538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x4W (17x4W.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 0.0620 0.0260 0.003 0.185 0.163 2.183 0.021 0.726 33.899 0.07 41209. 0.4740
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0.22 0.0138 0.0321 0.0605 0.0260 0.003 0.184 0.159 2.179 0.021 0.708 33.127 0.07 41224. 0.4575
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0.44 0.0276 0.0628 0.0589 0.0259 0.003 0.184 0.155 2.174 0.021 0.689 32.343 0.07 41239. 0.4408
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0.66 0.0414 0.0919 0.0573 0.0258 0.003 0.183 0.151 2.167 0.021 0.671 31.548 0.07 41255. 0.4240
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0.89 0.0552 0.1193 0.0556 0.0257 0.003 0.183 0.146 2.160 0.021 0.651 30.743 0.07 41272. 0.4072
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1.11 0.0690 0.1452 0.0539 0.0256 0.003 0.182 0.142 2.150 0.021 0.631 29.927 0.07 41289. 0.3902
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1.33 0.0827 0.1694 0.0522 0.0255 0.003 0.181 0.137 2.140 0.020 0.611 29.098 0.07 41307. 0.3732
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1.55 0.0965 0.1919 0.0504 0.0253 0.003 0.180 0.133 2.127 0.020 0.589 28.256 0.07 41325. 0.3561
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1.77 0.1103 0.2127 0.0485 0.0252 0.003 0.179 0.128 2.113 0.020 0.568 27.400 0.07 41344. 0.3389
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1.99 0.1241 0.2317 0.0466 0.0250 0.003 0.177 0.123 2.097 0.020 0.546 26.528 0.07 41364. 0.3216
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2.21 0.1379 0.2488 0.0447 0.0248 0.003 0.176 0.118 2.079 0.020 0.523 25.639 0.07 41385. 0.3043
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2.44 0.1517 0.2640 0.0427 0.0245 0.003 0.174 0.112 2.060 0.020 0.499 24.731 0.07 41407. 0.2869
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2.66 0.1655 0.2772 0.0406 0.0243 0.003 0.172 0.107 2.038 0.019 0.476 23.803 0.07 41429. 0.2694
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2.88 0.1793 0.2883 0.0386 0.0240 0.003 0.170 0.101 2.013 0.019 0.451 22.852 0.07 41452. 0.2520
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3.10 0.1931 0.2972 0.0364 0.0237 0.003 0.168 0.096 1.987 0.019 0.426 21.876 0.07 41476. 0.2344
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3.32 0.2069 0.3038 0.0342 0.0233 0.003 0.165 0.090 1.958 0.019 0.401 20.872 0.07 41501. 0.2169
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3.54 0.2207 0.3080 0.0320 0.0229 0.003 0.163 0.084 1.927 0.018 0.375 19.835 0.07 41527. 0.1993
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3.76 0.2344 0.3095 0.0298 0.0225 0.003 0.160 0.078 1.893 0.018 0.348 18.763 0.07 41553. 0.1817
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3.98 0.2482 0.3083 0.0275 0.0221 0.002 0.157 0.072 1.856 0.018 0.321 17.650 0.07 41581. 0.1642
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4.21 0.2620 0.3041 0.0251 0.0216 0.002 0.154 0.066 1.816 0.017 0.294 16.490 0.07 41609. 0.1467
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4.43 0.2758 0.2965 0.0227 0.0211 0.002 0.150 0.060 1.774 0.017 0.266 15.278 0.07 41638. 0.1293
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4.65 0.2896 0.2854 0.0203 0.0206 0.002 0.146 0.053 1.729 0.017 0.237 14.006 0.07 41669. 0.1120
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4.87 0.3034 0.2704 0.0178 0.0200 0.002 0.142 0.047 1.680 0.016 0.209 12.664 0.07 41700. 0.0950
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5.09 0.3172 0.2509 0.0153 0.0194 0.002 0.138 0.040 1.629 0.016 0.180 11.241 0.07 41732. 0.0782
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5.31 0.3310 0.2265 0.0128 0.0188 0.002 0.133 0.034 1.574 0.015 0.150 9.725 0.07 41765. 0.0619
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5.53 0.3448 0.1965 0.0103 0.0181 0.002 0.128 0.027 1.517 0.014 0.120 8.099 0.07 41799. 0.0461
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5.76 0.3586 0.1601 0.0077 0.0173 0.002 0.123 0.020 1.456 0.014 0.091 6.343 0.07 41833. 0.0313
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5.98 0.3724 0.1160 0.0052 0.0166 0.002 0.118 0.014 1.392 0.013 0.060 4.428 0.07 41868. 0.0179
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6.20 0.3861 0.0627 0.0026 0.0158 0.002 0.112 0.007 1.323 0.013 0.030 2.306 0.07 41901. 0.0065
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6.42 0.3999 -0.0068 -0.0003 0.0148 0.002 0.105 -0.001 1.246 0.012 -0.003 -0.243 0.07 41912. 0.0000
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PROP RPM = 2000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0623 0.0219 0.020 0.623 0.656 14.731 0.070 2.918 20.200 0.13 82418. 0.5664
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0.46 0.0143 0.0398 0.0608 0.0219 0.020 0.621 0.639 14.699 0.070 2.844 19.730 0.13 82448. 0.5461
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0.92 0.0287 0.0777 0.0591 0.0218 0.020 0.619 0.622 14.655 0.070 2.767 19.255 0.13 82480. 0.5257
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1.38 0.0430 0.1137 0.0574 0.0217 0.020 0.617 0.604 14.600 0.070 2.688 18.777 0.13 82513. 0.5053
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1.84 0.0574 0.1477 0.0557 0.0216 0.019 0.614 0.586 14.532 0.069 2.607 18.295 0.13 82548. 0.4849
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2.30 0.0717 0.1798 0.0539 0.0215 0.019 0.611 0.567 14.450 0.069 2.524 17.808 0.13 82584. 0.4643
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2.76 0.0861 0.2098 0.0521 0.0214 0.019 0.607 0.548 14.354 0.069 2.438 17.317 0.13 82621. 0.4438
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3.22 0.1004 0.2377 0.0502 0.0212 0.019 0.602 0.528 14.243 0.068 2.349 16.820 0.13 82660. 0.4231
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3.68 0.1148 0.2635 0.0483 0.0210 0.019 0.597 0.508 14.115 0.067 2.259 16.316 0.13 82701. 0.4025
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4.14 0.1291 0.2872 0.0463 0.0208 0.019 0.590 0.487 13.971 0.067 2.166 15.806 0.13 82743. 0.3818
