612 lines
109 KiB
Plaintext
612 lines
109 KiB
Plaintext
13x11 (13x11.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 0.1249 0.0694 0.002 0.131 0.114 1.547 0.015 0.506 33.334 0.05 21781. 0.5074
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0.43 0.0350 0.0613 0.1241 0.0708 0.002 0.133 0.113 1.577 0.015 0.502 32.483 0.05 21802. 0.4927
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0.86 0.0700 0.1194 0.1231 0.0721 0.002 0.136 0.112 1.607 0.015 0.498 31.614 0.05 21827. 0.4776
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1.29 0.1049 0.1741 0.1219 0.0735 0.002 0.138 0.111 1.637 0.016 0.494 30.736 0.05 21854. 0.4621
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1.72 0.1399 0.2254 0.1206 0.0749 0.002 0.141 0.110 1.668 0.016 0.488 29.852 0.05 21885. 0.4464
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2.15 0.1749 0.2734 0.1191 0.0762 0.002 0.143 0.108 1.697 0.016 0.482 28.970 0.05 21919. 0.4305
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2.58 0.2099 0.3182 0.1173 0.0774 0.002 0.146 0.107 1.724 0.016 0.475 28.095 0.05 21956. 0.4144
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3.01 0.2449 0.3598 0.1154 0.0785 0.002 0.148 0.105 1.749 0.017 0.467 27.228 0.05 21998. 0.3982
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3.44 0.2798 0.3983 0.1131 0.0795 0.002 0.150 0.103 1.770 0.017 0.458 26.375 0.05 22043. 0.3820
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3.88 0.3148 0.4339 0.1106 0.0802 0.002 0.151 0.101 1.787 0.017 0.448 25.536 0.05 22091. 0.3656
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4.31 0.3498 0.4665 0.1077 0.0808 0.002 0.152 0.098 1.799 0.017 0.436 24.712 0.05 22144. 0.3492
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4.74 0.3848 0.4964 0.1045 0.0810 0.002 0.153 0.095 1.805 0.017 0.423 23.903 0.05 22201. 0.3327
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5.17 0.4197 0.5234 0.1009 0.0809 0.002 0.152 0.092 1.803 0.017 0.409 23.107 0.05 22261. 0.3161
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5.60 0.4547 0.5478 0.0970 0.0805 0.002 0.152 0.088 1.794 0.017 0.393 22.322 0.05 22325. 0.2994
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6.03 0.4897 0.5694 0.0926 0.0797 0.002 0.150 0.084 1.775 0.017 0.375 21.546 0.05 22394. 0.2824
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6.46 0.5247 0.5883 0.0879 0.0784 0.002 0.148 0.080 1.747 0.017 0.356 20.775 0.05 22466. 0.2652
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6.89 0.5597 0.6042 0.0828 0.0767 0.002 0.144 0.075 1.709 0.016 0.335 20.003 0.05 22542. 0.2479
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7.32 0.5946 0.6170 0.0774 0.0746 0.002 0.140 0.070 1.661 0.016 0.313 19.225 0.05 22622. 0.2303
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7.75 0.6296 0.6264 0.0717 0.0720 0.002 0.136 0.065 1.605 0.015 0.290 18.434 0.05 22705. 0.2125
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8.18 0.6646 0.6319 0.0658 0.0692 0.002 0.130 0.060 1.541 0.015 0.266 17.618 0.05 22793. 0.1945
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8.61 0.6996 0.6331 0.0596 0.0659 0.002 0.124 0.054 1.468 0.014 0.241 16.767 0.05 22883. 0.1763
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9.04 0.7346 0.6290 0.0534 0.0623 0.002 0.117 0.049 1.389 0.013 0.216 15.865 0.05 22978. 0.1578
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9.47 0.7695 0.6185 0.0470 0.0584 0.002 0.110 0.043 1.302 0.012 0.190 14.893 0.05 23076. 0.1390
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9.90 0.8045 0.6001 0.0404 0.0542 0.002 0.102 0.037 1.208 0.012 0.164 13.821 0.05 23178. 0.1197
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10.33 0.8395 0.5713 0.0338 0.0497 0.001 0.094 0.031 1.108 0.011 0.137 12.610 0.05 23284. 0.0999
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10.77 0.8745 0.5286 0.0272 0.0449 0.001 0.085 0.025 1.001 0.010 0.110 11.200 0.05 23392. 0.0795
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11.20 0.9094 0.4660 0.0204 0.0399 0.001 0.075 0.019 0.888 0.008 0.083 9.494 0.05 23505. 0.0584
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11.63 0.9444 0.3736 0.0137 0.0345 0.001 0.065 0.012 0.769 0.007 0.055 7.331 0.05 23621. 0.0369
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12.06 0.9794 0.2334 0.0069 0.0290 0.001 0.055 0.006 0.645 0.006 0.028 4.416 0.05 23740. 0.0158
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12.49 1.0144 0.0078 0.0002 0.0232 0.001 0.044 0.000 0.517 0.005 0.001 0.143 0.05 23862. 0.0001
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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 0.1255 0.0622 0.015 0.469 0.457 11.093 0.053 2.032 18.683 0.10 43561. 0.5700
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0.87 0.0353 0.0691 0.1247 0.0636 0.015 0.479 0.454 11.341 0.054 2.019 18.152 0.10 43605. 0.5519
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1.74 0.0706 0.1341 0.1237 0.0651 0.016 0.490 0.450 11.596 0.055 2.003 17.614 0.10 43654. 0.5335
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2.61 0.1058 0.1950 0.1226 0.0665 0.016 0.501 0.446 11.855 0.057 1.985 17.072 0.10 43710. 0.5147
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3.47 0.1411 0.2518 0.1213 0.0680 0.016 0.512 0.441 12.113 0.058 1.964 16.532 0.10 43772. 0.4958
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4.34 0.1764 0.3046 0.1198 0.0694 0.017 0.522 0.436 12.363 0.059 1.940 15.997 0.10 43841. 0.4768
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5.21 0.2117 0.3534 0.1180 0.0707 0.017 0.533 0.430 12.601 0.060 1.912 15.470 0.10 43917. 0.4577
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6.08 0.2469 0.3985 0.1161 0.0719 0.017 0.542 0.423 12.818 0.061 1.880 14.953 0.10 44000. 0.4387
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6.95 0.2822 0.4401 0.1138 0.0730 0.017 0.550 0.414 13.009 0.062 1.843 14.448 0.10 44091. 0.4198
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7.82 0.3175 0.4783 0.1113 0.0739 0.018 0.556 0.405 13.164 0.063 1.802 13.956 0.10 44190. 0.4009
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8.69 0.3528 0.5132 0.1084 0.0745 0.018 0.561 0.395 13.277 0.063 1.755 13.479 0.10 44297. 0.3821
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9.55 0.3880 0.5451 0.1051 0.0748 0.018 0.564 0.383 13.340 0.064 1.703 13.015 0.10 44412. 0.3634
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10.42 0.4233 0.5741 0.1015 0.0749 0.018 0.564 0.370 13.345 0.064 1.644 12.564 0.10 44535. 0.3448
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11.29 0.4586 0.6002 0.0975 0.0745 0.018 0.561 0.355 13.282 0.063 1.579 12.126 0.10 44665. 0.3261
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12.16 0.4939 0.6236 0.0931 0.0738 0.018 0.556 0.339 13.145 0.063 1.508 11.698 0.10 44804. 0.3074
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13.03 0.5292 0.6442 0.0883 0.0725 0.017 0.546 0.321 12.929 0.062 1.430 11.279 0.10 44951. 0.2887
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13.90 0.5644 0.6621 0.0831 0.0709 0.017 0.534 0.303 12.630 0.060 1.346 10.867 0.10 45105. 0.2698
