501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x8 (18x8.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 0.0717 0.0282 0.004 0.270 0.240 3.199 0.031 1.066 33.990 0.07 25384. 0.5425
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0.37 0.0218 0.0540 0.0704 0.0285 0.004 0.273 0.235 3.227 0.031 1.047 33.082 0.07 25397. 0.5232
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0.74 0.0437 0.1050 0.0690 0.0287 0.004 0.275 0.231 3.253 0.031 1.026 32.174 0.07 25412. 0.5038
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1.12 0.0655 0.1531 0.0675 0.0289 0.004 0.277 0.226 3.274 0.031 1.004 31.268 0.07 25428. 0.4843
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1.49 0.0874 0.1983 0.0659 0.0290 0.004 0.278 0.220 3.291 0.031 0.980 30.366 0.07 25445. 0.4647
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1.86 0.1092 0.2405 0.0642 0.0291 0.004 0.279 0.215 3.303 0.032 0.955 29.468 0.07 25463. 0.4450
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2.23 0.1311 0.2799 0.0623 0.0292 0.004 0.280 0.208 3.309 0.032 0.927 28.575 0.07 25483. 0.4253
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2.61 0.1529 0.3164 0.0604 0.0292 0.004 0.280 0.202 3.309 0.032 0.899 27.686 0.07 25504. 0.4056
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2.98 0.1748 0.3500 0.0583 0.0291 0.004 0.279 0.195 3.303 0.032 0.868 26.801 0.07 25526. 0.3860
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3.35 0.1966 0.3808 0.0562 0.0290 0.004 0.278 0.188 3.289 0.031 0.836 25.918 0.07 25550. 0.3663
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3.72 0.2185 0.4087 0.0539 0.0288 0.004 0.276 0.180 3.268 0.031 0.802 25.037 0.07 25576. 0.3467
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4.10 0.2403 0.4338 0.0516 0.0286 0.004 0.274 0.173 3.240 0.031 0.767 24.155 0.07 25602. 0.3271
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4.47 0.2622 0.4559 0.0491 0.0283 0.004 0.271 0.164 3.203 0.031 0.731 23.271 0.07 25631. 0.3075
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4.84 0.2840 0.4750 0.0466 0.0279 0.004 0.267 0.156 3.159 0.030 0.693 22.382 0.07 25661. 0.2880
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5.21 0.3059 0.4910 0.0440 0.0274 0.004 0.262 0.147 3.106 0.030 0.654 21.484 0.07 25692. 0.2686
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5.59 0.3277 0.5038 0.0413 0.0268 0.004 0.257 0.138 3.043 0.029 0.614 20.573 0.07 25725. 0.2492
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5.96 0.3495 0.5131 0.0385 0.0262 0.004 0.251 0.129 2.972 0.028 0.573 19.645 0.07 25760. 0.2298
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6.33 0.3714 0.5188 0.0356 0.0255 0.004 0.244 0.119 2.892 0.028 0.530 18.693 0.07 25797. 0.2104
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6.70 0.3932 0.5204 0.0327 0.0247 0.004 0.237 0.109 2.802 0.027 0.487 17.710 0.07 25835. 0.1910
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7.08 0.4151 0.5176 0.0297 0.0238 0.004 0.228 0.099 2.703 0.026 0.442 16.686 0.07 25875. 0.1715
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7.45 0.4369 0.5096 0.0267 0.0229 0.003 0.219 0.089 2.594 0.025 0.397 15.609 0.07 25916. 0.1520
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7.82 0.4588 0.4958 0.0236 0.0218 0.003 0.209 0.079 2.475 0.024 0.351 14.463 0.07 25959. 0.1324
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8.19 0.4806 0.4751 0.0205 0.0207 0.003 0.198 0.068 2.346 0.022 0.304 13.229 0.07 26004. 0.1128
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8.56 0.5025 0.4459 0.0173 0.0195 0.003 0.187 0.058 2.207 0.021 0.257 11.876 0.07 26051. 0.0931
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8.94 0.5243 0.4063 0.0141 0.0182 0.003 0.174 0.047 2.059 0.020 0.209 10.369 0.07 26099. 0.0733
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9.31 0.5462 0.3532 0.0108 0.0168 0.003 0.161 0.036 1.901 0.018 0.161 8.654 0.07 26150. 0.0537
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9.68 0.5680 0.2823 0.0076 0.0153 0.002 0.146 0.025 1.733 0.017 0.113 6.651 0.07 26201. 0.0346
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10.05 0.5899 0.1869 0.0044 0.0137 0.002 0.132 0.015 1.557 0.015 0.065 4.241 0.07 26255. 0.0167
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10.43 0.6117 0.0560 0.0011 0.0121 0.002 0.116 0.004 1.371 0.013 0.016 1.225 0.07 26310. 0.0024
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10.80 0.6335
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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 0.0720 0.0247 0.030 0.946 0.964 22.380 0.107 4.286 19.530 0.14 50767. 0.6250
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0.73 0.0215 0.0608 0.0708 0.0250 0.030 0.957 0.947 22.641 0.108 4.212 18.968 0.14 50794. 0.6017
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1.46 0.0429 0.1181 0.0694 0.0252 0.031 0.967 0.929 22.877 0.109 4.131 18.412 0.14 50822. 0.5784
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2.20 0.0644 0.1719 0.0679 0.0254 0.031 0.976 0.909 23.084 0.110 4.044 17.863 0.14 50854. 0.5552
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2.93 0.0859 0.2223 0.0664 0.0256 0.031 0.983 0.888 23.255 0.111 3.950 17.322 0.14 50887. 0.5321
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3.66 0.1073 0.2693 0.0647 0.0258 0.031 0.988 0.866 23.387 0.112 3.851 16.789 0.14 50923. 0.5092
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4.39 0.1288 0.3131 0.0629 0.0259 0.031 0.992 0.842 23.476 0.112 3.744 16.265 0.14 50961. 0.4865
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5.12 0.1502 0.3536 0.0610 0.0259 0.032 0.994 0.817 23.516 0.112 3.632 15.749 0.14 51002. 0.4639
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5.85 0.1717 0.3911 0.0590 0.0259 0.032 0.993 0.790 23.505 0.112 3.513 15.242 0.14 51046. 0.4416
