 0.0215 2.388 16.720 19.802 1780.363 1.889 88.077 5.045 0.64 332565. 0.7318
|
|
7.12 0.0464 0.1541 0.0712 0.0214 2.377 16.643 19.284 1772.196 1.880 85.773 4.935 0.64 332729. 0.7065
|
|
9.50 0.0619 0.2009 0.0692 0.0213 2.363 16.545 18.747 1761.747 1.869 83.387 4.827 0.64 332900. 0.6812
|
|
11.87 0.0774 0.2455 0.0671 0.0212 2.346 16.427 18.192 1749.116 1.856 80.919 4.717 0.64 333078. 0.6559
|
|
14.24 0.0928 0.2877 0.0650 0.0210 2.325 16.280 17.613 1733.463 1.839 78.341 4.608 0.64 333264. 0.6305
|
|
16.62 0.1083 0.3277 0.0628 0.0208 2.300 16.109 17.015 1715.300 1.820 75.682 4.499 0.64 333458. 0.6050
|
|
18.99 0.1238 0.3654 0.0605 0.0205 2.272 15.908 16.393 1693.942 1.797 72.918 4.389 0.64 333659. 0.5794
|
|
21.36 0.1393 0.4008 0.0581 0.0202 2.239 15.679 15.750 1669.537 1.771 70.057 4.279 0.64 333868. 0.5536
|
|
23.74 0.1547 0.4337 0.0557 0.0199 2.202 15.419 15.084 1641.777 1.742 67.092 4.167 0.64 334085. 0.5276
|
|
26.11 0.1702 0.4641 0.0531 0.0195 2.160 15.127 14.397 1610.776 1.709 64.038 4.054 0.64 334310. 0.5014
|
|
28.49 0.1857 0.4919 0.0505 0.0191 2.114 14.805 13.691 1576.487 1.673 60.897 3.939 0.64 334543. 0.4751
|
|
30.86 0.2012 0.5170 0.0478 0.0186 2.064 14.452 12.966 1538.834 1.633 57.674 3.822 0.64 334785. 0.4486
|
|
33.23 0.2166 0.5393 0.0451 0.0181 2.008 14.066 12.223 1497.729 1.589 54.369 3.702 0.64 335036. 0.4219
|
|
35.61 0.2321 0.5585 0.0423 0.0176 1.949 13.646 11.463 1453.083 1.542 50.986 3.578 0.64 335295. 0.3949
|
|
37.98 0.2476 0.5744 0.0394 0.0170 1.884 13.193 10.685 1404.809 1.491 47.527 3.450 0.64 335563. 0.3676
|
|
40.35 0.2630 0.5867 0.0365 0.0164 1.814 12.705 9.891 1352.823 1.435 43.994 3.316 0.64 335840. 0.3400
|
|
42.73 0.2785 0.5948 0.0335 0.0157 1.739 12.181 9.081 1297.047 1.376 40.391 3.175 0.65 336126. 0.3119
|
|
45.10 0.2940 0.5983 0.0305 0.0150 1.659 11.621 8.256 1237.418 1.313 36.721 3.026 0.65 336421. 0.2834
|
|
47.48 0.3095 0.5964 0.0274 0.0142 1.574 11.024 7.417 1173.882 1.246 32.990 2.866 0.65 336726. 0.2544
|
|
49.85 0.3249 0.5882 0.0242 0.0134 1.484 10.391 6.565 1106.410 1.174 29.202 2.691 0.65 337041. 0.2248
|
|
52.22 0.3404 0.5722 0.0210 0.0125 1.388 9.720 5.703 1034.998 1.098 25.366 2.499 0.65 337365. 0.1945
|
|
54.60 0.3559 0.5465 0.0178 0.0116 1.287 9.013 4.831 959.681 1.018 21.489 2.283 0.65 337699. 0.1636
|
|
56.97 0.3714 0.5086 0.0146 0.0107 1.181 8.270 3.953 880.560 0.934 17.584 2.036 0.65 338043. 0.1320
|
|
59.34 0.3868 0.4545 0.0113 0.0097 1.070 7.493 3.073 797.869 0.847 13.670 1.747 0.65 338398. 0.0998
|
|
61.72 0.4023 0.3785 0.0081 0.0086 0.955 6.687 2.196 711.994 0.755 9.768 1.399 0.65 338762. 0.0676
|
|