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14.77 0.5997 0.6771 0.0776 0.0687 0.016 0.518 0.283 12.253 0.059 1.257 10.459 0.10 45267. 0.2509
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15.63 0.6350 0.6889 0.0718 0.0662 0.016 0.499 0.262 11.801 0.056 1.163 10.052 0.11 45437. 0.2320
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16.50 0.6703 0.6974 0.0658 0.0633 0.015 0.477 0.240 11.279 0.054 1.066 9.639 0.11 45614. 0.2130
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17.37 0.7055 0.7019 0.0597 0.0600 0.014 0.452 0.217 10.690 0.051 0.966 9.217 0.11 45799. 0.1939
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18.24 0.7408 0.7017 0.0533 0.0563 0.013 0.424 0.194 10.036 0.048 0.864 8.776 0.11 45991. 0.1745
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19.11 0.7761 0.6958 0.0469 0.0523 0.012 0.394 0.171 9.320 0.045 0.759 8.306 0.11 46190. 0.1549
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19.98 0.8114 0.6825 0.0403 0.0479 0.011 0.361 0.147 8.544 0.041 0.653 7.794 0.11 46397. 0.1348
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20.85 0.8466 0.6594 0.0337 0.0432 0.010 0.326 0.123 7.709 0.037 0.545 7.215 0.11 46611. 0.1140
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21.71 0.8819 0.6221 0.0270 0.0382 0.009 0.288 0.098 6.817 0.033 0.437 6.535 0.11 46832. 0.0924
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22.58 0.9172 0.5634 0.0202 0.0329 0.008 0.248 0.074 5.872 0.028 0.328 5.691 0.11 47060. 0.0697
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23.45 0.9525 0.4694 0.0135 0.0274 0.007 0.206 0.049 4.876 0.023 0.218 4.566 0.11 47296. 0.0457
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24.32 0.9878 0.3097 0.0067 0.0215 0.005 0.162 0.025 3.834 0.018 0.109 2.905 0.11 47538. 0.0205
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25.19 1.0230 0.0038 0.0001 0.0154 0.004 0.116 0.000 2.751 0.013 0.001 0.035 0.11 47786. 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 0.1258 0.0593 0.048 1.005 1.031 35.668 0.114 4.584 13.107 0.15 65341. 0.6006
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1.31 0.0354 0.0729 0.1250 0.0607 0.049 1.029 1.024 36.522 0.116 4.554 12.716 0.15 65407. 0.5808
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2.62 0.0708 0.1412 0.1240 0.0622 0.050 1.054 1.016 37.405 0.119 4.520 12.321 0.15 65481. 0.5606
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3.92 0.1062 0.2051 0.1229 0.0637 0.051 1.079 1.007 38.303 0.122 4.479 11.925 0.15 65565. 0.5401
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5.23 0.1416 0.2644 0.1217 0.0652 0.053 1.104 0.997 39.198 0.125 4.433 11.531 0.15 65658. 0.5196
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6.54 0.1770 0.3193 0.1202 0.0666 0.054 1.129 0.984 40.073 0.128 4.379 11.142 0.15 65762. 0.4990
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7.85 0.2124 0.3701 0.1185 0.0680 0.055 1.152 0.970 40.903 0.130 4.316 10.760 0.16 65877. 0.4784
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9.15 0.2478 0.4168 0.1165 0.0693 0.056 1.174 0.954 41.668 0.133 4.245 10.388 0.16 66003. 0.4580
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10.46 0.2832 0.4597 0.1142 0.0704 0.057 1.193 0.936 42.341 0.135 4.163 10.025 0.16 66140. 0.4377
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11.77 0.3186 0.4991 0.1117 0.0713 0.058 1.209 0.915 42.896 0.137 4.069 9.674 0.16 66290. 0.4176
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13.08 0.3540 0.5350 0.1088 0.0720 0.058 1.220 0.891 43.307 0.138 3.964 9.334 0.16 66451. 0.3977
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14.38 0.3894 0.5678 0.1056 0.0724 0.058 1.227 0.865 43.547 0.139 3.846 9.006 0.16 66624. 0.3780
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15.69 0.4248 0.5976 0.1019 0.0725 0.058 1.228 0.835 43.587 0.139 3.714 8.689 0.16 66810. 0.3583
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17.00 0.4602 0.6246 0.0979 0.0721 0.058 1.223 0.802 43.398 0.138 3.567 8.382 0.16 67007. 0.3388
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18.31 0.4956 0.6488 0.0935 0.0714 0.058 1.210 0.766 42.953 0.137 3.405 8.085 0.16 67216. 0.3193
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19.61 0.5311 0.6703 0.0886 0.0702 0.057 1.190 0.726 42.232 0.134 3.229 7.796 0.16 67438. 0.2998
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20.92 0.5665 0.6891 0.0834 0.0685 0.055 1.162 0.683 41.231 0.131 3.038 7.514 0.16 67671. 0.2803
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22.23 0.6019 0.7053 0.0778 0.0664 0.054 1.126 0.638 39.958 0.127 2.836 7.238 0.16 67915. 0.2608
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23.54 0.6373 0.7185 0.0720 0.0639 0.052 1.083 0.590 38.427 0.122 2.624 6.964 0.16 68171. 0.2414
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24.84 0.6727 0.7286 0.0660 0.0609 0.049 1.033 0.541 36.651 0.117 2.404 6.690 0.16 68439. 0.2220
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26.15 0.7081 0.7350 0.0598 0.0576 0.046 0.976 0.490 34.640 0.110 2.178 6.412 0.16 68718. 0.2025
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27.46 0.7435 0.7372 0.0534 0.0539 0.043 0.913 0.438 32.405 0.103 1.946 6.124 0.16 69008. 0.1829
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28.77 0.7789 0.7342 0.0469 0.0498 0.040 0.844 0.384 29.950 0.095 1.710 5.822 0.16 69309. 0.1629
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30.07 0.8143 0.7243 0.0403 0.0454 0.037 0.769 0.330 27.284 0.087 1.470 5.494 0.16 69622. 0.1426
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31.38 0.8497 0.7052 0.0337 0.0406 0.033 0.688 0.276 24.411 0.078 1.227 5.126 0.16 69945. 0.1215
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32.69 0.8851 0.6725 0.0270 0.0355 0.029 0.601 0.221 21.341 0.068 0.982 4.693 0.16 70279. 0.0995
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34.00 0.9205 0.6186 0.0202 0.0301 0.024 0.509 0.165 18.081 0.058 0.736 4.151 0.16 70623. 0.0762
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35.30 0.9559 0.5276 0.0134 0.0243 0.020 0.413 0.110 14.645 0.047 0.490 3.409 0.16 70978. 0.0510
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36.61 0.9913 0.3614 0.0067 0.0184 0.015 0.311 0.055 11.048 0.035 0.244 2.252 0.16 71344. 0.0238
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37.92 1.0267 0.0010 0.0000 0.0121 0.010 0.206 0.000 7.308 0.023 0.000 0.006 0.16 71717. 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 0.1261 0.0577 0.110 1.738 1.836 82.245 0.196 8.168 10.127 0.21 87121. 0.6194
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1.75 0.0355 0.0752 0.1253 0.0591 0.113 1.781 1.824 84.300 0.201 8.115 9.816 0.21 87208. 0.5985
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3.49 0.0710 0.1456 0.1243 0.0606 0.116 1.826 1.811 86.429 0.206 8.055 9.503 0.21 87307. 0.5772
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5.24 0.1064 0.2111 0.1233 0.0621 0.119 1.872 1.795 88.596 0.212 7.984 9.190 0.21 87419. 0.5557