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4.61 0.1435 0.3086 0.0442 0.0206 0.019 0.584 0.465 13.808 0.066 2.070 15.287 0.13 82787. 0.3610
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5.07 0.1578 0.3278 0.0421 0.0203 0.018 0.576 0.443 13.626 0.065 1.972 14.759 0.13 82832. 0.3402
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5.53 0.1721 0.3445 0.0400 0.0200 0.018 0.567 0.421 13.424 0.064 1.872 14.220 0.13 82880. 0.3193
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5.99 0.1865 0.3587 0.0378 0.0197 0.018 0.558 0.398 13.201 0.063 1.769 13.668 0.13 82929. 0.2984
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6.45 0.2008 0.3703 0.0356 0.0193 0.017 0.548 0.374 12.956 0.062 1.665 13.101 0.13 82980. 0.2774
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6.91 0.2152 0.3791 0.0333 0.0189 0.017 0.536 0.350 12.687 0.061 1.557 12.517 0.13 83032. 0.2564
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7.37 0.2295 0.3848 0.0309 0.0185 0.017 0.524 0.326 12.395 0.059 1.448 11.913 0.13 83087. 0.2353
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7.83 0.2439 0.3873 0.0286 0.0180 0.016 0.510 0.301 12.078 0.058 1.337 11.285 0.13 83143. 0.2141
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8.29 0.2582 0.3862 0.0261 0.0175 0.016 0.496 0.275 11.736 0.056 1.223 10.628 0.13 83202. 0.1929
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8.75 0.2726 0.3812 0.0237 0.0169 0.015 0.480 0.249 11.367 0.054 1.108 9.937 0.13 83262. 0.1717
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9.21 0.2869 0.3717 0.0212 0.0163 0.015 0.464 0.223 10.970 0.052 0.990 9.205 0.14 83325. 0.1504
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9.67 0.3012 0.3572 0.0186 0.0157 0.014 0.446 0.196 10.546 0.050 0.871 8.425 0.14 83389. 0.1291
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10.13 0.3156 0.3369 0.0160 0.0150 0.014 0.427 0.169 10.093 0.048 0.751 7.585 0.14 83456. 0.1079
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10.59 0.3299 0.3098 0.0134 0.0143 0.013 0.406 0.141 9.611 0.046 0.629 6.672 0.14 83524. 0.0868
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11.05 0.3443 0.2747 0.0108 0.0135 0.012 0.385 0.114 9.101 0.043 0.506 5.669 0.14 83595. 0.0662
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11.51 0.3586 0.2296 0.0082 0.0127 0.011 0.362 0.086 8.560 0.041 0.382 4.550 0.14 83666. 0.0462
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11.97 0.3730 0.1723 0.0055 0.0119 0.011 0.338 0.058 7.989 0.038 0.257 3.282 0.14 83739. 0.0273
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12.43 0.3873 0.0983 0.0028 0.0110 0.010 0.312 0.029 7.383 0.035 0.131 1.804 0.14 83807. 0.0107
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12.89 0.4017 -0.0128 -0.0003 0.0099 0.009 0.281 -0.003 6.642 0.032 -0.015 -0.226 0.14 83769. 0.0000
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13.36 0.4160
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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 0.0626 0.0203 0.062 1.296 1.483 45.990 0.146 6.598 14.629 0.20 123624. 0.6167
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0.67 0.0139 0.0421 0.0611 0.0202 0.062 1.293 1.447 45.884 0.146 6.435 14.302 0.20 123669. 0.5955
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1.34 0.0279 0.0822 0.0595 0.0202 0.061 1.289 1.409 45.740 0.146 6.268 13.973 0.20 123715. 0.5742
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2.01 0.0418 0.1204 0.0579 0.0201 0.061 1.284 1.370 45.558 0.145 6.095 13.642 0.20 123764. 0.5528
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2.68 0.0557 0.1566 0.0562 0.0200 0.061 1.277 1.330 45.334 0.144 5.917 13.310 0.20 123814. 0.5314
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3.36 0.0697 0.1909 0.0545 0.0199 0.060 1.270 1.289 45.066 0.143 5.735 12.976 0.20 123866. 0.5101
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4.03 0.0836 0.2231 0.0527 0.0197 0.060 1.261 1.247 44.751 0.142 5.547 12.640 0.20 123921. 0.4887
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4.70 0.0976 0.2534 0.0508 0.0196 0.060 1.251 1.204 44.386 0.141 5.355 12.302 0.20 123977. 0.4672
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5.37 0.1115 0.2815 0.0490 0.0194 0.059 1.239 1.159 43.969 0.140 5.157 11.960 0.20 124036. 0.4458
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6.04 0.1254 0.3076 0.0470 0.0192 0.058 1.225 1.114 43.495 0.138 4.954 11.615 0.20 124097. 0.4244
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6.71 0.1394 0.3315 0.0451 0.0190 0.058 1.210 1.067 42.963 0.137 4.747 11.266 0.20 124160. 0.4029
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7.38 0.1533 0.3532 0.0431 0.0187 0.057 1.194 1.019 42.369 0.135 4.534 10.912 0.20 124226. 0.3814
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8.05 0.1672 0.3725 0.0410 0.0184 0.056 1.175 0.970 41.710 0.133 4.316 10.552 0.20 124294. 0.3598
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8.72 0.1812 0.3896 0.0389 0.0181 0.055 1.155 0.920 40.983 0.130 4.093 10.185 0.20 124365. 0.3382
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9.40 0.1951 0.4041 0.0367 0.0177 0.054 1.132 0.869 40.185 0.128 3.866 9.809 0.20 124438. 0.3166
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10.07 0.2091 0.4159 0.0345 0.0173 0.053 1.108 0.817 39.312 0.125 3.633 9.424 0.20 124514. 0.2948
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10.74 0.2230 0.4249 0.0322 0.0169 0.051 1.081 0.763 38.362 0.122 3.396 9.027 0.20 124592. 0.2730
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11.41 0.2369 0.4309 0.0299 0.0165 0.050 1.052 0.709 37.332 0.119 3.154 8.615 0.20 124673. 0.2511
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12.08 0.2509 0.4336 0.0276 0.0160 0.049 1.020 0.654 36.218 0.115 2.908 8.186 0.20 124757. 0.2291
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12.75 0.2648 0.4325 0.0252 0.0154 0.047 0.987 0.597 35.019 0.111 2.657 7.737 0.20 124844. 0.2070
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13.42 0.2787 0.4274 0.0228 0.0149 0.045 0.950 0.540 33.732 0.107 2.403 7.263 0.20 124933. 0.1848
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14.09 0.2927 0.4175 0.0204 0.0143 0.043 0.912 0.482 32.354 0.103 2.144 6.758 0.20 125026. 0.1624