64.09 0.4178 0.2701 0.0049 0.0075 0.835 5.848 1.320 622.722 0.661 5.871 0.961 0.65 339134. 0.0360
|
|
66.47 0.4333 0.1101 0.0016 0.0064 0.710 4.974 0.441 529.628 0.562 1.962 0.378 0.65 339501. 0.0082
|
|
68.84 0.4487
|
|
|
|
|
|
|
|
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 0.0779 0.0220 3.348 21.101 26.077 2496.483 2.384 115.990 4.738 0.71 369140. 0.7887
|
|
2.59 0.0152 0.0528 0.0762 0.0220 3.339 21.046 25.487 2489.951 2.378 113.367 4.643 0.71 369306. 0.7641
|
|
5.18 0.0304 0.1034 0.0744 0.0219 3.328 20.975 24.880 2481.550 2.370 110.667 4.548 0.71 369479. 0.7394
|
|
7.78 0.0456 0.1518 0.0725 0.0218 3.312 20.873 24.242 2469.536 2.358 107.830 4.453 0.71 369660. 0.7146
|
|
10.37 0.0608 0.1981 0.0705 0.0216 3.291 20.743 23.580 2454.162 2.344 104.884 4.358 0.71 369848. 0.6898
|
|
12.96 0.0760 0.2422 0.0684 0.0215 3.267 20.590 22.898 2436.007 2.326 101.848 4.263 0.71 370044. 0.6650
|
|
15.55 0.0912 0.2842 0.0663 0.0213 3.237 20.401 22.184 2413.654 2.305 98.674 4.169 0.71 370248. 0.6401
|
|
18.15 0.1065 0.3241 0.0641 0.0211 3.202 20.183 21.449 2387.936 2.280 95.405 4.074 0.71 370460. 0.6151
|
|
20.74 0.1217 0.3617 0.0618 0.0208 3.162 19.929 20.684 2357.822 2.252 92.002 3.979 0.71 370681. 0.5899
|
|
23.33 0.1369 0.3972 0.0595 0.0205 3.116 19.641 19.895 2323.715 2.219 88.492 3.883 0.71 370909. 0.5646
|
|
25.92 0.1521 0.4303 0.0570 0.0202 3.064 19.313 19.076 2284.987 2.182 84.849 3.787 0.71 371146. 0.5391
|
|
28.51 0.1673 0.4611 0.0545 0.0198 3.006 18.949 18.232 2241.849 2.141 81.096 3.689 0.72 371392. 0.5134
|
|
31.11 0.1825 0.4895 0.0519 0.0194 2.943 18.546 17.365 2194.265 2.095 77.238 3.589 0.72 371647. 0.4876
|
|
33.70 0.1977 0.5153 0.0492 0.0189 2.873 18.106 16.475 2142.140 2.046 73.279 3.488 0.72 371910. 0.4615
|
|
36.29 0.2129 0.5385 0.0465 0.0184 2.797 17.626 15.562 2085.361 1.991 69.222 3.385 0.72 372183. 0.4353
|
|
38.88 0.2281 0.5589 0.0437 0.0178 2.714 17.106 14.629 2023.818 1.933 65.069 3.279 0.72 372465. 0.4088
|
|
41.47 0.2433 0.5761 0.0409 0.0173 2.625 16.544 13.674 1957.395 1.869 60.822 3.169 0.72 372756. 0.3819
|
|
44.07 0.2585 0.5900 0.0380 0.0166 2.529 15.941 12.699 1885.987 1.801 56.486 3.054 0.72 373057. 0.3548
|
|
46.66 0.2737 0.6001 0.0350 0.0160 2.427 15.294 11.705 1809.502 1.728 52.063 2.934 0.72 373367. 0.3272
|
|
49.25 0.2889 0.6060 0.0320 0.0152 2.317 14.604 10.692 1727.859 1.650 47.559 2.807 0.72 373688. 0.2992
|
|
51.84 0.3041 0.6070 0.0289 0.0145 2.201 13.870 9.662 1641.002 1.567 42.977 2.671 0.72 374018. 0.2706
|
|
54.44 0.3194 0.6021 0.0258 0.0137 2.077 13.092 8.616 1548.901 1.479 38.325 2.523 0.72 374359. 0.2414
|
|
57.03 0.3346 0.5903 0.0226 0.0128 1.947 12.269 7.556 1451.562 1.386 33.610 2.361 0.72 374710. 0.2116