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6.99 0.1419 0.2720 0.1220 0.0637 0.122 1.918 1.777 90.762 0.217 7.902 8.878 0.21 87544. 0.5341
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8.74 0.1774 0.3282 0.1205 0.0651 0.125 1.963 1.755 92.881 0.222 7.807 8.572 0.21 87683. 0.5126
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10.48 0.2129 0.3801 0.1188 0.0666 0.127 2.005 1.731 94.899 0.227 7.697 8.271 0.21 87836. 0.4911
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12.23 0.2483 0.4277 0.1169 0.0679 0.130 2.045 1.702 96.761 0.231 7.571 7.979 0.21 88005. 0.4698
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13.98 0.2838 0.4715 0.1146 0.0690 0.132 2.079 1.669 98.405 0.235 7.426 7.695 0.21 88189. 0.4488
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15.72 0.3193 0.5115 0.1121 0.0700 0.134 2.108 1.632 99.771 0.238 7.260 7.421 0.21 88389. 0.4279
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17.47 0.3548 0.5481 0.1092 0.0707 0.135 2.130 1.590 100.792 0.241 7.073 7.156 0.21 88604. 0.4073
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19.22 0.3903 0.5814 0.1059 0.0711 0.136 2.143 1.543 101.404 0.242 6.863 6.901 0.21 88836. 0.3869
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20.96 0.4257 0.6117 0.1023 0.0712 0.136 2.146 1.490 101.535 0.242 6.628 6.656 0.21 89085. 0.3667
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22.71 0.4612 0.6392 0.0983 0.0709 0.136 2.137 1.431 101.118 0.241 6.366 6.420 0.21 89349. 0.3466
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24.46 0.4967 0.6639 0.0938 0.0702 0.134 2.115 1.366 100.086 0.239 6.077 6.192 0.21 89629. 0.3267
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26.21 0.5322 0.6860 0.0889 0.0690 0.132 2.079 1.295 98.392 0.235 5.761 5.971 0.21 89925. 0.3067
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27.95 0.5676 0.7055 0.0837 0.0673 0.129 2.029 1.219 96.023 0.229 5.421 5.757 0.21 90237. 0.2869
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29.70 0.6031 0.7223 0.0781 0.0652 0.125 1.965 1.138 92.999 0.222 5.060 5.548 0.21 90565. 0.2671
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31.45 0.6386 0.7365 0.0723 0.0627 0.120 1.888 1.052 89.352 0.213 4.681 5.342 0.21 90908. 0.2474
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33.19 0.6741 0.7476 0.0662 0.0597 0.114 1.798 0.964 85.111 0.203 4.288 5.138 0.21 91266. 0.2277
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34.94 0.7096 0.7554 0.0600 0.0563 0.108 1.697 0.873 80.304 0.192 3.884 4.932 0.21 91640. 0.2080
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36.69 0.7450 0.7593 0.0536 0.0526 0.101 1.584 0.780 74.950 0.179 3.470 4.721 0.21 92028. 0.1882
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38.43 0.7805 0.7582 0.0471 0.0484 0.093 1.459 0.685 69.065 0.165 3.048 4.500 0.21 92431. 0.1681
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40.18 0.8160 0.7509 0.0404 0.0439 0.084 1.324 0.589 62.664 0.150 2.619 4.263 0.21 92849. 0.1476
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41.93 0.8515 0.7348 0.0337 0.0391 0.075 1.178 0.491 55.763 0.133 2.186 3.997 0.21 93281. 0.1265
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43.68 0.8869 0.7058 0.0270 0.0339 0.065 1.022 0.393 48.380 0.115 1.749 3.686 0.21 93728. 0.1043
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45.42 0.9224 0.6561 0.0202 0.0284 0.054 0.857 0.294 40.539 0.097 1.310 3.295 0.21 94190. 0.0807
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47.17 0.9579 0.5688 0.0134 0.0226 0.043 0.682 0.196 32.268 0.077 0.870 2.750 0.22 94665. 0.0549
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48.92 0.9934 0.4008 0.0067 0.0166 0.032 0.499 0.097 23.609 0.056 0.433 1.869 0.22 95154. 0.0263
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50.66 1.0289 -0.0018 0.0000 0.0102 0.020 0.308 0.000 14.598 0.035 -0.001 -0.008 0.22 95653. 0.0000
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PROP RPM = 5000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.1264 0.0567 0.212 2.669 2.875 157.883 0.302 12.789 8.260 0.26 108899. 0.6322
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2.19 0.0355 0.0767 0.1256 0.0581 0.217 2.738 2.857 161.947 0.309 12.709 8.003 0.26 109008. 0.6106
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4.37 0.0710 0.1484 0.1247 0.0597 0.223 2.809 2.836 166.162 0.317 12.617 7.743 0.26 109132. 0.5886
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6.56 0.1066 0.2152 0.1236 0.0612 0.229 2.882 2.812 170.461 0.326 12.509 7.483 0.26 109272. 0.5664
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8.75 0.1421 0.2770 0.1223 0.0628 0.234 2.954 2.784 174.764 0.334 12.383 7.225 0.26 109428. 0.5441
|
|
10.93 0.1776 0.3341 0.1209 0.0643 0.240 3.026 2.751 178.979 0.342 12.237 6.972 0.26 109602. 0.5219
|
|
13.12 0.2131 0.3867 0.1192 0.0657 0.245 3.094 2.713 183.002 0.350 12.067 6.724 0.26 109794. 0.4999
|
|
15.31 0.2487 0.4350 0.1173 0.0670 0.250 3.156 2.669 186.720 0.357 11.871 6.483 0.26 110005. 0.4780
|
|
17.49 0.2842 0.4793 0.1151 0.0682 0.255 3.212 2.618 190.015 0.363 11.646 6.250 0.26 110236. 0.4564
|
|
19.68 0.3197 0.5197 0.1125 0.0692 0.258 3.259 2.560 192.762 0.368 11.388 6.025 0.26 110486. 0.4351
|
|
21.87 0.3552 0.5567 0.1096 0.0700 0.261 3.294 2.495 194.832 0.372 11.097 5.808 0.26 110757. 0.4141
|
|
24.05 0.3907 0.5904 0.1064 0.0704 0.263 3.315 2.421 196.094 0.375 10.768 5.600 0.26 111048. 0.3933
|
|
26.24 0.4263 0.6211 0.1028 0.0705 0.263 3.320 2.338 196.410 0.375 10.400 5.400 0.26 111359. 0.3727
|
|
28.42 0.4618 0.6489 0.0987 0.0702 0.262 3.307 2.246 195.643 0.374 9.991 5.207 0.26 111690. 0.3522
|
|
30.61 0.4973 0.6740 0.0942 0.0695 0.260 3.274 2.144 193.662 0.370 9.538 5.022 0.26 112041. 0.3319
|
|
32.80 0.5328 0.6965 0.0893 0.0684 0.255 3.218 2.033 190.371 0.364 9.043 4.844 0.26 112412. 0.3117
|
|
34.98 0.5684 0.7164 0.0841 0.0667 0.249 3.140 1.913 185.745 0.355 8.509 4.671 0.26 112803. 0.2916
|
|
37.17 0.6039 0.7339 0.0785 0.0646 0.241 3.040 1.786 179.821 0.343 7.942 4.504 0.26 113214. 0.2716
|
|
39.36 0.6394 0.7487 0.0726 0.0620 0.232 2.919 1.652 172.660 0.330 7.348 4.339 0.26 113644. 0.2517
|
|
41.54 0.6749 0.7607 0.0665 0.0590 0.220 2.778 1.513 164.322 0.314 6.731 4.177 0.26 114093. 0.2319
|
|
43.73 0.7104 0.7695 0.0602 0.0556 0.208 2.618 1.370 154.858 0.296 6.096 4.014 0.26 114561. 0.2121
|
|
45.92 0.7460 0.7746 0.0538 0.0518 0.194 2.439 1.224 144.306 0.276 5.446 3.848 0.27 115047. 0.1922
|
|
48.10 0.7815 0.7752 0.0473 0.0476 0.178 2.243 1.075 132.697 0.253 4.783 3.676 0.27 115553. 0.1720
|
|
50.29 0.8170 0.7697 0.0406 0.0431 0.161 2.030 0.924 120.062 0.229 4.111 3.491 0.27 116076. 0.1515
|
|
52.48 0.8525 0.7561 0.0339 0.0382 0.143 1.799 0.771 106.432 0.203 3.430 3.287 0.27 116618. 0.1303
|
|
54.66 0.8881 0.7302 0.0271 0.0330 0.123 1.553 0.617 91.843 0.175 2.744 3.047 0.27 117178. 0.1080
|
|
56.85 0.9236 0.6842 0.0203 0.0274 0.102 1.290 0.462 76.340 0.146 2.055 2.745 0.27 117756. 0.0842
|
|
59.04 0.9591 0.6009 0.0135 0.0215 0.080 1.014 0.307 59.986 0.115 1.366 2.322 0.27 118352. 0.0581
|
|
