686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
12x12E (12x12E.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 0.1184 0.0698 0.001 0.088 0.078 1.043 0.010 0.348 34.019 0.05 14747. 0.4652
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0.45 0.0398 0.0661 0.1179 0.0710 0.001 0.090 0.078 1.061 0.010 0.347 33.311 0.05 14763. 0.4546
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0.90 0.0796 0.1291 0.1174 0.0724 0.001 0.091 0.078 1.081 0.010 0.345 32.559 0.05 14782. 0.4434
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1.36 0.1194 0.1890 0.1168 0.0738 0.001 0.093 0.077 1.102 0.011 0.343 31.768 0.05 14803. 0.4316
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1.81 0.1592 0.2454 0.1162 0.0754 0.002 0.095 0.077 1.125 0.011 0.341 30.943 0.05 14827. 0.4192
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2.26 0.1990 0.2983 0.1154 0.0770 0.002 0.097 0.076 1.150 0.011 0.339 30.092 0.05 14854. 0.4064
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2.71 0.2388 0.3477 0.1145 0.0787 0.002 0.099 0.076 1.175 0.011 0.337 29.223 0.05 14884. 0.3931
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3.17 0.2786 0.3934 0.1135 0.0804 0.002 0.101 0.075 1.200 0.011 0.334 28.344 0.05 14918. 0.3795
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3.62 0.3184 0.4357 0.1122 0.0820 0.002 0.103 0.074 1.224 0.012 0.330 27.463 0.05 14955. 0.3656
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4.07 0.3582 0.4745 0.1107 0.0835 0.002 0.105 0.073 1.247 0.012 0.325 26.587 0.05 14995. 0.3515
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4.52 0.3980 0.5100 0.1088 0.0849 0.002 0.107 0.072 1.268 0.012 0.320 25.721 0.05 15039. 0.3372
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4.98 0.4378 0.5425 0.1066 0.0860 0.002 0.109 0.070 1.285 0.012 0.313 24.872 0.05 15086. 0.3228
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5.43 0.4776 0.5721 0.1040 0.0868 0.002 0.110 0.069 1.296 0.012 0.306 24.042 0.05 15138. 0.3082
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5.88 0.5174 0.5989 0.1009 0.0872 0.002 0.110 0.067 1.302 0.012 0.297 23.234 0.05 15192. 0.2934
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6.33 0.5572 0.6231 0.0974 0.0871 0.002 0.110 0.064 1.301 0.012 0.286 22.447 0.05 15251. 0.2785
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6.78 0.5970 0.6448 0.0934 0.0865 0.002 0.109 0.062 1.291 0.012 0.275 21.680 0.05 15313. 0.2634
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7.24 0.6369 0.6640 0.0889 0.0852 0.002 0.108 0.059 1.273 0.012 0.261 20.928 0.05 15379. 0.2480
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7.69 0.6767 0.6804 0.0838 0.0834 0.002 0.105 0.055 1.245 0.012 0.246 20.184 0.05 15448. 0.2323
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8.14 0.7165 0.6937 0.0783 0.0808 0.002 0.102 0.052 1.207 0.012 0.230 19.437 0.05 15521. 0.2161
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8.59 0.7563 0.7035 0.0722 0.0776 0.002 0.098 0.048 1.159 0.011 0.212 18.673 0.05 15597. 0.1995
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9.05 0.7961 0.7090 0.0658 0.0738 0.001 0.093 0.043 1.102 0.011 0.193 17.877 0.05 15677. 0.1822
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9.50 0.8359 0.7089 0.0590 0.0695 0.001 0.088 0.039 1.038 0.010 0.173 17.025 0.05 15760. 0.1643
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9.95 0.8757 0.7019 0.0519 0.0648 0.001 0.082 0.034 0.967 0.009 0.153 16.091 0.05 15845. 0.1457
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10.40 0.9155 0.6859 0.0447 0.0596 0.001 0.075 0.030 0.890 0.008 0.131 15.039 0.05 15934. 0.1263
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10.86 0.9553 0.6578 0.0373 0.0541 0.001 0.068 0.025 0.808 0.008 0.109 13.822 0.05 16027. 0.1060
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11.31 0.9951 0.6130 0.0298 0.0483 0.001 0.061 0.020 0.721 0.007 0.087 12.365 0.05 16122. 0.0848
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11.76 1.0349 0.5442 0.0222 0.0423 0.001 0.053 0.015 0.631 0.006 0.065 10.555 0.05 16220. 0.0625
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12.21 1.0747 0.4388 0.0147 0.0360 0.001 0.045 0.010 0.538 0.005 0.043 8.196 0.05 16321. 0.0395
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12.66 1.1145 0.2736 0.0073 0.0296 0.001 0.037 0.005 0.443 0.004 0.021 4.928 0.05 16425. 0.0167
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13.12 1.1543 0.0001 0.0000 0.0232 0.000 0.029 0.000 0.346 0.003 0.000 0.002 0.05 16532. 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 0.1188 0.0645 0.010 0.326 0.314 7.710 0.037 1.396 18.467 0.10 29494. 0.5059
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0.91 0.0401 0.0721 0.1183 0.0658 0.011 0.332 0.313 7.858 0.038 1.391 18.051 0.10 29527. 0.4936
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1.82 0.0802 0.1406 0.1178 0.0672 0.011 0.339 0.311 8.023 0.038 1.385 17.609 0.10 29564. 0.4805
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2.73 0.1202 0.2054 0.1173 0.0687 0.011 0.347 0.310 8.203 0.039 1.379 17.145 0.10 29607. 0.4668
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3.64 0.1603 0.2662 0.1167 0.0703 0.011 0.355 0.308 8.395 0.040 1.372 16.663 0.10 29656. 0.4525
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4.55 0.2004 0.3228 0.1160 0.0720 0.012 0.363 0.307 8.599 0.041 1.363 16.168 0.10 29710. 0.4377
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5.47 0.2405 0.3753 0.1151 0.0737 0.012 0.372 0.304 8.809 0.042 1.353 15.664 0.10 29771. 0.4225
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6.38 0.2805 0.4236 0.1140 0.0755 0.012 0.381 0.301 9.021 0.043 1.341 15.157 0.10 29839. 0.4069
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7.29 0.3206 0.4680 0.1128 0.0773 0.012 0.390 0.298 9.229 0.044 1.326 14.650 0.10 29913. 0.3911
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8.20 0.3607 0.5085 0.1112 0.0789 0.013 0.398 0.294 9.425 0.045 1.308 14.150 0.10 29995. 0.3752
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9.11 0.4008 0.5454 0.1094 0.0804 0.013 0.406 0.289 9.601 0.046 1.286 13.658 0.10 30084. 0.3591
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10.02 0.4408 0.5789 0.1072 0.0816 0.013 0.412 0.283 9.748 0.047 1.260 13.180 0.10 30180. 0.3430
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10.93 0.4809 0.6093 0.1045 0.0825 0.013 0.417 0.276 9.856 0.047 1.229 12.715 0.10 30284. 0.3268
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11.84 0.5210 0.6368 0.1014 0.0830 0.013 0.419 0.268 9.914 0.047 1.193 12.267 0.10 30395. 0.3106
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12.75 0.5611 0.6616 0.0979 0.0830 0.013 0.419 0.259 9.914 0.047 1.151 11.835 0.10 30514. 0.2943
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13.66 0.6012 0.6839 0.0938 0.0824 0.013 0.416 0.248 9.846 0.047 1.102 11.418 0.10 30640. 0.2779
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14.57 0.6412 0.7037 0.0891 0.0812 0.013 0.410 0.236 9.704 0.046 1.048 11.014 0.10 30773. 0.2614
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15.48 0.6813 0.7209 0.0840 0.0794 0.013 0.401 0.222 9.482 0.045 0.988 10.620 0.10 30913. 0.2447
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16.40 0.7214 0.7354 0.0783 0.0768 0.012 0.388 0.207 9.179 0.044 0.921 10.232 0.10 31061. 0.2277
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17.31 0.7615 0.7467 0.0722 0.0736 0.012 0.372 0.191 8.794 0.042 0.849 9.842 0.10 31215. 0.2102
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18.22 0.8015 0.7542 0.0656 0.0698 0.011 0.352 0.174 8.334 0.040 0.772 9.444 0.10 31376. 0.1924
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19.13 0.8416 0.7569 0.0588 0.0654 0.010 0.330 0.155 7.807 0.037 0.691 9.026 0.10 31543. 0.1740
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20.04 0.8817 0.7535 0.0517 0.0605 0.010 0.305 0.137 7.222 0.034 0.607 8.577 0.10 31717. 0.1550
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20.95 0.9218 0.7419 0.0444 0.0551 0.009 0.278 0.117 6.586 0.031 0.522 8.079 0.10 31898. 0.1353