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14.76 0.3066 0.4023 0.0179 0.0136 0.041 0.870 0.423 30.884 0.098 1.882 6.215 0.20 125121. 0.1400
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15.44 0.3205 0.3807 0.0154 0.0129 0.039 0.826 0.364 29.320 0.093 1.617 5.625 0.20 125219. 0.1174
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16.11 0.3345 0.3514 0.0128 0.0122 0.037 0.779 0.303 27.661 0.088 1.350 4.976 0.20 125320. 0.0949
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16.78 0.3484 0.3127 0.0103 0.0114 0.035 0.730 0.243 25.906 0.082 1.080 4.252 0.20 125423. 0.0725
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17.45 0.3624 0.2622 0.0077 0.0106 0.032 0.678 0.182 24.055 0.077 0.809 3.427 0.20 125528. 0.0506
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18.12 0.3763 0.1960 0.0051 0.0097 0.030 0.623 0.120 22.102 0.070 0.535 2.468 0.20 125633. 0.0296
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18.79 0.3902 0.1076 0.0024 0.0088 0.027 0.564 0.058 20.023 0.064 0.257 1.306 0.20 125729. 0.0109
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19.46 0.4042
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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 0.0630 0.0194 0.140 2.204 2.652 104.291 0.249 11.797 11.535 0.27 164828. 0.6503
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0.91 0.0142 0.0450 0.0614 0.0194 0.139 2.198 2.586 104.024 0.248 11.502 11.275 0.27 164889. 0.6276
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1.82 0.0284 0.0880 0.0598 0.0193 0.139 2.191 2.517 103.666 0.247 11.197 11.014 0.27 164952. 0.6049
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2.73 0.0426 0.1288 0.0581 0.0192 0.138 2.181 2.447 103.209 0.246 10.882 10.752 0.27 165018. 0.5822
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3.64 0.0568 0.1676 0.0564 0.0191 0.138 2.169 2.374 102.647 0.245 10.559 10.489 0.27 165087. 0.5595
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4.56 0.0709 0.2042 0.0546 0.0190 0.137 2.155 2.299 101.974 0.243 10.226 10.226 0.27 165158. 0.5367
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5.47 0.0851 0.2387 0.0528 0.0188 0.136 2.138 2.222 101.183 0.242 9.884 9.961 0.27 165233. 0.5140
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6.38 0.0993 0.2711 0.0509 0.0187 0.134 2.119 2.143 100.266 0.239 9.533 9.695 0.27 165310. 0.4914
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7.29 0.1135 0.3012 0.0490 0.0185 0.133 2.096 2.062 99.215 0.237 9.173 9.428 0.27 165390. 0.4687
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8.20 0.1277 0.3292 0.0470 0.0182 0.131 2.071 1.979 98.023 0.234 8.803 9.157 0.27 165474. 0.4460
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9.11 0.1419 0.3548 0.0450 0.0180 0.130 2.043 1.894 96.683 0.231 8.424 8.885 0.27 165560. 0.4232
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10.02 0.1561 0.3782 0.0429 0.0177 0.128 2.011 1.806 95.187 0.227 8.035 8.608 0.27 165650. 0.4005
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10.93 0.1703 0.3991 0.0408 0.0174 0.125 1.976 1.717 93.525 0.223 7.638 8.327 0.27 165744. 0.3777
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11.84 0.1845 0.4175 0.0386 0.0171 0.123 1.938 1.626 91.692 0.219 7.231 8.041 0.27 165841. 0.3549
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12.75 0.1986 0.4333 0.0364 0.0167 0.120 1.895 1.532 89.678 0.214 6.815 7.749 0.27 165941. 0.3320
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13.67 0.2128 0.4463 0.0341 0.0163 0.117 1.848 1.437 87.476 0.209 6.390 7.449 0.27 166045. 0.3091
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14.58 0.2270 0.4562 0.0318 0.0158 0.114 1.798 1.339 85.079 0.203 5.957 7.140 0.27 166152. 0.2860
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15.49 0.2412 0.4630 0.0295 0.0153 0.111 1.743 1.240 82.478 0.197 5.515 6.819 0.27 166264. 0.2628
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16.40 0.2554 0.4661 0.0271 0.0148 0.107 1.683 1.139 79.667 0.190 5.065 6.483 0.27 166379. 0.2395
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17.31 0.2696 0.4652 0.0246 0.0143 0.103 1.619 1.036 76.639 0.183 4.608 6.130 0.27 166498. 0.2160
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18.22 0.2838 0.4598 0.0221 0.0137 0.098 1.551 0.931 73.389 0.175 4.143 5.756 0.27 166621. 0.1923
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19.13 0.2980 0.4491 0.0196 0.0130 0.094 1.477 0.825 69.910 0.167 3.671 5.355 0.27 166748. 0.1684
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20.04 0.3122 0.4322 0.0171 0.0123 0.089 1.399 0.718 66.199 0.158 3.193 4.919 0.27 166879. 0.1443
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20.95 0.3264 0.4078 0.0145 0.0116 0.083 1.315 0.609 62.253 0.149 2.710 4.439 0.27 167014. 0.1200
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21.86 0.3405 0.3741 0.0119 0.0108 0.078 1.227 0.500 58.069 0.139 2.223 3.903 0.27 167152. 0.0955
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22.78 0.3547 0.3286 0.0092 0.0100 0.072 1.134 0.389 53.644 0.128 1.731 3.291 0.27 167293. 0.0711
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23.69 0.3689 0.2673 0.0066 0.0091 0.066 1.035 0.278 48.975 0.117 1.236 2.574 0.27 167436. 0.0470
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24.60 0.3831 0.1840 0.0039 0.0082 0.059 0.931 0.166 44.036 0.105 0.737 1.706 0.27 167576. 0.0240
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25.51 0.3973 0.0638 0.0012 0.0072 0.052 0.816 0.049 38.635 0.092 0.216 0.571 0.27 167673. 0.0044
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26.42 0.4115
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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 0.0635 0.0189 0.266 3.353 4.174 198.344 0.379 18.565 9.545 0.34 206028. 0.6750
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1.16 0.0145 0.0475 0.0618 0.0188 0.265 3.343 4.067 197.784 0.378 18.090 9.327 0.34 206106. 0.6511
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2.33 0.0290 0.0928 0.0602 0.0188 0.264 3.331 3.957 197.033 0.376 17.600 9.108 0.34 206187. 0.6272
