686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
12x10E (12x10E.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 0.1152 0.0608 0.001 0.077 0.076 0.908 0.009 0.339 38.014 0.05 14786. 0.5128
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0.38 0.0337 0.0624 0.1144 0.0619 0.001 0.078 0.076 0.924 0.009 0.336 37.124 0.05 14800. 0.4991
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0.77 0.0675 0.1217 0.1135 0.0629 0.001 0.079 0.075 0.940 0.009 0.334 36.208 0.05 14816. 0.4849
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1.15 0.1012 0.1778 0.1125 0.0640 0.001 0.081 0.074 0.956 0.009 0.331 35.271 0.05 14833. 0.4703
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1.53 0.1349 0.2307 0.1114 0.0651 0.001 0.082 0.074 0.973 0.009 0.327 34.321 0.05 14853. 0.4553
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1.92 0.1687 0.2804 0.1101 0.0662 0.001 0.084 0.073 0.989 0.009 0.324 33.363 0.05 14874. 0.4400
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2.30 0.2024 0.3268 0.1086 0.0673 0.001 0.085 0.072 1.005 0.010 0.319 32.404 0.05 14898. 0.4245
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2.68 0.2362 0.3700 0.1070 0.0683 0.001 0.086 0.071 1.019 0.010 0.314 31.449 0.05 14925. 0.4088
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3.07 0.2699 0.4101 0.1051 0.0691 0.001 0.087 0.069 1.032 0.010 0.309 30.504 0.05 14953. 0.3930
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3.45 0.3036 0.4473 0.1029 0.0699 0.001 0.088 0.068 1.043 0.010 0.302 29.571 0.05 14984. 0.3770
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3.83 0.3374 0.4816 0.1005 0.0704 0.001 0.089 0.066 1.051 0.010 0.295 28.653 0.05 15018. 0.3610
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4.22 0.3711 0.5131 0.0977 0.0707 0.001 0.089 0.065 1.055 0.010 0.287 27.753 0.05 15054. 0.3448
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4.60 0.4048 0.5419 0.0946 0.0707 0.001 0.089 0.063 1.056 0.010 0.278 26.870 0.05 15093. 0.3286
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4.98 0.4386 0.5681 0.0912 0.0704 0.001 0.089 0.060 1.052 0.010 0.268 26.003 0.05 15134. 0.3122
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5.37 0.4723 0.5918 0.0875 0.0698 0.001 0.088 0.058 1.042 0.010 0.257 25.150 0.05 15178. 0.2956
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5.75 0.5060 0.6127 0.0833 0.0688 0.001 0.087 0.055 1.027 0.010 0.245 24.305 0.05 15224. 0.2788
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6.13 0.5398 0.6309 0.0788 0.0674 0.001 0.085 0.052 1.007 0.010 0.232 23.460 0.05 15273. 0.2618
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6.52 0.5735 0.6459 0.0739 0.0656 0.001 0.083 0.049 0.980 0.009 0.217 22.608 0.05 15324. 0.2444
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6.90 0.6073 0.6575 0.0687 0.0635 0.001 0.080 0.045 0.948 0.009 0.202 21.734 0.05 15378. 0.2265
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7.28 0.6410 0.6650 0.0632 0.0609 0.001 0.077 0.042 0.909 0.009 0.186 20.825 0.05 15434. 0.2081
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7.67 0.6747 0.6676 0.0574 0.0580 0.001 0.073 0.038 0.866 0.008 0.169 19.861 0.05 15493. 0.1891
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8.05 0.7085 0.6643 0.0513 0.0547 0.001 0.069 0.034 0.817 0.008 0.151 18.821 0.05 15554. 0.1695
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8.43 0.7422 0.6536 0.0451 0.0512 0.001 0.065 0.030 0.765 0.007 0.133 17.676 0.05 15618. 0.1492
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8.82 0.7759 0.6335 0.0388 0.0475 0.001 0.060 0.026 0.709 0.007 0.114 16.389 0.05 15683. 0.1283
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9.20 0.8097 0.6014 0.0323 0.0435 0.001 0.055 0.021 0.649 0.006 0.095 14.911 0.05 15751. 0.1065
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9.58 0.8434 0.5533 0.0258 0.0393 0.001 0.050 0.017 0.587 0.006 0.076 13.168 0.05 15822. 0.0841
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9.97 0.8771 0.4829 0.0193 0.0350 0.001 0.044 0.013 0.522 0.005 0.057 11.052 0.05 15895. 0.0610
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10.35 0.9109 0.3807 0.0128 0.0305 0.001 0.039 0.008 0.456 0.004 0.037 8.390 0.05 15969. 0.0377
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10.73 0.9446 0.2302 0.0063 0.0259 0.001 0.033 0.004 0.387 0.004 0.019 4.891 0.05 16047. 0.0155
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11.12 0.9784 0.0010 0.0000 0.0213 0.000 0.027 0.000 0.318 0.003 0.000 0.020 0.05 16126. 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 0.1156 0.0558 0.009 0.282 0.306 6.661 0.032 1.359 20.803 0.10 29572. 0.5623
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0.77 0.0340 0.0686 0.1148 0.0569 0.009 0.287 0.303 6.791 0.032 1.350 20.269 0.10 29600. 0.5460
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1.54 0.0679 0.1335 0.1139 0.0580 0.009 0.293 0.301 6.927 0.033 1.340 19.721 0.10 29631. 0.5292