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21.86 0.9618 0.7193 0.0370 0.0494 0.008 0.250 0.098 5.904 0.028 0.435 7.506 0.10 32084. 0.1147
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22.77 1.0019 0.6807 0.0295 0.0434 0.007 0.219 0.078 5.182 0.025 0.347 6.819 0.10 32277. 0.0931
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23.68 1.0420 0.6178 0.0220 0.0371 0.006 0.187 0.058 4.428 0.021 0.258 5.951 0.10 32476. 0.0701
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24.59 1.0821 0.5150 0.0145 0.0305 0.005 0.154 0.038 3.646 0.017 0.171 4.776 0.10 32680. 0.0458
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25.50 1.1221 0.3386 0.0072 0.0238 0.004 0.120 0.019 2.847 0.014 0.085 3.029 0.10 32891. 0.0204
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26.41 1.1622 0.0026 0.0000 0.0170 0.003 0.086 0.000 2.036 0.010 0.000 0.023 0.10 33107. 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 0.1190 0.0622 0.034 0.707 0.708 25.092 0.080 3.147 12.790 0.14 44241. 0.5261
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1.37 0.0402 0.0751 0.1185 0.0635 0.034 0.721 0.705 25.602 0.081 3.136 12.491 0.14 44290. 0.5128
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2.74 0.0804 0.1463 0.1181 0.0649 0.035 0.737 0.702 26.166 0.083 3.124 12.173 0.14 44347. 0.4988
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4.11 0.1206 0.2135 0.1176 0.0664 0.036 0.755 0.699 26.783 0.085 3.110 11.841 0.14 44411. 0.4841
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5.48 0.1609 0.2764 0.1170 0.0681 0.037 0.773 0.696 27.447 0.087 3.094 11.496 0.14 44484. 0.4688
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6.85 0.2011 0.3348 0.1163 0.0698 0.038 0.793 0.691 28.148 0.090 3.075 11.141 0.14 44566. 0.4530
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8.23 0.2413 0.3888 0.1154 0.0716 0.039 0.814 0.686 28.874 0.092 3.053 10.782 0.14 44658. 0.4368
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9.60 0.2815 0.4384 0.1144 0.0734 0.040 0.834 0.680 29.609 0.094 3.026 10.420 0.14 44760. 0.4202
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10.97 0.3217 0.4837 0.1131 0.0752 0.041 0.855 0.673 30.330 0.097 2.992 10.060 0.14 44873. 0.4035
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12.34 0.3619 0.5250 0.1116 0.0769 0.042 0.874 0.664 31.012 0.099 2.952 9.706 0.14 44996. 0.3866
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13.71 0.4021 0.5625 0.1097 0.0785 0.042 0.891 0.653 31.628 0.101 2.903 9.358 0.14 45130. 0.3697
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15.08 0.4424 0.5964 0.1075 0.0797 0.043 0.906 0.639 32.144 0.102 2.844 9.021 0.14 45276. 0.3527
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16.45 0.4826 0.6271 0.1049 0.0807 0.044 0.916 0.624 32.528 0.104 2.774 8.695 0.14 45432. 0.3358
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17.82 0.5228 0.6549 0.1017 0.0812 0.044 0.923 0.605 32.744 0.104 2.692 8.382 0.14 45600. 0.3188
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19.19 0.5630 0.6800 0.0981 0.0813 0.044 0.923 0.584 32.760 0.104 2.596 8.081 0.15 45779. 0.3019
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20.56 0.6032 0.7025 0.0940 0.0807 0.044 0.917 0.559 32.544 0.104 2.487 7.793 0.15 45969. 0.2849
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21.93 0.6434 0.7227 0.0893 0.0796 0.043 0.904 0.531 32.071 0.102 2.364 7.515 0.15 46170. 0.2679
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23.31 0.6836 0.7404 0.0841 0.0777 0.042 0.883 0.500 31.327 0.100 2.226 7.246 0.15 46382. 0.2507
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24.68 0.7239 0.7554 0.0784 0.0752 0.041 0.854 0.466 30.299 0.096 2.075 6.983 0.15 46605. 0.2332
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26.05 0.7641 0.7676 0.0722 0.0719 0.039 0.817 0.430 28.989 0.092 1.911 6.722 0.15 46838. 0.2154
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27.42 0.8043 0.7762 0.0656 0.0680 0.037 0.773 0.390 27.419 0.087 1.736 6.457 0.15 47081. 0.1973
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28.79 0.8445 0.7805 0.0587 0.0635 0.034 0.722 0.349 25.618 0.082 1.553 6.184 0.15 47333. 0.1787
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30.16 0.8847 0.7791 0.0516 0.0586 0.032 0.665 0.307 23.612 0.075 1.364 5.892 0.15 47596. 0.1596
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31.53 0.9249 0.7703 0.0443 0.0531 0.029 0.604 0.263 21.425 0.068 1.171 5.572 0.15 47868. 0.1398
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32.90 0.9651 0.7510 0.0368 0.0473 0.026 0.537 0.219 19.077 0.061 0.974 5.207 0.15 48150. 0.1191
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34.27 1.0053 0.7166 0.0293 0.0411 0.022 0.467 0.174 16.589 0.053 0.776 4.769 0.15 48440. 0.0974
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35.64 1.0456 0.6583 0.0218 0.0347 0.019 0.394 0.130 13.983 0.045 0.578 4.213 0.15 48740. 0.0742
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37.02 1.0858 0.5589 0.0144 0.0280 0.015 0.318 0.086 11.283 0.036 0.381 3.444 0.15 49049. 0.0493
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38.39 1.1260 0.3785 0.0071 0.0211 0.011 0.240 0.042 8.517 0.027 0.188 2.249 0.15 49367. 0.0226
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39.76 1.1662 -0.0003 0.0000 0.0142 0.008 0.161 0.000 5.716 0.018 0.000 -0.002 0.15 49693. 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 0.1191 0.0609 0.078 1.230 1.260 58.220 0.139 5.603 9.813 0.19 58988. 0.5385
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1.83 0.0403 0.0769 0.1187 0.0622 0.080 1.256 1.255 59.438 0.142 5.583 9.579 0.19 59053. 0.5248
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3.66 0.0806 0.1498 0.1183 0.0636 0.082 1.285 1.251 60.790 0.145 5.562 9.330 0.19 59129. 0.5102
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5.49 0.1209 0.2185 0.1178 0.0652 0.084 1.316 1.245 62.268 0.149 5.539 9.070 0.19 59215. 0.4949
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7.33 0.1612 0.2826 0.1172 0.0668 0.086 1.349 1.239 63.861 0.152 5.511 8.800 0.19 59312. 0.4790
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9.16 0.2015 0.3422 0.1165 0.0686 0.088 1.385 1.232 65.546 0.156 5.479 8.523 0.19 59422. 0.4625
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10.99 0.2417 0.3971 0.1157 0.0704 0.090 1.422 1.223 67.293 0.161 5.439 8.242 0.19 59545. 0.4457
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12.82 0.2820 0.4474 0.1146 0.0723 0.093 1.459 1.212 69.064 0.165 5.391 7.960 0.19 59682. 0.4285
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14.65 0.3223 0.4933 0.1134 0.0741 0.095 1.496 1.199 70.805 0.169 5.333 7.680 0.19 59832. 0.4112
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16.48 0.3626 0.5350 0.1119 0.0758 0.097 1.531 1.183 72.458 0.173 5.261 7.404 0.19 59997. 0.3938
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18.31 0.4029 0.5729 0.1100 0.0774 0.099 1.563 1.163 73.952 0.177 5.174 7.135 0.19 60177. 0.3763
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20.15 0.4432 0.6071 0.1078 0.0787 0.101 1.589 1.140 75.212 0.180 5.070 6.874 0.19 60371. 0.3588
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21.98 0.4835 0.6380 0.1052 0.0797 0.102 1.609 1.112 76.157 0.182 4.946 6.622 0.19 60581. 0.3414
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23.81 0.5238 0.6659 0.1020 0.0803 0.103 1.621 1.079 76.702 0.183 4.799 6.380 0.19 60805. 0.3241
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25.64 0.5641 0.6912 0.0984 0.0803 0.103 1.622 1.041 76.767 0.183 4.629 6.149 0.19 61045. 0.3067
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27.47 0.6044 0.7139 0.0943 0.0798 0.102 1.612 0.997 76.276 0.182 4.434 5.928 0.19 61299. 0.2894
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29.30 0.6447 0.7342 0.0896 0.0787 0.101 1.588 0.947 75.171 0.179 4.213 5.716 0.19 61569. 0.2720