61.22 0.9946 0.4338 0.0067 0.0154 0.057 0.724 0.153 42.857 0.082 0.679 1.616 0.27 118964. 0.0285
|
|
63.41 1.0302 -0.0015 0.0000 0.0090 0.034 0.423 0.000 25.028 0.048 -0.001 -0.005 0.27 119588. 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 0.1266 0.0561 0.362 3.801 4.150 269.810 0.429 18.458 6.976 0.31 130675. 0.6414
|
|
2.65 0.0359 0.0785 0.1259 0.0576 0.371 3.902 4.124 276.986 0.441 18.345 6.754 0.31 130808. 0.6191
|
|
5.30 0.0718 0.1518 0.1250 0.0591 0.381 4.007 4.095 284.441 0.453 18.214 6.530 0.31 130958. 0.5964
|
|
7.96 0.1077 0.2199 0.1239 0.0607 0.392 4.114 4.060 292.054 0.465 18.061 6.306 0.31 131128. 0.5735
|
|
10.61 0.1436 0.2829 0.1227 0.0623 0.402 4.222 4.020 299.681 0.477 17.881 6.084 0.31 131318. 0.5506
|
|
13.26 0.1795 0.3410 0.1212 0.0638 0.412 4.327 3.973 307.155 0.489 17.670 5.866 0.31 131530. 0.5277
|
|
15.91 0.2154 0.3944 0.1196 0.0653 0.421 4.427 3.917 314.288 0.500 17.425 5.653 0.31 131765. 0.5051
|
|
18.56 0.2513 0.4433 0.1176 0.0667 0.430 4.520 3.853 320.875 0.511 17.140 5.447 0.31 132022. 0.4826
|
|
21.22 0.2872 0.4880 0.1153 0.0679 0.438 4.602 3.780 326.698 0.520 16.812 5.247 0.31 132304. 0.4605
|
|
23.87 0.3231 0.5289 0.1128 0.0689 0.445 4.670 3.695 331.531 0.528 16.436 5.055 0.31 132610. 0.4386
|
|
26.52 0.3590 0.5663 0.1098 0.0696 0.449 4.721 3.599 335.143 0.533 16.009 4.871 0.31 132941. 0.4171
|
|
29.17 0.3949 0.6003 0.1065 0.0701 0.452 4.751 3.491 337.293 0.537 15.526 4.694 0.31 133296. 0.3958
|
|
31.82 0.4308 0.6312 0.1028 0.0702 0.453 4.758 3.369 337.734 0.538 14.984 4.524 0.31 133677. 0.3748
|
|
34.47 0.4667 0.6592 0.0987 0.0699 0.451 4.736 3.233 336.215 0.535 14.380 4.361 0.31 134082. 0.3540
|
|
37.13 0.5026 0.6844 0.0941 0.0691 0.446 4.684 3.083 332.507 0.529 13.712 4.205 0.31 134512. 0.3333
|
|
39.78 0.5385 0.7071 0.0891 0.0678 0.438 4.599 2.918 326.449 0.520 12.981 4.055 0.31 134966. 0.3127
|
|
42.43 0.5744 0.7273 0.0837 0.0661 0.426 4.480 2.741 318.011 0.506 12.194 3.910 0.31 135445. 0.2922
|
|
45.08 0.6103 0.7450 0.0779 0.0638 0.412 4.329 2.554 307.268 0.489 11.359 3.770 0.32 135947. 0.2719
|
|
47.73 0.6462 0.7601 0.0719 0.0612 0.395 4.146 2.357 294.334 0.468 10.484 3.632 0.32 136473. 0.2517
|
|
50.39 0.6821 0.7724 0.0657 0.0580 0.375 3.935 2.153 279.311 0.445 9.577 3.497 0.32 137022. 0.2316
|
|
53.04 0.7180 0.7815 0.0593 0.0545 0.352 3.695 1.943 262.285 0.417 8.645 3.361 0.32 137595. 0.2115
|
|
55.69 0.7540 0.7868 0.0528 0.0506 0.326 3.428 1.729 243.323 0.387 7.690 3.223 0.32 138190. 0.1913
|
|
58.34 0.7899 0.7876 0.0461 0.0462 0.298 3.134 1.510 222.481 0.354 6.718 3.079 0.32 138808. 0.1708
|
|
60.99 0.8258 0.7822 0.0393 0.0415 0.268 2.815 1.289 199.812 0.318 5.732 2.925 0.32 139449. 0.1499
|
|
63.65 0.8617 0.7682 0.0325 0.0364 0.235 2.471 1.065 175.374 0.279 4.735 2.753 0.32 140112. 0.1282
|
|
66.30 0.8976 0.7408 0.0256 0.0310 0.200 2.102 0.839 149.235 0.238 3.730 2.549 0.32 140797. 0.1054
|
|
68.95 0.9335 0.6907 0.0187 0.0252 0.163 1.711 0.612 121.484 0.193 2.722 2.285 0.32 141504. 0.0807
|
|
71.60 0.9694 0.5951 0.0118 0.0192 0.124 1.299 0.386 92.241 0.147 1.715 1.896 0.32 142232. 0.0531
|
|
74.25 1.0053 0.3841 0.0049 0.0128 0.083 0.869 0.160 61.655 0.098 0.714 1.180 0.32 142981. 0.0213
|
|
76.90 1.0412
|
|
|
|
|
|
|
|
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 0.1270 0.0557 0.571 5.138 5.662 425.498 0.580 25.186 6.036 0.36 152450. 0.6483
|
|
3.07 0.0356 0.0785 0.1262 0.0572 0.586 5.276 5.629 436.909 0.596 25.039 5.844 0.36 152603. 0.6258
|
|
6.13 0.0712 0.1519 0.1254 0.0587 0.602 5.419 5.591 448.782 0.612 24.868 5.651 0.36 152777. 0.6031
|
|
9.20 0.1067 0.2201 0.1243 0.0603 0.618 5.566 5.546 460.927 0.629 24.668 5.457 0.36 152972. 0.5801
|
|
12.26 0.1423 0.2831 0.1232 0.0619 0.634 5.713 5.493 473.122 0.645 24.433 5.266 0.36 153191. 0.5571
|
|
15.33 0.1779 0.3413 0.1218 0.0635 0.651 5.857 5.431 485.105 0.662 24.157 5.078 0.36 153435. 0.5341
|
|
18.40 0.2135 0.3947 0.1201 0.0650 0.666 5.996 5.359 496.581 0.677 23.835 4.894 0.36 153705. 0.5114
|
|
21.46 0.2490 0.4437 0.1183 0.0664 0.680 6.125 5.274 507.230 0.692 23.460 4.716 0.36 154001. 0.4889
|
|
24.53 0.2846 0.4886 0.1161 0.0676 0.693 6.239 5.177 516.710 0.705 23.027 4.544 0.36 154325. 0.4667
|
|
27.59 0.3202 0.5297 0.1136 0.0687 0.704 6.335 5.065 524.666 0.716 22.529 4.379 0.36 154677. 0.4448
|
|
30.66 0.3558 0.5672 0.1107 0.0694 0.712 6.408 4.938 530.733 0.724 21.963 4.220 0.36 155057. 0.4232
|
|
33.72 0.3914 0.6014 0.1075 0.0699 0.717 6.454 4.794 534.536 0.729 21.322 4.067 0.36 155465. 0.4020
|
|
36.79 0.4269 0.6325 0.1039 0.0701 0.718 6.468 4.632 535.691 0.731 20.602 3.922 0.36 155902. 0.3809
|
|
39.86 0.4625 0.6608 0.0998 0.0698 0.716 6.445 4.451 533.805 0.728 19.798 3.782 0.36 156368. 0.3601
|
|
42.92 0.4981 0.6864 0.0953 0.0692 0.709 6.382 4.251 528.509 0.721 18.907 3.648 0.37 156862. 0.3395
|
|
45.99 0.5337 0.7095 0.0904 0.0680 0.697 6.273 4.031 519.530 0.709 17.931 3.519 0.37 157384. 0.3189
|
|
49.05 0.5692 0.7302 0.0851 0.0663 0.680 6.119 3.794 506.785 0.691 16.876 3.396 0.37 157933. 0.2985
|
|
52.12 0.6048 0.7485 0.0794 0.0642 0.658 5.921 3.542 490.375 0.669 15.754 3.276 0.37 158510. 0.2783
|
|
55.19 0.6404 0.7644 0.0735 0.0616 0.631 5.681 3.277 470.469 0.642 14.577 3.160 0.37 159115. 0.2582
|
|
58.25 0.6760 0.7776 0.0673 0.0585 0.600 5.400 3.003 447.235 0.610 13.356 3.045 0.37 159746. 0.2382
|
|
61.32 0.7115 0.7880 0.0610 0.0551 0.564 5.081 2.720 420.811 0.574 12.097 2.931 0.37 160403. 0.2182
|
|
64.38 0.7471 0.7950 0.0545 0.0512 0.525 4.725 2.430 391.308 0.534 10.808 2.816 0.37 161087. 0.1982
|
|
67.45 0.7827 0.7978 0.0479 0.0470 0.481 4.333 2.134 358.814 0.489 9.494 2.698 0.37 161796. 0.1779
|
|
70.51 0.8183 0.7953 0.0411 0.0423 0.434 3.905 1.835 323.413 0.441 8.160 2.573 0.37 162532. 0.1573
|
|
73.58 0.8539 0.7855 0.0343 0.0373 0.382 3.444 1.531 285.190 0.389 6.810 2.435 0.37 163293. 0.1360
|
|
76.65 0.8894 0.7644 0.0275 0.0320 0.328 2.949 1.225 244.250 0.333 5.449 2.275 0.38 164080. 0.1136
|
|
79.71 0.9250 0.7246 0.0206 0.0263 0.269 2.424 0.918 200.723 0.274 4.082 2.074 0.38 164891. 0.0897
|
|
82.78 0.9606 0.6488 0.0137 0.0203 0.208 1.869 0.610 154.783 0.211 2.714 1.788 0.38 165728. 0.0630
|
|
85.84 0.9962 0.4864 0.0068 0.0140 0.143 1.288 0.304 106.654 0.145 1.352 1.292 0.38 166588. 0.0322
|
|
88.91 1.0317 0.0008 0.0000 0.0074 0.076 0.683 0.000 56.526 0.077 0.001 0.002 0.38 167460. 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 0.1273 0.0555 0.849 6.685 7.416 632.732 0.755 32.984 5.316 0.41 174223. 0.6534
|
|
3.51 0.0356 0.0791 0.1266 0.0570 0.872 6.867 7.374 649.971 0.776 32.801 5.146 0.41 174398. 0.6308
|
|
7.01 0.0712 0.1530 0.1258 0.0586 0.896 7.057 7.326 667.943 0.797 32.587 4.975 0.41 174596. 0.6078
|
|
10.52 0.1068 0.2215 0.1248 0.0602 0.920 7.252 7.269 686.359 0.819 32.334 4.804 0.41 174819. 0.5846
|
|
14.03 0.1424 0.2850 0.1236 0.0618 0.945 7.447 7.202 704.884 0.841 32.037 4.635 0.41 175070. 0.5614
|
|
17.53 0.1780 0.3434 0.1223 0.0634 0.970 7.640 7.124 723.120 0.863 31.686 4.468 0.41 175348. 0.5383
|
|