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3.49 0.0435 0.1359 0.0584 0.0187 0.263 3.315 3.843 196.078 0.374 17.094 8.890 0.34 206272. 0.6033
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4.65 0.0579 0.1768 0.0567 0.0186 0.261 3.295 3.726 194.906 0.372 16.574 8.671 0.34 206360. 0.5794
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5.81 0.0724 0.2154 0.0548 0.0184 0.259 3.271 3.606 193.501 0.370 16.038 8.452 0.34 206452. 0.5556
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|
6.98 0.0869 0.2517 0.0529 0.0183 0.257 3.243 3.482 191.850 0.366 15.488 8.232 0.34 206548. 0.5318
|
|
8.14 0.1014 0.2858 0.0510 0.0181 0.255 3.211 3.355 189.935 0.363 14.922 8.011 0.34 206647. 0.5080
|
|
9.30 0.1159 0.3176 0.0490 0.0179 0.252 3.174 3.224 187.743 0.359 14.341 7.789 0.34 206751. 0.4842
|
|
10.46 0.1304 0.3470 0.0470 0.0177 0.248 3.132 3.090 185.257 0.354 13.745 7.566 0.34 206858. 0.4604
|
|
11.63 0.1449 0.3741 0.0449 0.0174 0.245 3.084 2.953 182.459 0.348 13.134 7.340 0.34 206970. 0.4366
|
|
12.79 0.1593 0.3987 0.0428 0.0171 0.240 3.032 2.812 179.335 0.343 12.507 7.112 0.34 207086. 0.4128
|
|
13.95 0.1738 0.4208 0.0406 0.0168 0.236 2.973 2.668 175.867 0.336 11.866 6.880 0.34 207207. 0.3890
|
|
15.11 0.1883 0.4402 0.0383 0.0164 0.231 2.908 2.520 172.039 0.329 11.209 6.644 0.34 207332. 0.3651
|
|
16.28 0.2028 0.4569 0.0360 0.0160 0.225 2.837 2.369 167.834 0.321 10.538 6.403 0.34 207461. 0.3412
|
|
17.44 0.2173 0.4705 0.0337 0.0156 0.219 2.759 2.215 163.235 0.312 9.853 6.155 0.34 207595. 0.3171
|
|
18.60 0.2318 0.4810 0.0313 0.0151 0.212 2.675 2.058 158.228 0.302 9.153 5.899 0.34 207735. 0.2929
|
|
19.76 0.2463 0.4880 0.0289 0.0146 0.205 2.583 1.898 152.796 0.292 8.440 5.633 0.34 207879. 0.2686
|
|
20.93 0.2607 0.4912 0.0264 0.0140 0.197 2.484 1.734 146.926 0.281 7.714 5.354 0.34 208028. 0.2441
|
|
22.09 0.2752 0.4899 0.0238 0.0134 0.189 2.377 1.568 140.603 0.269 6.976 5.059 0.34 208182. 0.2193
|
|
23.25 0.2897 0.4836 0.0213 0.0127 0.179 2.262 1.400 133.816 0.256 6.226 4.744 0.34 208341. 0.1943
|
|
24.41 0.3042 0.4713 0.0187 0.0121 0.170 2.139 1.229 126.555 0.242 5.465 4.404 0.34 208505. 0.1690
|
|
25.58 0.3187 0.4519 0.0161 0.0113 0.159 2.008 1.056 118.812 0.227 4.695 4.030 0.34 208674. 0.1433
|
|
26.74 0.3332 0.4234 0.0134 0.0105 0.148 1.869 0.881 110.580 0.211 3.917 3.612 0.34 208849. 0.1174
|
|
27.90 0.3476 0.3836 0.0107 0.0097 0.137 1.722 0.704 101.856 0.195 3.132 3.136 0.34 209027. 0.0911
|
|
29.06 0.3621 0.3285 0.0080 0.0088 0.124 1.566 0.526 92.634 0.177 2.342 2.578 0.34 209209. 0.0647
|
|
30.23 0.3766 0.2519 0.0053 0.0079 0.111 1.401 0.347 82.892 0.158 1.545 1.901 0.34 209391. 0.0388
|
|
31.39 0.3911 0.1421 0.0025 0.0069 0.097 1.225 0.165 72.494 0.138 0.734 1.033 0.34 209556. 0.0145
|
|
32.55 0.4056
|
|
33.71 0.4201
|
|
|
|
|
|
|
|
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 0.0640 0.0186 0.453 4.755 6.063 337.546 0.537 26.967 8.147 0.40 247223. 0.6944
|
|
1.39 0.0144 0.0485 0.0624 0.0186 0.451 4.741 5.908 336.526 0.536 26.280 7.963 0.40 247317. 0.6701
|
|
2.78 0.0288 0.0947 0.0607 0.0185 0.449 4.722 5.749 335.171 0.533 25.571 7.780 0.40 247414. 0.6457
|
|
4.16 0.0432 0.1387 0.0590 0.0184 0.447 4.698 5.585 333.462 0.531 24.841 7.596 0.40 247516. 0.6214
|
|
5.55 0.0577 0.1804 0.0572 0.0183 0.444 4.668 5.416 331.374 0.527 24.090 7.413 0.40 247622. 0.5972
|
|
6.94 0.0721 0.2200 0.0554 0.0181 0.441 4.633 5.242 328.882 0.523 23.317 7.229 0.40 247732. 0.5730
|
|
8.33 0.0865 0.2573 0.0535 0.0180 0.437 4.592 5.063 325.962 0.519 22.522 7.046 0.40 247847. 0.5488
|
|
9.72 0.1009 0.2923 0.0515 0.0178 0.433 4.544 4.880 322.585 0.513 21.706 6.861 0.40 247966. 0.5247
|
|
11.10 0.1153 0.3250 0.0495 0.0176 0.427 4.490 4.691 318.727 0.507 20.868 6.676 0.40 248090. 0.5006
|
|
12.49 0.1297 0.3554 0.0475 0.0173 0.422 4.428 4.498 314.359 0.500 20.008 6.490 0.40 248218. 0.4765
|
|
13.88 0.1441 0.3835 0.0454 0.0171 0.415 4.359 4.300 309.453 0.493 19.126 6.302 0.40 248352. 0.4524
|
|
15.27 0.1585 0.4092 0.0433 0.0168 0.408 4.282 4.097 303.981 0.484 18.223 6.113 0.40 248491. 0.4283
|
|
16.66 0.1730 0.4324 0.0411 0.0164 0.400 4.197 3.889 297.915 0.474 17.298 5.921 0.40 248634. 0.4042
|
|
18.05 0.1874 0.4529 0.0388 0.0161 0.391 4.103 3.676 291.225 0.463 16.352 5.725 0.40 248784. 0.3800
|
|
19.43 0.2018 0.4708 0.0365 0.0157 0.381 3.999 3.459 283.884 0.452 15.384 5.526 0.40 248938. 0.3558
|
|
20.82 0.2162 0.4858 0.0342 0.0152 0.370 3.886 3.237 275.863 0.439 14.397 5.322 0.40 249099. 0.3314
|
|
22.21 0.2306 0.4976 0.0318 0.0147 0.358 3.763 3.010 267.137 0.425 13.389 5.111 0.40 249265. 0.3069
|
|
23.60 0.2450 0.5061 0.0293 0.0142 0.346 3.630 2.779 257.677 0.410 12.361 4.892 0.40 249437. 0.2823
|
|
24.99 0.2594 0.5107 0.0269 0.0136 0.332 3.486 2.544 247.460 0.394 11.315 4.663 0.40 249614. 0.2574
|
|
26.37 0.2738 0.5111 0.0243 0.0130 0.317 3.331 2.305 236.462 0.376 10.251 4.421 0.40 249798. 0.2323
|
|
27.76 0.2883 0.5066 0.0218 0.0124 0.301 3.165 2.062 224.663 0.358 9.171 4.163 0.41 249988. 0.2069
|
|
29.15 0.3027 0.4962 0.0192 0.0117 0.284 2.987 1.815 212.044 0.337 8.075 3.883 0.41 250183. 0.1811
|
|
30.54 0.3171 0.4788 0.0165 0.0109 0.266 2.798 1.566 198.592 0.316 6.965 3.577 0.41 250385. 0.1549
|
|
31.93 0.3315 0.4526 0.0139 0.0102 0.247 2.596 1.314 184.297 0.293 5.844 3.234 0.41 250593. 0.1283
|
|
33.31 0.3459 0.4149 0.0112 0.0093 0.227 2.383 1.060 169.153 0.269 4.713 2.841 0.41 250806. 0.1012
|
|
34.70 0.3603 0.3619 0.0085 0.0084 0.205 2.157 0.803 153.150 0.244 3.573 2.379 0.41 251023. 0.0738
|
|
36.09 0.3747 0.2872 0.0058 0.0075 0.183 1.919 0.545 136.257 0.217 2.425 1.815 0.41 251241. 0.0464
|
|
37.48 0.3891 0.1785 0.0030 0.0065 0.159 1.667 0.283 118.300 0.188 1.260 1.086 0.41 251444. 0.0200
|
|
38.87 0.4036
|
|
40.25 0.4180
|
|
|
|
|
|
|
|
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 0.0647 0.0185 0.714 6.428 8.339 532.352 0.726 37.091 7.105 0.47 288411. 0.7102
|
|
1.59 0.0142 0.0484 0.0631 0.0184 0.712 6.407 8.130 530.645 0.724 36.163 6.949 0.47 288519. 0.6859
|
|
3.18 0.0283 0.0947 0.0614 0.0183 0.709 6.380 7.915 528.418 0.721 35.206 6.794 0.47 288632. 0.6616