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6.59 0.1932 0.4256 0.0569 0.0258 0.031 0.991 0.762 23.438 0.112 3.388 14.742 0.14 51092. 0.4194
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7.32 0.2146 0.4571 0.0547 0.0257 0.031 0.985 0.732 23.313 0.111 3.258 14.249 0.14 51142. 0.3975
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8.05 0.2361 0.4856 0.0524 0.0255 0.031 0.977 0.702 23.127 0.110 3.121 13.762 0.14 51194. 0.3758
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8.78 0.2576 0.5112 0.0501 0.0252 0.031 0.967 0.670 22.877 0.109 2.979 13.280 0.14 51249. 0.3543
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9.51 0.2790 0.5339 0.0476 0.0249 0.030 0.953 0.637 22.559 0.108 2.832 12.802 0.14 51307. 0.3330
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10.24 0.3005 0.5535 0.0450 0.0244 0.030 0.937 0.603 22.172 0.106 2.680 12.326 0.14 51368. 0.3119
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10.98 0.3220 0.5702 0.0424 0.0239 0.029 0.918 0.567 21.713 0.104 2.523 11.849 0.14 51433. 0.2909
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11.71 0.3434 0.5836 0.0397 0.0233 0.028 0.895 0.531 21.180 0.101 2.362 11.371 0.14 51500. 0.2701
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12.44 0.3649 0.5937 0.0369 0.0227 0.028 0.869 0.494 20.571 0.098 2.196 10.887 0.14 51571. 0.2494
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13.17 0.3864 0.6002 0.0341 0.0219 0.027 0.840 0.456 19.884 0.095 2.027 10.394 0.14 51645. 0.2287
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13.90 0.4078 0.6027 0.0311 0.0211 0.026 0.808 0.417 19.117 0.091 1.854 9.888 0.14 51722. 0.2081
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14.63 0.4293 0.6006 0.0282 0.0201 0.024 0.772 0.377 18.269 0.087 1.677 9.362 0.14 51803. 0.1874
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15.37 0.4507 0.5934 0.0252 0.0191 0.023 0.733 0.337 17.339 0.083 1.498 8.809 0.14 51886. 0.1666
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16.10 0.4722 0.5800 0.0221 0.0180 0.022 0.690 0.296 16.327 0.078 1.316 8.218 0.14 51973. 0.1457
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16.83 0.4937 0.5588 0.0190 0.0168 0.020 0.644 0.254 15.232 0.073 1.131 7.574 0.14 52064. 0.1245
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17.56 0.5151 0.5279 0.0159 0.0155 0.019 0.594 0.212 14.054 0.067 0.945 6.857 0.14 52158. 0.1030
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18.29 0.5366 0.4841 0.0127 0.0141 0.017 0.541 0.170 12.796 0.061 0.757 6.036 0.14 52255. 0.0812
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19.02 0.5581 0.4222 0.0096 0.0126 0.015 0.484 0.128 11.458 0.055 0.569 5.062 0.15 52355. 0.0590
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19.76 0.5795 0.3341 0.0064 0.0111 0.013 0.424 0.085 10.043 0.048 0.380 3.857 0.15 52459. 0.0367
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20.49 0.6010 0.2047 0.0032 0.0094 0.011 0.362 0.043 8.555 0.041 0.191 2.279 0.15 52565. 0.0154
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21.22 0.6225 0.0014 0.0000 0.0077 0.009 0.295 0.000 6.976 0.033 0.001 0.015 0.15 52670. 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 0.0724 0.0233 0.096 2.007 2.179 71.252 0.227 9.691 13.870 0.21 76149. 0.6674
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1.10 0.0215 0.0649 0.0711 0.0236 0.097 2.034 2.141 72.188 0.230 9.523 13.452 0.21 76189. 0.6416
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2.20 0.0431 0.1259 0.0697 0.0239 0.098 2.058 2.100 73.041 0.232 9.341 13.040 0.21 76233. 0.6160
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3.30 0.0646 0.1830 0.0683 0.0241 0.099 2.079 2.056 73.793 0.235 9.144 12.636 0.21 76279. 0.5906
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4.40 0.0861 0.2364 0.0667 0.0243 0.100 2.097 2.008 74.426 0.237 8.933 12.240 0.21 76330. 0.5654
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5.51 0.1077 0.2861 0.0650 0.0245 0.100 2.111 1.958 74.923 0.238 8.708 11.852 0.21 76384. 0.5406
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6.61 0.1292 0.3323 0.0632 0.0246 0.101 2.121 1.904 75.270 0.240 8.468 11.472 0.21 76442. 0.5160
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7.71 0.1507 0.3751 0.0613 0.0246 0.101 2.126 1.847 75.451 0.240 8.214 11.101 0.21 76504. 0.4917
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8.81 0.1723 0.4147 0.0593 0.0246 0.101 2.126 1.786 75.454 0.240 7.945 10.737 0.21 76570. 0.4678
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9.91 0.1938 0.4510 0.0572 0.0246 0.101 2.121 1.723 75.266 0.240 7.662 10.381 0.21 76640. 0.4441
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11.01 0.2153 0.4843 0.0550 0.0245 0.100 2.110 1.656 74.875 0.238 7.366 10.032 0.21 76714. 0.4208
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12.11 0.2369 0.5145 0.0527 0.0243 0.100 2.092 1.587 74.269 0.236 7.057 9.689 0.21 76793. 0.3978
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13.21 0.2584 0.5418 0.0503 0.0240 0.098 2.069 1.514 73.440 0.234 6.736 9.352 0.21 76876. 0.3752
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14.32 0.2799 0.5661 0.0478 0.0236 0.097 2.039 1.439 72.377 0.230 6.402 9.020 0.22 76964. 0.3528
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15.42 0.3015 0.5874 0.0452 0.0232 0.095 2.002 1.362 71.070 0.226 6.057 8.691 0.22 77057. 0.3306
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16.52 0.3230 0.6057 0.0426 0.0227 0.093 1.958 1.282 69.511 0.221 5.702 8.364 0.22 77154. 0.3087
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17.62 0.3446 0.6209 0.0398 0.0221 0.091 1.907 1.200 67.693 0.215 5.336 8.038 0.22 77256. 0.2870
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18.72 0.3661 0.6328 0.0370 0.0214 0.088 1.848 1.115 65.606 0.209 4.961 7.711 0.22 77362. 0.2655