21.04 0.2136 0.3972 0.1207 0.0649 0.993 7.825 7.031 740.617 0.884 31.273 4.306 0.41 175657. 0.5153
|
|
24.55 0.2492 0.4464 0.1188 0.0663 1.015 7.997 6.923 756.883 0.903 30.792 4.148 0.41 175996. 0.4927
|
|
28.05 0.2848 0.4915 0.1167 0.0676 1.034 8.150 6.797 771.395 0.921 30.233 3.997 0.41 176367. 0.4703
|
|
31.56 0.3205 0.5327 0.1142 0.0687 1.051 8.279 6.652 783.610 0.935 29.589 3.850 0.41 176769. 0.4483
|
|
35.07 0.3561 0.5704 0.1114 0.0695 1.063 8.378 6.487 792.971 0.947 28.854 3.710 0.42 177205. 0.4265
|
|
38.57 0.3917 0.6048 0.1081 0.0700 1.071 8.441 6.299 798.909 0.954 28.020 3.576 0.42 177673. 0.4051
|
|
42.08 0.4273 0.6361 0.1045 0.0702 1.074 8.461 6.088 800.839 0.956 27.080 3.448 0.42 178173. 0.3840
|
|
45.59 0.4629 0.6646 0.1005 0.0700 1.070 8.433 5.852 798.168 0.953 26.030 3.325 0.42 178707. 0.3631
|
|
49.09 0.4985 0.6904 0.0960 0.0693 1.060 8.350 5.590 790.335 0.943 24.864 3.208 0.42 179272. 0.3423
|
|
52.60 0.5341 0.7138 0.0910 0.0681 1.042 8.208 5.302 776.921 0.927 23.584 3.095 0.42 179870. 0.3217
|
|
56.11 0.5697 0.7348 0.0857 0.0664 1.016 8.006 4.991 757.799 0.905 22.200 2.987 0.42 180500. 0.3012
|
|
59.61 0.6053 0.7534 0.0800 0.0643 0.983 7.746 4.660 733.114 0.875 20.726 2.883 0.42 181161. 0.2809
|
|
63.12 0.6409 0.7697 0.0740 0.0616 0.943 7.429 4.312 703.125 0.839 19.179 2.782 0.42 181852. 0.2607
|
|
66.63 0.6765 0.7834 0.0678 0.0586 0.896 7.059 3.951 668.087 0.797 17.573 2.682 0.42 182575. 0.2406
|
|
70.13 0.7121 0.7944 0.0614 0.0551 0.842 6.637 3.578 628.211 0.750 15.917 2.584 0.42 183328. 0.2206
|
|
73.64 0.7477 0.8021 0.0549 0.0512 0.783 6.167 3.197 583.666 0.697 14.221 2.485 0.42 184111. 0.2005
|
|
77.15 0.7833 0.8059 0.0482 0.0469 0.717 5.648 2.808 534.584 0.638 12.492 2.383 0.43 184923. 0.1802
|
|
80.65 0.8189 0.8046 0.0414 0.0422 0.645 5.083 2.414 481.093 0.574 10.736 2.275 0.43 185766. 0.1596
|
|
84.16 0.8545 0.7962 0.0346 0.0371 0.568 4.473 2.014 423.323 0.505 8.958 2.158 0.43 186637. 0.1382
|
|
87.67 0.8901 0.7770 0.0277 0.0317 0.485 3.819 1.611 361.431 0.431 7.166 2.022 0.43 187537. 0.1158
|
|
91.17 0.9257 0.7397 0.0207 0.0259 0.396 3.123 1.206 295.616 0.353 5.365 1.851 0.43 188466. 0.0917
|
|
94.68 0.9614 0.6669 0.0138 0.0198 0.303 2.389 0.801 226.142 0.270 3.563 1.607 0.43 189424. 0.0649
|
|
98.19 0.9970 0.5063 0.0068 0.0134 0.206 1.620 0.398 153.352 0.183 1.769 1.176 0.43 190408. 0.0335
|
|
101.69 1.0326 -0.0064 0.0000 0.0068 0.104 0.819 -0.002 77.511 0.093 -0.011 -0.014 0.43 191404. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1277 0.0554 1.206 8.449 9.413 899.685 0.955 41.868 4.745 0.46 195994. 0.6571
|
|
3.95 0.0357 0.0796 0.1270 0.0569 1.240 8.683 9.363 924.584 0.981 41.648 4.593 0.46 196190. 0.6344
|
|
7.91 0.0714 0.1539 0.1262 0.0585 1.275 8.927 9.305 950.596 1.009 41.388 4.440 0.46 196413. 0.6113
|
|
11.86 0.1071 0.2229 0.1253 0.0602 1.311 9.178 9.236 977.310 1.037 41.082 4.286 0.46 196665. 0.5880
|
|
15.82 0.1428 0.2867 0.1242 0.0618 1.347 9.431 9.154 1004.237 1.066 40.718 4.135 0.46 196947. 0.5646
|
|
19.77 0.1784 0.3454 0.1229 0.0635 1.382 9.681 9.057 1030.795 1.094 40.286 3.985 0.46 197262. 0.5414
|
|
23.73 0.2141 0.3994 0.1213 0.0650 1.417 9.920 8.943 1056.320 1.121 39.777 3.840 0.47 197610. 0.5183
|
|
27.68 0.2498 0.4488 0.1195 0.0665 1.448 10.144 8.808 1080.087 1.146 39.178 3.699 0.47 197993. 0.4955
|
|
31.63 0.2855 0.4941 0.1173 0.0678 1.477 10.343 8.651 1101.326 1.169 38.479 3.563 0.47 198411. 0.4730
|
|
35.59 0.3212 0.5355 0.1149 0.0689 1.501 10.511 8.469 1119.237 1.188 37.671 3.432 0.47 198866. 0.4508
|
|
39.54 0.3569 0.5733 0.1121 0.0698 1.519 10.640 8.261 1133.003 1.202 36.745 3.307 0.47 199358. 0.4290
|
|
43.50 0.3926 0.6078 0.1088 0.0703 1.531 10.723 8.024 1141.790 1.211 35.690 3.187 0.47 199887. 0.4075
|
|
47.45 0.4283 0.6393 0.1052 0.0705 1.535 10.751 7.756 1144.747 1.215 34.499 3.073 0.47 200454. 0.3863
|
|
51.41 0.4640 0.6679 0.1011 0.0702 1.530 10.716 7.456 1141.011 1.211 33.164 2.964 0.47 201057. 0.3653
|
|
55.36 0.4997 0.6939 0.0966 0.0696 1.515 10.610 7.122 1129.770 1.199 31.679 2.859 0.47 201696. 0.3444
|
|
59.31 0.5353 0.7175 0.0916 0.0684 1.489 10.428 6.755 1110.416 1.178 30.048 2.759 0.47 202372. 0.3237
|
|
63.27 0.5710 0.7387 0.0862 0.0667 1.452 10.169 6.358 1082.763 1.149 28.281 2.663 0.47 203084. 0.3031
|
|
67.22 0.6067 0.7577 0.0805 0.0645 1.404 9.833 5.935 1047.029 1.111 26.398 2.571 0.47 203832. 0.2827
|
|
71.18 0.6424 0.7743 0.0745 0.0618 1.346 9.425 5.490 1003.592 1.065 24.421 2.481 0.47 204614. 0.2624
|
|
75.13 0.6781 0.7884 0.0682 0.0587 1.278 8.948 5.029 952.826 1.011 22.367 2.394 0.47 205431. 0.2423
|
|
79.09 0.7138 0.7999 0.0617 0.0551 1.200 8.406 4.552 895.040 0.950 20.249 2.307 0.48 206282. 0.2222
|
|
83.04 0.7495 0.8081 0.0551 0.0511 1.114 7.799 4.065 830.477 0.881 18.079 2.220 0.48 207167. 0.2020
|
|
86.99 0.7852 0.8126 0.0484 0.0468 1.018 7.131 3.567 759.335 0.806 15.867 2.131 0.48 208086. 0.1816
|
|
90.95 0.8209 0.8121 0.0415 0.0420 0.914 6.403 3.062 681.794 0.723 13.619 2.037 0.48 209037. 0.1609
|
|
94.90 0.8566 0.8047 0.0346 0.0368 0.802 5.616 2.550 598.046 0.635 11.344 1.934 0.48 210022. 0.1394
|
|
98.86 0.8922 0.7867 0.0276 0.0313 0.682 4.774 2.034 508.321 0.539 9.049 1.815 0.48 211040. 0.1169
|
|
102.81 0.9279 0.7506 0.0206 0.0254 0.554 3.878 1.516 412.911 0.438 6.743 1.665 0.48 212089. 0.0925
|
|
106.77 0.9636 0.6782 0.0135 0.0192 0.419 2.932 0.997 312.207 0.331 4.436 1.449 0.49 213171. 0.0653
|
|
110.72 0.9993 0.5123 0.0065 0.0127 0.277 1.941 0.481 206.717 0.219 2.140 1.055 0.49 214283. 0.0330
|
|
114.67 1.0350 -0.0757 -0.0004 0.0059 0.130 0.907 -0.032 96.620 0.103 -0.143 -0.150 0.49 215395. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 10000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1281 0.0554 1.656 10.439 11.657 1235.005 1.179 51.851 4.281 0.52 217762. 0.6598
|
|
4.39 0.0356 0.0797 0.1274 0.0570 1.702 10.730 11.600 1269.521 1.212 51.597 4.144 0.52 217979. 0.6371
|
|
8.77 0.0712 0.1540 0.1267 0.0586 1.751 11.036 11.532 1305.674 1.247 51.296 4.006 0.52 218226. 0.6141
|
|
13.16 0.1069 0.2231 0.1258 0.0603 1.801 11.351 11.452 1342.898 1.282 50.938 3.868 0.52 218504. 0.5908
|
|
17.54 0.1425 0.2869 0.1248 0.0620 1.851 11.668 11.356 1380.519 1.318 50.511 3.731 0.52 218817. 0.5675
|
|
21.93 0.1781 0.3457 0.1235 0.0636 1.901 11.983 11.241 1417.723 1.354 50.002 3.596 0.52 219165. 0.5443
|
|
26.31 0.2137 0.3997 0.1220 0.0652 1.949 12.286 11.105 1453.586 1.388 49.396 3.465 0.52 219550. 0.5212
|
|
30.70 0.2494 0.4492 0.1202 0.0667 1.994 12.569 10.944 1487.085 1.420 48.679 3.338 0.52 219974. 0.4984
|
|
35.08 0.2850 0.4945 0.1182 0.0681 2.035 12.823 10.755 1517.132 1.449 47.839 3.215 0.52 220438. 0.4760
|
|
39.47 0.3206 0.5360 0.1157 0.0692 2.069 13.038 10.535 1542.605 1.473 46.861 3.098 0.52 220942. 0.4538
|
|
43.85 0.3562 0.5739 0.1130 0.0701 2.095 13.205 10.282 1562.354 1.492 45.735 2.985 0.52 221487. 0.4320
|
|
48.24 0.3919 0.6085 0.1098 0.0707 2.112 13.314 9.993 1575.221 1.504 44.449 2.877 0.52 222074. 0.4106
|
|
52.63 0.4275 0.6401 0.1062 0.0709 2.119 13.355 9.665 1580.021 1.509 42.992 2.775 0.52 222701. 0.3893
|
|