|
|
59.62 0.3498 0.5698 0.0194 0.0119 1.809 11.402 6.484 1349.049 1.288 28.842 2.180 0.72 375071. 0.1810
|
|
62.21 0.3650 0.5384 0.0162 0.0109 1.665 10.493 5.403 1241.501 1.186 24.033 1.974 0.72 375443. 0.1496
|
|
64.80 0.3802 0.4926 0.0129 0.0100 1.514 9.544 4.317 1129.196 1.078 19.201 1.734 0.72 375826. 0.1174
|
|
67.40 0.3954 0.4277 0.0097 0.0089 1.358 8.560 3.232 1012.710 0.967 14.375 1.447 0.72 376219. 0.0848
|
|
69.99 0.4106 0.3352 0.0064 0.0079 1.196 7.541 2.149 892.204 0.852 9.560 1.093 0.72 376622. 0.0522
|
|
72.58 0.4258 0.2007 0.0032 0.0068 1.029 6.487 1.067 767.510 0.733 4.748 0.631 0.72 377030. 0.0212
|
|
75.17 0.4410 -0.0160 -0.0002 0.0056 0.848 5.342 -0.068 632.007 0.604 -0.301 -0.049 0.72 377320. 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 0.0796 0.0226 4.566 26.162 32.202 3404.852 2.956 143.237 4.290 0.79 406007. 0.7935
|
|
2.88 0.0153 0.0530 0.0777 0.0225 4.550 26.073 31.466 3393.235 2.946 139.961 4.206 0.79 406193. 0.7691
|
|
5.75 0.0307 0.1039 0.0759 0.0224 4.531 25.964 30.708 3379.014 2.933 136.590 4.122 0.79 406388. 0.7446
|
|
8.63 0.0460 0.1527 0.0739 0.0223 4.506 25.820 29.914 3360.269 2.917 133.058 4.038 0.79 406591. 0.7199
|
|
11.50 0.0613 0.1994 0.0719 0.0221 4.475 25.638 29.087 3336.670 2.897 129.378 3.954 0.79 406802. 0.6951
|
|
14.38 0.0767 0.2439 0.0698 0.0219 4.438 25.428 28.235 3309.283 2.873 125.589 3.870 0.79 407022. 0.6703
|
|
17.25 0.0920 0.2863 0.0676 0.0217 4.393 25.174 27.344 3276.170 2.844 121.626 3.786 0.79 407252. 0.6453
|
|
20.13 0.1073 0.3266 0.0653 0.0215 4.343 24.883 26.426 3238.391 2.811 117.542 3.701 0.79 407490. 0.6202
|
|
23.00 0.1227 0.3647 0.0629 0.0212 4.284 24.547 25.470 3194.578 2.773 113.291 3.616 0.79 407737. 0.5949
|
|
25.88 0.1380 0.4005 0.0605 0.0208 4.218 24.168 24.484 3145.234 2.730 108.904 3.531 0.79 407994. 0.5695
|
|
28.75 0.1533 0.4341 0.0580 0.0205 4.143 23.740 23.460 3089.587 2.682 104.352 3.444 0.79 408260. 0.5438
|
|
31.63 0.1687 0.4654 0.0554 0.0201 4.061 23.266 22.406 3027.933 2.629 99.661 3.356 0.79 408536. 0.5179
|
|
34.50 0.1840 0.4942 0.0527 0.0196 3.970 22.746 21.322 2960.240 2.570 94.840 3.267 0.79 408821. 0.4918
|
|
37.38 0.1993 0.5204 0.0499 0.0191 3.871 22.179 20.209 2886.428 2.506 89.892 3.176 0.79 409116. 0.4654
|
|
40.25 0.2147 0.5439 0.0471 0.0186 3.763 21.564 19.069 2806.418 2.436 84.820 3.082 0.79 409422. 0.4387
|
|
43.13 0.2300 0.5644 0.0442 0.0180 3.648 20.901 17.902 2720.124 2.361 79.629 2.985 0.79 409737. 0.4117
|
|
46.00 0.2454 0.5817 0.0413 0.0174 3.523 20.189 16.709 2627.457 2.281 74.321 2.884 0.79 410064. 0.3843
|
|