|
|
4.77 0.0425 0.1388 0.0597 0.0183 0.705 6.347 7.694 525.638 0.717 34.221 6.639 0.47 288749. 0.6374
|
|
6.36 0.0566 0.1808 0.0579 0.0181 0.700 6.306 7.466 522.269 0.712 33.207 6.484 0.47 288871. 0.6133
|
|
7.95 0.0708 0.2206 0.0561 0.0180 0.695 6.258 7.232 518.275 0.707 32.166 6.329 0.47 288997. 0.5891
|
|
9.54 0.0849 0.2582 0.0542 0.0178 0.689 6.202 6.991 513.616 0.701 31.096 6.174 0.47 289129. 0.5651
|
|
11.13 0.0991 0.2937 0.0523 0.0176 0.682 6.137 6.744 508.253 0.693 29.997 6.018 0.47 289265. 0.5410
|
|
12.72 0.1132 0.3270 0.0504 0.0174 0.673 6.063 6.491 502.145 0.685 28.870 5.863 0.47 289407. 0.5170
|
|
14.31 0.1274 0.3580 0.0483 0.0172 0.664 5.980 6.231 495.251 0.676 27.714 5.706 0.47 289554. 0.4931
|
|
15.90 0.1415 0.3868 0.0463 0.0169 0.654 5.887 5.964 487.529 0.665 26.529 5.549 0.47 289707. 0.4691
|
|
17.49 0.1557 0.4133 0.0442 0.0166 0.642 5.783 5.691 478.936 0.653 25.315 5.390 0.47 289866. 0.4451
|
|
19.08 0.1698 0.4375 0.0420 0.0163 0.630 5.668 5.412 469.429 0.640 24.073 5.229 0.47 290030. 0.4211
|
|
20.67 0.1840 0.4592 0.0398 0.0159 0.615 5.542 5.127 458.965 0.626 22.803 5.066 0.47 290200. 0.3971
|
|
22.26 0.1981 0.4783 0.0375 0.0155 0.600 5.403 4.835 447.501 0.610 21.506 4.900 0.47 290376. 0.3730
|
|
23.85 0.2123 0.4947 0.0352 0.0151 0.583 5.252 4.537 434.996 0.593 20.180 4.731 0.47 290559. 0.3488
|
|
25.44 0.2265 0.5082 0.0328 0.0146 0.565 5.088 4.233 421.406 0.575 18.829 4.556 0.47 290748. 0.3245
|
|
27.03 0.2406 0.5186 0.0304 0.0141 0.545 4.911 3.923 406.693 0.555 17.451 4.375 0.47 290943. 0.3000
|
|
28.62 0.2548 0.5254 0.0280 0.0136 0.524 4.719 3.608 390.819 0.533 16.048 4.187 0.47 291145. 0.2753
|
|
30.21 0.2689 0.5284 0.0255 0.0130 0.501 4.513 3.287 373.747 0.510 14.621 3.989 0.47 291354. 0.2504
|
|
31.81 0.2831 0.5269 0.0230 0.0123 0.477 4.292 2.961 355.445 0.485 13.172 3.779 0.47 291569. 0.2251
|
|
33.40 0.2972 0.5201 0.0204 0.0117 0.450 4.056 2.631 335.885 0.458 11.701 3.552 0.47 291791. 0.1995
|
|
34.99 0.3114 0.5070 0.0178 0.0109 0.422 3.804 2.296 315.043 0.430 10.212 3.305 0.47 292020. 0.1734
|
|
36.58 0.3255 0.4860 0.0152 0.0102 0.393 3.537 1.957 292.902 0.400 8.706 3.031 0.47 292255. 0.1468
|
|
38.17 0.3397 0.4550 0.0125 0.0094 0.361 3.254 1.616 269.451 0.368 7.186 2.720 0.47 292497. 0.1197
|
|
39.76 0.3538 0.4107 0.0099 0.0085 0.328 2.954 1.271 244.681 0.334 5.654 2.356 0.47 292744. 0.0920
|
|
41.35 0.3680 0.3477 0.0072 0.0076 0.293 2.639 0.924 218.568 0.298 4.112 1.918 0.47 292994. 0.0639
|
|
42.94 0.3821 0.2568 0.0045 0.0066 0.256 2.306 0.575 191.002 0.261 2.556 1.365 0.47 293240. 0.0358
|
|
44.53 0.3963 0.1171 0.0017 0.0056 0.216 1.946 0.213 161.170 0.220 0.948 0.600 0.47 293429. 0.0096
|
|
46.12 0.4104
|
|
|
|
|
|
|
|
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 0.0655 0.0185 1.066 8.397 11.028 794.740 0.949 49.053 6.294 0.54 329591. 0.7235
|
|
1.84 0.0143 0.0496 0.0638 0.0184 1.062 8.367 10.749 791.933 0.945 47.810 6.156 0.54 329717. 0.6987
|
|
3.68 0.0287 0.0971 0.0621 0.0183 1.057 8.329 10.460 788.309 0.941 46.527 6.018 0.54 329849. 0.6738
|
|
5.52 0.0430 0.1423 0.0604 0.0182 1.051 8.281 10.163 783.820 0.936 45.206 5.881 0.54 329985. 0.6490
|
|
7.36 0.0573 0.1853 0.0585 0.0181 1.044 8.224 9.858 778.412 0.929 43.848 5.744 0.54 330128. 0.6243
|
|
9.20 0.0716 0.2261 0.0567 0.0180 1.035 8.157 9.544 772.025 0.922 42.451 5.607 0.54 330275. 0.5996
|
|
11.04 0.0860 0.2647 0.0548 0.0178 1.025 8.078 9.221 764.600 0.913 41.016 5.470 0.54 330429. 0.5750
|
|
12.88 0.1003 0.3011 0.0528 0.0176 1.014 7.988 8.890 756.074 0.902 39.543 5.333 0.54 330588. 0.5505
|
|
14.72 0.1146 0.3352 0.0508 0.0174 1.001 7.886 8.550 746.385 0.891 38.031 5.196 0.54 330754. 0.5259
|
|
16.56 0.1289 0.3671 0.0487 0.0171 0.986 7.770 8.201 735.469 0.878 36.480 5.058 0.54 330926. 0.5014
|
|
18.40 0.1433 0.3967 0.0466 0.0168 0.970 7.641 7.844 723.260 0.863 34.891 4.919 0.54 331104. 0.4769
|
|
20.24 0.1576 0.4240 0.0444 0.0165 0.952 7.498 7.478 709.692 0.847 33.263 4.779 0.54 331289. 0.4524
|
|
22.08 0.1719 0.4489 0.0422 0.0162 0.932 7.340 7.104 694.698 0.829 31.597 4.638 0.54 331481. 0.4279
|
|
23.92 0.1862 0.4712 0.0399 0.0158 0.909 7.166 6.720 678.211 0.810 29.893 4.494 0.54 331680. 0.4033
|
|
25.76 0.2006 0.4910 0.0376 0.0154 0.885 6.975 6.329 660.166 0.788 28.151 4.348 0.54 331886. 0.3787
|
|
27.60 0.2149 0.5080 0.0352 0.0149 0.859 6.767 5.929 640.495 0.765 26.373 4.199 0.54 332099. 0.3539
|
|
29.43 0.2292 0.5220 0.0328 0.0144 0.830 6.541 5.522 619.137 0.739 24.560 4.045 0.54 332320. 0.3290
|
|
31.27 0.2435 0.5327 0.0303 0.0139 0.799 6.297 5.106 596.029 0.711 22.711 3.886 0.54 332548. 0.3039
|
|
33.11 0.2579 0.5399 0.0278 0.0133 0.766 6.034 4.683 571.112 0.682 20.829 3.719 0.54 332784. 0.2786
|
|
34.95 0.2722 0.5430 0.0253 0.0127 0.730 5.751 4.253 544.332 0.650 18.915 3.543 0.54 333028. 0.2530
|
|
36.79 0.2865 0.5414 0.0227 0.0120 0.691 5.448 3.816 515.641 0.616 16.972 3.356 0.54 333279. 0.2269
|
|
38.63 0.3009 0.5342 0.0200 0.0113 0.650 5.124 3.372 484.995 0.579 15.000 3.154 0.54 333538. 0.2005
|
|
40.47 0.3152 0.5201 0.0174 0.0105 0.607 4.779 2.924 452.362 0.540 13.004 2.931 0.54 333806. 0.1735
|
|
42.31 0.3295 0.4975 0.0147 0.0097 0.560 4.413 2.470 417.718 0.499 10.986 2.682 0.54 334081. 0.1459
|
|
44.15 0.3438 0.4636 0.0120 0.0089 0.511 4.026 2.012 381.047 0.455 8.950 2.395 0.54 334363. 0.1176
|
|
45.99 0.3582 0.4143 0.0092 0.0080 0.459 3.617 1.551 342.335 0.409 6.898 2.055 0.54 334650. 0.0886
|
|
47.83 0.3725 0.3427 0.0065 0.0070 0.404 3.186 1.086 301.527 0.360 4.833 1.634 0.54 334940. 0.0590
|
|
49.67 0.3868 0.2357 0.0037 0.0060 0.346 2.729 0.617 258.327 0.308 2.742 1.083 0.54 335218. 0.0294
|
|
51.51 0.4011 0.0519 0.0006 0.0049 0.280 2.208 0.106 208.980 0.249 0.471 0.230 0.54 335275. 0.0026
|
|
53.35 0.4155
|
|
|
|
|
|
|
|
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 0.0665 0.0186 1.527 10.696 14.166 1138.927 1.208 63.009 5.641 0.61 370760. 0.7350
|
|
2.07 0.0143 0.0501 0.0648 0.0185 1.521 10.655 13.806 1134.524 1.204 61.408 5.519 0.61 370904. 0.7099
|
|
4.14 0.0287 0.0981 0.0630 0.0184 1.514 10.602 13.435 1128.930 1.198 59.757 5.398 0.61 371053. 0.6849