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2.32 0.1019 0.1946 0.1130 0.0592 0.009 0.299 0.299 7.067 0.034 1.328 19.163 0.10 29667. 0.5120
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3.09 0.1359 0.2518 0.1118 0.0604 0.010 0.305 0.296 7.209 0.034 1.315 18.600 0.10 29707. 0.4945
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3.86 0.1698 0.3052 0.1106 0.0615 0.010 0.311 0.292 7.350 0.035 1.300 18.035 0.10 29750. 0.4767
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4.63 0.2038 0.3548 0.1091 0.0627 0.010 0.316 0.288 7.486 0.036 1.283 17.473 0.10 29799. 0.4588
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5.40 0.2378 0.4008 0.1074 0.0637 0.010 0.322 0.284 7.614 0.036 1.263 16.917 0.10 29852. 0.4408
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6.18 0.2718 0.4432 0.1055 0.0647 0.010 0.327 0.279 7.729 0.037 1.241 16.370 0.10 29910. 0.4228
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6.95 0.3057 0.4823 0.1034 0.0655 0.010 0.331 0.273 7.826 0.037 1.215 15.834 0.10 29972. 0.4047
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7.72 0.3397 0.5182 0.1009 0.0661 0.011 0.334 0.267 7.901 0.038 1.186 15.311 0.10 30040. 0.3867
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8.49 0.3737 0.5511 0.0981 0.0665 0.011 0.336 0.259 7.948 0.038 1.154 14.803 0.10 30113. 0.3687
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9.26 0.4076 0.5812 0.0950 0.0666 0.011 0.336 0.251 7.962 0.038 1.117 14.309 0.10 30192. 0.3507
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10.04 0.4416 0.6085 0.0916 0.0664 0.011 0.335 0.242 7.937 0.038 1.076 13.830 0.10 30275. 0.3327
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10.81 0.4756 0.6332 0.0877 0.0659 0.011 0.333 0.232 7.871 0.038 1.031 13.363 0.10 30364. 0.3147
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11.58 0.5095 0.6553 0.0835 0.0649 0.010 0.328 0.221 7.758 0.037 0.982 12.907 0.10 30458. 0.2966
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12.35 0.5435 0.6747 0.0790 0.0636 0.010 0.321 0.209 7.598 0.036 0.928 12.458 0.10 30557. 0.2783
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13.12 0.5775 0.6912 0.0740 0.0618 0.010 0.312 0.196 7.387 0.035 0.870 12.012 0.10 30661. 0.2598
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13.90 0.6115 0.7044 0.0687 0.0596 0.010 0.301 0.182 7.125 0.034 0.808 11.563 0.10 30770. 0.2410
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14.67 0.6454 0.7140 0.0631 0.0570 0.009 0.288 0.167 6.813 0.033 0.742 11.104 0.10 30884. 0.2217
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15.44 0.6794 0.7193 0.0572 0.0541 0.009 0.273 0.151 6.457 0.031 0.673 10.626 0.10 31003. 0.2021
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16.21 0.7134 0.7191 0.0511 0.0507 0.008 0.256 0.135 6.059 0.029 0.601 10.118 0.10 31126. 0.1819
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16.98 0.7473 0.7122 0.0449 0.0471 0.008 0.238 0.119 5.625 0.027 0.528 9.565 0.10 31255. 0.1611
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17.76 0.7813 0.6967 0.0385 0.0432 0.007 0.218 0.102 5.158 0.025 0.453 8.950 0.10 31388. 0.1396
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18.53 0.8153 0.6695 0.0320 0.0390 0.006 0.197 0.085 4.661 0.022 0.377 8.243 0.10 31526. 0.1173
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19.30 0.8492 0.6262 0.0255 0.0346 0.006 0.175 0.068 4.138 0.020 0.300 7.401 0.10 31668. 0.0940
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20.07 0.8832 0.5593 0.0190 0.0301 0.005 0.152 0.050 3.592 0.017 0.224 6.356 0.10 31816. 0.0697
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20.84 0.9172 0.4554 0.0126 0.0253 0.004 0.128 0.033 3.027 0.014 0.148 4.984 0.10 31967. 0.0444
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21.62 0.9511 0.2888 0.0062 0.0205 0.003 0.104 0.016 2.449 0.012 0.073 3.048 0.10 32124. 0.0191
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22.39 0.9851 0.0014 0.0000 0.0156 0.002 0.079 0.000 1.863 0.009 0.000 0.014 0.10 32284. 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 0.1158 0.0536 0.029 0.608 0.689 21.595 0.069 3.064 14.468 0.14 44357. 0.5872
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1.16 0.0341 0.0717 0.1151 0.0547 0.030 0.621 0.684 22.044 0.070 3.044 14.080 0.14 44399. 0.5695
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2.32 0.0682 0.1394 0.1142 0.0558 0.030 0.634 0.679 22.515 0.072 3.021 13.683 0.14 44447. 0.5514
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3.49 0.1022 0.2029 0.1132 0.0571 0.031 0.648 0.673 23.002 0.073 2.995 13.279 0.14 44501. 0.5328
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4.65 0.1363 0.2622 0.1121 0.0583 0.032 0.662 0.667 23.496 0.075 2.966 12.873 0.14 44560. 0.5140
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5.81 0.1704 0.3175 0.1109 0.0595 0.032 0.676 0.659 23.987 0.076 2.933 12.467 0.14 44626. 0.4950