57.01 0.4631 0.6689 0.1021 0.0707 2.113 13.317 9.297 1575.560 1.505 41.355 2.677 0.52 223370. 0.3684
|
|
61.40 0.4987 0.6952 0.0976 0.0700 2.093 13.191 8.887 1560.707 1.490 39.530 2.583 0.52 224079. 0.3475
|
|
65.78 0.5343 0.7190 0.0927 0.0689 2.058 12.971 8.435 1534.599 1.465 37.520 2.493 0.52 224829. 0.3268
|
|
70.17 0.5700 0.7405 0.0873 0.0672 2.007 12.652 7.945 1496.939 1.429 35.338 2.407 0.52 225618. 0.3063
|
|
74.55 0.6056 0.7598 0.0815 0.0650 1.942 12.239 7.421 1448.005 1.383 33.010 2.325 0.53 226447. 0.2858
|
|
78.94 0.6412 0.7768 0.0755 0.0623 1.862 11.734 6.871 1388.325 1.326 30.561 2.245 0.53 227314. 0.2656
|
|
83.32 0.6768 0.7915 0.0692 0.0592 1.768 11.144 6.298 1318.428 1.259 28.014 2.167 0.53 228219. 0.2454
|
|
87.71 0.7125 0.8035 0.0627 0.0556 1.661 10.470 5.707 1238.754 1.183 25.386 2.090 0.53 229162. 0.2253
|
|
92.09 0.7481 0.8126 0.0560 0.0516 1.542 9.717 5.101 1149.648 1.098 22.691 2.013 0.53 230143. 0.2052
|
|
96.48 0.7837 0.8181 0.0493 0.0472 1.410 8.887 4.483 1051.389 1.004 19.942 1.934 0.53 231161. 0.1848
|
|
100.86 0.8193 0.8188 0.0424 0.0424 1.266 7.981 3.855 944.229 0.902 17.147 1.852 0.53 232216. 0.1641
|
|
105.25 0.8550 0.8132 0.0354 0.0372 1.111 7.002 3.219 828.429 0.791 14.317 1.762 0.53 233307. 0.1427
|
|
109.64 0.8906 0.7976 0.0283 0.0316 0.944 5.953 2.577 704.302 0.673 11.461 1.659 0.54 234434. 0.1202
|
|
114.02 0.9262 0.7652 0.0212 0.0257 0.767 4.837 1.931 572.248 0.546 8.590 1.531 0.54 235597. 0.0960
|
|
118.41 0.9618 0.6991 0.0141 0.0194 0.580 3.658 1.285 432.799 0.413 5.716 1.347 0.54 236795. 0.0689
|
|
122.79 0.9974 0.5463 0.0070 0.0129 0.384 2.423 0.641 286.652 0.274 2.853 1.015 0.54 238027. 0.0367
|
|
127.18 1.0331 0.0045 0.0000 0.0060 0.180 1.135 0.002 134.303 0.128 0.011 0.008 0.54 239271. 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 0.1285 0.0556 2.210 12.662 14.152 1647.925 1.431 62.949 3.895 0.57 239527. 0.6614
|
|
4.83 0.0356 0.0798 0.1279 0.0571 2.272 13.020 14.088 1694.496 1.471 62.664 3.771 0.57 239765. 0.6389
|
|
9.65 0.0713 0.1543 0.1272 0.0588 2.338 13.396 14.012 1743.426 1.513 62.326 3.645 0.57 240036. 0.6159
|
|
14.48 0.1069 0.2234 0.1264 0.0605 2.406 13.785 13.921 1793.963 1.557 61.921 3.520 0.57 240342. 0.5927
|
|
19.31 0.1426 0.2874 0.1254 0.0622 2.474 14.178 13.811 1845.196 1.602 61.433 3.395 0.57 240685. 0.5695
|
|
24.13 0.1782 0.3462 0.1242 0.0639 2.543 14.569 13.680 1896.013 1.646 60.847 3.272 0.57 241068. 0.5463
|
|
28.96 0.2139 0.4003 0.1228 0.0656 2.608 14.946 13.521 1945.142 1.689 60.143 3.153 0.57 241491. 0.5233
|
|
33.79 0.2495 0.4499 0.1211 0.0671 2.670 15.300 13.333 1991.164 1.729 59.304 3.037 0.57 241958. 0.5005
|
|
38.61 0.2851 0.4952 0.1190 0.0685 2.726 15.618 13.110 2032.575 1.765 58.313 2.925 0.57 242469. 0.4781
|
|
43.44 0.3208 0.5367 0.1167 0.0697 2.773 15.889 12.849 2067.817 1.795 57.152 2.818 0.57 243024. 0.4560
|
|
48.27 0.3564 0.5747 0.1139 0.0707 2.810 16.100 12.547 2095.305 1.819 55.808 2.716 0.57 243625. 0.4342
|
|
53.09 0.3921 0.6094 0.1108 0.0713 2.834 16.239 12.200 2113.448 1.835 54.265 2.618 0.57 244271. 0.4128
|
|
57.92 0.4277 0.6411 0.1072 0.0715 2.844 16.295 11.805 2120.635 1.841 52.511 2.525 0.57 244963. 0.3916
|
|
62.75 0.4634 0.6701 0.1032 0.0713 2.837 16.253 11.361 2115.244 1.836 50.532 2.436 0.57 245700. 0.3706
|
|
67.57 0.4990 0.6965 0.0986 0.0707 2.810 16.103 10.864 2095.745 1.819 48.322 2.351 0.57 246482. 0.3498
|
|
72.40 0.5347 0.7205 0.0937 0.0695 2.764 15.836 10.315 2060.954 1.789 45.881 2.270 0.58 247309. 0.3291
|
|
77.23 0.5703 0.7423 0.0882 0.0678 2.696 15.448 9.718 2010.448 1.745 43.226 2.192 0.58 248179. 0.3085
|
|
82.05 0.6059 0.7619 0.0824 0.0656 2.608 14.942 9.080 1944.596 1.688 40.389 2.118 0.58 249092. 0.2881
|
|
86.88 0.6416 0.7793 0.0763 0.0629 2.500 14.324 8.408 1864.120 1.618 37.401 2.046 0.58 250048. 0.2678
|
|
91.71 0.6772 0.7943 0.0700 0.0597 2.373 13.599 7.709 1769.755 1.536 34.289 1.976 0.58 251046. 0.2476
|
|
96.53 0.7129 0.8069 0.0634 0.0560 2.229 12.771 6.987 1662.110 1.443 31.077 1.907 0.58 252086. 0.2275
|
|
101.36 0.7485 0.8166 0.0567 0.0520 2.067 11.846 6.246 1541.665 1.338 27.782 1.838 0.58 253167. 0.2073
|
|
106.19 0.7842 0.8227 0.0498 0.0475 1.889 10.825 5.489 1408.802 1.223 24.417 1.767 0.58 254288. 0.1869
|
|
111.01 0.8198 0.8244 0.0429 0.0426 1.695 9.711 4.720 1263.863 1.097 20.996 1.694 0.59 255450. 0.1661
|
|
115.84 0.8554 0.8199 0.0358 0.0373 1.485 8.508 3.941 1107.202 0.961 17.530 1.614 0.59 256652. 0.1447
|
|
120.67 0.8911 0.8058 0.0286 0.0317 1.260 7.217 3.154 939.242 0.815 14.031 1.523 0.59 257894. 0.1221
|
|
125.49 0.9267 0.7754 0.0215 0.0256 1.020 5.844 2.363 760.524 0.660 10.512 1.409 0.59 259175. 0.0978
|
|
130.32 0.9624 0.7120 0.0143 0.0193 0.767 4.393 1.571 571.769 0.496 6.987 1.246 0.59 260494. 0.0705
|
|
135.15 0.9980 0.5616 0.0071 0.0126 0.501 2.873 0.781 373.928 0.325 3.476 0.948 0.60 261851. 0.0378
|
|
139.97 1.0337 -0.0047 0.0000 0.0057 0.225 1.288 -0.003 167.602 0.145 -0.013 -0.008 0.60 263217. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1290 0.0558 2.882 15.139 16.901 2149.368 1.710 75.176 3.567 0.62 261289. 0.6618
|
|
5.27 0.0357 0.0798 0.1284 0.0574 2.964 15.570 16.832 2210.504 1.759 74.868 3.454 0.62 261548. 0.6395
|
|
10.53 0.0713 0.1542 0.1278 0.0591 3.051 16.024 16.749 2274.985 1.810 74.500 3.339 0.62 261843. 0.6168
|
|
15.80 0.1070 0.2234 0.1270 0.0608 3.140 16.495 16.649 2341.849 1.864 74.056 3.225 0.62 262176. 0.5939
|
|
21.07 0.1426 0.2873 0.1261 0.0626 3.232 16.974 16.528 2409.908 1.918 73.517 3.111 0.62 262549. 0.5708
|
|
26.34 0.1783 0.3462 0.1250 0.0644 3.323 17.452 16.381 2477.689 1.972 72.861 2.999 0.62 262966. 0.5478
|
|
31.60 0.2139 0.4003 0.1236 0.0661 3.411 17.915 16.202 2543.481 2.024 72.066 2.889 0.62 263428. 0.5249
|
|
36.87 0.2496 0.4499 0.1220 0.0677 3.494 18.351 15.987 2605.366 2.073 71.110 2.783 0.62 263937. 0.5023
|
|
42.14 0.2852 0.4953 0.1200 0.0691 3.569 18.745 15.730 2661.282 2.118 69.968 2.681 0.62 264494. 0.4799
|
|
47.41 0.3209 0.5368 0.1177 0.0704 3.633 19.082 15.428 2709.098 2.156 68.622 2.583 0.62 265100. 0.4579
|
|
52.67 0.3566 0.5748 0.1150 0.0713 3.683 19.346 15.074 2746.657 2.186 67.050 2.489 0.62 265756. 0.4362
|
|
57.94 0.3922 0.6096 0.1119 0.0720 3.717 19.523 14.666 2771.812 2.206 65.236 2.400 0.62 266463. 0.4148
|
|
63.21 0.4279 0.6414 0.1083 0.0723 3.731 19.598 14.200 2782.417 2.214 63.162 2.315 0.62 267219. 0.3937
|
|
68.48 0.4635 0.6705 0.1043 0.0721 3.723 19.555 13.672 2776.320 2.209 60.815 2.234 0.63 268025. 0.3728
|
|
73.74 0.4992 0.6971 0.0998 0.0715 3.690 19.380 13.081 2751.494 2.190 58.184 2.156 0.63 268880. 0.3520
|
|
79.01 0.5348 0.7213 0.0948 0.0703 3.629 19.062 12.426 2706.362 2.154 55.270 2.082 0.63 269783. 0.3313
|
|
84.28 0.5705 0.7433 0.0894 0.0686 3.541 18.597 11.712 2640.324 2.101 52.094 2.012 0.63 270734. 0.3108
|
|
89.54 0.6061 0.7632 0.0835 0.0663 3.425 17.988 10.947 2553.854 2.032 48.692 1.944 0.63 271733. 0.2903
|
|
94.81 0.6418 0.7810 0.0774 0.0636 3.283 17.242 10.140 2447.922 1.948 45.104 1.879 0.63 272778. 0.2700
|
|