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31.13 0.6849 0.7523 0.0844 0.0768 0.098 1.551 0.892 73.410 0.175 3.968 5.511 0.19 61852. 0.2545
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32.97 0.7252 0.7677 0.0786 0.0743 0.095 1.500 0.831 70.967 0.169 3.697 5.312 0.20 62150. 0.2368
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34.80 0.7655 0.7805 0.0724 0.0710 0.091 1.434 0.765 67.844 0.162 3.404 5.116 0.20 62461. 0.2188
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36.63 0.8058 0.7899 0.0657 0.0671 0.086 1.354 0.695 64.094 0.153 3.092 4.919 0.20 62787. 0.2005
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38.46 0.8461 0.7953 0.0588 0.0626 0.080 1.263 0.622 59.784 0.143 2.765 4.717 0.20 63125. 0.1819
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40.29 0.8864 0.7954 0.0516 0.0575 0.074 1.162 0.546 54.976 0.131 2.428 4.503 0.20 63476. 0.1627
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42.12 0.9267 0.7885 0.0443 0.0520 0.067 1.051 0.468 49.726 0.119 2.082 4.270 0.20 63840. 0.1429
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43.95 0.9670 0.7718 0.0368 0.0461 0.059 0.931 0.389 44.082 0.105 1.732 4.006 0.20 64217. 0.1222
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45.79 1.0073 0.7406 0.0293 0.0399 0.051 0.805 0.310 38.096 0.091 1.378 3.690 0.20 64606. 0.1004
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47.62 1.0476 0.6861 0.0218 0.0333 0.043 0.672 0.231 31.821 0.076 1.026 3.287 0.20 65007. 0.0772
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49.45 1.0879 0.5904 0.0144 0.0265 0.034 0.535 0.152 25.317 0.060 0.676 2.723 0.20 65420. 0.0519
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51.28 1.1281 0.4093 0.0071 0.0195 0.025 0.394 0.075 18.651 0.045 0.333 1.821 0.20 65846. 0.0244
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53.11 1.1684 -0.0007 0.0000 0.0125 0.016 0.251 0.000 11.902 0.028 0.000 -0.003 0.20 66282. 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 0.1193 0.0601 0.150 1.896 1.971 112.150 0.214 8.765 7.970 0.24 73734. 0.5471
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2.29 0.0403 0.0782 0.1189 0.0614 0.154 1.936 1.964 114.545 0.219 8.736 7.777 0.24 73816. 0.5329
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4.58 0.0807 0.1522 0.1185 0.0628 0.157 1.981 1.957 117.204 0.224 8.704 7.573 0.24 73911. 0.5180
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6.88 0.1210 0.2219 0.1180 0.0644 0.161 2.030 1.949 120.116 0.229 8.668 7.359 0.24 74018. 0.5023
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9.17 0.1614 0.2869 0.1174 0.0660 0.165 2.084 1.939 123.255 0.235 8.626 7.137 0.24 74141. 0.4860
|
|
11.46 0.2017 0.3472 0.1167 0.0678 0.170 2.140 1.928 126.581 0.242 8.577 6.909 0.24 74278. 0.4691
|
|
13.75 0.2421 0.4027 0.1159 0.0697 0.174 2.198 1.915 130.037 0.248 8.517 6.679 0.24 74432. 0.4519
|
|
16.05 0.2824 0.4536 0.1149 0.0715 0.179 2.257 1.898 133.541 0.255 8.443 6.447 0.24 74603. 0.4343
|
|
18.34 0.3228 0.4999 0.1137 0.0734 0.184 2.316 1.878 136.996 0.262 8.353 6.218 0.24 74791. 0.4166
|
|
20.63 0.3631 0.5419 0.1122 0.0752 0.188 2.371 1.853 140.281 0.268 8.243 5.992 0.24 74998. 0.3988
|
|
22.92 0.4035 0.5800 0.1103 0.0768 0.192 2.422 1.823 143.259 0.274 8.108 5.771 0.24 75223. 0.3810
|
|
25.22 0.4438 0.6144 0.1081 0.0781 0.195 2.464 1.786 145.779 0.278 7.945 5.558 0.24 75467. 0.3632
|
|
27.51 0.4842 0.6454 0.1055 0.0791 0.198 2.496 1.743 147.681 0.282 7.751 5.352 0.24 75729. 0.3455
|
|
29.80 0.5245 0.6735 0.1024 0.0797 0.200 2.515 1.691 148.798 0.284 7.522 5.155 0.24 76011. 0.3278
|
|
32.09 0.5649 0.6988 0.0987 0.0798 0.200 2.518 1.631 148.968 0.285 7.256 4.967 0.24 76311. 0.3102
|
|
34.39 0.6052 0.7217 0.0946 0.0793 0.199 2.503 1.563 148.043 0.283 6.951 4.788 0.24 76630. 0.2926
|
|
36.68 0.6455 0.7422 0.0899 0.0782 0.196 2.466 1.485 145.904 0.279 6.605 4.616 0.24 76968. 0.2750
|
|
38.97 0.6859 0.7605 0.0846 0.0763 0.191 2.408 1.398 142.467 0.272 6.219 4.451 0.24 77323. 0.2574
|
|
41.26 0.7262 0.7763 0.0789 0.0738 0.185 2.327 1.303 137.681 0.263 5.794 4.291 0.24 77696. 0.2395
|
|
43.56 0.7666 0.7895 0.0726 0.0705 0.176 2.224 1.199 131.547 0.251 5.334 4.134 0.24 78087. 0.2214
|
|
45.85 0.8069 0.7995 0.0659 0.0665 0.167 2.099 1.089 124.167 0.237 4.844 3.978 0.25 78494. 0.2030
|
|
48.14 0.8473 0.8057 0.0589 0.0620 0.155 1.955 0.974 115.674 0.221 4.331 3.818 0.25 78918. 0.1842
|
|
50.43 0.8876 0.8070 0.0517 0.0569 0.142 1.795 0.855 106.189 0.203 3.801 3.650 0.25 79359. 0.1650
|
|
52.73 0.9280 0.8016 0.0443 0.0513 0.128 1.620 0.733 95.820 0.183 3.259 3.468 0.25 79815. 0.1451
|
|
55.02 0.9683 0.7869 0.0369 0.0454 0.114 1.431 0.609 84.664 0.162 2.709 3.263 0.25 80287. 0.1245
|
|
57.31 1.0087 0.7582 0.0293 0.0390 0.098 1.231 0.485 72.823 0.139 2.155 3.018 0.25 80775. 0.1027
|
|
59.60 1.0490 0.7069 0.0218 0.0324 0.081 1.021 0.360 60.404 0.115 1.603 2.705 0.25 81277. 0.0794
|
|
61.90 1.0894 0.6143 0.0144 0.0255 0.064 0.803 0.237 47.527 0.091 1.055 2.264 0.25 81795. 0.0539
|
|
64.19 1.1297 0.4333 0.0071 0.0184 0.046 0.580 0.117 34.328 0.066 0.518 1.540 0.25 82328. 0.0257
|
|
66.48 1.1700 -0.0040 0.0000 0.0112 0.028 0.354 -0.001 20.964 0.040 -0.003 -0.014 0.25 82875. 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 0.1194 0.0595 0.258 2.705 2.841 192.019 0.306 12.638 6.711 0.29 88480. 0.5532
|
|
2.75 0.0404 0.0790 0.1190 0.0608 0.263 2.764 2.832 196.175 0.312 12.597 6.548 0.29 88579. 0.5388
|
|
5.51 0.0807 0.1539 0.1186 0.0623 0.269 2.829 2.822 200.794 0.320 12.553 6.375 0.29 88692. 0.5237
|
|
8.26 0.1211 0.2242 0.1182 0.0638 0.276 2.900 2.811 205.856 0.328 12.503 6.193 0.29 88821. 0.5077
|
|
11.01 0.1615 0.2899 0.1176 0.0655 0.283 2.977 2.798 211.322 0.336 12.445 6.005 0.29 88968. 0.4911
|
|
13.76 0.2019 0.3507 0.1170 0.0673 0.291 3.059 2.782 217.121 0.346 12.375 5.812 0.29 89133. 0.4740
|
|
16.52 0.2422 0.4067 0.1162 0.0692 0.299 3.144 2.763 223.154 0.355 12.291 5.617 0.29 89318. 0.4565
|
|
19.27 0.2826 0.4579 0.1152 0.0711 0.307 3.230 2.740 229.282 0.365 12.188 5.420 0.29 89523. 0.4387
|
|
22.02 0.3230 0.5045 0.1140 0.0730 0.316 3.315 2.711 235.334 0.375 12.060 5.226 0.29 89750. 0.4208
|
|
24.77 0.3634 0.5468 0.1125 0.0748 0.323 3.396 2.676 241.102 0.384 11.903 5.034 0.29 89998. 0.4027
|
|
27.53 0.4037 0.5850 0.1107 0.0764 0.330 3.470 2.633 246.345 0.392 11.711 4.848 0.29 90268. 0.3846
|
|
30.28 0.4441 0.6195 0.1085 0.0778 0.336 3.533 2.581 250.800 0.399 11.479 4.667 0.29 90561. 0.3666
|
|
33.03 0.4845 0.6507 0.1059 0.0788 0.341 3.581 2.518 254.183 0.405 11.201 4.494 0.29 90877. 0.3487
|
|
35.78 0.5248 0.6789 0.1027 0.0794 0.344 3.609 2.444 256.206 0.408 10.872 4.327 0.29 91215. 0.3308
|
|
38.54 0.5652 0.7043 0.0991 0.0796 0.344 3.614 2.358 256.581 0.408 10.490 4.169 0.29 91576. 0.3130
|
|
41.29 0.6056 0.7273 0.0950 0.0791 0.342 3.593 2.259 255.047 0.406 10.049 4.018 0.29 91959. 0.2953
|
|
44.04 0.6460 0.7480 0.0903 0.0779 0.337 3.541 2.147 251.393 0.400 9.550 3.874 0.29 92364. 0.2776
|
|
46.80 0.6863 0.7664 0.0850 0.0761 0.329 3.458 2.022 245.474 0.391 8.993 3.736 0.29 92792. 0.2598
|
|
49.55 0.7267 0.7825 0.0792 0.0735 0.318 3.341 1.884 237.194 0.378 8.380 3.602 0.29 93240. 0.2418
|
|
52.30 0.7671 0.7961 0.0729 0.0702 0.304 3.191 1.734 226.553 0.361 7.714 3.472 0.29 93709. 0.2236
|
|
55.05 0.8074 0.8067 0.0662 0.0663 0.287 3.011 1.575 213.726 0.340 7.005 3.342 0.29 94199. 0.2051
|
|
57.81 0.8478 0.8136 0.0592 0.0617 0.267 2.803 1.408 198.943 0.317 6.263 3.210 0.30 94709. 0.1863
|
|
60.56 0.8882 0.8158 0.0519 0.0566 0.245 2.570 1.236 182.414 0.290 5.497 3.073 0.30 95238. 0.1670
|
|
63.31 0.9286 0.8117 0.0445 0.0509 0.220 2.315 1.060 164.326 0.262 4.713 2.925 0.30 95786. 0.1472
|
|
66.06 0.9689 0.7988 0.0370 0.0449 0.194 2.041 0.881 144.850 0.231 3.918 2.758 0.30 96353. 0.1266
|
|
68.82 1.0093 0.7724 0.0295 0.0385 0.167 1.749 0.701 124.164 0.198 3.117 2.560 0.30 96939. 0.1048
|
|
71.57 1.0497 0.7240 0.0219 0.0318 0.137 1.443 0.521 102.455 0.163 2.319 2.308 0.30 97543. 0.0815
|
|
74.32 1.0901 0.6350 0.0144 0.0248 0.107 1.126 0.343 79.938 0.127 1.528 1.949 0.30 98165. 0.0558