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6.97 0.2045 0.3686 0.1094 0.0607 0.033 0.689 0.651 24.464 0.078 2.894 12.063 0.14 44699. 0.4758
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8.13 0.2385 0.4159 0.1077 0.0618 0.033 0.702 0.641 24.914 0.079 2.850 11.666 0.14 44779. 0.4566
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9.29 0.2726 0.4594 0.1058 0.0628 0.034 0.713 0.629 25.320 0.081 2.800 11.275 0.14 44866. 0.4374
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10.46 0.3067 0.4994 0.1037 0.0637 0.034 0.723 0.617 25.667 0.082 2.742 10.895 0.14 44961. 0.4183
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11.62 0.3408 0.5360 0.1012 0.0643 0.035 0.731 0.602 25.938 0.083 2.677 10.525 0.14 45064. 0.3992
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12.78 0.3749 0.5696 0.0984 0.0648 0.035 0.736 0.585 26.113 0.083 2.603 10.166 0.14 45174. 0.3803
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13.94 0.4089 0.6002 0.0953 0.0649 0.035 0.737 0.567 26.176 0.083 2.521 9.820 0.14 45292. 0.3615
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15.10 0.4430 0.6280 0.0918 0.0648 0.035 0.736 0.546 26.108 0.083 2.429 9.485 0.14 45418. 0.3427
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16.26 0.4771 0.6532 0.0879 0.0642 0.035 0.730 0.523 25.896 0.082 2.327 9.161 0.14 45552. 0.3240
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17.43 0.5112 0.6759 0.0837 0.0633 0.034 0.719 0.498 25.525 0.081 2.215 8.847 0.14 45693. 0.3052
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18.59 0.5452 0.6959 0.0791 0.0620 0.034 0.704 0.470 24.988 0.080 2.093 8.540 0.14 45843. 0.2864
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19.75 0.5793 0.7131 0.0741 0.0602 0.033 0.684 0.441 24.277 0.077 1.961 8.237 0.15 45999. 0.2674
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20.91 0.6134 0.7274 0.0688 0.0580 0.031 0.659 0.409 23.388 0.074 1.820 7.934 0.15 46164. 0.2481
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22.07 0.6475 0.7381 0.0631 0.0554 0.030 0.629 0.375 22.327 0.071 1.670 7.628 0.15 46336. 0.2286
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23.23 0.6815 0.7449 0.0572 0.0524 0.028 0.595 0.340 21.108 0.067 1.514 7.313 0.15 46515. 0.2086
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24.40 0.7156 0.7466 0.0511 0.0490 0.026 0.556 0.304 19.746 0.063 1.352 6.981 0.15 46702. 0.1882
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25.56 0.7497 0.7421 0.0448 0.0453 0.024 0.514 0.267 18.255 0.058 1.186 6.624 0.15 46896. 0.1672
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26.72 0.7838 0.7295 0.0384 0.0413 0.022 0.469 0.229 16.646 0.053 1.017 6.228 0.15 47097. 0.1456
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27.88 0.8179 0.7058 0.0320 0.0370 0.020 0.421 0.190 14.931 0.048 0.845 5.774 0.15 47305. 0.1231
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29.04 0.8519 0.6663 0.0255 0.0325 0.018 0.370 0.151 13.121 0.042 0.673 5.233 0.15 47520. 0.0996
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30.20 0.8860 0.6030 0.0190 0.0279 0.015 0.316 0.113 11.230 0.036 0.501 4.554 0.15 47742. 0.0748
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31.37 0.9201 0.5007 0.0125 0.0230 0.012 0.261 0.074 9.273 0.030 0.331 3.641 0.15 47971. 0.0486
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32.53 0.9542 0.3273 0.0062 0.0180 0.010 0.205 0.037 7.268 0.023 0.164 2.295 0.15 48207. 0.0215
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33.69 0.9882 0.0012 0.0000 0.0130 0.007 0.147 0.000 5.234 0.017 0.000 0.008 0.15 48449. 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 0.1160 0.0523 0.067 1.056 1.227 49.984 0.119 5.457 11.132 0.19 59142. 0.6029
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1.55 0.0341 0.0737 0.1153 0.0534 0.068 1.079 1.219 51.066 0.122 5.421 10.826 0.19 59199. 0.5844
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3.10 0.0683 0.1431 0.1144 0.0546 0.070 1.103 1.210 52.203 0.125 5.382 10.512 0.19 59263. 0.5654
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4.66 0.1024 0.2081 0.1135 0.0559 0.072 1.128 1.200 53.378 0.127 5.336 10.195 0.19 59334. 0.5460
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6.21 0.1366 0.2688 0.1124 0.0571 0.073 1.153 1.188 54.572 0.130 5.285 9.875 0.19 59414. 0.5263
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7.76 0.1707 0.3251 0.1111 0.0584 0.075 1.178 1.175 55.763 0.133 5.226 9.556 0.19 59502. 0.5065
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9.31 0.2049 0.3772 0.1097 0.0596 0.076 1.203 1.160 56.921 0.136 5.158 9.240 0.19 59599. 0.4865
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10.87 0.2390 0.4253 0.1080 0.0607 0.078 1.226 1.142 58.015 0.138 5.080 8.929 0.19 59706. 0.4666
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12.42 0.2732 0.4695 0.1061 0.0617 0.079 1.247 1.122 59.008 0.141 4.990 8.624 0.19 59823. 0.4466
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13.97 0.3073 0.5100 0.1039 0.0626 0.080 1.265 1.099 59.860 0.143 4.888 8.327 0.19 59950. 0.4269