48.88 0.2607 0.5954 0.0383 0.0168 3.391 19.428 15.490 2528.369 2.195 68.900 2.779 0.79 410400. 0.3565
|
|
51.75 0.2760 0.6051 0.0352 0.0161 3.249 18.617 14.247 2422.843 2.103 63.372 2.667 0.79 410748. 0.3282
|
|
54.63 0.2914 0.6102 0.0321 0.0153 3.099 17.757 12.982 2310.916 2.006 57.742 2.548 0.79 411106. 0.2993
|
|
57.50 0.3067 0.6098 0.0289 0.0145 2.940 16.848 11.694 2192.655 1.903 52.016 2.419 0.79 411476. 0.2697
|
|
60.38 0.3220 0.6030 0.0257 0.0137 2.774 15.892 10.387 2068.200 1.795 46.201 2.278 0.79 411857. 0.2393
|
|
63.25 0.3374 0.5882 0.0224 0.0128 2.599 14.890 9.062 1937.772 1.682 40.309 2.121 0.79 412249. 0.2082
|
|
66.13 0.3527 0.5636 0.0191 0.0119 2.416 13.844 7.723 1801.689 1.564 34.351 1.944 0.79 412653. 0.1761
|
|
69.00 0.3680 0.5266 0.0157 0.0110 2.227 12.758 6.372 1660.401 1.441 28.344 1.741 0.79 413069. 0.1432
|
|
71.88 0.3834 0.4734 0.0124 0.0100 2.031 11.638 5.016 1514.595 1.315 22.313 1.502 0.79 413497. 0.1097
|
|
74.76 0.3987 0.3988 0.0090 0.0090 1.831 10.491 3.663 1365.367 1.185 16.294 1.217 0.79 413936. 0.0759
|
|
77.63 0.4140 0.2941 0.0057 0.0080 1.626 9.319 2.311 1212.862 1.053 10.280 0.864 0.79 414385. 0.0428
|
|
80.51 0.4294 0.1452 0.0024 0.0070 1.417 8.121 0.958 1056.834 0.917 4.263 0.411 0.79 414835. 0.0131
|
|
83.38 0.4447
|
|
|
|
|
|
|
|
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 0.0816 0.0238 6.263 32.898 39.290 4670.684 3.717 174.761 3.815 0.86 442848. 0.7796
|
|
3.15 0.0154 0.0518 0.0797 0.0237 6.222 32.682 38.389 4639.944 3.692 170.754 3.753 0.86 443056. 0.7579
|
|
6.30 0.0308 0.1018 0.0778 0.0235 6.177 32.443 37.460 4606.022 3.665 166.621 3.689 0.86 443273. 0.7360
|
|
9.45 0.0462 0.1500 0.0758 0.0233 6.125 32.172 36.492 4567.616 3.635 162.316 3.624 0.86 443498. 0.7136
|
|
12.59 0.0616 0.1964 0.0736 0.0231 6.065 31.858 35.479 4523.024 3.599 157.812 3.558 0.86 443734. 0.6908
|
|
15.74 0.0770 0.2409 0.0715 0.0228 6.000 31.513 34.437 4474.095 3.560 153.176 3.491 0.86 443978. 0.6678
|
|
18.89 0.0924 0.2835 0.0692 0.0226 5.925 31.121 33.347 4418.422 3.516 148.328 3.423 0.86 444233. 0.6444
|
|
22.04 0.1077 0.3241 0.0669 0.0222 5.843 30.690 32.223 4357.132 3.467 143.328 3.354 0.86 444497. 0.6207
|
|
25.19 0.1231 0.3625 0.0645 0.0219 5.754 30.220 31.053 4290.429 3.414 138.123 3.283 0.86 444771. 0.5963
|
|
28.34 0.1385 0.3986 0.0620 0.0215 5.658 29.716 29.845 4218.862 3.357 132.752 3.209 0.86 445056. 0.5714
|
|
31.48 0.1539 0.4323 0.0594 0.0211 5.553 29.164 28.592 4140.560 3.295 127.175 3.132 0.86 445351. 0.5459
|
|
34.63 0.1693 0.4633 0.0567 0.0207 5.442 28.581 27.299 4057.807 3.229 121.428 3.051 0.86 445656. 0.5197
|
|