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19.82 0.3876 0.6413 0.0342 0.0207 0.085 1.782 1.029 63.246 0.201 4.577 7.380 0.22 77474. 0.2440
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20.92 0.4092 0.6459 0.0312 0.0198 0.081 1.707 0.941 60.605 0.193 4.185 7.041 0.22 77590. 0.2226
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22.02 0.4307 0.6461 0.0283 0.0188 0.077 1.625 0.851 57.680 0.184 3.785 6.692 0.22 77712. 0.2012
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23.13 0.4522 0.6413 0.0252 0.0178 0.073 1.535 0.760 54.466 0.173 3.379 6.326 0.22 77838. 0.1797
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24.23 0.4738 0.6304 0.0222 0.0166 0.068 1.436 0.667 50.961 0.162 2.966 5.936 0.22 77970. 0.1580
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25.33 0.4953 0.6119 0.0190 0.0154 0.063 1.329 0.573 47.166 0.150 2.549 5.511 0.22 78106. 0.1360
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26.43 0.5168 0.5834 0.0159 0.0141 0.058 1.214 0.478 43.081 0.137 2.127 5.035 0.22 78248. 0.1135
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27.53 0.5384 0.5413 0.0127 0.0126 0.052 1.091 0.383 38.711 0.123 1.703 4.485 0.22 78394. 0.0905
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28.63 0.5599 0.4795 0.0095 0.0111 0.046 0.960 0.287 34.062 0.108 1.276 3.820 0.22 78546. 0.0667
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29.73 0.5814 0.3872 0.0063 0.0095 0.039 0.821 0.191 29.145 0.093 0.849 2.970 0.22 78702. 0.0423
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30.83 0.6030 0.2429 0.0032 0.0078 0.032 0.675 0.095 23.968 0.076 0.422 1.797 0.22 78863. 0.0180
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31.93 0.6245 -0.0082 -0.0001 0.0060 0.025 0.519 -0.002 18.429 0.059 -0.011 -0.059 0.22 79016. 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 0.0728 0.0226 0.220 3.460 3.897 163.726 0.391 17.332 10.794 0.29 101530. 0.6946
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1.49 0.0218 0.0681 0.0715 0.0229 0.223 3.509 3.828 166.054 0.396 17.029 10.457 0.29 101584. 0.6670
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2.97 0.0436 0.1319 0.0701 0.0232 0.226 3.554 3.755 168.181 0.402 16.701 10.126 0.29 101642. 0.6396
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4.46 0.0653 0.1915 0.0687 0.0234 0.228 3.593 3.675 170.059 0.406 16.347 9.802 0.29 101706. 0.6126
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5.94 0.0871 0.2470 0.0671 0.0237 0.230 3.627 3.590 171.644 0.410 15.967 9.486 0.29 101774. 0.5859
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7.43 0.1089 0.2987 0.0654 0.0238 0.232 3.653 3.498 172.896 0.413 15.560 9.177 0.29 101847. 0.5595
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8.91 0.1307 0.3467 0.0635 0.0239 0.233 3.672 3.401 173.776 0.415 15.126 8.876 0.29 101926. 0.5335
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10.40 0.1525 0.3911 0.0616 0.0240 0.234 3.682 3.297 174.246 0.416 14.665 8.582 0.29 102010. 0.5080
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11.88 0.1743 0.4321 0.0596 0.0240 0.234 3.682 3.188 174.273 0.416 14.178 8.296 0.29 102099. 0.4828
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13.37 0.1960 0.4698 0.0574 0.0240 0.233 3.673 3.072 173.826 0.415 13.666 8.017 0.29 102195. 0.4581
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14.85 0.2178 0.5042 0.0551 0.0238 0.232 3.653 2.952 172.875 0.413 13.129 7.744 0.29 102296. 0.4337
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16.34 0.2396 0.5355 0.0528 0.0236 0.230 3.622 2.826 171.393 0.409 12.568 7.478 0.29 102403. 0.4097
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17.82 0.2614 0.5638 0.0503 0.0233 0.227 3.579 2.694 169.354 0.404 11.985 7.216 0.29 102516. 0.3861
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19.31 0.2832 0.5891 0.0478 0.0230 0.224 3.523 2.558 166.732 0.398 11.380 6.960 0.29 102636. 0.3629
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20.79 0.3049 0.6113 0.0452 0.0225 0.219 3.455 2.418 163.505 0.390 10.754 6.707 0.29 102761. 0.3399
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22.28 0.3267 0.6305 0.0425 0.0220 0.214 3.374 2.273 159.650 0.381 10.108 6.456 0.29 102894. 0.3173
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23.76 0.3485 0.6467 0.0397 0.0214 0.208 3.278 2.123 155.148 0.370 9.445 6.208 0.29 103032. 0.2949
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25.25 0.3703 0.6595 0.0368 0.0207 0.201 3.169 1.970 149.979 0.358 8.764 5.959 0.29 103178. 0.2726
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26.73 0.3921 0.6689 0.0339 0.0199 0.193 3.046 1.814 144.128 0.344 8.067 5.707 0.29 103329. 0.2506
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28.22 0.4139 0.6744 0.0309 0.0190 0.184 2.907 1.654 137.579 0.328 7.355 5.452 0.29 103488. 0.2285
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29.70 0.4356 0.6756 0.0278 0.0180 0.175 2.754 1.491 130.321 0.311 6.630 5.188 0.29 103653. 0.2065
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31.19 0.4574 0.6716 0.0248 0.0169 0.164 2.585 1.325 122.346 0.292 5.893 4.912 0.29 103826. 0.1843
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32.67 0.4792 0.6613 0.0216 0.0157 0.152 2.401 1.157 113.649 0.271 5.146 4.617 0.29 104005. 0.1619
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34.16 0.5010 0.6430 0.0184 0.0144 0.140 2.202 0.987 104.230 0.249 4.389 4.294 0.29 104190. 0.1390
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35.64 0.5228 0.6139 0.0152 0.0130 0.126 1.988 0.815 94.095 0.225 3.625 3.929 0.29 104383. 0.1156
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37.13 0.5445 0.5695 0.0120 0.0115 0.112 1.759 0.642 83.255 0.199 2.857 3.499 0.29 104583. 0.0914
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38.61 0.5663 0.5018 0.0088 0.0099 0.096 1.516 0.469 71.731 0.171 2.085 2.964 0.29 104789. 0.0662