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15.52 0.3415 0.5471 0.1015 0.0633 0.081 1.279 1.073 60.529 0.145 4.772 8.040 0.19 60087. 0.4072
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17.07 0.3756 0.5810 0.0987 0.0638 0.082 1.288 1.043 60.972 0.146 4.641 7.762 0.19 60235. 0.3877
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18.63 0.4098 0.6119 0.0955 0.0640 0.082 1.292 1.010 61.145 0.146 4.494 7.494 0.19 60393. 0.3683
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20.18 0.4439 0.6401 0.0921 0.0638 0.082 1.289 0.973 61.006 0.146 4.329 7.236 0.19 60561. 0.3491
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21.73 0.4781 0.6656 0.0882 0.0633 0.081 1.279 0.932 60.519 0.144 4.147 6.987 0.19 60740. 0.3299
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23.28 0.5122 0.6886 0.0839 0.0624 0.080 1.260 0.887 59.652 0.142 3.947 6.747 0.19 60930. 0.3107
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24.83 0.5464 0.7091 0.0793 0.0611 0.078 1.234 0.838 58.383 0.139 3.729 6.513 0.19 61130. 0.2916
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26.39 0.5805 0.7268 0.0743 0.0593 0.076 1.198 0.785 56.694 0.135 3.493 6.283 0.19 61340. 0.2723
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27.94 0.6147 0.7417 0.0689 0.0571 0.073 1.153 0.729 54.575 0.130 3.241 6.056 0.19 61560. 0.2527
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29.49 0.6488 0.7533 0.0632 0.0545 0.070 1.100 0.668 52.039 0.124 2.973 5.827 0.19 61790. 0.2329
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31.04 0.6830 0.7611 0.0573 0.0514 0.066 1.038 0.606 49.120 0.117 2.694 5.592 0.19 62030. 0.2128
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32.60 0.7171 0.7642 0.0511 0.0480 0.061 0.969 0.541 45.854 0.109 2.405 5.348 0.20 62280. 0.1923
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34.15 0.7512 0.7614 0.0448 0.0442 0.057 0.893 0.474 42.272 0.101 2.108 5.086 0.20 62540. 0.1712
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35.70 0.7854 0.7508 0.0384 0.0402 0.051 0.811 0.406 38.401 0.092 1.807 4.797 0.20 62809. 0.1495
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37.25 0.8195 0.7297 0.0319 0.0359 0.046 0.724 0.338 34.268 0.082 1.501 4.468 0.20 63087. 0.1269
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38.80 0.8537 0.6932 0.0254 0.0313 0.040 0.632 0.269 29.905 0.071 1.195 4.075 0.20 63375. 0.1033
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40.36 0.8878 0.6329 0.0189 0.0265 0.034 0.535 0.200 25.342 0.060 0.889 3.577 0.20 63672. 0.0782
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41.91 0.9220 0.5325 0.0125 0.0216 0.028 0.436 0.132 20.617 0.049 0.586 2.898 0.20 63978. 0.0514
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43.46 0.9561 0.3553 0.0061 0.0165 0.021 0.333 0.065 15.775 0.038 0.288 1.865 0.20 64294. 0.0232
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45.01 0.9903 -0.0020 0.0000 0.0114 0.015 0.230 0.000 10.863 0.026 -0.001 -0.010 0.20 64618. 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 0.1162 0.0515 0.129 1.625 1.920 96.128 0.184 8.541 9.060 0.24 73927. 0.6139
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1.94 0.0342 0.0750 0.1155 0.0526 0.132 1.661 1.908 98.267 0.188 8.487 8.807 0.24 73998. 0.5948
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3.89 0.0684 0.1456 0.1147 0.0539 0.135 1.699 1.894 100.516 0.192 8.426 8.548 0.24 74077. 0.5752
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5.83 0.1026 0.2117 0.1137 0.0551 0.138 1.739 1.879 102.844 0.196 8.356 8.285 0.24 74167. 0.5553
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7.77 0.1368 0.2732 0.1126 0.0564 0.141 1.779 1.861 105.213 0.201 8.276 8.021 0.24 74267. 0.5350
|
|
9.71 0.1709 0.3303 0.1114 0.0576 0.144 1.819 1.840 107.578 0.205 8.185 7.758 0.24 74377. 0.5146
|
|
11.66 0.2051 0.3831 0.1100 0.0589 0.147 1.858 1.816 109.883 0.210 8.080 7.498 0.24 74499. 0.4941
|
|
13.60 0.2393 0.4317 0.1083 0.0600 0.150 1.894 1.789 112.064 0.214 7.958 7.242 0.24 74633. 0.4736
|
|
15.54 0.2735 0.4763 0.1064 0.0611 0.153 1.928 1.758 114.048 0.218 7.819 6.991 0.24 74779. 0.4533
|
|
17.48 0.3077 0.5172 0.1042 0.0620 0.155 1.957 1.722 115.758 0.221 7.660 6.748 0.24 74938. 0.4330
|
|
19.43 0.3419 0.5546 0.1018 0.0627 0.157 1.980 1.681 117.111 0.224 7.479 6.512 0.24 75110. 0.4129
|
|
21.37 0.3761 0.5888 0.0990 0.0632 0.158 1.995 1.635 118.018 0.225 7.274 6.285 0.24 75295. 0.3930
|
|
23.31 0.4103 0.6200 0.0959 0.0634 0.159 2.001 1.584 118.394 0.226 7.044 6.067 0.24 75493. 0.3733
|
|
25.25 0.4445 0.6484 0.0923 0.0633 0.158 1.997 1.526 118.155 0.226 6.786 5.857 0.24 75704. 0.3537
|
|
27.20 0.4786 0.6741 0.0885 0.0628 0.157 1.982 1.461 117.228 0.224 6.500 5.654 0.24 75929. 0.3342
|
|
29.14 0.5128 0.6974 0.0842 0.0619 0.155 1.953 1.391 115.551 0.221 6.187 5.460 0.24 76166. 0.3148
|
|
31.08 0.5470 0.7182 0.0795 0.0606 0.152 1.912 1.314 113.077 0.216 5.845 5.271 0.24 76417. 0.2954