37.78 0.1847 0.4914 0.0539 0.0203 5.324 27.964 25.971 3970.127 3.159 115.519 2.967 0.86 445972. 0.4929
|
|
40.93 0.2001 0.5168 0.0511 0.0198 5.197 27.298 24.608 3875.541 3.084 109.455 2.880 0.86 446299. 0.4657
|
|
44.08 0.2155 0.5390 0.0482 0.0193 5.061 26.583 23.210 3774.142 3.003 103.240 2.789 0.86 446636. 0.4381
|
|
47.23 0.2309 0.5579 0.0452 0.0187 4.916 25.822 21.780 3666.116 2.917 96.878 2.695 0.86 446985. 0.4099
|
|
50.37 0.2463 0.5730 0.0422 0.0181 4.763 25.019 20.318 3551.985 2.827 90.375 2.595 0.86 447345. 0.3812
|
|
53.52 0.2617 0.5838 0.0391 0.0175 4.602 24.170 18.825 3431.585 2.731 83.734 2.488 0.86 447717. 0.3519
|
|
56.67 0.2771 0.5899 0.0359 0.0169 4.432 23.280 17.303 3305.196 2.630 76.962 2.374 0.86 448100. 0.3220
|
|
59.82 0.2925 0.5905 0.0327 0.0162 4.255 22.350 15.752 3173.171 2.525 70.065 2.252 0.86 448496. 0.2913
|
|
62.97 0.3078 0.5846 0.0294 0.0155 4.071 21.385 14.175 3036.052 2.416 63.052 2.118 0.86 448903. 0.2599
|
|
66.12 0.3232 0.5712 0.0261 0.0148 3.881 20.386 12.575 2894.348 2.303 55.932 1.971 0.86 449323. 0.2278
|
|
69.27 0.3386 0.5488 0.0227 0.0140 3.686 19.360 10.953 2748.604 2.187 48.717 1.807 0.86 449755. 0.1950
|
|
72.41 0.3540 0.5158 0.0193 0.0133 3.486 18.310 9.313 2599.579 2.069 41.424 1.625 0.86 450199. 0.1616
|
|
75.56 0.3694 0.4701 0.0159 0.0125 3.283 17.244 7.660 2448.236 1.948 34.072 1.419 0.86 450657. 0.1280
|
|
78.71 0.3848 0.4091 0.0125 0.0117 3.079 16.170 6.001 2295.782 1.827 26.694 1.186 0.86 451127. 0.0947
|
|
81.86 0.4002 0.3300 0.0090 0.0109 2.875 15.101 4.346 2143.893 1.706 19.332 0.919 0.86 451610. 0.0625
|
|
85.01 0.4156 0.2284 0.0056 0.0102 2.672 14.035 2.692 1992.661 1.586 11.975 0.613 0.86 452104. 0.0328
|
|
88.16 0.4310 0.0986 0.0022 0.0094 2.469 12.967 1.036 1840.931 1.465 4.607 0.255 0.86 452597. 0.0085
|
|
91.30 0.4464
|
|
|
|
|
|
|
|
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 0.0837 0.0271 9.064 43.947 47.327 6759.310 4.965 210.511 3.176 0.93 479669. 0.7122
|
|
3.39 0.0153 0.0467 0.0818 0.0268 8.957 43.426 46.267 6679.214 4.906 205.795 3.142 0.93 479896. 0.6967
|
|
6.79 0.0306 0.0924 0.0799 0.0265 8.844 42.877 45.168 6594.643 4.844 200.908 3.107 0.93 480132. 0.6806
|
|
10.18 0.0459 0.1370 0.0779 0.0261 8.725 42.300 44.031 6506.002 4.779 195.849 3.070 0.93 480379. 0.6640
|
|
13.58 0.0613 0.1804 0.0758 0.0257 8.596 41.674 42.836 6409.692 4.708 190.534 3.031 0.93 480636. 0.6467
|
|
16.97 0.0766 0.2225 0.0736 0.0253 8.460 41.015 41.603 6308.334 4.634 185.052 2.991 0.93 480902. 0.6289
|
|
20.36 0.0919 0.2633 0.0713 0.0249 8.314 40.310 40.317 6199.897 4.554 179.330 2.949 0.93 481180. 0.6105
|
|
23.76 0.1072 0.3027 0.0690 0.0244 8.160 39.562 38.986 6084.789 4.470 173.410 2.906 0.93 481468. 0.5915