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40.10 0.5881 0.3954 0.0055 0.0082 0.080 1.258 0.295 59.547 0.142 1.314 2.249 0.29 105002. 0.0398
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41.58 0.6099 0.2161 0.0023 0.0064 0.063 0.987 0.122 46.715 0.112 0.543 1.185 0.29 105220. 0.0135
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43.07 0.6317
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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 0.0733 0.0222 0.422 5.317 6.133 314.508 0.601 27.280 8.845 0.36 126907. 0.7140
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1.84 0.0216 0.0692 0.0721 0.0225 0.428 5.395 6.028 319.159 0.610 26.812 8.566 0.36 126975. 0.6856
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3.68 0.0432 0.1340 0.0707 0.0228 0.434 5.467 5.914 323.420 0.618 26.304 8.293 0.36 127047. 0.6574
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5.53 0.0648 0.1945 0.0692 0.0231 0.439 5.531 5.790 327.199 0.625 25.756 8.027 0.36 127126. 0.6296
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7.37 0.0865 0.2509 0.0677 0.0233 0.443 5.585 5.658 330.410 0.631 25.167 7.767 0.36 127211. 0.6022
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9.21 0.1081 0.3034 0.0660 0.0235 0.447 5.629 5.516 332.971 0.636 24.535 7.514 0.36 127302. 0.5753
|
|
11.05 0.1297 0.3522 0.0641 0.0236 0.449 5.660 5.365 334.806 0.639 23.862 7.268 0.36 127399. 0.5487
|
|
12.90 0.1513 0.3973 0.0622 0.0237 0.450 5.677 5.204 335.845 0.641 23.147 7.028 0.36 127503. 0.5226
|
|
14.74 0.1729 0.4390 0.0602 0.0237 0.451 5.680 5.034 336.020 0.642 22.392 6.795 0.36 127614. 0.4970
|
|
16.58 0.1945 0.4774 0.0581 0.0237 0.450 5.668 4.855 335.270 0.640 21.596 6.568 0.36 127732. 0.4718
|
|
18.42 0.2161 0.5126 0.0558 0.0235 0.447 5.638 4.668 333.538 0.637 20.762 6.348 0.36 127857. 0.4471
|
|
20.26 0.2378 0.5448 0.0535 0.0233 0.444 5.591 4.472 330.769 0.632 19.891 6.132 0.36 127990. 0.4227
|
|
22.11 0.2594 0.5739 0.0510 0.0231 0.438 5.526 4.268 326.912 0.624 18.984 5.922 0.36 128130. 0.3988
|
|
23.95 0.2810 0.6001 0.0485 0.0227 0.432 5.442 4.057 321.919 0.615 18.043 5.715 0.36 128278. 0.3753
|
|
25.79 0.3026 0.6233 0.0459 0.0223 0.423 5.338 3.838 315.745 0.603 17.070 5.513 0.36 128433. 0.3521
|
|
27.63 0.3242 0.6436 0.0432 0.0218 0.413 5.212 3.612 308.346 0.589 16.067 5.313 0.36 128596. 0.3292
|
|
29.47 0.3458 0.6610 0.0404 0.0211 0.402 5.066 3.380 299.683 0.572 15.034 5.116 0.36 128767. 0.3066
|
|
31.32 0.3674 0.6753 0.0376 0.0204 0.389 4.898 3.142 289.718 0.553 13.974 4.919 0.36 128947. 0.2842
|
|
33.16 0.3891 0.6863 0.0346 0.0196 0.373 4.707 2.898 278.421 0.532 12.890 4.721 0.36 129134. 0.2620
|
|
35.00 0.4107 0.6937 0.0317 0.0188 0.356 4.493 2.649 265.760 0.508 11.782 4.521 0.36 129330. 0.2398
|
|
36.84 0.4323 0.6970 0.0286 0.0178 0.338 4.255 2.395 251.712 0.481 10.652 4.315 0.36 129534. 0.2177
|
|
38.69 0.4539 0.6957 0.0255 0.0167 0.317 3.994 2.137 236.261 0.451 9.504 4.102 0.36 129746. 0.1955
|
|
40.53 0.4755 0.6886 0.0224 0.0155 0.294 3.709 1.875 219.395 0.419 8.339 3.876 0.36 129967. 0.1730
|
|
42.37 0.4971 0.6743 0.0192 0.0142 0.270 3.400 1.610 201.112 0.384 7.159 3.630 0.36 130196. 0.1501
|
|
44.21 0.5188 0.6502 0.0160 0.0128 0.243 3.067 1.342 181.421 0.346 5.968 3.355 0.36 130434. 0.1267
|
|
46.05 0.5404 0.6123 0.0128 0.0113 0.215 2.711 1.072 160.344 0.306 4.769 3.033 0.36 130680. 0.1024
|
|
47.90 0.5620 0.5533 0.0096 0.0097 0.185 2.331 0.801 137.915 0.263 3.564 2.635 0.36 130934. 0.0769
|
|
49.74 0.5836 0.4592 0.0063 0.0081 0.153 1.930 0.530 114.182 0.218 2.358 2.106 0.36 131197. 0.0500
|
|
51.58 0.6052 0.2983 0.0031 0.0063 0.120 1.508 0.259 89.186 0.170 1.154 1.319 0.36 131466. 0.0219
|
|
53.42 0.6268 -0.0408 -0.0003 0.0043 0.083 1.041 -0.024 61.570 0.118 -0.105 -0.174 0.36 131683. 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 0.0740 0.0220 0.724 7.601 8.911 539.608 0.859 39.635 7.490 0.43 152282. 0.7288
|
|
2.21 0.0216 0.0703 0.0727 0.0224 0.735 7.718 8.760 547.879 0.872 38.962 7.252 0.43 152363. 0.6996
|
|
4.42 0.0433 0.1361 0.0714 0.0227 0.745 7.825 8.595 555.467 0.884 38.232 7.019 0.43 152450. 0.6708
|
|
6.64 0.0649 0.1975 0.0699 0.0230 0.754 7.920 8.418 562.207 0.895 37.442 6.791 0.43 152545. 0.6423
|
|
8.85 0.0865 0.2548 0.0683 0.0232 0.762 8.001 8.227 567.944 0.904 36.592 6.570 0.43 152647. 0.6143
|
|
11.06 0.1081 0.3081 0.0666 0.0234 0.768 8.065 8.022 572.536 0.911 35.680 6.355 0.43 152757. 0.5867
|
|
13.27 0.1298 0.3576 0.0648 0.0235 0.772 8.112 7.803 575.846 0.916 34.706 6.146 0.43 152874. 0.5596
|
|
15.48 0.1514 0.4034 0.0629 0.0236 0.775 8.139 7.570 577.749 0.920 33.672 5.943 0.43 152999. 0.5330
|
|
17.69 0.1730 0.4457 0.0608 0.0236 0.775 8.144 7.324 578.127 0.920 32.577 5.746 0.43 153133. 0.5069
|
|
19.91 0.1946 0.4847 0.0587 0.0236 0.774 8.126 7.065 576.872 0.918 31.424 5.555 0.43 153275. 0.4813
|
|
22.12 0.2163 0.5206 0.0564 0.0234 0.770 8.084 6.793 573.882 0.913 30.214 5.369 0.43 153426. 0.4561
|
|
24.33 0.2379 0.5533 0.0540 0.0232 0.763 8.016 6.508 569.063 0.906 28.950 5.188 0.43 153585. 0.4314
|
|
26.54 0.2595 0.5831 0.0516 0.0230 0.754 7.922 6.212 562.326 0.895 27.633 5.011 0.43 153754. 0.4071
|
|
28.75 0.2811 0.6099 0.0490 0.0226 0.742 7.798 5.905 553.586 0.881 26.266 4.838 0.43 153931. 0.3833
|
|
30.96 0.3028 0.6338 0.0464 0.0222 0.728 7.646 5.587 542.762 0.864 24.853 4.669 0.43 154118. 0.3598
|
|
33.18 0.3244 0.6549 0.0437 0.0216 0.710 7.463 5.259 529.782 0.843 23.394 4.503 0.43 154315. 0.3366
|
|
35.39 0.3460 0.6731 0.0409 0.0210 0.690 7.249 4.922 514.573 0.819 21.893 4.338 0.43 154521. 0.3138
|
|
37.60 0.3676 0.6882 0.0380 0.0203 0.667 7.002 4.576 497.074 0.791 20.353 4.175 0.43 154736. 0.2911
|
|
39.81 0.3893 0.7002 0.0350 0.0195 0.640 6.723 4.221 477.224 0.760 18.775 4.012 0.43 154962. 0.2687
|
|