|
|
77.07 1.1304 0.4559 0.0071 0.0176 0.076 0.801 0.169 56.854 0.090 0.752 1.349 0.30 98805. 0.0271
|
|
79.83 1.1708 -0.0002 0.0000 0.0104 0.045 0.472 0.000 33.478 0.053 0.000 0.000 0.30 99462. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 7000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1196 0.0592 0.406 3.660 3.872 303.084 0.413 17.225 5.795 0.33 103226. 0.5576
|
|
3.21 0.0404 0.0797 0.1192 0.0605 0.415 3.740 3.860 309.705 0.422 17.171 5.654 0.33 103340. 0.5432
|
|
6.43 0.0808 0.1551 0.1188 0.0619 0.425 3.829 3.847 317.073 0.433 17.113 5.504 0.33 103473. 0.5278
|
|
9.64 0.1212 0.2260 0.1184 0.0635 0.436 3.926 3.833 325.159 0.444 17.047 5.346 0.33 103624. 0.5118
|
|
12.86 0.1616 0.2921 0.1178 0.0652 0.448 4.032 3.815 333.900 0.456 16.971 5.183 0.33 103795. 0.4950
|
|
16.07 0.2020 0.3533 0.1172 0.0670 0.460 4.144 3.795 343.189 0.468 16.880 5.016 0.33 103988. 0.4778
|
|
19.28 0.2424 0.4097 0.1164 0.0689 0.473 4.261 3.770 352.866 0.481 16.769 4.846 0.33 104204. 0.4601
|
|
22.50 0.2828 0.4612 0.1155 0.0708 0.486 4.380 3.739 362.715 0.495 16.632 4.676 0.33 104443. 0.4421
|
|
25.71 0.3232 0.5080 0.1143 0.0727 0.499 4.497 3.701 372.458 0.508 16.462 4.507 0.33 104708. 0.4240
|
|
28.92 0.3636 0.5505 0.1128 0.0745 0.512 4.610 3.654 381.763 0.521 16.252 4.341 0.34 104998. 0.4057
|
|
32.14 0.4040 0.5888 0.1110 0.0762 0.523 4.712 3.596 390.244 0.532 15.994 4.179 0.34 105313. 0.3875
|
|
35.35 0.4444 0.6235 0.1089 0.0776 0.533 4.799 3.525 397.475 0.542 15.680 4.023 0.34 105656. 0.3693
|
|
38.57 0.4848 0.6547 0.1063 0.0787 0.540 4.866 3.441 403.000 0.550 15.304 3.872 0.34 106024. 0.3512
|
|
41.78 0.5252 0.6830 0.1032 0.0793 0.545 4.907 3.341 406.350 0.554 14.859 3.729 0.34 106420. 0.3332
|
|
44.99 0.5656 0.7085 0.0996 0.0795 0.546 4.915 3.224 407.063 0.555 14.338 3.592 0.34 106841. 0.3153
|
|
48.21 0.6060 0.7316 0.0954 0.0790 0.543 4.887 3.089 404.715 0.552 13.739 3.462 0.34 107289. 0.2975
|
|
51.42 0.6464 0.7524 0.0907 0.0779 0.535 4.817 2.936 398.963 0.544 13.058 3.338 0.34 107763. 0.2796
|
|
54.64 0.6868 0.7710 0.0854 0.0761 0.522 4.704 2.765 389.569 0.531 12.298 3.219 0.34 108262. 0.2617
|
|
57.85 0.7272 0.7874 0.0796 0.0735 0.505 4.545 2.576 376.376 0.513 11.459 3.105 0.34 108786. 0.2437
|
|
61.06 0.7676 0.8012 0.0732 0.0702 0.482 4.339 2.372 359.381 0.490 10.549 2.993 0.34 109335. 0.2254
|
|
64.28 0.8080 0.8123 0.0665 0.0662 0.454 4.092 2.154 338.860 0.462 9.579 2.883 0.34 109907. 0.2068
|
|
67.49 0.8485 0.8198 0.0595 0.0615 0.423 3.806 1.925 315.181 0.430 8.564 2.771 0.35 110502. 0.1880
|
|
70.70 0.8889 0.8228 0.0522 0.0564 0.387 3.486 1.690 288.680 0.394 7.515 2.655 0.35 111121. 0.1687
|
|
73.92 0.9293 0.8198 0.0447 0.0507 0.348 3.135 1.448 259.654 0.354 6.442 2.530 0.35 111761. 0.1489
|
|
77.13 0.9697 0.8083 0.0372 0.0446 0.306 2.758 1.204 228.382 0.312 5.354 2.390 0.35 112424. 0.1282
|
|
80.35 1.0101 0.7838 0.0296 0.0381 0.262 2.356 0.957 195.149 0.266 4.258 2.225 0.35 113108. 0.1065
|
|
83.56 1.0505 0.7377 0.0220 0.0313 0.215 1.935 0.712 160.260 0.219 3.165 2.014 0.35 113814. 0.0831
|
|
86.77 1.0909 0.6513 0.0145 0.0242 0.166 1.498 0.468 124.061 0.169 2.083 1.712 0.35 114541. 0.0573
|
|
89.99 1.1313 0.4731 0.0071 0.0170 0.117 1.050 0.230 86.949 0.119 1.023 1.199 0.35 115288. 0.0281
|
|
93.20 1.1717 -0.0049 0.0000 0.0096 0.066 0.596 -0.001 49.370 0.067 -0.006 -0.012 0.36 116056. 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 0.1198 0.0590 0.604 4.762 5.065 450.765 0.538 22.529 5.096 0.38 117970. 0.5608
|
|
3.67 0.0404 0.0801 0.1194 0.0603 0.618 4.867 5.050 460.670 0.550 22.462 4.972 0.38 118101. 0.5463
|
|
7.35 0.0808 0.1559 0.1190 0.0617 0.633 4.984 5.034 471.706 0.563 22.389 4.840 0.38 118252. 0.5310
|
|
11.02 0.1212 0.2272 0.1186 0.0633 0.649 5.112 5.015 483.833 0.578 22.307 4.701 0.38 118425. 0.5148
|
|
14.69 0.1616 0.2936 0.1181 0.0650 0.666 5.251 4.994 496.963 0.593 22.212 4.558 0.38 118621. 0.4980
|
|
18.37 0.2021 0.3552 0.1175 0.0668 0.685 5.398 4.968 510.939 0.610 22.098 4.410 0.38 118841. 0.4807
|
|
22.04 0.2425 0.4117 0.1167 0.0687 0.705 5.552 4.937 525.525 0.627 21.959 4.261 0.38 119088. 0.4629
|
|
25.72 0.2829 0.4635 0.1158 0.0707 0.725 5.709 4.898 540.398 0.645 21.785 4.111 0.38 119362. 0.4448
|
|
29.39 0.3233 0.5105 0.1147 0.0726 0.744 5.865 4.849 555.143 0.663 21.569 3.962 0.38 119664. 0.4266
|
|
33.06 0.3637 0.5531 0.1132 0.0745 0.763 6.014 4.789 569.260 0.680 21.301 3.816 0.38 119996. 0.4083
|
|
36.74 0.4041 0.5916 0.1115 0.0761 0.781 6.151 4.714 582.165 0.695 20.969 3.673 0.38 120357. 0.3900
|
|
40.41 0.4445 0.6263 0.1093 0.0776 0.796 6.267 4.623 593.211 0.708 20.565 3.535 0.38 120748. 0.3717
|
|
44.08 0.4849 0.6576 0.1067 0.0787 0.807 6.357 4.514 601.709 0.718 20.078 3.403 0.39 121169. 0.3535
|
|
47.76 0.5253 0.6859 0.1037 0.0794 0.814 6.413 4.384 606.944 0.724 19.500 3.276 0.39 121621. 0.3354
|
|
51.43 0.5658 0.7116 0.1001 0.0796 0.816 6.426 4.232 608.215 0.726 18.823 3.156 0.39 122104. 0.3174
|
|
55.11 0.6062 0.7347 0.0959 0.0791 0.811 6.391 4.056 604.876 0.722 18.041 3.041 0.39 122616. 0.2995
|
|
58.78 0.6466 0.7557 0.0912 0.0780 0.800 6.301 3.856 596.403 0.712 17.152 2.933 0.39 123158. 0.2816
|
|
62.45 0.6870 0.7745 0.0859 0.0762 0.781 6.154 3.632 582.426 0.695 16.156 2.829 0.39 123729. 0.2636
|
|
66.13 0.7274 0.7911 0.0800 0.0736 0.755 5.945 3.385 562.706 0.672 15.058 2.729 0.39 124328. 0.2455
|
|
69.80 0.7678 0.8052 0.0737 0.0703 0.720 5.676 3.117 537.229 0.641 13.864 2.631 0.39 124955. 0.2272
|
|
73.47 0.8082 0.8167 0.0669 0.0662 0.679 5.350 2.831 506.402 0.604 12.591 2.535 0.39 125610. 0.2086
|
|
77.15 0.8486 0.8248 0.0598 0.0616 0.631 4.974 2.531 470.779 0.562 11.259 2.439 0.39 126291. 0.1897
|
|
80.82 0.8890 0.8286 0.0525 0.0564 0.578 4.552 2.221 430.865 0.514 9.881 2.339 0.40 126998. 0.1704
|
|
84.50 0.9295 0.8266 0.0450 0.0506 0.519 4.090 1.904 387.110 0.462 8.471 2.231 0.40 127730. 0.1506
|
|
88.17 0.9699 0.8164 0.0374 0.0445 0.456 3.592 1.583 339.935 0.406 7.041 2.112 0.40 128488. 0.1299
|
|
91.84 1.0103 0.7936 0.0298 0.0379 0.389 3.062 1.259 289.772 0.346 5.601 1.971 0.40 129271. 0.1082
|
|
95.52 1.0507 0.7500 0.0221 0.0310 0.318 2.505 0.936 237.086 0.283 4.164 1.791 0.40 130078. 0.0847
|
|
99.19 1.0911 0.6666 0.0146 0.0239 0.245 1.927 0.616 182.404 0.218 2.742 1.533 0.40 130908. 0.0589
|
|
102.86 1.1315 0.4908 0.0072 0.0165 0.169 1.335 0.303 126.329 0.151 1.348 1.088 0.40 131763. 0.0293
|
|
106.54 1.1719 -0.0019 0.0000 0.0091 0.093 0.735 -0.001 69.546 0.083 -0.003 -0.004 0.41 132641. 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 0.1199 0.0589 0.859 6.017 6.420 640.692 0.680 28.555 4.545 0.43 132714. 0.5631
|
|
4.13 0.0404 0.0804 0.1196 0.0602 0.878 6.150 6.402 654.815 0.695 28.474 4.434 0.43 132862. 0.5486
|
|
8.27 0.0808 0.1564 0.1192 0.0616 0.899 6.298 6.382 670.574 0.712 28.387 4.317 0.43 133032. 0.5332
|
|
12.40 0.1212 0.2280 0.1188 0.0632 0.923 6.460 6.360 687.918 0.730 28.289 4.193 0.43 133226. 0.5171
|
|
16.53 0.1617 0.2947 0.1183 0.0649 0.948 6.637 6.334 706.726 0.750 28.175 4.065 0.43 133446. 0.5003
|
|
20.67 0.2021 0.3564 0.1178 0.0668 0.975 6.825 6.304 726.783 0.771 28.038 3.934 0.43 133694. 0.4829
|
|
24.80 0.2425 0.4132 0.1171 0.0687 1.003 7.022 6.266 747.758 0.793 27.869 3.800 0.43 133971. 0.4652
|
|
28.93 0.2829 0.4651 0.1162 0.0707 1.032 7.224 6.218 769.191 0.816 27.658 3.667 0.43 134279. 0.4471
|
|
33.07 0.3233 0.5123 0.1151 0.0726 1.060 7.424 6.159 790.493 0.839 27.393 3.534 0.43 134619. 0.4288
|
|
37.20 0.3637 0.5550 0.1137 0.0745 1.087 7.616 6.084 810.939 0.860 27.062 3.403 0.43 134992. 0.4104
|
|
41.33 0.4042 0.5935 0.1119 0.0762 1.113 7.792 5.992 829.691 0.880 26.651 3.276 0.43 135398. 0.3920
|
|
45.47 0.4446 0.6284 0.1098 0.0777 1.134 7.943 5.879 845.811 0.897 26.148 3.152 0.43 135839. 0.3737
|
|
49.60 0.4850 0.6598 0.1073 0.0788 1.151 8.061 5.742 858.298 0.911 25.539 3.034 0.43 136313. 0.3555
|
|
53.73 0.5254 0.6882 0.1042 0.0796 1.161 8.134 5.578 866.118 0.919 24.812 2.921 0.43 136822. 0.3374
|
|