100.08 0.6775 0.7964 0.0710 0.0604 3.116 16.366 9.299 2323.528 1.849 41.363 1.815 0.63 273869. 0.2499
|
|
105.35 0.7131 0.8095 0.0643 0.0567 2.925 15.366 8.430 2181.506 1.736 37.498 1.753 0.63 275005. 0.2297
|
|
110.61 0.7488 0.8198 0.0575 0.0525 2.712 14.246 7.538 2022.508 1.609 33.529 1.691 0.64 276186. 0.2095
|
|
115.88 0.7844 0.8267 0.0506 0.0480 2.477 13.010 6.627 1847.051 1.470 29.475 1.627 0.64 277411. 0.1891
|
|
121.15 0.8201 0.8293 0.0435 0.0430 2.220 11.661 5.699 1655.589 1.317 25.351 1.561 0.64 278680. 0.1683
|
|
126.42 0.8557 0.8259 0.0363 0.0376 1.943 10.203 4.759 1448.585 1.153 21.170 1.490 0.64 279993. 0.1467
|
|
131.68 0.8914 0.8133 0.0291 0.0319 1.645 8.640 3.810 1226.599 0.976 16.947 1.409 0.64 281349. 0.1241
|
|
136.95 0.9270 0.7849 0.0218 0.0257 1.328 6.976 2.855 990.342 0.788 12.697 1.307 0.65 282748. 0.0997
|
|
142.22 0.9627 0.7243 0.0145 0.0192 0.993 5.218 1.897 740.771 0.589 8.439 1.162 0.65 284189. 0.0722
|
|
147.48 0.9984 0.5772 0.0072 0.0124 0.643 3.375 0.943 479.147 0.381 4.195 0.893 0.65 285670. 0.0391
|
|
152.75 1.0340 -0.0081 0.0000 0.0054 0.277 1.452 -0.005 206.194 0.164 -0.024 -0.012 0.65 287158. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 13000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1294 0.0564 3.704 17.958 19.905 2761.999 2.029 88.540 3.269 0.67 283049. 0.6583
|
|
5.71 0.0357 0.0793 0.1289 0.0580 3.808 18.464 19.833 2839.858 2.086 88.217 3.168 0.67 283328. 0.6367
|
|
11.42 0.0713 0.1534 0.1284 0.0597 3.919 19.000 19.746 2922.267 2.147 87.831 3.065 0.67 283646. 0.6147
|
|
17.12 0.1070 0.2223 0.1277 0.0615 4.034 19.557 19.641 3008.022 2.210 87.362 2.962 0.67 284005. 0.5924
|
|
22.83 0.1427 0.2861 0.1268 0.0632 4.151 20.127 19.511 3095.616 2.274 86.786 2.859 0.67 284409. 0.5700
|
|
28.54 0.1783 0.3450 0.1258 0.0650 4.269 20.696 19.352 3183.165 2.338 86.076 2.757 0.67 284859. 0.5475
|
|
34.25 0.2140 0.3991 0.1245 0.0668 4.383 21.251 19.156 3268.459 2.401 85.205 2.658 0.67 285358. 0.5251
|
|
39.95 0.2497 0.4488 0.1230 0.0684 4.491 21.774 18.917 3349.011 2.460 84.142 2.562 0.67 285909. 0.5029
|
|
45.66 0.2853 0.4943 0.1211 0.0699 4.589 22.250 18.629 3422.140 2.514 82.860 2.469 0.67 286512. 0.4810
|
|
51.37 0.3210 0.5359 0.1189 0.0712 4.674 22.659 18.285 3485.050 2.560 81.331 2.380 0.67 287170. 0.4593
|
|
57.08 0.3567 0.5741 0.1162 0.0722 4.740 22.983 17.880 3534.892 2.597 79.531 2.294 0.67 287881. 0.4379
|
|
62.79 0.3923 0.6090 0.1132 0.0729 4.786 23.203 17.409 3568.817 2.622 77.436 2.213 0.68 288648. 0.4167
|
|
68.49 0.4280 0.6410 0.1097 0.0732 4.806 23.302 16.867 3583.965 2.633 75.026 2.135 0.68 289468. 0.3957
|
|
74.20 0.4636 0.6702 0.1056 0.0731 4.797 23.260 16.251 3577.479 2.628 72.285 2.060 0.68 290343. 0.3749
|
|
79.91 0.4993 0.6970 0.1011 0.0725 4.756 23.059 15.557 3546.657 2.605 69.199 1.990 0.68 291271. 0.3542
|
|
85.62 0.5350 0.7214 0.0961 0.0713 4.679 22.687 14.787 3489.369 2.563 65.771 1.922 0.68 292252. 0.3336
|
|
91.32 0.5706 0.7437 0.0906 0.0696 4.566 22.137 13.944 3404.783 2.501 62.022 1.858 0.68 293285. 0.3131
|
|
97.03 0.6063 0.7639 0.0848 0.0673 4.417 21.413 13.039 3293.464 2.419 57.998 1.796 0.68 294369. 0.2927
|
|
102.74 0.6420 0.7820 0.0786 0.0645 4.233 20.524 12.083 3156.695 2.319 53.745 1.736 0.68 295503. 0.2724
|
|
108.45 0.6776 0.7979 0.0721 0.0612 4.017 19.478 11.085 2995.817 2.201 49.306 1.678 0.69 296687. 0.2522
|
|
114.16 0.7133 0.8115 0.0654 0.0574 3.771 18.283 10.052 2811.959 2.066 44.713 1.621 0.69 297920. 0.2320
|
|
119.86 0.7490 0.8223 0.0585 0.0532 3.495 16.944 8.991 2606.002 1.914 39.993 1.565 0.69 299202. 0.2118
|
|
125.57 0.7846 0.8300 0.0514 0.0486 3.190 15.465 7.907 2378.639 1.747 35.169 1.508 0.69 300531. 0.1913
|
|
131.28 0.8203 0.8335 0.0442 0.0435 2.857 13.852 6.802 2130.454 1.565 30.256 1.448 0.69 301908. 0.1705
|
|
136.99 0.8560 0.8312 0.0369 0.0380 2.497 12.106 5.682 1862.043 1.368 25.274 1.384 0.69 303333. 0.1489
|
|
142.69 0.8916 0.8201 0.0296 0.0322 2.111 10.235 4.550 1574.127 1.156 20.237 1.311 0.70 304803. 0.1262
|
|
148.40 0.9273 0.7937 0.0222 0.0259 1.700 8.242 3.410 1267.628 0.931 15.166 1.220 0.70 306320. 0.1017
|
|
154.11 0.9630 0.7359 0.0147 0.0193 1.266 6.136 2.267 943.814 0.693 10.082 1.089 0.70 307882. 0.0740
|
|
159.82 0.9986 0.5922 0.0073 0.0123 0.811 3.930 1.127 604.485 0.444 5.011 0.845 0.70 309488. 0.0405
|
|
165.53 1.0343 -0.0103 -0.0001 0.0051 0.336 1.631 -0.008 250.829 0.184 -0.035 -0.014 0.71 311097. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1298 0.0578 4.743 21.352 23.163 3536.702 2.412 103.028 2.971 0.72 304805. 0.6453
|
|
6.15 0.0357 0.0777 0.1294 0.0594 4.872 21.935 23.089 3633.228 2.478 102.701 2.882 0.72 305105. 0.6252
|
|
12.29 0.0713 0.1505 0.1289 0.0611 5.010 22.553 23.002 3735.649 2.548 102.311 2.793 0.72 305445. 0.6046
|
|
18.44 0.1070 0.2185 0.1283 0.0628 5.153 23.198 22.894 3842.446 2.621 101.834 2.702 0.72 305830. 0.5836
|
|
24.59 0.1427 0.2816 0.1276 0.0646 5.299 23.858 22.761 3951.674 2.695 101.242 2.613 0.72 306263. 0.5626
|
|
30.74 0.1783 0.3401 0.1267 0.0664 5.446 24.517 22.595 4060.887 2.770 100.502 2.524 0.72 306746. 0.5414
|
|
36.88 0.2140 0.3940 0.1255 0.0682 5.588 25.159 22.387 4167.215 2.842 99.579 2.437 0.72 307282. 0.5204
|
|
43.03 0.2497 0.4437 0.1241 0.0698 5.723 25.764 22.130 4267.479 2.911 98.435 2.352 0.72 307874. 0.4994
|
|
49.18 0.2854 0.4895 0.1223 0.0713 5.845 26.312 21.815 4358.275 2.973 97.034 2.270 0.72 308523. 0.4786
|
|
55.33 0.3210 0.5316 0.1202 0.0726 5.949 26.782 21.434 4436.093 3.026 95.341 2.192 0.73 309231. 0.4580
|
|
61.47 0.3567 0.5702 0.1176 0.0736 6.031 27.152 20.981 4497.396 3.068 93.322 2.116 0.73 309998. 0.4375
|
|
67.62 0.3924 0.6058 0.1146 0.0742 6.086 27.401 20.447 4538.679 3.096 90.949 2.043 0.73 310824. 0.4170
|
|
73.77 0.4280 0.6383 0.1111 0.0745 6.110 27.509 19.829 4556.437 3.108 88.198 1.974 0.73 311709. 0.3967
|
|
79.92 0.4637 0.6682 0.1072 0.0744 6.098 27.453 19.120 4547.151 3.102 85.046 1.907 0.73 312653. 0.3764
|
|
86.06 0.4994 0.6955 0.1027 0.0737 6.045 27.213 18.318 4507.419 3.074 81.479 1.843 0.73 313655. 0.3561
|
|
92.21 0.5350 0.7204 0.0977 0.0725 5.947 26.772 17.423 4434.464 3.025 77.497 1.782 0.73 314713. 0.3357
|
|
98.36 0.5707 0.7431 0.0922 0.0708 5.803 26.124 16.441 4327.039 2.951 73.127 1.723 0.73 315828. 0.3154
|
|
104.51 0.6064 0.7637 0.0862 0.0685 5.613 25.270 15.383 4185.632 2.855 68.422 1.667 0.74 316998. 0.2951
|
|
110.65 0.6420 0.7822 0.0799 0.0656 5.380 24.220 14.262 4011.696 2.736 63.438 1.613 0.74 318222. 0.2749
|
|
116.80 0.6777 0.7986 0.0734 0.0623 5.105 22.983 13.090 3806.854 2.597 58.226 1.560 0.74 319500. 0.2547
|
|
122.95 0.7134 0.8127 0.0666 0.0584 4.791 21.568 11.876 3572.531 2.437 52.826 1.508 0.74 320830. 0.2345
|
|
129.10 0.7490 0.8242 0.0596 0.0541 4.439 19.983 10.627 3309.875 2.258 47.271 1.456 0.74 322212. 0.2143
|
|
135.24 0.7847 0.8326 0.0524 0.0494 4.050 18.232 9.350 3019.805 2.060 41.587 1.404 0.74 323646. 0.1938
|
|
141.39 0.8204 0.8370 0.0451 0.0442 3.625 16.319 8.048 2703.076 1.844 35.795 1.350 0.75 325131. 0.1729
|
|
147.54 0.8561 0.8359 0.0377 0.0386 3.165 14.251 6.726 2360.471 1.610 29.915 1.292 0.75 326666. 0.1513