|
|
6.22 0.0430 0.1438 0.0613 0.0183 1.505 10.538 13.052 1122.071 1.191 58.057 5.276 0.61 371209. 0.6599
|
|
8.29 0.0574 0.1873 0.0594 0.0182 1.494 10.461 12.660 1113.870 1.182 56.310 5.155 0.61 371370. 0.6349
|
|
10.36 0.0717 0.2286 0.0575 0.0180 1.481 10.370 12.256 1104.242 1.172 54.513 5.034 0.61 371538. 0.6101
|
|
12.43 0.0861 0.2678 0.0556 0.0179 1.466 10.266 11.841 1093.102 1.160 52.667 4.913 0.61 371713. 0.5852
|
|
14.50 0.1004 0.3047 0.0536 0.0176 1.449 10.146 11.415 1080.364 1.146 50.773 4.792 0.61 371894. 0.5605
|
|
16.57 0.1147 0.3394 0.0515 0.0174 1.429 10.011 10.978 1065.935 1.131 48.829 4.671 0.61 372082. 0.5357
|
|
18.65 0.1291 0.3719 0.0494 0.0171 1.408 9.858 10.529 1049.725 1.114 46.835 4.550 0.61 372277. 0.5110
|
|
20.72 0.1434 0.4021 0.0473 0.0169 1.383 9.689 10.070 1031.638 1.095 44.792 4.427 0.61 372479. 0.4864
|
|
22.79 0.1578 0.4301 0.0451 0.0165 1.357 9.500 9.600 1011.581 1.073 42.700 4.304 0.61 372689. 0.4617
|
|
24.86 0.1721 0.4556 0.0428 0.0162 1.327 9.292 9.119 989.459 1.050 40.560 4.180 0.61 372906. 0.4369
|
|
26.93 0.1864 0.4787 0.0405 0.0158 1.294 9.064 8.627 965.175 1.024 38.371 4.054 0.61 373131. 0.4122
|
|
29.01 0.2008 0.4992 0.0381 0.0153 1.259 8.815 8.124 938.637 0.996 36.134 3.926 0.61 373365. 0.3873
|
|
31.08 0.2151 0.5169 0.0357 0.0149 1.220 8.544 7.610 909.750 0.965 33.850 3.794 0.61 373606. 0.3623
|
|
33.15 0.2295 0.5318 0.0333 0.0144 1.178 8.250 7.087 878.423 0.932 31.521 3.659 0.61 373856. 0.3372
|
|
35.22 0.2438 0.5434 0.0308 0.0138 1.133 7.932 6.553 844.568 0.896 29.147 3.519 0.61 374114. 0.3119
|
|
37.29 0.2582 0.5515 0.0282 0.0132 1.084 7.589 6.010 808.101 0.857 26.731 3.373 0.61 374380. 0.2862
|
|
39.37 0.2725 0.5555 0.0256 0.0126 1.031 7.221 5.457 768.944 0.816 24.274 3.219 0.61 374656. 0.2603
|
|
41.44 0.2868 0.5549 0.0230 0.0119 0.975 6.828 4.896 727.029 0.771 21.778 3.055 0.61 374940. 0.2340
|
|
43.51 0.3012 0.5487 0.0203 0.0111 0.915 6.408 4.327 682.295 0.724 19.247 2.877 0.61 375233. 0.2071
|
|
45.58 0.3155 0.5356 0.0176 0.0104 0.851 5.961 3.751 634.695 0.673 16.684 2.681 0.61 375535. 0.1797
|
|
47.65 0.3299 0.5139 0.0149 0.0095 0.783 5.486 3.168 584.196 0.620 14.093 2.460 0.61 375845. 0.1516
|
|
49.72 0.3442 0.4808 0.0121 0.0087 0.712 4.985 2.581 530.778 0.563 11.479 2.205 0.61 376163. 0.1226
|
|
51.80 0.3585 0.4317 0.0093 0.0078 0.636 4.455 1.989 474.421 0.503 8.846 1.901 0.61 376488. 0.0928
|
|
53.87 0.3729 0.3594 0.0065 0.0068 0.557 3.898 1.393 415.046 0.440 6.194 1.522 0.61 376815. 0.0622
|
|
55.94 0.3872 0.2493 0.0037 0.0058 0.472 3.308 0.789 352.219 0.374 3.511 1.016 0.61 377127. 0.0313
|
|
58.01 0.4016 0.0537 0.0006 0.0046 0.376 2.631 0.130 280.119 0.297 0.580 0.211 0.61 377170. 0.0026
|
|
60.08 0.4159
|
|
|
|
|
|
|
|
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 0.0677 0.0188 2.122 13.375 17.798 1582.468 1.511 79.167 5.101 0.67 411915. 0.7450
|
|
2.29 0.0143 0.0501 0.0659 0.0188 2.113 13.319 17.348 1575.792 1.505 77.166 4.994 0.67 412076. 0.7200
|
|
4.58 0.0285 0.0980 0.0642 0.0187 2.102 13.248 16.884 1567.445 1.497 75.102 4.886 0.67 412243. 0.6950
|
|
6.86 0.0428 0.1438 0.0624 0.0185 2.088 13.163 16.407 1557.348 1.487 72.978 4.778 0.67 412416. 0.6700
|
|
9.15 0.0570 0.1874 0.0605 0.0184 2.072 13.062 15.916 1545.388 1.476 70.796 4.671 0.67 412597. 0.6451
|
|
11.44 0.0713 0.2289 0.0586 0.0182 2.054 12.944 15.412 1531.450 1.462 68.553 4.565 0.67 412784. 0.6203
|
|
13.73 0.0855 0.2683 0.0566 0.0180 2.032 12.809 14.894 1515.425 1.447 66.249 4.458 0.67 412978. 0.5956
|
|
16.02 0.0998 0.3055 0.0546 0.0178 2.008 12.655 14.363 1497.190 1.430 63.886 4.351 0.67 413180. 0.5708
|
|
18.30 0.1140 0.3406 0.0525 0.0176 1.980 12.481 13.818 1476.625 1.410 61.462 4.244 0.67 413389. 0.5462
|
|
20.59 0.1283 0.3735 0.0504 0.0173 1.949 12.286 13.259 1453.607 1.388 58.977 4.137 0.67 413606. 0.5215
|
|
22.88 0.1425 0.4042 0.0482 0.0170 1.915 12.070 12.687 1428.008 1.364 56.431 4.030 0.67 413830. 0.4969
|
|
25.17 0.1568 0.4327 0.0460 0.0167 1.877 11.831 12.101 1399.703 1.337 53.825 3.921 0.67 414063. 0.4722
|
|
27.46 0.1711 0.4588 0.0437 0.0163 1.835 11.567 11.502 1368.561 1.307 51.159 3.812 0.67 414304. 0.4475
|
|
29.74 0.1853 0.4826 0.0414 0.0159 1.790 11.279 10.889 1334.457 1.274 48.434 3.701 0.67 414554. 0.4228
|
|
32.03 0.1996 0.5039 0.0390 0.0154 1.740 10.965 10.263 1297.263 1.239 45.650 3.588 0.67 414812. 0.3979
|
|
34.32 0.2138 0.5226 0.0366 0.0150 1.685 10.623 9.624 1256.852 1.200 42.808 3.473 0.67 415079. 0.3730
|
|
36.61 0.2281 0.5384 0.0341 0.0144 1.627 10.253 8.972 1213.100 1.158 39.909 3.355 0.67 415355. 0.3479
|
|
38.90 0.2423 0.5512 0.0316 0.0139 1.563 9.854 8.308 1165.892 1.113 36.956 3.232 0.67 415641. 0.3225
|
|
41.19 0.2566 0.5605 0.0290 0.0133 1.495 9.425 7.633 1115.112 1.065 33.950 3.105 0.67 415935. 0.2969
|
|
43.47 0.2708 0.5660 0.0264 0.0126 1.422 8.965 6.945 1060.658 1.013 30.893 2.970 0.67 416240. 0.2710
|
|
45.76 0.2851 0.5671 0.0237 0.0119 1.344 8.473 6.247 1002.430 0.957 27.788 2.827 0.68 416553. 0.2446
|
|
48.05 0.2993 0.5628 0.0211 0.0112 1.261 7.948 5.539 940.351 0.898 24.639 2.672 0.68 416877. 0.2177
|
|
50.34 0.3136 0.5521 0.0183 0.0104 1.173 7.390 4.823 874.354 0.835 21.451 2.502 0.68 417210. 0.1902
|
|
52.63 0.3279 0.5331 0.0156 0.0096 1.079 6.799 4.098 804.392 0.768 18.227 2.311 0.68 417552. 0.1619
|
|
54.91 0.3421 0.5032 0.0128 0.0087 0.980 6.174 3.366 730.438 0.698 14.973 2.090 0.68 417903. 0.1328
|
|
57.20 0.3564 0.4583 0.0100 0.0078 0.875 5.515 2.629 652.467 0.623 11.695 1.828 0.68 418262. 0.1026
|
|
59.49 0.3706 0.3914 0.0072 0.0068 0.765 4.821 1.887 570.408 0.545 8.394 1.501 0.68 418624. 0.0714
|
|
61.78 0.3849 0.2889 0.0043 0.0058 0.649 4.089 1.138 483.834 0.462 5.061 1.067 0.68 418976. 0.0394
|
|
64.07 0.3991 0.1156 0.0013 0.0046 0.522 3.288 0.353 388.967 0.371 1.570 0.412 0.68 419197. 0.0085
|
|
66.35 0.4134
|
|
|
|
|
|
|
|
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 0.0691 0.0192 2.881 16.510 21.992 2148.693 1.865 97.819 4.642 0.74 453052. 0.7536
|
|
2.49 0.0141 0.0496 0.0674 0.0191 2.868 16.433 21.441 2138.684 1.857 95.370 4.547 0.74 453229. 0.7289