57.87 0.5658 0.7138 0.1006 0.0798 1.164 8.154 5.386 868.249 0.921 23.959 2.814 0.44 137364. 0.3193
|
|
62.00 0.6062 0.7371 0.0965 0.0794 1.158 8.112 5.164 863.752 0.916 22.971 2.712 0.44 137941. 0.3014
|
|
66.13 0.6466 0.7582 0.0918 0.0783 1.142 8.000 4.912 851.858 0.904 21.846 2.615 0.44 138551. 0.2834
|
|
70.27 0.6871 0.7772 0.0865 0.0764 1.116 7.814 4.628 832.027 0.883 20.585 2.523 0.44 139194. 0.2654
|
|
74.40 0.7275 0.7940 0.0806 0.0739 1.078 7.550 4.314 803.904 0.853 19.190 2.434 0.44 139869. 0.2472
|
|
78.53 0.7679 0.8084 0.0742 0.0705 1.029 7.207 3.973 767.457 0.814 17.672 2.348 0.44 140575. 0.2289
|
|
82.67 0.8083 0.8203 0.0674 0.0664 0.970 6.792 3.609 723.259 0.767 16.054 2.263 0.44 141311. 0.2103
|
|
86.80 0.8487 0.8289 0.0603 0.0617 0.901 6.312 3.228 672.105 0.713 14.357 2.178 0.44 142078. 0.1914
|
|
90.94 0.8891 0.8334 0.0529 0.0565 0.824 5.773 2.833 614.722 0.652 12.602 2.090 0.45 142874. 0.1721
|
|
95.07 0.9296 0.8323 0.0454 0.0507 0.740 5.182 2.429 551.761 0.585 10.806 1.997 0.45 143698. 0.1522
|
|
99.20 0.9700 0.8233 0.0377 0.0444 0.649 4.544 2.019 483.832 0.513 8.982 1.893 0.45 144551. 0.1315
|
|
103.34 1.0104 0.8022 0.0300 0.0378 0.552 3.865 1.607 411.557 0.437 7.147 1.771 0.45 145432. 0.1098
|
|
107.47 1.0508 0.7607 0.0223 0.0308 0.450 3.152 1.195 335.612 0.356 5.314 1.615 0.45 146340. 0.0863
|
|
111.60 1.0912 0.6802 0.0147 0.0236 0.344 2.411 0.787 256.763 0.272 3.500 1.390 0.45 147275. 0.0603
|
|
115.74 1.1316 0.5068 0.0072 0.0162 0.236 1.652 0.387 175.891 0.187 1.723 0.999 0.46 148237. 0.0304
|
|
119.87 1.1721 -0.0002 0.0000 0.0086 0.126 0.883 0.000 93.992 0.100 0.000 0.000 0.46 149224. 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 0.1201 0.0589 1.178 7.427 7.938 878.757 0.839 35.308 4.097 0.48 147458. 0.5645
|
|
4.59 0.0404 0.0805 0.1198 0.0602 1.204 7.591 7.917 898.148 0.858 35.214 3.998 0.48 147621. 0.5501
|
|
9.19 0.0808 0.1568 0.1195 0.0616 1.233 7.775 7.894 919.819 0.878 35.113 3.893 0.48 147810. 0.5348
|
|
13.78 0.1213 0.2285 0.1191 0.0632 1.266 7.976 7.869 943.711 0.901 35.000 3.782 0.48 148025. 0.5187
|
|
18.37 0.1617 0.2953 0.1186 0.0649 1.300 8.196 7.839 969.671 0.926 34.868 3.667 0.48 148270. 0.5020
|
|
22.97 0.2021 0.3573 0.1181 0.0668 1.338 8.430 7.803 997.411 0.952 34.708 3.548 0.48 148545. 0.4847
|
|
27.56 0.2425 0.4142 0.1174 0.0687 1.377 8.676 7.759 1026.484 0.980 34.510 3.428 0.48 148854. 0.4669
|
|
32.15 0.2829 0.4662 0.1166 0.0707 1.416 8.928 7.703 1056.266 1.009 34.261 3.308 0.48 149196. 0.4489
|
|
36.75 0.3234 0.5135 0.1155 0.0727 1.456 9.179 7.632 1085.943 1.037 33.947 3.188 0.48 149574. 0.4306
|
|
41.34 0.3638 0.5563 0.1141 0.0746 1.495 9.420 7.543 1114.514 1.064 33.550 3.070 0.48 149988. 0.4122
|
|
45.93 0.4042 0.5950 0.1125 0.0764 1.530 9.642 7.432 1140.807 1.089 33.056 2.955 0.48 150439. 0.3939
|
|
50.53 0.4446 0.6299 0.1104 0.0779 1.560 9.834 7.294 1163.514 1.111 32.445 2.844 0.48 150928. 0.3755
|
|
55.12 0.4851 0.6613 0.1079 0.0791 1.584 9.984 7.128 1181.230 1.128 31.704 2.737 0.48 151456. 0.3573
|
|
59.71 0.5255 0.6898 0.1048 0.0799 1.599 10.079 6.928 1192.504 1.139 30.815 2.635 0.48 152021. 0.3391
|
|
64.31 0.5659 0.7156 0.1013 0.0801 1.604 10.108 6.692 1195.905 1.142 29.768 2.538 0.48 152625. 0.3211
|
|
68.90 0.6063 0.7389 0.0971 0.0797 1.596 10.059 6.419 1190.111 1.136 28.552 2.446 0.48 153266. 0.3031
|
|
73.49 0.6467 0.7601 0.0924 0.0786 1.574 9.923 6.107 1174.035 1.121 27.163 2.359 0.49 153944. 0.2851
|
|
78.09 0.6872 0.7793 0.0871 0.0768 1.538 9.694 5.756 1146.912 1.095 25.603 2.276 0.49 154659. 0.2670
|
|
82.68 0.7276 0.7963 0.0812 0.0742 1.486 9.367 5.368 1108.239 1.058 23.875 2.197 0.49 155409. 0.2489
|
|
87.27 0.7680 0.8110 0.0748 0.0709 1.419 8.942 4.944 1057.950 1.010 21.993 2.120 0.49 156194. 0.2305
|
|
91.87 0.8084 0.8233 0.0680 0.0668 1.337 8.425 4.492 996.827 0.952 19.983 2.044 0.49 157013. 0.2119
|
|
96.46 0.8488 0.8324 0.0608 0.0620 1.242 7.826 4.018 925.967 0.884 17.874 1.968 0.49 157865. 0.1929
|
|
101.05 0.8893 0.8375 0.0534 0.0567 1.135 7.154 3.528 846.388 0.808 15.691 1.890 0.49 158750. 0.1736
|
|
105.65 0.9297 0.8372 0.0458 0.0508 1.018 6.415 3.025 758.996 0.725 13.455 1.808 0.50 159667. 0.1537
|
|
110.24 0.9701 0.8293 0.0381 0.0445 0.891 5.618 2.514 664.641 0.635 11.184 1.716 0.50 160615. 0.1330
|
|
114.83 1.0105 0.8096 0.0303 0.0378 0.757 4.769 2.001 564.193 0.539 8.898 1.608 0.50 161594. 0.1112
|
|
119.43 1.0510 0.7701 0.0225 0.0307 0.615 3.876 1.487 458.598 0.438 6.615 1.471 0.50 162603. 0.0877
|
|
124.02 1.0914 0.6920 0.0148 0.0234 0.468 2.949 0.979 348.930 0.333 4.355 1.273 0.50 163643. 0.0616
|
|
128.61 1.1318 0.5205 0.0073 0.0158 0.317 1.998 0.481 236.429 0.226 2.140 0.923 0.51 164712. 0.0313
|
|
133.21 1.1722 -0.0033 0.0000 0.0082 0.164 1.035 -0.002 122.498 0.117 -0.007 -0.006 0.51 165809. 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 0.1203 0.0589 1.571 8.999 9.621 1171.175 1.017 42.794 3.726 0.52 162200. 0.5651
|
|
5.05 0.0404 0.0806 0.1200 0.0602 1.605 9.197 9.597 1196.987 1.039 42.688 3.637 0.52 162380. 0.5509
|
|
10.11 0.0808 0.1569 0.1197 0.0617 1.644 9.420 9.572 1225.887 1.064 42.574 3.541 0.52 162587. 0.5357
|
|
15.16 0.1213 0.2287 0.1193 0.0633 1.687 9.665 9.543 1257.812 1.092 42.447 3.441 0.52 162824. 0.5198
|
|
20.21 0.1617 0.2957 0.1189 0.0650 1.733 9.932 9.510 1292.571 1.122 42.299 3.337 0.52 163093. 0.5032
|
|
25.26 0.2021 0.3577 0.1184 0.0669 1.783 10.218 9.469 1329.800 1.154 42.118 3.230 0.52 163396. 0.4860
|
|
30.32 0.2425 0.4147 0.1178 0.0689 1.836 10.519 9.419 1368.918 1.188 41.894 3.121 0.53 163734. 0.4683
|
|
35.37 0.2829 0.4669 0.1170 0.0709 1.890 10.827 9.354 1409.102 1.223 41.609 3.011 0.53 164111. 0.4503
|
|
40.42 0.3234 0.5143 0.1160 0.0729 1.943 11.136 9.273 1449.266 1.258 41.245 2.902 0.53 164526. 0.4321
|
|
45.47 0.3638 0.5571 0.1147 0.0749 1.996 11.434 9.169 1488.062 1.292 40.784 2.795 0.53 164981. 0.4138
|
|
50.53 0.4042 0.5959 0.1130 0.0767 2.044 11.709 9.038 1523.908 1.323 40.203 2.690 0.53 165478. 0.3955
|
|
55.58 0.4446 0.6308 0.1110 0.0782 2.085 11.949 8.876 1555.022 1.350 39.481 2.589 0.53 166016. 0.3772
|
|
60.63 0.4850 0.6624 0.1085 0.0795 2.118 12.137 8.678 1579.490 1.371 38.599 2.492 0.53 166596. 0.3589
|
|
65.68 0.5255 0.6909 0.1055 0.0803 2.139 12.258 8.439 1595.333 1.385 37.536 2.399 0.53 167218. 0.3408
|
|
70.74 0.5659 0.7167 0.1020 0.0805 2.146 12.299 8.156 1600.595 1.390 36.278 2.311 0.53 167882. 0.3228
|
|
75.79 0.6063 0.7402 0.0979 0.0802 2.137 12.244 7.827 1593.469 1.383 34.813 2.228 0.53 168588. 0.3048
|
|
80.84 0.6467 0.7615 0.0932 0.0791 2.109 12.083 7.449 1572.460 1.365 33.135 2.149 0.53 169334. 0.2868
|
|
85.89 0.6872 0.7808 0.0878 0.0773 2.060 11.806 7.024 1536.514 1.334 31.244 2.074 0.54 170121. 0.2687
|
|
90.95 0.7276 0.7980 0.0820 0.0747 1.991 11.410 6.553 1484.932 1.289 29.147 2.002 0.54 170946. 0.2505
|
|
96.00 0.7680 0.8131 0.0755 0.0713 1.901 10.893 6.038 1417.600 1.231 26.858 1.932 0.54 171810. 0.2321
|
|
101.05 0.8084 0.8257 0.0686 0.0672 1.791 10.262 5.488 1335.544 1.159 24.410 1.864 0.54 172712. 0.2135
|
|
106.10 0.8488 0.8352 0.0614 0.0624 1.663 9.530 4.910 1240.243 1.077 21.839 1.796 0.54 173650. 0.1945
|
|
111.16 0.8893 0.8410 0.0539 0.0570 1.519 8.706 4.311 1133.077 0.984 19.176 1.726 0.54 174624. 0.1752
|
|
116.21 0.9297 0.8415 0.0462 0.0511 1.362 7.801 3.697 1015.273 0.881 16.445 1.652 0.55 175632. 0.1553
|
|
121.26 0.9701 0.8346 0.0384 0.0447 1.191 6.823 3.074 887.986 0.771 13.672 1.570 0.55 176675. 0.1346
|
|
126.31 1.0105 0.8164 0.0306 0.0379 1.009 5.781 2.446 752.396 0.653 10.878 1.474 0.55 177752. 0.1127
|
|
131.37 1.0509 0.7788 0.0227 0.0307 0.818 4.686 1.818 609.788 0.529 8.086 1.352 0.55 178863. 0.0892
|
|
136.42 1.0914 0.7031 0.0150 0.0232 0.619 3.547 1.197 461.626 0.401 5.322 1.176 0.55 180006. 0.0629
|
|
141.47 1.1318 0.5336 0.0073 0.0156 0.415 2.379 0.587 309.602 0.269 2.612 0.860 0.56 181182. 0.0322
|
|
146.53 1.1722 -0.0060 0.0000 0.0078 0.209 1.196 -0.003 155.643 0.135 -0.014 -0.009 0.56 182389. 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 0.1205 0.0591 2.044 10.738 11.470 1524.576 1.213 51.018 3.412 0.57 176941. 0.5651