42.02 0.4109 0.7087 0.0320 0.0186 0.610 6.409 3.859 454.974 0.724 17.164 3.847 0.43 155197. 0.2463
|
|
44.24 0.4325 0.7133 0.0290 0.0176 0.577 6.061 3.490 430.281 0.685 15.521 3.678 0.43 155442. 0.2240
|
|
46.45 0.4542 0.7134 0.0259 0.0165 0.541 5.679 3.114 403.115 0.642 13.851 3.504 0.43 155697. 0.2015
|
|
48.66 0.4758 0.7080 0.0227 0.0152 0.501 5.261 2.733 373.457 0.594 12.156 3.319 0.43 155963. 0.1789
|
|
50.87 0.4974 0.6956 0.0195 0.0139 0.458 4.808 2.347 341.303 0.543 10.439 3.119 0.43 156238. 0.1558
|
|
53.08 0.5190 0.6736 0.0163 0.0125 0.411 4.320 1.957 306.669 0.488 8.706 2.895 0.43 156524. 0.1320
|
|
55.29 0.5407 0.6381 0.0130 0.0110 0.362 3.798 1.565 269.592 0.429 6.959 2.632 0.43 156819. 0.1073
|
|
57.51 0.5623 0.5815 0.0097 0.0094 0.309 3.242 1.170 230.135 0.366 5.206 2.307 0.44 157125. 0.0813
|
|
59.72 0.5839 0.4890 0.0064 0.0077 0.253 2.654 0.776 188.382 0.300 3.450 1.868 0.44 157441. 0.0536
|
|
61.93 0.6055 0.3254 0.0032 0.0059 0.194 2.034 0.382 144.403 0.230 1.697 1.199 0.44 157764. 0.0241
|
|
64.14 0.6272 -0.0624 -0.0004 0.0038 0.126 1.322 -0.046 93.840 0.149 -0.204 -0.222 0.44 157942. 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 0.0748 0.0220 1.149 10.347 12.259 856.956 1.169 54.529 6.489 0.50 177652. 0.7406
|
|
2.58 0.0216 0.0710 0.0735 0.0224 1.167 10.511 12.054 870.478 1.187 53.618 6.281 0.50 177746. 0.7109
|
|
5.16 0.0432 0.1374 0.0722 0.0227 1.184 10.661 11.831 882.892 1.204 52.626 6.078 0.50 177849. 0.6815
|
|
7.74 0.0648 0.1994 0.0707 0.0230 1.199 10.794 11.590 893.930 1.219 51.553 5.881 0.50 177960. 0.6526
|
|
10.31 0.0864 0.2572 0.0691 0.0232 1.211 10.908 11.330 903.345 1.232 50.395 5.689 0.50 178079. 0.6242
|
|
12.89 0.1081 0.3110 0.0674 0.0234 1.222 10.999 11.050 910.898 1.243 49.152 5.502 0.50 178207. 0.5962
|
|
15.47 0.1297 0.3609 0.0656 0.0236 1.229 11.065 10.751 916.368 1.250 47.822 5.322 0.50 178345. 0.5688
|
|
18.05 0.1513 0.4072 0.0636 0.0236 1.233 11.103 10.433 919.551 1.254 46.408 5.146 0.50 178491. 0.5419
|
|
20.63 0.1729 0.4500 0.0616 0.0237 1.234 11.112 10.097 920.257 1.255 44.910 4.976 0.50 178647. 0.5155
|
|
23.21 0.1945 0.4895 0.0594 0.0236 1.231 11.088 9.742 918.312 1.253 43.330 4.812 0.50 178814. 0.4895
|
|
25.79 0.2161 0.5258 0.0572 0.0235 1.225 11.031 9.369 913.553 1.246 41.672 4.651 0.50 178990. 0.4641
|
|
28.36 0.2377 0.5591 0.0548 0.0233 1.215 10.938 8.979 905.830 1.236 39.938 4.496 0.50 179176. 0.4392
|
|
30.94 0.2593 0.5893 0.0523 0.0230 1.200 10.807 8.573 894.998 1.221 38.131 4.344 0.50 179373. 0.4147
|
|
33.52 0.2809 0.6167 0.0497 0.0227 1.181 10.637 8.151 880.925 1.202 36.255 4.197 0.50 179580. 0.3906
|
|
36.10 0.3026 0.6413 0.0471 0.0222 1.158 10.426 7.714 863.484 1.178 34.313 4.052 0.50 179799. 0.3669
|
|
38.68 0.3242 0.6630 0.0443 0.0217 1.130 10.174 7.264 842.554 1.149 32.309 3.910 0.50 180028. 0.3435
|
|
41.26 0.3458 0.6819 0.0415 0.0210 1.097 9.877 6.800 818.026 1.116 30.246 3.770 0.50 180268. 0.3205
|
|
43.84 0.3674 0.6979 0.0386 0.0203 1.059 9.536 6.324 789.795 1.077 28.129 3.632 0.50 180520. 0.2977
|
|
46.41 0.3890 0.7108 0.0356 0.0195 1.016 9.150 5.836 757.769 1.034 25.960 3.493 0.50 180783. 0.2751
|
|
48.99 0.4106 0.7204 0.0326 0.0186 0.968 8.716 5.338 721.866 0.985 23.743 3.354 0.50 181057. 0.2526
|
|
51.57 0.4322 0.7262 0.0295 0.0175 0.915 8.235 4.830 682.019 0.930 21.484 3.212 0.50 181343. 0.2301
|
|
54.15 0.4538 0.7277 0.0263 0.0164 0.856 7.706 4.313 638.177 0.871 19.185 3.065 0.50 181641. 0.2075
|
|
56.73 0.4754 0.7239 0.0231 0.0152 0.792 7.128 3.788 590.309 0.805 16.851 2.911 0.51 181950. 0.1847
|
|
59.31 0.4970 0.7134 0.0199 0.0138 0.722 6.501 3.257 538.410 0.734 14.488 2.744 0.51 182272. 0.1614
|
|
61.89 0.5187 0.6938 0.0166 0.0124 0.647 5.826 2.720 482.502 0.658 12.101 2.557 0.51 182605. 0.1375
|
|
64.46 0.5403 0.6611 0.0133 0.0109 0.567 5.103 2.180 422.645 0.577 9.696 2.339 0.51 182949. 0.1126
|
|
67.04 0.5619 0.6078 0.0100 0.0092 0.481 4.334 1.637 358.939 0.490 7.280 2.068 0.51 183306. 0.0862
|
|
69.62 0.5835 0.5189 0.0067 0.0075 0.391 3.520 1.093 291.522 0.398 4.860 1.700 0.51 183673. 0.0579
|
|
72.20 0.6051 0.3578 0.0034 0.0057 0.296 2.663 0.550 220.510 0.301 2.444 1.130 0.51 184051. 0.0273
|
|
74.78 0.6267 -0.0132 -0.0001 0.0037 0.192 1.726 -0.013 142.929 0.195 -0.056 -0.040 0.51 184374. 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 0.0757 0.0222 1.726 13.600 16.217 1287.230 1.537 72.132 5.714 0.57 203016. 0.7501
|
|
2.95 0.0217 0.0716 0.0745 0.0225 1.754 13.821 15.950 1308.143 1.561 70.946 5.530 0.57 203125. 0.7200
|
|
5.91 0.0433 0.1386 0.0731 0.0229 1.780 14.024 15.659 1327.351 1.584 69.653 5.351 0.57 203243. 0.6903
|
|
8.86 0.0650 0.2011 0.0717 0.0232 1.803 14.204 15.344 1344.437 1.605 68.250 5.177 0.57 203371. 0.6610
|
|
11.82 0.0866 0.2594 0.0701 0.0234 1.822 14.358 15.003 1359.012 1.622 66.732 5.007 0.57 203508. 0.6322
|
|
14.77 0.1083 0.3136 0.0684 0.0236 1.838 14.482 14.636 1370.707 1.636 65.099 4.843 0.57 203656. 0.6040
|
|
17.72 0.1300 0.3639 0.0665 0.0238 1.850 14.571 14.242 1379.178 1.646 63.349 4.684 0.57 203814. 0.5762
|
|
20.68 0.1516 0.4106 0.0646 0.0238 1.856 14.624 13.823 1384.110 1.652 61.485 4.530 0.57 203983. 0.5490
|
|
23.63 0.1733 0.4538 0.0625 0.0239 1.858 14.635 13.379 1385.213 1.653 59.508 4.381 0.57 204162. 0.5223
|
|
26.58 0.1950 0.4937 0.0603 0.0238 1.854 14.604 12.909 1382.219 1.650 57.420 4.236 0.57 204354. 0.4961
|
|
29.54 0.2166 0.5304 0.0580 0.0237 1.844 14.526 12.416 1374.884 1.641 55.226 4.096 0.57 204556. 0.4705
|
|
32.49 0.2383 0.5641 0.0556 0.0235 1.828 14.400 11.900 1362.978 1.627 52.930 3.960 0.57 204771. 0.4453
|
|
35.45 0.2599 0.5948 0.0531 0.0232 1.805 14.224 11.361 1346.287 1.607 50.536 3.828 0.57 204997. 0.4206
|
|
38.40 0.2816 0.6227 0.0505 0.0228 1.776 13.995 10.802 1324.611 1.581 48.048 3.699 0.57 205236. 0.3963
|
|