|
|
4.98 0.0282 0.0972 0.0656 0.0190 2.852 16.339 20.873 2126.447 1.846 92.844 4.452 0.74 453413. 0.7041
|
|
7.47 0.0423 0.1427 0.0637 0.0189 2.832 16.227 20.290 2111.867 1.833 90.248 4.358 0.74 453604. 0.6795
|
|
9.96 0.0564 0.1861 0.0619 0.0187 2.809 16.096 19.690 2094.809 1.819 87.581 4.263 0.74 453803. 0.6549
|
|
12.45 0.0705 0.2275 0.0599 0.0186 2.783 15.945 19.074 2075.121 1.801 84.842 4.169 0.74 454009. 0.6303
|
|
14.94 0.0846 0.2668 0.0579 0.0184 2.753 15.772 18.442 2052.661 1.782 82.031 4.075 0.74 454222. 0.6058
|
|
17.43 0.0987 0.3041 0.0559 0.0181 2.719 15.577 17.794 2027.275 1.760 79.147 3.981 0.74 454443. 0.5813
|
|
19.91 0.1128 0.3394 0.0538 0.0179 2.680 15.359 17.129 1998.803 1.735 76.192 3.887 0.74 454673. 0.5569
|
|
22.40 0.1269 0.3725 0.0517 0.0176 2.638 15.115 16.449 1967.089 1.708 73.163 3.793 0.74 454910. 0.5325
|
|
24.89 0.1410 0.4036 0.0495 0.0173 2.591 14.845 15.751 1931.969 1.677 70.062 3.698 0.74 455156. 0.5081
|
|
27.38 0.1551 0.4325 0.0472 0.0169 2.539 14.548 15.038 1893.282 1.644 66.889 3.603 0.74 455411. 0.4836
|
|
29.87 0.1692 0.4592 0.0450 0.0166 2.482 14.222 14.309 1850.861 1.607 63.645 3.506 0.74 455674. 0.4591
|
|
32.36 0.1833 0.4837 0.0426 0.0161 2.420 13.866 13.563 1804.542 1.567 60.329 3.409 0.74 455946. 0.4346
|
|
34.85 0.1974 0.5057 0.0402 0.0157 2.352 13.479 12.802 1754.159 1.523 56.942 3.310 0.74 456228. 0.4100
|
|
37.34 0.2115 0.5253 0.0378 0.0152 2.279 13.059 12.025 1699.551 1.475 53.487 3.209 0.74 456519. 0.3852
|
|
39.83 0.2256 0.5423 0.0353 0.0147 2.200 12.606 11.233 1640.567 1.424 49.963 3.106 0.74 456820. 0.3603
|
|
42.32 0.2397 0.5563 0.0328 0.0141 2.115 12.118 10.426 1577.051 1.369 46.373 2.998 0.74 457130. 0.3352
|
|
44.81 0.2538 0.5671 0.0302 0.0135 2.023 11.594 9.604 1508.875 1.310 42.720 2.887 0.74 457451. 0.3097
|
|
47.30 0.2679 0.5744 0.0275 0.0128 1.926 11.033 8.769 1435.913 1.247 39.005 2.770 0.74 457781. 0.2839
|
|
49.79 0.2820 0.5774 0.0249 0.0122 1.821 10.435 7.921 1358.061 1.179 35.232 2.645 0.74 458122. 0.2577
|
|
52.28 0.2961 0.5755 0.0222 0.0114 1.710 9.799 7.060 1275.234 1.107 31.405 2.511 0.74 458473. 0.2310
|
|
54.77 0.3102 0.5676 0.0194 0.0106 1.592 9.124 6.189 1187.374 1.031 27.528 2.364 0.74 458834. 0.2036
|
|
57.26 0.3243 0.5521 0.0167 0.0098 1.468 8.410 5.308 1094.455 0.950 23.608 2.200 0.74 459205. 0.1754
|
|
59.74 0.3384 0.5267 0.0139 0.0089 1.336 7.657 4.418 996.478 0.865 19.650 2.011 0.74 459586. 0.1463
|
|
62.23 0.3525 0.4876 0.0111 0.0080 1.198 6.865 3.521 893.467 0.776 15.660 1.787 0.74 459975. 0.1161
|
|
64.72 0.3666 0.4289 0.0082 0.0070 1.053 6.035 2.618 785.425 0.682 11.643 1.512 0.74 460370. 0.0847
|
|
67.21 0.3807 0.3395 0.0054 0.0060 0.901 5.164 1.707 672.054 0.583 7.594 1.152 0.74 460760. 0.0521
|
|
69.70 0.3948 0.1952 0.0024 0.0049 0.739 4.235 0.776 551.189 0.478 3.452 0.639 0.75 461094. 0.0195
|
|
72.19 0.4089
|
|
|
|
|
|
|
|
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 0.0709 0.0199 3.864 20.294 26.840 2881.270 2.293 119.384 4.225 0.81 494162. 0.7577
|
|
2.78 0.0144 0.0504 0.0690 0.0197 3.841 20.174 26.151 2864.243 2.279 116.321 4.141 0.81 494363. 0.7331
|
|
5.55 0.0288 0.0987 0.0672 0.0196 3.814 20.033 25.441 2844.237 2.263 113.163 4.057 0.81 494573. 0.7084
|
|
8.33 0.0432 0.1450 0.0652 0.0194 3.783 19.871 24.711 2821.105 2.245 109.916 3.973 0.81 494790. 0.6837
|
|
11.10 0.0576 0.1893 0.0633 0.0193 3.748 19.684 23.961 2794.636 2.224 106.578 3.889 0.81 495016. 0.6590
|
|
13.88 0.0721 0.2315 0.0612 0.0191 3.707 19.473 23.190 2764.618 2.200 103.150 3.805 0.81 495250. 0.6342
|
|
16.66 0.0865 0.2716 0.0591 0.0188 3.662 19.235 22.399 2730.848 2.173 99.632 3.720 0.81 495492. 0.6095
|
|
19.43 0.1009 0.3097 0.0570 0.0186 3.611 18.969 21.588 2693.093 2.143 96.022 3.636 0.81 495744. 0.5848
|
|
22.21 0.1153 0.3457 0.0548 0.0183 3.555 18.674 20.756 2651.292 2.110 92.321 3.551 0.81 496004. 0.5600
|
|
24.98 0.1297 0.3795 0.0525 0.0180 3.494 18.351 19.903 2605.409 2.073 88.529 3.465 0.81 496274. 0.5351
|
|
27.76 0.1441 0.4111 0.0502 0.0176 3.426 17.996 19.030 2554.942 2.033 84.645 3.378 0.81 496554. 0.5102
|
|
30.53 0.1585 0.4405 0.0479 0.0172 3.352 17.608 18.136 2499.854 1.989 80.671 3.291 0.81 496843. 0.4851
|
|
33.31 0.1729 0.4676 0.0455 0.0168 3.272 17.185 17.223 2439.802 1.942 76.606 3.202 0.81 497142. 0.4600
|
|
36.09 0.1873 0.4922 0.0430 0.0164 3.184 16.726 16.289 2374.618 1.890 72.452 3.111 0.81 497452. 0.4347
|
|
38.86 0.2018 0.5143 0.0405 0.0159 3.090 16.230 15.335 2304.264 1.834 68.210 3.019 0.81 497772. 0.4092
|
|
41.64 0.2162 0.5336 0.0379 0.0154 2.988 15.696 14.362 2228.461 1.773 63.881 2.923 0.81 498103. 0.3835
|
|
44.41 0.2306 0.5499 0.0353 0.0148 2.879 15.123 13.369 2147.070 1.709 59.466 2.824 0.81 498444. 0.3575
|
|
47.19 0.2450 0.5629 0.0326 0.0142 2.763 14.510 12.358 2060.043 1.639 54.969 2.721 0.81 498797. 0.3311
|
|
49.97 0.2594 0.5722 0.0299 0.0136 2.638 13.856 11.329 1967.256 1.565 50.392 2.612 0.81 499161. 0.3043
|
|
52.74 0.2738 0.5771 0.0271 0.0129 2.506 13.162 10.283 1868.620 1.487 45.739 2.496 0.81 499536. 0.2771
|
|
55.52 0.2882 0.5770 0.0243 0.0122 2.366 12.426 9.221 1764.116 1.404 41.014 2.371 0.81 499923. 0.2492
|
|
58.29 0.3026 0.5708 0.0215 0.0114 2.218 11.648 8.143 1653.769 1.316 36.222 2.233 0.81 500321. 0.2206
|
|
61.07 0.3171 0.5570 0.0186 0.0106 2.062 10.830 7.053 1537.607 1.224 31.370 2.080 0.81 500731. 0.1913
|
|
63.85 0.3315 0.5336 0.0157 0.0098 1.899 9.972 5.950 1415.745 1.127 26.466 1.906 0.81 501152. 0.1610
|
|
66.62 0.3459 0.4974 0.0128 0.0089 1.728 9.074 4.837 1288.323 1.025 21.517 1.703 0.81 501583. 0.1297
|
|
69.40 0.3603 0.4438 0.0098 0.0080 1.549 8.138 3.716 1155.455 0.919 16.530 1.459 0.81 502023. 0.0974
|
|
72.17 0.3747 0.3651 0.0068 0.0070 1.364 7.164 2.587 1017.077 0.809 11.508 1.154 0.81 502465. 0.0642
|
|
74.95 0.3891 0.2468 0.0038 0.0060 1.169 6.140 1.444 871.724 0.694 6.421 0.751 0.81 502884. 0.0312
|
|
77.73 0.4035 0.0350 0.0004 0.0048 0.927 4.869 0.157 691.321 0.550 0.696 0.103 0.81 502753. 0.0014
|
|
80.50 0.4179
|
|
|
|
|
|
|
|
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 0.0730 0.0214 5.299 25.691 32.454 3951.344 2.903 144.356 3.725 0.87 535237. 0.7347