|
|
5.51 0.0404 0.0805 0.1203 0.0604 2.089 10.974 11.444 1558.061 1.240 50.901 3.331 0.57 177137. 0.5510
|
|
11.02 0.0808 0.1568 0.1200 0.0618 2.140 11.239 11.416 1595.628 1.270 50.776 3.245 0.57 177363. 0.5361
|
|
16.53 0.1212 0.2286 0.1196 0.0635 2.196 11.532 11.384 1637.215 1.303 50.638 3.154 0.57 177621. 0.5203
|
|
22.04 0.1617 0.2956 0.1193 0.0652 2.256 11.851 11.348 1682.604 1.339 50.477 3.059 0.57 177914. 0.5039
|
|
27.55 0.2021 0.3577 0.1188 0.0671 2.322 12.195 11.304 1731.342 1.378 50.280 2.961 0.57 178244. 0.4868
|
|
33.07 0.2425 0.4149 0.1182 0.0691 2.391 12.557 11.248 1782.702 1.419 50.032 2.862 0.57 178613. 0.4693
|
|
38.58 0.2829 0.4671 0.1175 0.0711 2.462 12.929 11.177 1835.629 1.461 49.715 2.762 0.57 179023. 0.4515
|
|
44.09 0.3233 0.5145 0.1165 0.0732 2.533 13.303 11.085 1888.715 1.503 49.307 2.662 0.57 179476. 0.4334
|
|
49.60 0.3637 0.5575 0.1153 0.0752 2.602 13.666 10.967 1940.196 1.544 48.782 2.564 0.58 179973. 0.4152
|
|
55.11 0.4041 0.5963 0.1137 0.0770 2.666 14.002 10.817 1987.975 1.582 48.116 2.468 0.58 180514. 0.3969
|
|
60.62 0.4445 0.6313 0.1117 0.0787 2.722 14.296 10.630 2029.689 1.615 47.281 2.375 0.58 181101. 0.3787
|
|
66.13 0.4850 0.6629 0.1093 0.0799 2.766 14.529 10.398 2062.782 1.642 46.252 2.286 0.58 181733. 0.3605
|
|
71.64 0.5254 0.6915 0.1063 0.0808 2.796 14.683 10.118 2084.613 1.659 45.007 2.202 0.58 182412. 0.3424
|
|
77.15 0.5658 0.7174 0.1028 0.0811 2.806 14.739 9.785 2092.566 1.665 43.524 2.121 0.58 183136. 0.3244
|
|
82.66 0.6062 0.7409 0.0987 0.0808 2.795 14.680 9.395 2084.223 1.659 41.790 2.045 0.58 183906. 0.3064
|
|
88.17 0.6466 0.7624 0.0940 0.0797 2.759 14.493 8.947 2057.575 1.637 39.797 1.972 0.58 184721. 0.2885
|
|
93.69 0.6870 0.7819 0.0887 0.0779 2.697 14.166 8.441 2011.193 1.600 37.546 1.904 0.58 185579. 0.2704
|
|
99.20 0.7274 0.7993 0.0828 0.0753 2.607 13.694 7.878 1944.134 1.547 35.042 1.838 0.59 186480. 0.2523
|
|
104.71 0.7679 0.8146 0.0763 0.0719 2.489 13.074 7.263 1856.208 1.477 32.304 1.775 0.59 187423. 0.2339
|
|
110.22 0.8083 0.8276 0.0694 0.0678 2.345 12.317 6.603 1748.719 1.392 29.372 1.713 0.59 188406. 0.2152
|
|
115.73 0.8487 0.8376 0.0621 0.0629 2.177 11.436 5.910 1623.617 1.292 26.287 1.651 0.59 189430. 0.1962
|
|
121.24 0.8891 0.8439 0.0545 0.0575 1.988 10.444 5.191 1482.729 1.180 23.088 1.588 0.59 190492. 0.1769
|
|
126.75 0.9295 0.8453 0.0468 0.0515 1.780 9.352 4.453 1327.684 1.057 19.806 1.521 0.60 191593. 0.1570
|
|
132.26 0.9699 0.8395 0.0389 0.0450 1.556 8.171 3.703 1160.016 0.923 16.470 1.448 0.60 192731. 0.1362
|
|
137.77 1.0103 0.8226 0.0310 0.0380 1.316 6.912 2.947 981.286 0.781 13.106 1.362 0.60 193906. 0.1143
|
|
143.28 1.0507 0.7869 0.0230 0.0307 1.064 5.587 2.191 793.197 0.631 9.744 1.253 0.60 195117. 0.0907
|
|
148.79 1.0912 0.7137 0.0152 0.0232 0.802 4.210 1.442 597.700 0.476 6.413 1.094 0.60 196364. 0.0642
|
|
154.31 1.1316 0.5467 0.0074 0.0154 0.532 2.797 0.707 397.053 0.316 3.147 0.808 0.61 197647. 0.0332
|
|
159.82 1.1720 -0.0072 0.0000 0.0075 0.260 1.365 -0.004 193.836 0.154 -0.019 -0.010 0.61 198963. 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 0.1208 0.0593 2.610 12.656 13.486 1946.504 1.430 59.985 3.142 0.62 191682. 0.5643
|
|
5.97 0.0404 0.0803 0.1205 0.0606 2.667 12.932 13.458 1988.935 1.461 59.859 3.069 0.62 191894. 0.5505
|
|
11.94 0.0808 0.1565 0.1202 0.0621 2.731 13.242 13.428 2036.658 1.496 59.727 2.990 0.62 192138. 0.5358
|
|
17.90 0.1212 0.2282 0.1199 0.0637 2.802 13.586 13.395 2089.627 1.535 59.582 2.908 0.62 192417. 0.5203
|
|
23.87 0.1616 0.2952 0.1196 0.0655 2.880 13.963 13.357 2147.606 1.578 59.412 2.821 0.62 192734. 0.5041
|
|
29.84 0.2020 0.3574 0.1192 0.0674 2.964 14.369 13.310 2210.059 1.623 59.204 2.732 0.62 193091. 0.4873
|
|
35.81 0.2424 0.4145 0.1187 0.0694 3.052 14.799 13.251 2276.095 1.672 58.939 2.641 0.62 193490. 0.4700
|
|
41.78 0.2828 0.4668 0.1180 0.0715 3.144 15.243 13.174 2344.405 1.722 58.596 2.549 0.62 193934. 0.4523
|
|
47.75 0.3232 0.5143 0.1171 0.0736 3.236 15.690 13.073 2413.205 1.773 58.149 2.457 0.62 194424. 0.4344
|
|
53.71 0.3636 0.5573 0.1159 0.0756 3.326 16.126 12.942 2480.228 1.822 57.567 2.367 0.62 194961. 0.4163
|
|
59.68 0.4040 0.5962 0.1144 0.0775 3.410 16.532 12.774 2542.759 1.868 56.819 2.279 0.62 195547. 0.3982
|
|
65.65 0.4444 0.6312 0.1125 0.0792 3.484 16.890 12.561 2597.711 1.908 55.873 2.193 0.62 196182. 0.3801
|
|
71.62 0.4848 0.6629 0.1101 0.0805 3.543 17.176 12.297 2641.732 1.941 54.697 2.111 0.63 196867. 0.3620
|
|
77.59 0.5252 0.6915 0.1072 0.0814 3.582 17.368 11.974 2671.357 1.962 53.262 2.033 0.63 197602. 0.3440
|
|
83.55 0.5656 0.7175 0.1038 0.0818 3.598 17.445 11.588 2683.149 1.971 51.544 1.959 0.63 198387. 0.3261
|
|
89.52 0.6060 0.7412 0.0997 0.0815 3.586 17.385 11.134 2673.920 1.964 49.524 1.889 0.63 199221. 0.3081
|
|
95.49 0.6464 0.7628 0.0950 0.0805 3.542 17.171 10.610 2641.015 1.940 47.193 1.822 0.63 200103. 0.2902
|
|
101.46 0.6868 0.7824 0.0897 0.0787 3.463 16.791 10.016 2582.533 1.897 44.550 1.759 0.63 201033. 0.2722
|
|
107.43 0.7272 0.8001 0.0838 0.0761 3.349 16.236 9.354 2497.220 1.834 41.604 1.699 0.64 202009. 0.2541
|
|
113.40 0.7676 0.8157 0.0773 0.0727 3.198 15.505 8.627 2384.768 1.752 38.375 1.641 0.64 203031. 0.2357
|
|
119.36 0.8080 0.8290 0.0703 0.0685 3.013 14.608 7.848 2246.799 1.650 34.908 1.584 0.64 204096. 0.2170
|
|
125.33 0.8484 0.8396 0.0629 0.0636 2.797 13.561 7.027 2085.830 1.532 31.255 1.528 0.64 205205. 0.1981
|
|
131.30 0.8888 0.8465 0.0553 0.0580 2.554 12.381 6.174 1904.242 1.399 27.462 1.471 0.64 206356. 0.1787
|
|
137.27 0.9292 0.8486 0.0474 0.0519 2.285 11.080 5.298 1704.157 1.252 23.567 1.410 0.65 207548. 0.1587
|
|
143.24 0.9696 0.8438 0.0395 0.0453 1.995 9.672 4.407 1487.571 1.093 19.604 1.344 0.65 208781. 0.1379
|
|
149.20 1.0100 0.8284 0.0314 0.0383 1.685 8.170 3.508 1256.513 0.923 15.605 1.266 0.65 210053. 0.1160
|
|
155.17 1.0504 0.7945 0.0234 0.0309 1.359 6.588 2.609 1013.202 0.744 11.604 1.168 0.65 211365. 0.0922
|
|
161.14 1.0908 0.7239 0.0154 0.0232 1.019 4.942 1.717 760.176 0.558 7.639 1.025 0.66 212716. 0.0657
|
|
167.11 1.1312 0.5596 0.0075 0.0153 0.671 3.253 0.843 500.399 0.368 3.749 0.764 0.66 214104. 0.0343
|
|
173.08 1.1716 -0.0076 0.0000 0.0072 0.318 1.543 -0.005 237.297 0.174 -0.023 -0.010 0.66 215530. 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 0.1210 0.0598 3.287 14.798 15.669 2451.018 1.672 69.698 2.900 0.67 206421. 0.5613
|
|
6.42 0.0404 0.0798 0.1208 0.0611 3.357 15.114 15.640 2503.373 1.708 69.566 2.834 0.67 206649. 0.5480
|
|
12.85 0.0808 0.1556 0.1205 0.0625 3.436 15.470 15.609 2562.421 1.748 69.430 2.763 0.67 206911. 0.5338
|
|
19.27 0.1211 0.2271 0.1203 0.0641 3.524 15.867 15.576 2628.143 1.793 69.282 2.688 0.67 207211. 0.5188
|
|
25.70 0.1615 0.2940 0.1200 0.0659 3.621 16.303 15.537 2700.300 1.842 69.110 2.610 0.67 207552. 0.5030
|
|
32.12 0.2019 0.3561 0.1196 0.0678 3.726 16.773 15.490 2778.293 1.895 68.898 2.529 0.67 207935. 0.4866
|
|
38.54 0.2423 0.4133 0.1191 0.0698 3.837 17.273 15.428 2861.075 1.952 68.625 2.446 0.67 208365. 0.4698
|
|
44.97 0.2827 0.4657 0.1185 0.0719 3.952 17.792 15.348 2947.085 2.010 68.267 2.362 0.67 208842. 0.4525
|
|
51.39 0.3230 0.5133 0.1177 0.0741 4.069 18.318 15.241 3034.150 2.070 67.791 2.278 0.67 209369. 0.4349
|
|
57.82 0.3634 0.5565 0.1166 0.0761 4.183 18.833 15.099 3119.471 2.128 67.162 2.195 0.67 209946. 0.4171
|
|
64.24 0.4038 0.5955 0.1152 0.0781 4.291 19.317 14.915 3199.630 2.182 66.342 2.114 0.67 210577. 0.3993
|
|
70.67 0.4442 0.6306 0.1133 0.0798 4.386 19.746 14.679 3270.682 2.231 65.292 2.036 0.67 211260. 0.3814
|
|
77.09 0.4846 0.6624 0.1110 0.0812 4.463 20.094 14.382 3328.301 2.270 63.971 1.960 0.67 211997. 0.3634
|
|
83.51 0.5249 0.6911 0.1082 0.0822 4.517 20.333 14.017 3367.964 2.297 62.346 1.888 0.68 212788. 0.3456
|
|
89.94 0.5653 0.7172 0.1048 0.0826 4.540 20.437 13.576 3385.159 2.309 60.385 1.819 0.68 213632. 0.3277
|
|