|
|
33.02 0.5812 0.7363 0.0745 0.0588 0.147 1.856 1.231 109.773 0.210 5.475 5.086 0.24 76680. 0.2759
|
|
34.97 0.6154 0.7517 0.0691 0.0566 0.142 1.785 1.142 105.614 0.202 5.079 4.904 0.24 76956. 0.2562
|
|
36.91 0.6496 0.7640 0.0634 0.0539 0.135 1.701 1.047 100.628 0.192 4.659 4.721 0.24 77244. 0.2363
|
|
38.85 0.6838 0.7726 0.0574 0.0508 0.127 1.604 0.949 94.880 0.181 4.220 4.536 0.24 77545. 0.2160
|
|
40.79 0.7180 0.7767 0.0513 0.0474 0.119 1.495 0.847 88.439 0.169 3.767 4.343 0.24 77858. 0.1954
|
|
42.74 0.7521 0.7752 0.0449 0.0436 0.109 1.375 0.742 81.366 0.155 3.302 4.138 0.24 78183. 0.1743
|
|
44.68 0.7863 0.7664 0.0385 0.0395 0.099 1.246 0.636 73.715 0.141 2.829 3.913 0.25 78520. 0.1526
|
|
46.62 0.8205 0.7473 0.0320 0.0351 0.088 1.108 0.528 65.542 0.125 2.350 3.657 0.25 78869. 0.1300
|
|
48.56 0.8547 0.7134 0.0254 0.0305 0.076 0.962 0.420 56.903 0.109 1.870 3.351 0.25 79230. 0.1062
|
|
50.51 0.8889 0.6560 0.0189 0.0256 0.064 0.809 0.313 47.865 0.091 1.391 2.963 0.25 79602. 0.0810
|
|
52.45 0.9231 0.5580 0.0125 0.0206 0.052 0.651 0.206 38.504 0.074 0.916 2.427 0.25 79986. 0.0539
|
|
54.39 0.9573 0.3793 0.0061 0.0155 0.039 0.489 0.101 28.907 0.055 0.451 1.591 0.25 80381. 0.0248
|
|
56.33 0.9915 -0.0022 0.0000 0.0103 0.026 0.324 0.000 19.172 0.037 -0.002 -0.009 0.25 80787. 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 0.1165 0.0510 0.220 2.316 2.770 164.396 0.262 12.323 7.644 0.29 88711. 0.6221
|
|
2.33 0.0342 0.0760 0.1157 0.0521 0.225 2.368 2.753 168.131 0.268 12.246 7.427 0.29 88796. 0.6026
|
|
4.67 0.0684 0.1474 0.1149 0.0533 0.231 2.424 2.734 172.060 0.274 12.159 7.206 0.29 88892. 0.5826
|
|
7.00 0.1026 0.2142 0.1140 0.0546 0.236 2.481 2.712 176.131 0.280 12.061 6.983 0.29 88999. 0.5622
|
|
9.33 0.1368 0.2764 0.1129 0.0559 0.242 2.540 2.686 180.280 0.287 11.948 6.758 0.29 89119. 0.5416
|
|
11.66 0.1711 0.3341 0.1117 0.0572 0.247 2.598 2.657 184.426 0.294 11.817 6.534 0.29 89252. 0.5208
|
|
14.00 0.2053 0.3873 0.1103 0.0584 0.253 2.655 2.623 188.474 0.300 11.667 6.312 0.29 89398. 0.4999
|
|
16.33 0.2395 0.4363 0.1086 0.0596 0.258 2.709 2.584 192.310 0.306 11.494 6.095 0.29 89559. 0.4791
|
|
18.66 0.2737 0.4812 0.1067 0.0607 0.263 2.758 2.539 195.810 0.312 11.295 5.882 0.29 89735. 0.4583
|
|
20.99 0.3079 0.5224 0.1046 0.0616 0.267 2.801 2.488 198.836 0.316 11.067 5.676 0.29 89926. 0.4378
|
|
23.33 0.3421 0.5600 0.1021 0.0624 0.270 2.835 2.430 201.242 0.320 10.807 5.476 0.29 90132. 0.4174
|
|
25.66 0.3763 0.5944 0.0993 0.0629 0.272 2.858 2.363 202.875 0.323 10.513 5.284 0.29 90354. 0.3972
|
|
27.99 0.4105 0.6257 0.0962 0.0631 0.273 2.868 2.289 203.583 0.324 10.181 5.099 0.29 90592. 0.3772
|
|
30.32 0.4447 0.6543 0.0927 0.0630 0.273 2.863 2.205 203.220 0.323 9.809 4.922 0.29 90846. 0.3574
|
|
32.66 0.4790 0.6803 0.0888 0.0625 0.270 2.841 2.113 201.656 0.321 9.397 4.752 0.29 91116. 0.3377
|
|
34.99 0.5132 0.7038 0.0845 0.0616 0.267 2.800 2.011 198.781 0.316 8.944 4.588 0.29 91401. 0.3181
|
|
37.32 0.5474 0.7248 0.0799 0.0603 0.261 2.740 1.900 194.514 0.310 8.450 4.430 0.29 91702. 0.2986
|
|
39.65 0.5816 0.7433 0.0748 0.0585 0.253 2.660 1.780 188.793 0.300 7.916 4.276 0.29 92019. 0.2789
|
|
41.99 0.6158 0.7591 0.0694 0.0563 0.243 2.558 1.651 181.577 0.289 7.344 4.124 0.29 92350. 0.2591
|
|
44.32 0.6500 0.7719 0.0637 0.0536 0.232 2.436 1.515 172.907 0.275 6.737 3.973 0.29 92697. 0.2391
|
|
46.65 0.6842 0.7812 0.0577 0.0505 0.218 2.295 1.372 162.900 0.259 6.102 3.820 0.29 93059. 0.2188
|
|
48.98 0.7184 0.7862 0.0515 0.0470 0.203 2.137 1.224 151.675 0.241 5.446 3.661 0.29 93435. 0.1981
|
|
51.32 0.7526 0.7859 0.0451 0.0432 0.187 1.963 1.073 139.334 0.222 4.773 3.493 0.29 93825. 0.1769
|
|
53.65 0.7869 0.7785 0.0386 0.0391 0.169 1.775 0.919 125.975 0.200 4.089 3.310 0.29 94230. 0.1552
|
|
55.98 0.8211 0.7613 0.0321 0.0346 0.150 1.573 0.764 111.692 0.178 3.398 3.102 0.30 94650. 0.1326
|
|
58.31 0.8553 0.7296 0.0255 0.0299 0.130 1.361 0.608 96.588 0.154 2.703 2.854 0.30 95083. 0.1088
|
|
60.65 0.8895 0.6749 0.0190 0.0250 0.108 1.138 0.452 80.778 0.129 2.011 2.538 0.30 95530. 0.0834
|
|
62.98 0.9237 0.5795 0.0125 0.0200 0.086 0.907 0.298 64.397 0.102 1.326 2.099 0.30 95991. 0.0560
|
|
65.31 0.9579 0.4008 0.0062 0.0148 0.064 0.671 0.147 47.601 0.076 0.653 1.400 0.30 96466. 0.0262
|
|
67.65 0.9921 0.0001 0.0000 0.0095 0.041 0.431 0.000 30.563 0.049 0.000 0.000 0.30 96953. 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 0.1167 0.0506 0.348 3.131 3.779 259.269 0.354 16.808 6.610 0.33 103494. 0.6283
|
|
2.72 0.0342 0.0767 0.1160 0.0518 0.356 3.203 3.756 265.256 0.362 16.705 6.422 0.33 103593. 0.6086
|
|
5.45 0.0685 0.1488 0.1152 0.0530 0.364 3.279 3.730 271.561 0.370 16.590 6.230 0.33 103705. 0.5883
|
|
8.17 0.1027 0.2162 0.1143 0.0543 0.373 3.358 3.700 278.102 0.379 16.458 6.035 0.33 103830. 0.5676
|
|
10.89 0.1370 0.2789 0.1132 0.0556 0.382 3.439 3.666 284.775 0.388 16.307 5.839 0.33 103970. 0.5467