|
|
153.69 0.8917 0.8262 0.0302 0.0326 2.673 12.033 5.388 1993.060 1.359 23.967 1.226 0.75 328251. 0.1285
|
|
159.83 0.9274 0.8014 0.0226 0.0262 2.149 9.674 4.040 1602.426 1.093 17.972 1.144 0.75 329886. 0.1038
|
|
165.98 0.9631 0.7449 0.0151 0.0195 1.597 7.190 2.688 1190.878 0.812 11.955 1.024 0.76 331569. 0.0758
|
|
172.13 0.9987 0.6007 0.0075 0.0125 1.021 4.598 1.337 761.589 0.519 5.946 0.796 0.76 333299. 0.0415
|
|
178.28 1.0344 -0.0110 -0.0001 0.0052 0.425 1.913 -0.010 316.908 0.216 -0.044 -0.014 0.76 335031. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1302 0.0608 6.127 25.744 26.665 4568.739 2.909 118.608 2.647 0.77 326559. 0.6170
|
|
6.59 0.0357 0.0743 0.1299 0.0623 6.284 26.405 26.593 4686.060 2.983 118.286 2.574 0.77 326878. 0.5991
|
|
13.17 0.0713 0.1443 0.1294 0.0640 6.451 27.108 26.507 4810.859 3.063 117.904 2.499 0.77 327240. 0.5807
|
|
19.76 0.1070 0.2099 0.1289 0.0657 6.626 27.843 26.402 4941.195 3.146 117.437 2.424 0.77 327650. 0.5621
|
|
26.34 0.1427 0.2712 0.1283 0.0675 6.805 28.594 26.271 5074.472 3.231 116.854 2.348 0.77 328111. 0.5432
|
|
32.93 0.1783 0.3282 0.1275 0.0693 6.983 29.342 26.105 5207.346 3.315 116.114 2.274 0.77 328626. 0.5244
|
|
39.51 0.2140 0.3813 0.1264 0.0710 7.156 30.067 25.893 5335.906 3.397 115.174 2.201 0.78 329198. 0.5055
|
|
46.10 0.2496 0.4305 0.1251 0.0726 7.316 30.743 25.627 5455.848 3.473 113.987 2.130 0.78 329830. 0.4868
|
|
52.68 0.2853 0.4763 0.1235 0.0740 7.460 31.345 25.293 5562.744 3.541 112.505 2.062 0.78 330523. 0.4682
|
|
59.27 0.3210 0.5188 0.1215 0.0752 7.580 31.849 24.883 5652.188 3.598 110.682 1.997 0.78 331280. 0.4496
|
|
65.85 0.3566 0.5583 0.1191 0.0761 7.671 32.231 24.387 5719.905 3.641 108.475 1.934 0.78 332102. 0.4310
|
|
72.44 0.3923 0.5949 0.1162 0.0766 7.727 32.467 23.796 5761.798 3.668 105.846 1.873 0.78 332987. 0.4125
|
|
79.03 0.4280 0.6288 0.1128 0.0768 7.743 32.535 23.103 5773.931 3.676 102.764 1.815 0.78 333937. 0.3937
|
|
85.61 0.4636 0.6600 0.1089 0.0765 7.714 32.414 22.303 5752.420 3.662 99.202 1.759 0.78 334950. 0.3748
|
|
92.20 0.4993 0.6887 0.1044 0.0757 7.635 32.082 21.389 5693.476 3.625 95.140 1.704 0.78 336025. 0.3557
|
|
98.78 0.5349 0.7150 0.0994 0.0744 7.502 31.521 20.364 5593.947 3.561 90.578 1.651 0.78 337162. 0.3363
|
|
105.37 0.5706 0.7390 0.0939 0.0725 7.312 30.723 19.233 5452.398 3.471 85.548 1.600 0.79 338359. 0.3167
|
|
111.95 0.6063 0.7608 0.0879 0.0701 7.066 29.693 18.010 5269.466 3.355 80.109 1.550 0.79 339615. 0.2969
|
|
118.54 0.6419 0.7805 0.0816 0.0671 6.768 28.438 16.711 5046.845 3.213 74.330 1.502 0.79 340928. 0.2771
|
|
125.12 0.6776 0.7978 0.0749 0.0637 6.419 26.970 15.349 4786.384 3.047 68.270 1.454 0.79 342300. 0.2572
|
|
131.71 0.7133 0.8128 0.0680 0.0597 6.021 25.299 13.935 4489.702 2.858 61.981 1.408 0.79 343727. 0.2372
|
|
138.29 0.7489 0.8252 0.0609 0.0553 5.576 23.430 12.478 4158.010 2.647 55.500 1.361 0.80 345210. 0.2170
|
|
144.88 0.7846 0.8345 0.0536 0.0504 5.086 21.369 10.985 3792.355 2.414 48.861 1.314 0.80 346748. 0.1965
|
|
151.46 0.8202 0.8397 0.0462 0.0451 4.551 19.125 9.462 3394.017 2.161 42.088 1.265 0.80 348341. 0.1756
|
|
158.05 0.8559 0.8391 0.0386 0.0394 3.975 16.703 7.914 2964.309 1.887 35.203 1.211 0.80 349987. 0.1538
|
|
164.64 0.8916 0.8292 0.0310 0.0333 3.360 14.118 6.346 2505.495 1.595 28.229 1.149 0.80 351686. 0.1306
|
|
171.22 0.9272 0.8026 0.0233 0.0269 2.710 11.387 4.763 2020.772 1.286 21.188 1.069 0.81 353438. 0.1053
|
|
177.81 0.9629 0.7406 0.0155 0.0201 2.031 8.533 3.172 1514.378 0.964 14.109 0.950 0.81 355242. 0.0764
|
|
184.39 0.9986 0.5838 0.0077 0.0132 1.330 5.588 1.579 991.661 0.631 7.024 0.722 0.81 357096. 0.0410
|
|
190.98 1.0342 -0.0097 -0.0001 0.0061 0.613 2.575 -0.012 456.942 0.291 -0.052 -0.012 0.81 358955. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1305 0.0659 8.066 31.776 30.396 6015.131 3.590 135.203 2.292 0.83 348308. 0.5704
|
|
7.03 0.0357 0.0688 0.1301 0.0675 8.255 32.520 30.325 6155.928 3.674 134.885 2.234 0.83 348646. 0.5554
|
|
14.05 0.0713 0.1340 0.1298 0.0691 8.457 33.314 30.242 6306.330 3.764 134.517 2.175 0.83 349031. 0.5399
|
|
21.08 0.1070 0.1954 0.1294 0.0708 8.668 34.147 30.143 6463.911 3.858 134.074 2.115 0.83 349466. 0.5241
|
|
28.10 0.1427 0.2532 0.1288 0.0726 8.884 34.998 30.018 6625.157 3.954 133.519 2.055 0.83 349954. 0.5082
|
|
35.13 0.1783 0.3073 0.1281 0.0744 9.100 35.846 29.858 6785.621 4.050 132.810 1.996 0.83 350500. 0.4922
|
|
42.15 0.2140 0.3581 0.1273 0.0760 9.306 36.659 29.652 6939.580 4.142 131.894 1.938 0.83 351106. 0.4763
|
|
49.18 0.2497 0.4058 0.1261 0.0776 9.495 37.405 29.386 7080.661 4.226 130.711 1.882 0.83 351777. 0.4606
|
|
56.20 0.2853 0.4507 0.1247 0.0789 9.658 38.047 29.046 7202.292 4.299 129.198 1.829 0.83 352515. 0.4450
|
|
63.23 0.3210 0.4930 0.1228 0.0800 9.787 38.555 28.619 7298.485 4.356 127.297 1.779 0.83 353321. 0.4294
|
|
70.25 0.3567 0.5329 0.1206 0.0807 9.875 38.901 28.091 7363.970 4.395 124.950 1.730 0.83 354196. 0.4139
|
|
77.28 0.3923 0.5705 0.1178 0.0810 9.916 39.061 27.452 7394.123 4.413 122.108 1.684 0.83 355141. 0.3982
|
|
84.31 0.4280 0.6059 0.1146 0.0809 9.903 39.011 26.692 7384.765 4.407 118.728 1.639 0.83 356156. 0.3823
|
|
91.33 0.4637 0.6391 0.1107 0.0803 9.832 38.732 25.803 7331.934 4.376 114.772 1.596 0.83 357238. 0.3660
|
|
98.36 0.4993 0.6701 0.1063 0.0792 9.698 38.205 24.779 7232.148 4.316 110.218 1.554 0.84 358389. 0.3492
|
|
105.38 0.5350 0.6988 0.1014 0.0776 9.498 37.415 23.620 7082.621 4.227 105.062 1.513 0.84 359605. 0.3318
|
|
112.41 0.5707 0.7253 0.0958 0.0754 9.229 36.357 22.333 6882.402 4.108 99.338 1.472 0.84 360885. 0.3139
|
|
119.43 0.6064 0.7495 0.0898 0.0727 8.895 35.040 20.935 6632.987 3.959 93.118 1.432 0.84 362229. 0.2956
|
|
126.46 0.6420 0.7715 0.0834 0.0694 8.498 33.477 19.443 6337.083 3.782 86.484 1.392 0.84 363635. 0.2770
|
|
133.48 0.6777 0.7911 0.0767 0.0657 8.042 31.681 17.875 5997.209 3.579 79.507 1.352 0.84 365101. 0.2580
|
|
140.51 0.7134 0.8082 0.0697 0.0615 7.530 29.662 16.242 5614.997 3.351 72.246 1.312 0.85 366628. 0.2387
|
|
147.53 0.7490 0.8225 0.0625 0.0569 6.962 27.426 14.557 5191.709 3.099 64.747 1.272 0.85 368213. 0.2190
|
|
154.56 0.7847 0.8337 0.0550 0.0518 6.341 24.979 12.826 4728.446 2.822 57.051 1.230 0.85 369858. 0.1989
|
|
161.59 0.8204 0.8391 0.0475 0.0464 5.677 22.365 11.057 4233.651 2.527 49.182 1.185 0.85 371559. 0.1778
|
|
168.61 0.8560 0.8367 0.0397 0.0406 4.974 19.592 9.255 3708.740 2.213 41.166 1.132 0.86 373318. 0.1554
|
|
175.64 0.8917 0.8222 0.0319 0.0346 4.230 16.664 7.426 3154.389 1.883 33.033 1.068 0.86 375133. 0.1313
|
|
182.66 0.9274 0.7864 0.0239 0.0282 3.454 13.608 5.577 2576.020 1.537 24.807 0.982 0.86 377004. 0.1047
|
|
189.69 0.9630 0.7072 0.0159 0.0217 2.656 10.465 3.714 1980.948 1.182 16.522 0.850 0.86 378930. 0.0740
|
|
196.71 0.9987 0.5246 0.0079 0.0151 1.848 7.279 1.848 1377.826 0.822 8.219 0.608 0.87 380908. 0.0373
|
|
203.74 1.0344 -0.0087 -0.0001 0.0085 1.037 4.086 -0.017 773.479 0.462 -0.074 -0.010 0.87 382903. 0.0000
|
|
|
|
|
|
|