96.36 0.6057 0.7410 0.1008 0.0824 4.527 20.380 13.054 3375.695 2.303 58.066 1.754 0.68 214530. 0.3099
|
|
102.79 0.6461 0.7627 0.0961 0.0814 4.474 20.141 12.450 3336.096 2.276 55.376 1.693 0.68 215480. 0.2920
|
|
109.21 0.6865 0.7825 0.0908 0.0797 4.377 19.705 11.761 3263.867 2.226 52.314 1.634 0.68 216481. 0.2741
|
|
115.63 0.7268 0.8004 0.0849 0.0771 4.234 19.062 10.991 3157.368 2.154 48.890 1.579 0.68 217532. 0.2560
|
|
122.06 0.7672 0.8164 0.0783 0.0736 4.045 18.209 10.145 3016.109 2.057 45.125 1.526 0.69 218632. 0.2376
|
|
128.48 0.8076 0.8301 0.0713 0.0694 3.811 17.158 9.234 2842.055 1.939 41.073 1.474 0.69 219780. 0.2190
|
|
134.91 0.8480 0.8411 0.0639 0.0644 3.538 15.929 8.272 2638.396 1.800 36.796 1.422 0.69 220974. 0.2000
|
|
141.33 0.8884 0.8486 0.0561 0.0588 3.229 14.539 7.272 2408.195 1.643 32.347 1.370 0.69 222213. 0.1806
|
|
147.75 0.9287 0.8516 0.0482 0.0526 2.889 13.006 6.244 2154.189 1.469 27.773 1.315 0.69 223497. 0.1606
|
|
154.18 0.9691 0.8478 0.0401 0.0459 2.520 11.344 5.196 1878.928 1.282 23.113 1.254 0.70 224824. 0.1398
|
|
160.60 1.0095 0.8337 0.0319 0.0387 2.126 9.569 4.138 1585.005 1.081 18.406 1.184 0.70 226193. 0.1178
|
|
167.03 1.0499 0.8018 0.0238 0.0311 1.710 7.699 3.079 1275.306 0.870 13.694 1.095 0.70 227605. 0.0939
|
|
173.45 1.0903 0.7336 0.0157 0.0233 1.278 5.755 2.028 953.241 0.650 9.019 0.965 0.71 229059. 0.0672
|
|
179.87 1.1306 0.5717 0.0077 0.0152 0.835 3.761 0.996 622.929 0.425 4.429 0.725 0.71 230553. 0.0354
|
|
186.30 1.1710 -0.0073 0.0000 0.0071 0.388 1.746 -0.006 289.261 0.197 -0.025 -0.009 0.71 232087. 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 0.1212 0.0609 4.114 17.287 18.019 3067.841 1.953 80.148 2.664 0.71 221158. 0.5530
|
|
6.88 0.0403 0.0786 0.1210 0.0621 4.199 17.642 17.989 3130.945 1.993 80.013 2.606 0.71 221402. 0.5404
|
|
13.75 0.0807 0.1534 0.1208 0.0635 4.294 18.044 17.958 3202.296 2.039 79.878 2.544 0.71 221683. 0.5271
|
|
20.63 0.1210 0.2241 0.1206 0.0651 4.401 18.493 17.926 3281.910 2.089 79.733 2.477 0.71 222003. 0.5129
|
|
27.51 0.1614 0.2904 0.1203 0.0669 4.519 18.987 17.888 3369.529 2.145 79.566 2.408 0.71 222367. 0.4980
|
|
34.39 0.2017 0.3521 0.1200 0.0687 4.646 19.522 17.842 3464.468 2.206 79.359 2.336 0.72 222777. 0.4824
|
|
41.26 0.2421 0.4092 0.1196 0.0708 4.781 20.091 17.781 3565.507 2.270 79.090 2.262 0.72 223236. 0.4664
|
|
48.14 0.2824 0.4616 0.1190 0.0728 4.923 20.684 17.700 3670.781 2.337 78.728 2.187 0.72 223746. 0.4499
|
|
55.02 0.3228 0.5094 0.1183 0.0750 5.066 21.287 17.590 3777.681 2.405 78.239 2.112 0.72 224309. 0.4331
|
|
61.90 0.3631 0.5529 0.1173 0.0770 5.207 21.879 17.442 3882.796 2.472 77.581 2.037 0.72 224927. 0.4161
|
|
68.77 0.4035 0.5922 0.1160 0.0790 5.340 22.438 17.245 3981.940 2.535 76.706 1.964 0.72 225601. 0.3989
|
|
75.65 0.4438 0.6279 0.1143 0.0808 5.458 22.935 16.989 4070.243 2.591 75.568 1.893 0.72 226331. 0.3816
|
|
82.53 0.4842 0.6601 0.1121 0.0822 5.555 23.342 16.663 4142.363 2.637 74.117 1.825 0.72 227120. 0.3642
|
|
89.40 0.5245 0.6893 0.1093 0.0832 5.623 23.625 16.257 4192.702 2.669 72.309 1.759 0.72 227966. 0.3467
|
|
96.28 0.5649 0.7158 0.1060 0.0837 5.653 23.754 15.762 4215.657 2.684 70.108 1.696 0.73 228870. 0.3292
|
|
103.16 0.6052 0.7399 0.1020 0.0835 5.640 23.700 15.172 4205.926 2.678 67.483 1.636 0.73 229830. 0.3116
|
|
110.04 0.6455 0.7619 0.0974 0.0825 5.577 23.435 14.483 4158.945 2.648 64.420 1.579 0.73 230848. 0.2939
|
|
116.91 0.6859 0.7820 0.0921 0.0808 5.460 22.941 13.695 4071.292 2.592 60.915 1.526 0.73 231920. 0.2761
|
|
123.79 0.7262 0.8002 0.0862 0.0782 5.284 22.205 12.810 3940.621 2.509 56.979 1.474 0.73 233045. 0.2580
|
|
130.67 0.7666 0.8164 0.0796 0.0747 5.050 21.221 11.834 3766.035 2.398 52.637 1.425 0.73 234223. 0.2397
|
|
137.55 0.8069 0.8306 0.0725 0.0704 4.760 20.003 10.780 3549.800 2.260 47.950 1.377 0.74 235452. 0.2211
|
|
144.42 0.8473 0.8421 0.0650 0.0654 4.420 18.572 9.665 3295.906 2.098 42.990 1.330 0.74 236731. 0.2022
|
|
151.30 0.8876 0.8504 0.0572 0.0597 4.034 16.951 8.503 3008.243 1.915 37.821 1.282 0.74 238057. 0.1828
|
|
158.18 0.9280 0.8541 0.0491 0.0534 3.608 15.159 7.306 2690.317 1.713 32.496 1.232 0.74 239432. 0.1628
|
|
165.06 0.9683 0.8514 0.0409 0.0465 3.145 13.217 6.085 2345.510 1.493 27.065 1.177 0.75 240852. 0.1419
|
|
171.93 1.0087 0.8385 0.0326 0.0392 2.652 11.142 4.850 1977.376 1.259 21.571 1.112 0.75 242318. 0.1198
|
|
178.81 1.0490 0.8075 0.0243 0.0316 2.132 8.959 3.611 1590.005 1.012 16.063 1.030 0.75 243829. 0.0957
|
|
185.69 1.0894 0.7397 0.0160 0.0236 1.594 6.696 2.381 1188.362 0.757 10.590 0.909 0.76 245385. 0.0686
|
|
192.56 1.1297 0.5757 0.0079 0.0154 1.044 4.387 1.171 778.510 0.496 5.207 0.682 0.76 246984. 0.0361
|
|
199.44 1.1701 -0.0063 0.0000 0.0073 0.493 2.071 -0.006 367.563 0.234 -0.026 -0.007 0.76 248625. 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 0.1214 0.0629 5.162 20.333 20.531 3849.048 2.297 91.321 2.419 0.76 235895. 0.5360
|
|
7.38 0.0406 0.0767 0.1212 0.0642 5.263 20.731 20.500 3924.399 2.342 91.184 2.369 0.76 236156. 0.5245
|
|
14.77 0.0812 0.1499 0.1210 0.0656 5.377 21.183 20.470 4009.897 2.393 91.050 2.315 0.76 236457. 0.5122
|
|
22.15 0.1219 0.2193 0.1208 0.0671 5.506 21.688 20.439 4105.579 2.450 90.912 2.258 0.76 236802. 0.4992
|
|
29.54 0.1625 0.2846 0.1206 0.0689 5.647 22.246 20.403 4211.121 2.513 90.755 2.198 0.76 237193. 0.4854
|
|
36.92 0.2031 0.3456 0.1203 0.0707 5.801 22.851 20.360 4325.687 2.582 90.559 2.135 0.76 237635. 0.4710
|
|
44.31 0.2437 0.4021 0.1200 0.0727 5.965 23.496 20.301 4447.754 2.655 90.300 2.070 0.76 238129. 0.4561
|
|
51.69 0.2843 0.4543 0.1195 0.0748 6.135 24.168 20.221 4574.971 2.730 89.942 2.005 0.76 238678. 0.4408
|
|
59.08 0.3249 0.5022 0.1189 0.0769 6.308 24.850 20.109 4704.040 2.808 89.445 1.939 0.77 239285. 0.4252
|
|
66.46 0.3656 0.5459 0.1180 0.0790 6.478 25.518 19.955 4830.613 2.883 88.759 1.874 0.77 239950. 0.4093
|
|
73.85 0.4062 0.5858 0.1167 0.0809 6.637 26.146 19.745 4949.336 2.954 87.827 1.809 0.77 240677. 0.3932
|
|
81.23 0.4468 0.6222 0.1151 0.0826 6.778 26.698 19.467 5053.992 3.016 86.589 1.747 0.77 241466. 0.3769
|
|
88.62 0.4874 0.6553 0.1129 0.0840 6.890 27.141 19.106 5137.798 3.066 84.984 1.687 0.77 242317. 0.3605
|
|
96.00 0.5280 0.6855 0.1102 0.0849 6.965 27.437 18.651 5193.753 3.100 82.958 1.629 0.77 243231. 0.3439
|
|
103.39 0.5686 0.7131 0.1069 0.0853 6.993 27.549 18.089 5215.002 3.112 80.461 1.573 0.77 244207. 0.3272
|
|
110.77 0.6093 0.7383 0.1029 0.0849 6.967 27.444 17.414 5195.193 3.101 77.457 1.520 0.78 245245. 0.3102
|
|
118.16 0.6499 0.7613 0.0982 0.0839 6.878 27.094 16.620 5128.955 3.061 73.927 1.470 0.78 246345. 0.2930
|
|
125.54 0.6905 0.7823 0.0929 0.0820 6.722 26.478 15.707 5012.304 2.991 69.867 1.421 0.78 247503. 0.2755
|
|
132.93 0.7311 0.8012 0.0868 0.0792 6.494 25.581 14.678 4842.492 2.890 65.289 1.375 0.78 248720. 0.2576
|
|
140.31 0.7717 0.8180 0.0800 0.0755 6.193 24.398 13.540 4618.441 2.756 60.227 1.330 0.78 249993. 0.2393
|
|
147.70 0.8123 0.8325 0.0728 0.0710 5.824 22.942 12.310 4342.848 2.592 54.755 1.286 0.79 251321. 0.2206
|
|
155.08 0.8530 0.8443 0.0651 0.0657 5.392 21.239 11.007 4020.495 2.400 48.960 1.242 0.79 252703. 0.2014
|
|
162.47 0.8936 0.8525 0.0570 0.0598 4.903 19.314 9.648 3656.196 2.182 42.916 1.197 0.79 254136. 0.1818
|
|
169.85 0.9342 0.8559 0.0488 0.0532 4.365 17.194 8.248 3254.757 1.943 36.687 1.149 0.79 255621. 0.1614
|
|
177.24 0.9748 0.8518 0.0403 0.0461 3.783 14.903 6.819 2821.093 1.684 30.329 1.096 0.80 257155. 0.1400
|
|
184.62 1.0154 0.8354 0.0318 0.0386 3.166 12.471 5.372 2360.755 1.409 23.895 1.032 0.80 258738. 0.1170
|
|
192.01 1.0560 0.7962 0.0232 0.0307 2.522 9.933 3.921 1880.321 1.122 17.441 0.946 0.80 260369. 0.0916
|
|
199.39 1.0967 0.7081 0.0147 0.0227 1.861 7.331 2.479 1387.817 0.828 11.024 0.810 0.81 262048. 0.0624
|
|
206.78 1.1373 0.4880 0.0063 0.0146 1.197 4.716 1.060 892.650 0.533 4.713 0.538 0.81 263774. 0.0271
|
|
214.16 1.1779
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1215 0.0665 6.542 24.253 23.198 4878.055 2.740 103.184 2.157 0.81 250629. 0.5080