41.35 0.3033 0.6478 0.0477 0.0224 1.740 13.711 10.223 1297.760 1.549 45.472 3.573 0.57 205487. 0.3724
|
|
44.31 0.3249 0.6701 0.0450 0.0218 1.697 13.371 9.625 1265.556 1.511 42.812 3.450 0.57 205751. 0.3489
|
|
47.26 0.3466 0.6896 0.0421 0.0211 1.647 12.972 9.009 1227.832 1.466 40.073 3.328 0.57 206027. 0.3256
|
|
50.22 0.3682 0.7062 0.0391 0.0204 1.588 12.514 8.377 1184.432 1.414 37.261 3.208 0.58 206317. 0.3027
|
|
53.17 0.3899 0.7198 0.0361 0.0196 1.522 11.994 7.729 1135.220 1.355 34.379 3.088 0.58 206619. 0.2799
|
|
56.12 0.4116 0.7302 0.0330 0.0186 1.448 11.411 7.067 1080.071 1.289 31.434 2.968 0.58 206934. 0.2572
|
|
59.08 0.4332 0.7369 0.0299 0.0176 1.366 10.765 6.392 1018.879 1.216 28.430 2.845 0.58 207263. 0.2345
|
|
62.03 0.4549 0.7394 0.0266 0.0164 1.276 10.054 5.705 951.573 1.136 25.374 2.719 0.58 207605. 0.2117
|
|
64.98 0.4766 0.7368 0.0234 0.0151 1.178 9.277 5.007 878.106 1.048 22.271 2.586 0.58 207961. 0.1886
|
|
67.94 0.4982 0.7276 0.0201 0.0138 1.071 8.436 4.300 798.470 0.953 19.128 2.443 0.58 208329. 0.1651
|
|
70.89 0.5199 0.7094 0.0168 0.0123 0.956 7.530 3.586 712.704 0.851 15.952 2.282 0.58 208712. 0.1409
|
|
73.85 0.5415 0.6780 0.0134 0.0107 0.833 6.560 2.867 620.899 0.741 12.753 2.094 0.58 209108. 0.1156
|
|
76.80 0.5632 0.6259 0.0100 0.0090 0.702 5.528 2.144 523.214 0.625 9.538 1.859 0.58 209517. 0.0887
|
|
79.75 0.5849 0.5366 0.0066 0.0072 0.563 4.436 1.421 419.864 0.501 6.319 1.535 0.58 209939. 0.0596
|
|
82.71 0.6065 0.3690 0.0033 0.0054 0.417 3.286 0.698 311.016 0.371 3.104 1.018 0.58 210372. 0.0277
|
|
85.66 0.6282
|
|
|
|
|
|
|
|
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 0.0769 0.0224 2.488 17.423 20.833 1855.258 1.968 92.665 5.093 0.64 228374. 0.7578
|
|
3.34 0.0218 0.0722 0.0756 0.0228 2.530 17.715 20.497 1886.348 2.001 91.172 4.929 0.64 228497. 0.7274
|
|
6.68 0.0435 0.1396 0.0743 0.0232 2.568 17.984 20.130 1914.911 2.032 89.538 4.768 0.64 228632. 0.6973
|
|
10.02 0.0653 0.2026 0.0728 0.0235 2.602 18.222 19.730 1940.311 2.059 87.758 4.612 0.64 228777. 0.6678
|
|
13.36 0.0871 0.2613 0.0712 0.0237 2.631 18.426 19.296 1961.966 2.082 85.827 4.461 0.64 228933. 0.6388
|
|
16.70 0.1089 0.3158 0.0695 0.0239 2.654 18.588 18.827 1979.314 2.100 83.742 4.314 0.64 229101. 0.6102
|
|
20.04 0.1306 0.3666 0.0676 0.0241 2.671 18.706 18.324 1991.839 2.113 81.504 4.173 0.64 229281. 0.5822
|
|
23.38 0.1524 0.4136 0.0656 0.0242 2.681 18.774 17.786 1999.075 2.121 79.113 4.035 0.64 229473. 0.5548
|
|
26.72 0.1742 0.4572 0.0635 0.0242 2.683 18.788 17.215 2000.587 2.123 76.572 3.903 0.64 229678. 0.5279
|
|
30.06 0.1959 0.4974 0.0613 0.0241 2.677 18.745 16.611 1995.987 2.118 73.885 3.775 0.64 229895. 0.5015
|
|
33.40 0.2177 0.5345 0.0590 0.0240 2.662 18.641 15.975 1984.918 2.106 71.057 3.650 0.64 230126. 0.4756
|
|
36.74 0.2395 0.5685 0.0565 0.0238 2.638 18.473 15.309 1967.050 2.087 68.094 3.530 0.64 230371. 0.4502
|
|
40.08 0.2613 0.5997 0.0539 0.0235 2.604 18.239 14.613 1942.075 2.061 65.001 3.413 0.64 230628. 0.4253
|
|
43.42 0.2830 0.6280 0.0513 0.0231 2.561 17.935 13.890 1909.704 2.026 61.785 3.299 0.65 230900. 0.4008
|
|
46.76 0.3048 0.6535 0.0485 0.0226 2.507 17.559 13.141 1869.675 1.984 58.452 3.188 0.65 231186. 0.3767
|
|
50.10 0.3266 0.6763 0.0456 0.0220 2.443 17.109 12.367 1821.729 1.933 55.009 3.079 0.65 231486. 0.3530
|
|
53.44 0.3483 0.6963 0.0427 0.0214 2.368 16.582 11.570 1765.630 1.873 51.463 2.972 0.65 231801. 0.3296
|
|
56.78 0.3701 0.7135 0.0397 0.0206 2.281 15.976 10.751 1701.157 1.805 47.819 2.866 0.65 232130. 0.3064
|
|
60.12 0.3919 0.7277 0.0366 0.0197 2.183 15.290 9.911 1628.110 1.727 44.085 2.761 0.65 232473. 0.2834
|
|
63.46 0.4136 0.7387 0.0334 0.0187 2.074 14.522 9.053 1546.311 1.641 40.267 2.655 0.65 232832. 0.2604
|
|
66.80 0.4354 0.7462 0.0302 0.0176 1.952 13.670 8.177 1455.616 1.544 36.372 2.548 0.65 233206. 0.2375
|
|
70.14 0.4572 0.7494 0.0269 0.0164 1.818 12.734 7.286 1355.916 1.439 32.409 2.437 0.65 233595. 0.2145
|
|
73.48 0.4790 0.7476 0.0235 0.0151 1.672 11.712 6.381 1247.150 1.323 28.383 2.321 0.65 233999. 0.1911
|
|
76.82 0.5007 0.7391 0.0202 0.0137 1.514 10.606 5.464 1129.314 1.198 24.306 2.195 0.65 234418. 0.1672
|
|
80.16 0.5225 0.7215 0.0167 0.0121 1.344 9.415 4.538 1002.470 1.064 20.185 2.053 0.65 234853. 0.1426
|
|
83.50 0.5443 0.6905 0.0133 0.0105 1.162 8.140 3.605 866.766 0.920 16.033 1.886 0.65 235302. 0.1167
|
|
86.84 0.5660 0.6374 0.0098 0.0087 0.969 6.785 2.667 722.445 0.767 11.863 1.674 0.65 235767. 0.0891
|
|
90.18 0.5878 0.5438 0.0064 0.0069 0.764 5.352 1.728 569.838 0.605 7.687 1.376 0.65 236247. 0.0589
|
|
93.52 0.6096 0.3591 0.0029 0.0049 0.549 3.842 0.790 409.131 0.434 3.515 0.876 0.65 236737. 0.0254
|
|
96.86 0.6314
|
|
|
|
|
|
|
|
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 0.0782 0.0230 3.498 22.047 26.170 2608.457 2.491 116.404 4.551 0.71 253722. 0.7589
|
|
3.69 0.0217 0.0714 0.0770 0.0234 3.554 22.398 25.766 2649.938 2.531 114.606 4.410 0.71 253859. 0.7297
|
|
7.38 0.0433 0.1382 0.0757 0.0237 3.605 22.721 25.321 2688.133 2.567 112.628 4.272 0.71 254008. 0.7008
|
|
11.07 0.0650 0.2008 0.0742 0.0240 3.650 23.009 24.835 2722.177 2.599 110.464 4.138 0.71 254169. 0.6722
|
|
14.76 0.0866 0.2593 0.0727 0.0243 3.690 23.254 24.305 2751.271 2.627 108.108 4.007 0.71 254343. 0.6439
|
|
18.45 0.1083 0.3138 0.0709 0.0245 3.721 23.452 23.731 2774.619 2.650 105.555 3.879 0.71 254529. 0.6160
|
|
22.14 0.1299 0.3646 0.0691 0.0246 3.743 23.594 23.113 2791.491 2.666 102.806 3.755 0.71 254728. 0.5885
|
|
25.83 0.1516 0.4117 0.0671 0.0247 3.756 23.676 22.451 2801.200 2.675 99.860 3.635 0.71 254941. 0.5615
|
|
29.52 0.1732 0.4554 0.0650 0.0247 3.759 23.693 21.745 2803.116 2.677 96.723 3.519 0.72 255168. 0.5349
|
|
33.21 0.1949 0.4959 0.0628 0.0247 3.750 23.638 20.998 2796.649 2.671 93.398 3.405 0.72 255410. 0.5087
|
|