|
|
13.62 0.1712 0.3369 0.1120 0.0569 0.391 3.519 3.627 291.454 0.398 16.132 5.644 0.33 104125. 0.5256
|
|
16.34 0.2054 0.3905 0.1106 0.0582 0.400 3.598 3.581 297.982 0.407 15.930 5.451 0.33 104297. 0.5044
|
|
19.06 0.2397 0.4398 0.1090 0.0594 0.408 3.673 3.529 304.179 0.415 15.697 5.262 0.33 104485. 0.4833
|
|
21.79 0.2739 0.4850 0.1071 0.0605 0.416 3.741 3.468 309.845 0.423 15.428 5.077 0.33 104690. 0.4624
|
|
24.51 0.3081 0.5263 0.1050 0.0615 0.422 3.801 3.399 314.757 0.429 15.119 4.898 0.33 104913. 0.4416
|
|
27.23 0.3424 0.5641 0.1025 0.0622 0.427 3.848 3.320 318.678 0.435 14.766 4.725 0.34 105154. 0.4210
|
|
29.96 0.3766 0.5987 0.0997 0.0627 0.431 3.880 3.230 321.365 0.438 14.366 4.558 0.34 105414. 0.4006
|
|
32.68 0.4109 0.6302 0.0966 0.0630 0.433 3.895 3.128 322.571 0.440 13.914 4.399 0.34 105692. 0.3804
|
|
35.41 0.4451 0.6589 0.0931 0.0629 0.432 3.889 3.014 322.060 0.439 13.408 4.245 0.34 105989. 0.3604
|
|
38.13 0.4793 0.6851 0.0892 0.0624 0.429 3.859 2.888 319.619 0.436 12.846 4.099 0.34 106304. 0.3406
|
|
40.85 0.5136 0.7088 0.0849 0.0615 0.423 3.804 2.749 315.072 0.430 12.228 3.958 0.34 106637. 0.3208
|
|
43.58 0.5478 0.7300 0.0802 0.0602 0.413 3.722 2.597 308.286 0.421 11.553 3.821 0.34 106989. 0.3011
|
|
46.30 0.5820 0.7488 0.0751 0.0584 0.401 3.612 2.433 299.160 0.408 10.823 3.689 0.34 107359. 0.2814
|
|
49.02 0.6163 0.7649 0.0697 0.0562 0.386 3.473 2.257 287.626 0.392 10.040 3.559 0.34 107747. 0.2615
|
|
51.75 0.6505 0.7782 0.0639 0.0535 0.367 3.305 2.070 273.751 0.373 9.209 3.430 0.34 108152. 0.2413
|
|
54.47 0.6848 0.7880 0.0579 0.0503 0.346 3.112 1.875 257.718 0.352 8.341 3.300 0.34 108574. 0.2210
|
|
57.19 0.7190 0.7938 0.0517 0.0468 0.321 2.894 1.673 239.716 0.327 7.443 3.166 0.34 109014. 0.2003
|
|
59.92 0.7532 0.7944 0.0453 0.0429 0.295 2.655 1.466 219.912 0.300 6.522 3.024 0.34 109471. 0.1791
|
|
62.64 0.7875 0.7882 0.0388 0.0387 0.266 2.396 1.256 198.458 0.271 5.586 2.870 0.34 109944. 0.1573
|
|
65.36 0.8217 0.7725 0.0322 0.0343 0.235 2.119 1.043 175.510 0.239 4.640 2.696 0.34 110434. 0.1346
|
|
68.09 0.8559 0.7426 0.0256 0.0295 0.203 1.826 0.830 151.233 0.206 3.690 2.488 0.35 110940. 0.1108
|
|
70.81 0.8902 0.6901 0.0190 0.0246 0.169 1.519 0.617 125.813 0.172 2.743 2.223 0.35 111462. 0.0853
|
|
73.53 0.9244 0.5967 0.0125 0.0194 0.133 1.201 0.406 99.469 0.136 1.806 1.851 0.35 112001. 0.0577
|
|
76.26 0.9587 0.4172 0.0062 0.0141 0.097 0.875 0.199 72.456 0.099 0.887 1.248 0.35 112556. 0.0272
|
|
78.98 0.9929 -0.0048 0.0000 0.0088 0.060 0.544 -0.001 45.053 0.061 -0.006 -0.014 0.35 113125. 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 0.1170 0.0504 0.517 4.072 4.947 385.372 0.460 22.003 5.822 0.38 118276. 0.6332
|
|
3.11 0.0342 0.0772 0.1163 0.0516 0.529 4.167 4.918 394.387 0.471 21.873 5.655 0.38 118389. 0.6132
|
|
6.23 0.0685 0.1497 0.1155 0.0528 0.542 4.267 4.884 403.891 0.482 21.726 5.485 0.38 118517. 0.5928
|
|
9.34 0.1027 0.2175 0.1146 0.0541 0.555 4.372 4.847 413.761 0.494 21.557 5.313 0.38 118660. 0.5719
|
|
12.45 0.1370 0.2806 0.1136 0.0554 0.568 4.478 4.803 423.846 0.506 21.364 5.140 0.38 118820. 0.5508
|
|
15.56 0.1712 0.3390 0.1124 0.0568 0.582 4.585 4.753 433.951 0.518 21.139 4.967 0.38 118998. 0.5295
|
|
18.68 0.2055 0.3928 0.1110 0.0581 0.595 4.689 4.694 443.844 0.530 20.880 4.797 0.38 119193. 0.5082
|
|
21.79 0.2397 0.4423 0.1094 0.0593 0.608 4.789 4.627 453.254 0.541 20.579 4.630 0.38 119408. 0.4869
|
|
24.90 0.2739 0.4877 0.1075 0.0604 0.619 4.880 4.548 461.873 0.551 20.231 4.467 0.38 119643. 0.4658
|
|
28.02 0.3082 0.5292 0.1054 0.0614 0.629 4.959 4.458 469.368 0.560 19.831 4.308 0.38 119898. 0.4448
|
|
31.13 0.3424 0.5671 0.1030 0.0622 0.637 5.023 4.355 475.381 0.567 19.373 4.156 0.38 120174. 0.4241
|
|
34.24 0.3767 0.6018 0.1002 0.0627 0.643 5.066 4.238 479.541 0.572 18.852 4.009 0.38 120471. 0.4035
|
|
37.36 0.4109 0.6334 0.0971 0.0630 0.646 5.087 4.106 481.473 0.575 18.263 3.868 0.38 120789. 0.3832
|
|
40.47 0.4452 0.6623 0.0936 0.0629 0.645 5.080 3.957 480.820 0.574 17.603 3.733 0.38 121128. 0.3631
|
|
43.58 0.4794 0.6886 0.0897 0.0624 0.640 5.042 3.792 477.258 0.570 16.869 3.604 0.39 121489. 0.3432
|
|
46.69 0.5136 0.7125 0.0854 0.0615 0.631 4.971 3.610 470.517 0.562 16.059 3.480 0.39 121870. 0.3234
|
|
49.81 0.5479 0.7339 0.0807 0.0602 0.617 4.864 3.412 460.394 0.550 15.176 3.361 0.39 122273. 0.3036
|
|
52.92 0.5821 0.7530 0.0756 0.0584 0.599 4.720 3.197 446.734 0.533 14.219 3.246 0.39 122696. 0.2837
|
|
56.03 0.6164 0.7695 0.0701 0.0562 0.576 4.537 2.966 429.434 0.513 13.191 3.132 0.39 123139. 0.2638
|
|
59.15 0.6506 0.7831 0.0643 0.0534 0.548 4.317 2.721 408.587 0.488 12.102 3.020 0.39 123602. 0.2436
|
|
62.26 0.6849 0.7935 0.0583 0.0503 0.516 4.062 2.464 384.469 0.459 10.962 2.907 0.39 124086. 0.2232
|
|
65.37 0.7191 0.8000 0.0520 0.0467 0.479 3.776 2.199 357.361 0.427 9.783 2.791 0.39 124588. 0.2024
|
|
68.49 0.7533 0.8015 0.0456 0.0428 0.439 3.460 1.928 327.515 0.391 8.574 2.670 0.39 125110. 0.1812