|
|
7.78 0.0403 0.0722 0.1213 0.0677 6.659 24.688 23.167 4965.543 2.789 103.045 2.116 0.81 250903. 0.4980
|
|
15.56 0.0805 0.1413 0.1212 0.0690 6.792 25.183 23.137 5065.068 2.845 102.916 2.072 0.81 251220. 0.4873
|
|
23.34 0.1208 0.2072 0.1210 0.0706 6.942 25.738 23.109 5176.692 2.908 102.788 2.025 0.81 251581. 0.4759
|
|
31.12 0.1611 0.2694 0.1208 0.0722 7.107 26.351 23.078 5300.048 2.977 102.649 1.975 0.81 251991. 0.4639
|
|
38.90 0.2014 0.3279 0.1206 0.0741 7.287 27.018 23.039 5434.142 3.052 102.478 1.923 0.81 252453. 0.4513
|
|
46.68 0.2416 0.3826 0.1204 0.0760 7.479 27.729 22.988 5577.169 3.133 102.250 1.870 0.81 252970. 0.4383
|
|
54.46 0.2819 0.4334 0.1200 0.0781 7.679 28.471 22.916 5726.357 3.217 101.929 1.815 0.81 253545. 0.4249
|
|
62.24 0.3222 0.4803 0.1195 0.0801 7.882 29.224 22.812 5877.729 3.302 101.469 1.760 0.81 254179. 0.4111
|
|
70.02 0.3625 0.5237 0.1187 0.0821 8.081 29.961 22.666 6026.022 3.385 100.818 1.706 0.81 254875. 0.3972
|
|
77.80 0.4027 0.5637 0.1176 0.0840 8.267 30.650 22.462 6164.692 3.463 99.910 1.653 0.82 255635. 0.3830
|
|
85.58 0.4430 0.6006 0.1162 0.0857 8.430 31.254 22.184 6286.094 3.531 98.676 1.601 0.82 256459. 0.3687
|
|
93.36 0.4833 0.6347 0.1142 0.0870 8.558 31.730 21.818 6381.882 3.585 97.045 1.551 0.82 257349. 0.3542
|
|
101.14 0.5236 0.6662 0.1118 0.0878 8.641 32.037 21.346 6443.546 3.619 94.946 1.503 0.82 258304. 0.3394
|
|
108.92 0.5638 0.6955 0.1087 0.0881 8.667 32.133 20.755 6462.984 3.630 92.318 1.457 0.82 259326. 0.3245
|
|
116.70 0.6041 0.7227 0.1049 0.0877 8.627 31.984 20.035 6432.960 3.614 89.114 1.413 0.82 260413. 0.3092
|
|
124.48 0.6444 0.7479 0.1004 0.0865 8.512 31.559 19.178 6347.428 3.565 85.303 1.370 0.83 261563. 0.2934
|
|
132.26 0.6847 0.7710 0.0952 0.0845 8.317 30.837 18.183 6202.240 3.484 80.877 1.330 0.83 262777. 0.2772
|
|
140.04 0.7249 0.7921 0.0893 0.0817 8.039 29.805 17.051 5994.647 3.367 75.845 1.290 0.83 264051. 0.2605
|
|
147.82 0.7652 0.8110 0.0827 0.0780 7.675 28.456 15.791 5723.437 3.215 70.237 1.251 0.83 265385. 0.2431
|
|
155.60 0.8055 0.8274 0.0755 0.0735 7.230 26.805 14.418 5391.245 3.028 64.130 1.213 0.84 266777. 0.2252
|
|
163.38 0.8457 0.8410 0.0678 0.0682 6.710 24.879 12.954 5003.963 2.811 57.621 1.174 0.84 268224. 0.2067
|
|
171.16 0.8860 0.8506 0.0598 0.0623 6.127 22.718 11.420 4569.208 2.567 50.796 1.134 0.84 269726. 0.1873
|
|
178.94 0.9263 0.8547 0.0515 0.0558 5.489 20.350 9.832 4093.062 2.299 43.731 1.089 0.84 271281. 0.1670
|
|
186.72 0.9666 0.8507 0.0430 0.0488 4.802 17.803 8.204 3580.793 2.011 36.493 1.039 0.85 272889. 0.1456
|
|
194.50 1.0068 0.8336 0.0343 0.0414 4.077 15.114 6.552 3039.960 1.708 29.143 0.978 0.85 274547. 0.1224
|
|
202.28 1.0471 0.7928 0.0256 0.0338 3.326 12.331 4.889 2480.137 1.393 21.745 0.894 0.85 276256. 0.0967
|
|
210.06 1.0874 0.7053 0.0169 0.0261 2.565 9.508 3.229 1912.368 1.074 14.363 0.766 0.86 278014. 0.0673
|
|
217.84 1.1277 0.5104 0.0083 0.0184 1.809 6.708 1.590 1349.190 0.758 7.071 0.534 0.86 279821. 0.0330
|
|
225.62 1.1679 -0.0051 0.0000 0.0110 1.078 3.998 -0.009 804.160 0.452 -0.040 -0.005 0.86 281675. 0.0000
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PROP RPM = 18000
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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 0.1213 0.0717 8.370 29.307 25.980 6241.359 3.311 115.557 1.888 0.86 265368. 0.4705
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8.25 0.0403 0.0671 0.1212 0.0729 8.508 29.790 25.947 6344.192 3.366 115.411 1.855 0.86 265658. 0.4620
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16.49 0.0806 0.1316 0.1210 0.0742 8.664 30.339 25.917 6461.032 3.428 115.281 1.819 0.86 265992. 0.4529
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24.74 0.1210 0.1932 0.1209 0.0757 8.841 30.956 25.890 6592.491 3.497 115.160 1.781 0.86 266375. 0.4432
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32.99 0.1613 0.2518 0.1208 0.0774 9.036 31.641 25.862 6738.398 3.575 115.036 1.741 0.86 266809. 0.4329
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41.24 0.2016 0.3071 0.1206 0.0792 9.250 32.389 25.829 6897.613 3.659 114.890 1.698 0.86 267298. 0.4221
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49.48 0.2419 0.3590 0.1204 0.0812 9.478 33.189 25.786 7067.942 3.750 114.694 1.655 0.86 267845. 0.4109
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57.73 0.2822 0.4075 0.1201 0.0832 9.717 34.024 25.722 7245.837 3.844 114.411 1.610 0.86 268453. 0.3993
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65.98 0.3226 0.4528 0.1197 0.0853 9.959 34.871 25.628 7426.155 3.940 113.993 1.565 0.86 269124. 0.3875
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74.23 0.3629 0.4949 0.1191 0.0873 10.194 35.697 25.490 7601.994 4.033 113.379 1.521 0.86 269861. 0.3754
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82.47 0.4032 0.5342 0.1181 0.0892 10.413 36.461 25.291 7764.698 4.119 112.495 1.477 0.86 270666. 0.3633
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90.72 0.4435 0.5709 0.1168 0.0908 10.600 37.116 25.013 7904.171 4.193 111.259 1.435 0.87 271539. 0.3510
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98.97 0.4838 0.6054 0.1151 0.0920 10.740 37.607 24.636 8008.800 4.249 109.582 1.395 0.87 272482. 0.3386
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107.22 0.5242 0.6379 0.1128 0.0927 10.820 37.887 24.142 8068.381 4.280 107.381 1.357 0.87 273495. 0.3261
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115.46 0.5645 0.6687 0.1098 0.0927 10.826 37.909 23.512 8073.045 4.283 104.580 1.321 0.87 274579. 0.3132
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123.71 0.6048 0.6978 0.1062 0.0920 10.747 37.632 22.733 8014.098 4.252 101.116 1.287 0.87 275732. 0.3000
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131.96 0.6451 0.7253 0.1018 0.0905 10.574 37.025 21.795 7884.814 4.183 96.944 1.254 0.87 276954. 0.2862
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140.21 0.6854 0.7511 0.0967 0.0882 10.300 36.066 20.694 7680.673 4.075 92.047 1.222 0.88 278243. 0.2718
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148.45 0.7258 0.7751 0.0908 0.0850 9.924 34.749 19.432 7400.155 3.926 86.434 1.191 0.88 279597. 0.2567
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156.70 0.7661 0.7970 0.0841 0.0809 9.446 33.075 18.017 7043.611 3.737 80.138 1.160 0.88 281014. 0.2408
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164.95 0.8064 0.8164 0.0769 0.0760 8.872 31.065 16.468 6615.641 3.510 73.249 1.129 0.88 282492. 0.2240
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173.19 0.8467 0.8329 0.0692 0.0703 8.213 28.757 14.811 6124.070 3.249 65.880 1.097 0.89 284030. 0.2064
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181.44 0.8870 0.8444 0.0610 0.0641 7.487 26.218 13.068 5583.387 2.962 58.125 1.062 0.89 285626. 0.1876
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189.69 0.9274 0.8484 0.0526 0.0575 6.711 23.499 11.257 5004.427 2.655 50.070 1.020 0.89 287277. 0.1674
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197.94 0.9677 0.8397 0.0439 0.0506 5.905 20.675 9.394 4403.016 2.336 41.783 0.968 0.90 288984. 0.1450
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206.18 1.0080 0.8141 0.0350 0.0434 5.065 17.736 7.500 3777.059 2.004 33.358 0.901 0.90 290745. 0.1206
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214.43 1.0483 0.7591 0.0261 0.0361 4.212 14.749 5.592 3140.905 1.666 24.872 0.807 0.90 292558. 0.0934
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222.68 1.0887 0.6510 0.0172 0.0288 3.365 11.784 3.689 2509.543 1.331 16.410 0.667 0.91 294424. 0.0626
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230.93 1.1290 0.4388 0.0085 0.0218 2.548 8.921 1.816 1899.878 1.008 8.076 0.433 0.91 296342. 0.0286
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239.17 1.1693 -0.0003 0.0000 0.0152 1.780 6.233 -0.001 1327.361 0.704 -0.004 0.000 0.91 298312. 0.0000
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