36.90 0.2165 0.5332 0.0604 0.0245 3.730 23.508 20.210 2781.250 2.656 89.892 3.296 0.72 255665. 0.4830
|
|
40.60 0.2382 0.5676 0.0579 0.0243 3.696 23.298 19.382 2756.414 2.632 86.213 3.189 0.72 255936. 0.4577
|
|
44.29 0.2598 0.5991 0.0554 0.0240 3.650 23.004 18.518 2721.683 2.599 82.368 3.086 0.72 256221. 0.4329
|
|
47.98 0.2815 0.6279 0.0527 0.0236 3.589 22.624 17.618 2676.627 2.556 78.365 2.985 0.72 256521. 0.4085
|
|
51.67 0.3031 0.6540 0.0499 0.0231 3.515 22.152 16.685 2620.881 2.503 74.213 2.887 0.72 256837. 0.3845
|
|
55.36 0.3248 0.6775 0.0470 0.0225 3.425 21.588 15.719 2554.102 2.439 69.920 2.792 0.72 257169. 0.3608
|
|
59.05 0.3464 0.6982 0.0440 0.0218 3.320 20.928 14.724 2475.974 2.364 65.494 2.697 0.72 257516. 0.3374
|
|
62.74 0.3681 0.7163 0.0410 0.0210 3.200 20.169 13.701 2386.205 2.279 60.943 2.604 0.72 257879. 0.3142
|
|
66.43 0.3897 0.7315 0.0378 0.0201 3.064 19.309 12.652 2284.521 2.182 56.277 2.512 0.72 258259. 0.2913
|
|
70.12 0.4114 0.7437 0.0346 0.0191 2.911 18.347 11.579 2170.679 2.073 51.504 2.419 0.72 258654. 0.2684
|
|
73.81 0.4330 0.7526 0.0313 0.0180 2.742 17.280 10.484 2044.474 1.952 46.631 2.326 0.72 259066. 0.2455
|
|
77.50 0.4547 0.7575 0.0280 0.0168 2.556 16.108 9.368 1905.749 1.820 41.669 2.230 0.72 259495. 0.2225
|
|
81.19 0.4763 0.7577 0.0246 0.0155 2.353 14.829 8.234 1754.412 1.675 36.626 2.129 0.72 259940. 0.1991
|
|
84.88 0.4980 0.7519 0.0212 0.0140 2.133 13.443 7.085 1590.448 1.519 31.514 2.021 0.72 260402. 0.1753
|
|
88.57 0.5196 0.7378 0.0177 0.0125 1.896 11.951 5.923 1413.927 1.350 26.346 1.900 0.72 260880. 0.1507
|
|
92.26 0.5413 0.7115 0.0142 0.0108 1.643 10.354 4.751 1225.042 1.170 21.133 1.759 0.72 261376. 0.1250
|
|
95.95 0.5629 0.6656 0.0107 0.0090 1.373 8.656 3.573 1024.140 0.978 15.892 1.582 0.73 261887. 0.0975
|
|
99.64 0.5846 0.5839 0.0072 0.0072 1.089 6.861 2.392 811.743 0.775 10.640 1.337 0.73 262415. 0.0674
|
|
103.33 0.6062 0.4233 0.0036 0.0052 0.789 4.973 1.212 588.361 0.562 5.391 0.934 0.73 262956. 0.0335
|
|
107.02 0.6279 -0.0184 -0.0001 0.0030 0.457 2.879 -0.029 340.634 0.325 -0.131 -0.039 0.73 263372. 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 0.0798 0.0248 5.013 28.723 32.296 3738.138 3.245 143.654 3.919 0.79 279059. 0.7260
|
|
4.07 0.0217 0.0681 0.0786 0.0251 5.072 29.059 31.822 3781.867 3.283 141.542 3.816 0.79 279211. 0.7018
|
|
8.14 0.0434 0.1326 0.0773 0.0253 5.124 29.357 31.296 3820.627 3.317 139.203 3.715 0.79 279376. 0.6775
|
|
12.21 0.0651 0.1935 0.0759 0.0255 5.167 29.609 30.716 3853.401 3.345 136.626 3.615 0.79 279554. 0.6532
|
|
16.28 0.0868 0.2510 0.0743 0.0257 5.202 29.808 30.081 3879.247 3.368 133.802 3.517 0.79 279747. 0.6288
|
|
20.35 0.1085 0.3051 0.0726 0.0258 5.226 29.946 29.389 3897.295 3.383 130.724 3.420 0.79 279953. 0.6044
|
|
24.42 0.1302 0.3560 0.0708 0.0259 5.239 30.019 28.640 3906.753 3.392 127.392 3.325 0.79 280175. 0.5801
|
|
28.49 0.1519 0.4036 0.0688 0.0259 5.239 30.020 27.834 3906.887 3.392 123.806 3.231 0.79 280412. 0.5557
|
|
32.56 0.1736 0.4481 0.0666 0.0258 5.226 29.944 26.972 3897.041 3.383 119.972 3.139 0.79 280664. 0.5315
|
|
36.63 0.1954 0.4895 0.0644 0.0257 5.199 29.787 26.056 3876.587 3.365 115.896 3.049 0.79 280932. 0.5073
|
|
40.70 0.2171 0.5280 0.0620 0.0255 5.156 29.544 25.087 3844.906 3.338 111.587 2.959 0.79 281216. 0.4832
|
|
44.77 0.2388 0.5636 0.0595 0.0252 5.098 29.209 24.068 3801.383 3.300 107.053 2.872 0.79 281517. 0.4592
|
|
48.84 0.2605 0.5964 0.0568 0.0248 5.023 28.779 23.000 3745.400 3.251 102.306 2.785 0.79 281834. 0.4355
|
|
52.91 0.2822 0.6263 0.0541 0.0244 4.930 28.249 21.887 3676.349 3.192 97.354 2.700 0.79 282167. 0.4118
|
|
56.98 0.3039 0.6536 0.0512 0.0238 4.819 27.613 20.731 3593.638 3.120 92.210 2.617 0.79 282518. 0.3884
|
|
61.05 0.3256 0.6781 0.0483 0.0232 4.689 26.868 19.533 3496.682 3.036 86.885 2.534 0.79 282886. 0.3650
|
|
65.12 0.3473 0.6999 0.0452 0.0224 4.539 26.009 18.298 3384.919 2.939 81.389 2.452 0.79 283271. 0.3419
|
|
69.19 0.3690 0.7190 0.0421 0.0216 4.369 25.032 17.026 3257.793 2.828 75.734 2.371 0.79 283674. 0.3189
|
|
73.26 0.3907 0.7352 0.0388 0.0206 4.177 23.934 15.722 3114.792 2.704 69.930 2.289 0.79 284095. 0.2959
|
|
77.33 0.4124 0.7484 0.0355 0.0196 3.963 22.709 14.386 2955.442 2.566 63.989 2.208 0.79 284533. 0.2730
|
|
81.40 0.4341 0.7583 0.0322 0.0184 3.727 21.357 13.022 2779.412 2.413 57.921 2.125 0.79 284990. 0.2500
|
|
85.47 0.4558 0.7642 0.0287 0.0171 3.469 19.875 11.632 2586.605 2.245 51.738 2.040 0.79 285464. 0.2268
|
|
89.54 0.4775 0.7654 0.0252 0.0157 3.187 18.263 10.218 2376.833 2.063 45.451 1.950 0.79 285957. 0.2032
|
|
93.61 0.4992 0.7604 0.0217 0.0142 2.884 16.523 8.785 2150.291 1.867 39.075 1.853 0.80 286469. 0.1790
|
|
97.68 0.5209 0.7468 0.0181 0.0126 2.558 14.656 7.334 1907.431 1.656 32.623 1.744 0.80 286998. 0.1540
|
|
101.75 0.5426 0.7203 0.0145 0.0109 2.211 12.670 5.871 1648.963 1.431 26.113 1.615 0.80 287546. 0.1275
|
|
105.82 0.5644 0.6726 0.0109 0.0091 1.845 10.572 4.398 1375.925 1.194 19.563 1.450 0.80 288112. 0.0991
|
|
109.89 0.5861 0.5858 0.0072 0.0072 1.461 8.373 2.922 1089.672 0.946 12.995 1.216 0.80 288696. 0.0678
|
|
113.96 0.6078 0.4136 0.0036 0.0052 1.061 6.082 1.445 791.494 0.687 6.425 0.828 0.80 289294. 0.0324
|
|
118.03 0.6295
|
|
|
|
|
|
|
|
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 0.0814 0.0292 7.672 40.297 39.216 5721.104 4.553 174.432 3.109 0.86 304385. 0.6347
|
|
4.51 0.0220 0.0603 0.0803 0.0294 7.714 40.516 38.676 5752.164 4.577 172.032 3.050 0.86 304553. 0.6183
|
|
9.01 0.0441 0.1182 0.0790 0.0295 7.742 40.664 38.071 5773.206 4.594 169.342 2.991 0.86 304736. 0.6016
|
|
13.52 0.0661 0.1739 0.0776 0.0295 7.755 40.733 37.397 5783.011 4.602 166.344 2.933 0.86 304935. 0.5847
|
|
18.03 0.0881 0.2273 0.0761 0.0295 7.752 40.716 36.651 5780.551 4.600 163.024 2.876 0.86 305149. 0.5675
|
|