|
|
71.60 0.7876 0.7964 0.0390 0.0386 0.396 3.118 1.651 295.162 0.352 7.344 2.537 0.39 125651. 0.1594
|
|
74.71 0.8218 0.7821 0.0324 0.0341 0.349 2.753 1.372 260.536 0.311 6.101 2.388 0.39 126211. 0.1367
|
|
77.82 0.8561 0.7541 0.0258 0.0293 0.300 2.365 1.091 223.887 0.267 4.853 2.210 0.39 126790. 0.1129
|
|
80.94 0.8903 0.7039 0.0192 0.0243 0.249 1.960 0.811 185.501 0.221 3.609 1.984 0.40 127388. 0.0874
|
|
84.05 0.9246 0.6132 0.0126 0.0191 0.195 1.539 0.535 145.707 0.174 2.378 1.664 0.40 128004. 0.0595
|
|
87.16 0.9588 0.4349 0.0062 0.0137 0.141 1.108 0.263 104.896 0.125 1.171 1.138 0.40 128638. 0.0286
|
|
90.28 0.9930 -0.0010 0.0000 0.0083 0.085 0.671 0.000 63.494 0.076 -0.002 -0.002 0.40 129288. 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 0.1173 0.0503 0.734 5.142 6.276 547.523 0.581 27.917 5.199 0.43 133057. 0.6369
|
|
3.50 0.0343 0.0776 0.1166 0.0515 0.752 5.264 6.241 560.471 0.595 27.758 5.050 0.43 133185. 0.6169
|
|
7.01 0.0685 0.1504 0.1158 0.0527 0.770 5.392 6.200 574.140 0.609 27.577 4.898 0.43 133328. 0.5963
|
|
10.51 0.1028 0.2185 0.1150 0.0541 0.789 5.525 6.153 588.355 0.624 27.369 4.744 0.43 133489. 0.5754
|
|
14.01 0.1370 0.2819 0.1140 0.0554 0.808 5.662 6.099 602.898 0.640 27.130 4.589 0.43 133669. 0.5541
|
|
17.51 0.1713 0.3405 0.1128 0.0567 0.828 5.799 6.037 617.493 0.655 26.852 4.434 0.43 133869. 0.5327
|
|
21.02 0.2055 0.3945 0.1114 0.0580 0.847 5.933 5.964 631.803 0.670 26.529 4.282 0.43 134089. 0.5113
|
|
24.52 0.2398 0.4442 0.1099 0.0593 0.866 6.062 5.880 645.438 0.685 26.154 4.132 0.43 134331. 0.4899
|
|
28.02 0.2740 0.4897 0.1080 0.0604 0.882 6.179 5.782 657.955 0.698 25.719 3.986 0.43 134595. 0.4687
|
|
31.53 0.3083 0.5313 0.1059 0.0614 0.897 6.282 5.669 668.871 0.710 25.217 3.844 0.43 134883. 0.4476
|
|
35.03 0.3425 0.5694 0.1035 0.0623 0.909 6.364 5.540 677.667 0.719 24.642 3.708 0.43 135193. 0.4267
|
|
38.53 0.3768 0.6042 0.1007 0.0628 0.917 6.422 5.392 683.805 0.726 23.985 3.577 0.43 135527. 0.4061
|
|
42.04 0.4110 0.6360 0.0976 0.0631 0.921 6.449 5.225 686.745 0.729 23.241 3.451 0.43 135886. 0.3857
|
|
45.54 0.4453 0.6649 0.0941 0.0630 0.920 6.442 5.037 685.965 0.728 22.406 3.331 0.43 136268. 0.3655
|
|
49.04 0.4795 0.6914 0.0902 0.0626 0.913 6.395 4.828 680.993 0.723 21.476 3.216 0.43 136674. 0.3455
|
|
52.54 0.5138 0.7154 0.0859 0.0617 0.900 6.306 4.598 671.440 0.712 20.450 3.106 0.43 137103. 0.3256
|
|
56.05 0.5480 0.7371 0.0812 0.0604 0.881 6.170 4.345 657.005 0.697 19.328 3.000 0.43 137556. 0.3058
|
|
59.55 0.5823 0.7564 0.0761 0.0586 0.855 5.987 4.072 637.466 0.676 18.112 2.897 0.44 138033. 0.2859
|
|
63.05 0.6165 0.7731 0.0706 0.0563 0.822 5.754 3.778 612.670 0.650 16.805 2.797 0.44 138532. 0.2658
|
|
66.56 0.6508 0.7872 0.0648 0.0535 0.781 5.473 3.466 582.747 0.618 15.418 2.698 0.44 139054. 0.2456
|
|
70.06 0.6850 0.7981 0.0587 0.0504 0.735 5.147 3.140 548.088 0.582 13.967 2.598 0.44 139598. 0.2251
|
|
73.56 0.7193 0.8052 0.0524 0.0468 0.683 4.781 2.802 509.098 0.540 12.465 2.497 0.44 140164. 0.2044
|
|
77.06 0.7535 0.8074 0.0459 0.0428 0.625 4.378 2.456 466.140 0.495 10.925 2.390 0.44 140752. 0.1831
|
|
80.57 0.7878 0.8033 0.0393 0.0385 0.563 3.940 2.104 419.547 0.445 9.358 2.274 0.44 141361. 0.1613
|
|
84.07 0.8220 0.7903 0.0327 0.0340 0.496 3.472 1.748 369.657 0.392 7.774 2.144 0.44 141991. 0.1386
|
|
87.57 0.8563 0.7640 0.0260 0.0291 0.425 2.975 1.390 316.832 0.336 6.183 1.990 0.44 142643. 0.1147
|
|
91.08 0.8905 0.7157 0.0193 0.0240 0.351 2.456 1.033 261.487 0.277 4.597 1.793 0.45 143315. 0.0891
|
|
94.58 0.9248 0.6272 0.0127 0.0188 0.274 1.917 0.681 204.101 0.217 3.028 1.513 0.45 144009. 0.0610
|
|
98.08 0.9590 0.4495 0.0063 0.0133 0.195 1.364 0.335 145.243 0.154 1.489 1.045 0.45 144722. 0.0296
|
|
101.58 0.9933 -0.0027 0.0000 0.0079 0.115 0.803 -0.001 85.533 0.091 -0.005 -0.006 0.45 145455. 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 0.1176 0.0503 1.007 6.346 7.770 750.769 0.717 34.560 4.694 0.48 147837. 0.6398
|
|
3.89 0.0343 0.0778 0.1169 0.0515 1.031 6.497 7.727 768.689 0.734 34.370 4.559 0.48 147979. 0.6197
|
|
7.79 0.0685 0.1509 0.1162 0.0527 1.056 6.657 7.679 787.635 0.752 34.154 4.422 0.48 148138. 0.5991
|
|
11.68 0.1028 0.2192 0.1154 0.0541 1.083 6.824 7.623 807.367 0.771 33.906 4.282 0.48 148317. 0.5781
|
|
15.57 0.1370 0.2828 0.1144 0.0554 1.110 6.995 7.558 827.586 0.790 33.619 4.142 0.48 148517. 0.5569
|
|
19.46 0.1713 0.3416 0.1132 0.0568 1.137 7.167 7.483 847.909 0.810 33.284 4.003 0.48 148739. 0.5354
|
|
23.36 0.2055 0.3957 0.1119 0.0581 1.164 7.335 7.395 867.870 0.829 32.894 3.865 0.48 148983. 0.5139
|
|
27.25 0.2398 0.4455 0.1104 0.0594 1.189 7.497 7.293 886.927 0.847 32.439 3.730 0.48 149252. 0.4925
|
|
31.14 0.2740 0.4912 0.1086 0.0606 1.213 7.645 7.174 904.462 0.864 31.910 3.598 0.48 149546. 0.4712
|
|
35.03 0.3083 0.5329 0.1065 0.0616 1.233 7.774 7.036 919.798 0.878 31.297 3.470 0.48 149865. 0.4500
|
|