|
|
3.05 0.0146 0.0490 0.0711 0.0212 5.249 25.448 31.610 3913.992 2.875 140.603 3.663 0.87 535463. 0.7129
|
|
6.11 0.0293 0.0964 0.0691 0.0210 5.194 25.181 30.740 3873.027 2.845 136.732 3.600 0.87 535698. 0.6909
|
|
9.16 0.0439 0.1420 0.0671 0.0208 5.134 24.891 29.845 3828.306 2.812 132.750 3.536 0.87 535943. 0.6687
|
|
12.21 0.0585 0.1858 0.0651 0.0205 5.069 24.574 28.925 3779.600 2.776 128.657 3.471 0.87 536196. 0.6462
|
|
15.26 0.0731 0.2279 0.0629 0.0202 4.998 24.230 27.979 3726.661 2.737 124.453 3.405 0.87 536459. 0.6235
|
|
18.32 0.0878 0.2681 0.0607 0.0199 4.920 23.856 27.009 3669.208 2.695 120.136 3.339 0.87 536731. 0.6006
|
|
21.37 0.1024 0.3064 0.0585 0.0196 4.837 23.451 26.013 3606.950 2.650 115.707 3.271 0.87 537013. 0.5775
|
|
24.42 0.1170 0.3429 0.0562 0.0192 4.747 23.013 24.992 3539.584 2.600 111.166 3.203 0.87 537305. 0.5542
|
|
27.47 0.1317 0.3773 0.0539 0.0188 4.650 22.544 23.946 3467.363 2.547 106.512 3.132 0.87 537608. 0.5306
|
|
30.53 0.1463 0.4083 0.0514 0.0184 4.560 22.110 22.873 3400.670 2.498 101.741 3.051 0.88 537921. 0.5051
|
|
33.58 0.1609 0.4366 0.0490 0.0181 4.465 21.650 21.776 3329.871 2.446 96.858 2.966 0.88 538245. 0.4791
|
|
36.63 0.1755 0.4622 0.0465 0.0176 4.365 21.161 20.653 3254.631 2.391 91.863 2.878 0.88 538581. 0.4528
|
|
39.68 0.1902 0.4849 0.0439 0.0172 4.257 20.639 19.505 3174.354 2.332 86.758 2.787 0.88 538927. 0.4261
|
|
42.74 0.2048 0.5044 0.0412 0.0167 4.142 20.080 18.333 3088.473 2.269 81.545 2.692 0.88 539285. 0.3991
|
|
45.79 0.2194 0.5205 0.0385 0.0163 4.020 19.491 17.137 2997.831 2.202 76.225 2.593 0.88 539655. 0.3716
|
|
48.84 0.2341 0.5327 0.0358 0.0157 3.891 18.867 15.918 2901.780 2.132 70.801 2.488 0.88 540037. 0.3436
|
|
51.89 0.2487 0.5408 0.0330 0.0152 3.755 18.206 14.675 2800.138 2.057 65.276 2.377 0.88 540431. 0.3152
|
|
54.95 0.2633 0.5440 0.0302 0.0146 3.612 17.511 13.411 2693.320 1.978 59.654 2.259 0.88 540838. 0.2863
|
|
58.00 0.2779 0.5418 0.0273 0.0140 3.462 16.783 12.126 2581.383 1.896 53.938 2.131 0.88 541257. 0.2568
|
|
61.05 0.2926 0.5331 0.0243 0.0134 3.305 16.022 10.822 2464.222 1.810 48.136 1.992 0.88 541689. 0.2268
|
|
64.10 0.3072 0.5170 0.0214 0.0127 3.141 15.228 9.500 2342.136 1.720 42.254 1.840 0.88 542133. 0.1963
|
|
67.16 0.3218 0.4919 0.0184 0.0120 2.971 14.405 8.161 2215.522 1.627 36.300 1.671 0.88 542590. 0.1652
|
|
70.21 0.3365 0.4560 0.0153 0.0113 2.795 13.553 6.809 2084.538 1.531 30.285 1.481 0.88 543060. 0.1338
|
|
73.26 0.3511 0.4068 0.0122 0.0106 2.614 12.675 5.445 1949.552 1.432 24.218 1.267 0.88 543540. 0.1023
|
|
76.31 0.3657 0.3411 0.0092 0.0098 2.428 11.773 4.071 1810.730 1.330 18.107 1.020 0.88 544028. 0.0712
|
|
79.37 0.3803 0.2542 0.0060 0.0090 2.236 10.841 2.686 1667.373 1.225 11.948 0.731 0.88 544515. 0.0415
|
|
82.42 0.3950 0.1380 0.0029 0.0082 2.030 9.842 1.274 1513.721 1.112 5.669 0.382 0.88 544952. 0.0149
|
|
85.47 0.4096
|
|
88.52 0.4242
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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|
0.00 0.0000 0.0000 0.0754 0.0254 7.847 35.330 38.872 5851.873 3.992 172.904 3.013 0.94 576275. 0.6503
|
|
3.32 0.0148 0.0434 0.0734 0.0250 7.732 34.808 37.866 5765.490 3.933 168.428 2.979 0.94 576526. 0.6346
|
|
6.64 0.0295 0.0857 0.0714 0.0246 7.609 34.258 36.827 5674.362 3.870 163.806 2.944 0.94 576787. 0.6184
|
|
9.96 0.0443 0.1269 0.0693 0.0242 7.481 33.679 35.757 5578.504 3.805 159.046 2.907 0.94 577058. 0.6018
|
|
13.28 0.0591 0.1670 0.0672 0.0238 7.346 33.071 34.656 5477.744 3.736 154.148 2.870 0.94 577339. 0.5848
|
|
16.60 0.0739 0.2060 0.0650 0.0233 7.204 32.432 33.523 5371.934 3.664 149.112 2.830 0.94 577630. 0.5673
|
|
19.92 0.0886 0.2436 0.0628 0.0228 7.055 31.762 32.360 5260.900 3.588 143.939 2.790 0.94 577932. 0.5494
|
|
23.24 0.1034 0.2799 0.0604 0.0223 6.899 31.058 31.167 5144.394 3.509 138.630 2.748 0.94 578244. 0.5310
|
|
26.56 0.1182 0.3148 0.0581 0.0218 6.735 30.320 29.942 5022.174 3.426 133.183 2.704 0.94 578568. 0.5122
|
|
29.88 0.1330 0.3482 0.0556 0.0212 6.563 29.546 28.687 4893.922 3.338 127.601 2.659 0.94 578903. 0.4930
|
|
33.20 0.1477 0.3799 0.0531 0.0207 6.384 28.743 27.402 4760.810 3.247 121.882 2.611 0.94 579250. 0.4731
|
|
36.52 0.1625 0.4071 0.0506 0.0202 6.239 28.088 26.082 4652.415 3.173 116.014 2.543 0.94 579609. 0.4495
|
|
39.84 0.1773 0.4281 0.0480 0.0199 6.136 27.626 24.729 4575.906 3.121 109.993 2.451 0.94 579979. 0.4219
|
|
43.16 0.1920 0.4456 0.0453 0.0195 6.029 27.144 23.345 4496.015 3.067 103.839 2.355 0.94 580363. 0.3939
|
|
46.48 0.2068 0.4589 0.0425 0.0192 5.923 26.666 21.931 4416.797 3.013 97.550 2.252 0.94 580758. 0.3651
|
|
49.80 0.2216 0.4681 0.0397 0.0188 5.812 26.165 20.489 4333.933 2.956 91.133 2.144 0.94 581167. 0.3360
|
|
53.11 0.2364 0.4728 0.0369 0.0184 5.696 25.646 19.018 4247.855 2.897 84.591 2.031 0.94 581589. 0.3065
|
|
56.43 0.2511 0.4724 0.0340 0.0181 5.581 25.124 17.520 4161.505 2.839 77.927 1.909 0.94 582024. 0.2767
|
|
59.75 0.2659 0.4667 0.0310 0.0177 5.461 24.586 15.995 4072.285 2.778 71.148 1.782 0.94 582472. 0.2467
|
|
63.07 0.2807 0.4552 0.0280 0.0173 5.338 24.032 14.447 3980.564 2.715 64.259 1.646 0.95 582934. 0.2166
|
|
66.39 0.2954 0.4371 0.0250 0.0169 5.215 23.476 12.876 3888.516 2.652 57.271 1.502 0.95 583410. 0.1865
|
|
69.71 0.3102 0.4121 0.0219 0.0165 5.089 22.913 11.284 3795.237 2.589 50.192 1.349 0.95 583899. 0.1568
|
|
73.03 0.3250 0.3796 0.0188 0.0161 4.963 22.344 9.675 3700.973 2.524 43.035 1.186 0.95 584402. 0.1277
|
|
76.35 0.3398 0.3389 0.0156 0.0157 4.837 21.774 8.052 3606.632 2.460 35.814 1.013 0.95 584919. 0.0995
|
|
79.67 0.3545 0.2894 0.0124 0.0152 4.710 21.206 6.417 3512.486 2.396 28.543 0.829 0.95 585448. 0.0727
|
|
82.99 0.3693 0.2305 0.0093 0.0148 4.583 20.635 4.774 3417.914 2.331 21.234 0.633 0.95 585986. 0.0479
|
|
86.31 0.3841 0.1612 0.0061 0.0144 4.453 20.048 3.120 3320.658 2.265 13.876 0.426 0.95 586524. 0.0261
|
|
89.63 0.3989 0.0795 0.0028 0.0139 4.301 19.365 1.431 3207.576 2.188 6.365 0.202 0.95 587017. 0.0084
|
|
92.95 0.4136
|
|
96.27 0.4284
|
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