|
|
27.15 0.1225 0.3405 0.0665 0.0239 7.995 38.763 37.602 5961.909 4.379 167.253 2.861 0.93 481767. 0.5718
|
|
30.55 0.1378 0.3766 0.0640 0.0234 7.823 37.929 36.173 5833.720 4.285 160.896 2.812 0.93 482076. 0.5514
|
|
33.94 0.1532 0.4103 0.0614 0.0229 7.651 37.094 34.687 5705.328 4.191 154.288 2.758 0.93 482397. 0.5294
|
|
37.33 0.1685 0.4413 0.0586 0.0224 7.479 36.260 33.155 5576.923 4.097 147.473 2.696 0.93 482729. 0.5061
|
|
40.73 0.1838 0.4690 0.0559 0.0219 7.312 35.453 31.579 5452.923 4.006 140.462 2.627 0.93 483072. 0.4812
|
|
44.12 0.1991 0.4911 0.0530 0.0215 7.177 34.795 29.958 5351.665 3.931 133.254 2.539 0.93 483426. 0.4530
|
|
47.52 0.2144 0.5092 0.0501 0.0211 7.041 34.139 28.297 5250.734 3.857 125.865 2.444 0.93 483793. 0.4239
|
|
50.91 0.2297 0.5233 0.0470 0.0207 6.900 33.453 26.597 5145.284 3.780 118.303 2.345 0.93 484171. 0.3942
|
|
54.30 0.2451 0.5330 0.0440 0.0202 6.753 32.742 24.859 5035.847 3.699 110.573 2.239 0.93 484561. 0.3639
|
|
57.70 0.2604 0.5379 0.0408 0.0198 6.602 32.011 23.085 4923.461 3.617 102.683 2.127 0.93 484963. 0.3331
|
|
61.09 0.2757 0.5374 0.0376 0.0193 6.450 31.271 21.277 4809.679 3.533 94.639 2.006 0.93 485377. 0.3017
|
|
64.49 0.2910 0.5309 0.0344 0.0188 6.295 30.520 19.436 4694.100 3.448 86.453 1.878 0.93 485804. 0.2699
|
|
67.88 0.3063 0.5180 0.0311 0.0184 6.139 29.762 17.566 4577.568 3.363 78.135 1.741 0.93 486244. 0.2378
|
|
71.27 0.3216 0.4978 0.0277 0.0179 5.982 29.004 15.669 4460.963 3.277 69.698 1.593 0.93 486697. 0.2056
|
|
74.67 0.3370 0.4698 0.0243 0.0174 5.827 28.253 13.749 4345.471 3.192 61.157 1.435 0.93 487163. 0.1735
|
|
78.06 0.3523 0.4332 0.0209 0.0170 5.676 27.517 11.810 4232.262 3.109 52.533 1.266 0.93 487642. 0.1418
|
|
81.46 0.3676 0.3874 0.0174 0.0165 5.528 26.800 9.859 4122.041 3.028 43.852 1.085 0.93 488134. 0.1110
|
|
84.85 0.3829 0.3320 0.0140 0.0161 5.386 26.112 7.903 4016.131 2.950 35.151 0.893 0.94 488641. 0.0818
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88.24 0.3982 0.2668 0.0105 0.0157 5.252 25.463 5.955 3916.289 2.877 26.486 0.690 0.94 489161. 0.0549
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91.64 0.4135 0.1913 0.0071 0.0153 5.126 24.851 4.013 3822.193 2.808 17.850 0.476 0.94 489694. 0.0311
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95.03 0.4289 0.1051 0.0037 0.0150 5.004 24.262 2.076 3731.553 2.741 9.234 0.252 0.94 490238. 0.0119
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98.43 0.4442 0.0040 0.0001 0.0145 4.851 23.520 0.074 3617.526 2.657 0.329 0.009 0.94 490752. 0.0001
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