22.54 0.1102 0.2785 0.0744 0.0294 7.731 40.606 35.830 5764.949 4.588 159.371 2.819 0.86 305380. 0.5501
|
|
27.04 0.1322 0.3275 0.0725 0.0293 7.691 40.398 34.933 5735.522 4.564 155.381 2.763 0.86 305629. 0.5322
|
|
31.55 0.1543 0.3743 0.0705 0.0290 7.633 40.090 33.960 5691.781 4.529 151.055 2.706 0.86 305894. 0.5141
|
|
36.06 0.1763 0.4189 0.0683 0.0288 7.555 39.679 32.913 5633.413 4.483 146.399 2.650 0.86 306177. 0.4956
|
|
40.57 0.1983 0.4612 0.0660 0.0284 7.456 39.164 31.794 5560.265 4.425 141.420 2.594 0.86 306479. 0.4767
|
|
45.07 0.2204 0.5013 0.0635 0.0279 7.338 38.544 30.605 5472.192 4.355 136.132 2.537 0.86 306798. 0.4575
|
|
49.58 0.2424 0.5389 0.0609 0.0274 7.200 37.817 29.350 5369.049 4.273 130.547 2.479 0.86 307136. 0.4379
|
|
54.09 0.2644 0.5742 0.0582 0.0268 7.041 36.984 28.031 5250.701 4.178 124.681 2.421 0.86 307493. 0.4179
|
|
58.60 0.2865 0.6069 0.0553 0.0261 6.862 36.040 26.652 5116.791 4.072 118.549 2.363 0.86 307868. 0.3976
|
|
63.10 0.3085 0.6370 0.0523 0.0253 6.661 34.984 25.217 4966.842 3.952 112.165 2.303 0.86 308263. 0.3770
|
|
67.61 0.3305 0.6646 0.0493 0.0245 6.437 33.811 23.729 4800.226 3.820 105.545 2.242 0.86 308677. 0.3560
|
|
72.12 0.3526 0.6893 0.0461 0.0236 6.190 32.514 22.190 4616.187 3.673 98.702 2.180 0.86 309110. 0.3348
|
|
76.62 0.3746 0.7112 0.0428 0.0225 5.919 31.090 20.605 4413.927 3.512 91.650 2.117 0.86 309564. 0.3133
|
|
81.13 0.3966 0.7301 0.0394 0.0214 5.623 29.531 18.976 4192.703 3.336 84.405 2.053 0.86 310037. 0.2915
|
|
85.64 0.4187 0.7458 0.0359 0.0202 5.299 27.835 17.307 3951.789 3.145 76.981 1.986 0.86 310530. 0.2694
|
|
90.15 0.4407 0.7578 0.0324 0.0188 4.949 25.994 15.601 3690.490 2.937 69.393 1.917 0.87 311043. 0.2469
|
|
94.65 0.4628 0.7645 0.0288 0.0174 4.576 24.037 13.861 3412.567 2.716 61.655 1.842 0.87 311577. 0.2236
|
|
99.16 0.4848 0.7624 0.0251 0.0160 4.193 22.023 12.090 3126.661 2.488 53.777 1.754 0.87 312131. 0.1988
|
|
103.67 0.5068 0.7515 0.0214 0.0144 3.786 19.886 10.293 2823.238 2.247 45.784 1.654 0.87 312705. 0.1729
|
|
108.18 0.5289 0.7283 0.0176 0.0128 3.357 17.630 8.474 2503.046 1.992 37.694 1.536 0.87 313300. 0.1457
|
|
112.68 0.5509 0.6859 0.0138 0.0111 2.908 15.275 6.639 2168.724 1.726 29.531 1.389 0.87 313915. 0.1166
|
|
117.19 0.5729 0.6129 0.0100 0.0093 2.444 12.836 4.793 1822.439 1.450 21.321 1.193 0.87 314550. 0.0851
|
|
121.70 0.5950 0.4853 0.0061 0.0075 1.968 10.336 2.943 1467.451 1.168 13.090 0.910 0.87 315205. 0.0509
|
|
126.20 0.6170 0.2474 0.0023 0.0056 1.482 7.783 1.090 1104.963 0.879 4.846 0.447 0.87 315870. 0.0152
|
|
130.71 0.6390
|
|
|
|
|
|
|
|
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 0.0815 0.0349 11.648 56.472 46.077 8685.662 6.380 204.953 2.406 0.93 329745. 0.5324
|
|
4.91 0.0222 0.0509 0.0805 0.0351 11.717 56.806 45.538 8737.082 6.418 202.554 2.364 0.93 329924. 0.5200
|
|
9.83 0.0444 0.1001 0.0795 0.0352 11.765 57.043 44.926 8773.503 6.445 199.829 2.323 0.93 330120. 0.5075
|
|
14.74 0.0665 0.1475 0.0782 0.0353 11.790 57.162 44.233 8791.752 6.458 196.749 2.282 0.93 330333. 0.4947
|
|
19.66 0.0887 0.1933 0.0769 0.0353 11.786 57.142 43.455 8788.754 6.456 193.287 2.243 0.93 330564. 0.4819
|
|
24.57 0.1109 0.2375 0.0753 0.0352 11.750 56.966 42.585 8761.624 6.436 189.417 2.205 0.93 330813. 0.4690
|
|
29.49 0.1331 0.2802 0.0736 0.0350 11.677 56.616 41.619 8707.908 6.396 185.122 2.168 0.93 331082. 0.4559
|
|
34.40 0.1553 0.3216 0.0717 0.0346 11.567 56.083 40.556 8625.828 6.336 180.392 2.133 0.93 331370. 0.4427
|
|
39.32 0.1774 0.3617 0.0697 0.0342 11.418 55.358 39.394 8514.354 6.254 175.223 2.099 0.93 331678. 0.4294
|
|
44.23 0.1996 0.4006 0.0674 0.0336 11.229 54.441 38.134 8373.282 6.151 169.621 2.066 0.93 332007. 0.4158
|
|
49.15 0.2218 0.4382 0.0651 0.0329 11.001 53.334 36.779 8203.101 6.026 163.594 2.034 0.93 332356. 0.4020
|
|
54.06 0.2440 0.4745 0.0625 0.0321 10.735 52.045 35.332 8004.862 5.880 157.158 2.002 0.93 332726. 0.3879
|
|
58.98 0.2661 0.5094 0.0598 0.0312 10.433 50.583 33.797 7779.917 5.715 150.329 1.970 0.93 333118. 0.3734
|
|
63.89 0.2883 0.5429 0.0569 0.0302 10.098 48.957 32.178 7529.773 5.531 143.128 1.938 0.93 333530. 0.3584
|
|
68.80 0.3105 0.5747 0.0539 0.0291 9.730 47.176 30.481 7255.925 5.330 135.579 1.905 0.93 333964. 0.3429
|
|
73.72 0.3327 0.6047 0.0508 0.0279 9.333 45.247 28.710 6959.299 5.112 127.702 1.871 0.93 334419. 0.3268
|
|
78.63 0.3549 0.6327 0.0475 0.0267 8.905 43.174 26.870 6640.383 4.878 119.518 1.835 0.93 334896. 0.3101
|
|
83.55 0.3770 0.6584 0.0442 0.0253 8.448 40.958 24.965 6299.484 4.627 111.047 1.798 0.93 335395. 0.2928
|
|
88.46 0.3992 0.6815 0.0407 0.0238 7.961 38.600 23.002 5936.871 4.361 102.311 1.757 0.94 335915. 0.2747
|
|
93.38 0.4214 0.7017 0.0371 0.0223 7.446 36.102 20.983 5552.643 4.079 93.334 1.714 0.94 336458. 0.2559
|
|
98.29 0.4436 0.7183 0.0335 0.0207 6.902 33.462 18.916 5146.661 3.781 84.138 1.667 0.94 337022. 0.2363
|
|
103.21 0.4658 0.7308 0.0297 0.0189 6.328 30.681 16.805 4718.916 3.466 74.747 1.615 0.94 337609. 0.2158
|
|
108.12 0.4879 0.7309 0.0259 0.0173 5.778 28.015 14.648 4308.815 3.165 65.155 1.542 0.94 338218. 0.1924
|
|
113.04 0.5101 0.7080 0.0220 0.0159 5.299 25.692 12.447 3951.542 2.903 55.366 1.429 0.94 338849. 0.1643
|
|
117.95 0.5323 0.6680 0.0181 0.0144 4.811 23.326 10.218 3587.624 2.635 45.452 1.292 0.94 339502. 0.1346
|
|
122.87 0.5545 0.6049 0.0141 0.0129 4.317 20.930 7.970 3219.098 2.365 35.449 1.123 0.94 340178. 0.1033
|
|
127.78 0.5767 0.5087 0.0101 0.0114 3.825 18.544 5.710 2852.164 2.095 25.399 0.908 0.94 340876. 0.0707
|
|
132.70 0.5988 0.3658 0.0061 0.0100 3.338 16.184 3.451 2489.109 1.828 15.348 0.629 0.94 341594. 0.0381
|
|
137.61 0.6210 0.1532 0.0021 0.0085 2.856 13.847 1.193 2129.811 1.564 5.305 0.254 0.95 342326. 0.0090
|
|
142.52 0.6432
|
|
|
|
|
|
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