38.93 0.3426 0.5711 0.1041 0.0624 1.250 7.879 6.878 932.212 0.890 30.592 3.346 0.48 150211. 0.4291
|
|
42.82 0.3768 0.6060 0.1013 0.0630 1.262 7.953 6.696 940.953 0.899 29.786 3.228 0.48 150582. 0.4084
|
|
46.71 0.4111 0.6378 0.0982 0.0633 1.268 7.990 6.491 945.262 0.903 28.871 3.115 0.48 150981. 0.3880
|
|
50.61 0.4453 0.6669 0.0947 0.0632 1.266 7.982 6.259 944.409 0.902 27.841 3.006 0.48 151406. 0.3678
|
|
54.50 0.4796 0.6935 0.0908 0.0628 1.258 7.926 6.001 937.734 0.895 26.692 2.903 0.48 151857. 0.3477
|
|
58.39 0.5138 0.7177 0.0865 0.0619 1.240 7.816 5.716 924.686 0.883 25.423 2.804 0.48 152335. 0.3277
|
|
62.28 0.5481 0.7395 0.0818 0.0606 1.213 7.648 5.403 904.847 0.864 24.033 2.708 0.48 152839. 0.3078
|
|
66.18 0.5824 0.7590 0.0766 0.0588 1.177 7.420 5.064 877.899 0.838 22.525 2.616 0.48 153369. 0.2879
|
|
70.07 0.6166 0.7761 0.0711 0.0565 1.131 7.131 4.699 843.633 0.806 20.903 2.527 0.49 153924. 0.2678
|
|
73.96 0.6509 0.7905 0.0653 0.0537 1.076 6.781 4.312 802.218 0.766 19.180 2.438 0.49 154504. 0.2476
|
|
77.85 0.6851 0.8019 0.0591 0.0505 1.011 6.375 3.907 754.191 0.720 17.377 2.349 0.49 155109. 0.2271
|
|
81.75 0.7194 0.8096 0.0528 0.0469 0.939 5.918 3.487 700.116 0.669 15.509 2.259 0.49 155739. 0.2063
|
|
85.64 0.7536 0.8126 0.0462 0.0429 0.859 5.414 3.056 640.496 0.612 13.594 2.164 0.49 156392. 0.1850
|
|
89.53 0.7879 0.8094 0.0396 0.0386 0.772 4.867 2.618 575.796 0.550 11.644 2.062 0.49 157069. 0.1631
|
|
93.43 0.8221 0.7975 0.0329 0.0339 0.679 4.281 2.174 506.485 0.484 9.672 1.947 0.49 157770. 0.1404
|
|
97.32 0.8564 0.7727 0.0262 0.0290 0.581 3.660 1.729 433.072 0.414 7.691 1.811 0.49 158495. 0.1164
|
|
101.21 0.8907 0.7263 0.0194 0.0239 0.478 3.010 1.285 356.133 0.340 5.717 1.637 0.49 159242. 0.0907
|
|
105.10 0.9249 0.6398 0.0128 0.0185 0.371 2.336 0.846 276.344 0.264 3.763 1.389 0.50 160013. 0.0624
|
|
109.00 0.9592 0.4628 0.0063 0.0130 0.261 1.644 0.415 194.501 0.186 1.847 0.969 0.50 160806. 0.0305
|
|
112.89 0.9934 -0.0058 0.0000 0.0075 0.149 0.942 -0.003 111.474 0.106 -0.013 -0.012 0.50 161620. 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 0.1179 0.0503 1.342 7.687 9.429 1000.445 0.869 41.941 4.275 0.52 162616. 0.6419
|
|
4.28 0.0343 0.0779 0.1173 0.0515 1.374 7.872 9.380 1024.512 0.889 41.721 4.153 0.52 162771. 0.6219
|
|
8.56 0.0685 0.1512 0.1166 0.0528 1.408 8.068 9.323 1050.000 0.912 41.471 4.027 0.52 162946. 0.6013
|
|
12.85 0.1028 0.2197 0.1158 0.0542 1.444 8.272 9.258 1076.588 0.935 41.182 3.901 0.52 163143. 0.5803
|
|
17.13 0.1370 0.2833 0.1148 0.0555 1.480 8.482 9.183 1103.884 0.958 40.846 3.773 0.52 163363. 0.5591
|
|
21.41 0.1713 0.3422 0.1137 0.0569 1.517 8.693 9.095 1131.369 0.982 40.453 3.646 0.52 163606. 0.5377
|
|
25.69 0.2055 0.3965 0.1124 0.0583 1.553 8.901 8.991 1158.419 1.006 39.993 3.520 0.52 163876. 0.5162
|
|
29.97 0.2398 0.4464 0.1109 0.0596 1.588 9.100 8.870 1184.300 1.028 39.454 3.397 0.53 164171. 0.4947
|
|
34.25 0.2740 0.4921 0.1092 0.0608 1.620 9.283 8.729 1208.173 1.049 38.825 3.277 0.53 164495. 0.4734
|
|
38.54 0.3083 0.5339 0.1071 0.0618 1.648 9.444 8.564 1229.121 1.067 38.094 3.160 0.53 164846. 0.4522
|
|
42.82 0.3425 0.5722 0.1047 0.0627 1.671 9.575 8.375 1246.161 1.082 37.250 3.048 0.53 165226. 0.4313
|
|
47.10 0.3768 0.6071 0.1020 0.0633 1.687 9.668 8.157 1258.273 1.092 36.282 2.940 0.53 165635. 0.4106
|
|
51.38 0.4110 0.6391 0.0989 0.0636 1.696 9.716 7.909 1264.425 1.098 35.180 2.837 0.53 166073. 0.3901
|
|
55.66 0.4453 0.6683 0.0954 0.0636 1.695 9.710 7.630 1263.624 1.097 33.936 2.739 0.53 166541. 0.3699
|
|
59.94 0.4796 0.6950 0.0915 0.0631 1.683 9.643 7.317 1254.967 1.089 32.547 2.645 0.53 167038. 0.3498
|
|
64.23 0.5138 0.7193 0.0872 0.0623 1.660 9.510 6.971 1237.702 1.074 31.008 2.555 0.53 167564. 0.3298
|
|
68.51 0.5481 0.7413 0.0824 0.0609 1.624 9.307 6.592 1211.256 1.052 29.320 2.468 0.53 168119. 0.3099
|
|
72.79 0.5823 0.7611 0.0773 0.0591 1.576 9.030 6.180 1175.199 1.020 27.488 2.385 0.53 168702. 0.2899
|
|
77.07 0.6166 0.7785 0.0717 0.0568 1.514 8.677 5.736 1129.244 0.980 25.515 2.304 0.53 169313. 0.2698
|
|
81.35 0.6508 0.7932 0.0658 0.0540 1.440 8.249 5.265 1073.605 0.932 23.417 2.224 0.53 169952. 0.2495
|
|
85.63 0.6851 0.8051 0.0597 0.0508 1.353 7.753 4.770 1008.999 0.876 21.219 2.144 0.54 170618. 0.2290
|
|
89.92 0.7193 0.8133 0.0533 0.0471 1.255 7.194 4.258 936.188 0.813 18.942 2.063 0.54 171310. 0.2082
|
|
94.20 0.7536 0.8170 0.0467 0.0431 1.148 6.576 3.733 855.850 0.743 16.605 1.978 0.54 172029. 0.1869
|
|
98.48 0.7878 0.8147 0.0400 0.0387 1.031 5.906 3.198 768.616 0.667 14.224 1.887 0.54 172774. 0.1650
|
|
102.76 0.8221 0.8040 0.0332 0.0340 0.905 5.188 2.657 675.121 0.586 11.816 1.785 0.54 173546. 0.1422
|
|
107.04 0.8563 0.7806 0.0264 0.0290 0.773 4.426 2.113 576.054 0.500 9.397 1.663 0.54 174343. 0.1182
|
|
111.33 0.8906 0.7361 0.0196 0.0238 0.633 3.628 1.570 472.197 0.410 6.984 1.508 0.54 175165. 0.0924
|
|
115.61 0.9249 0.6518 0.0129 0.0183 0.489 2.801 1.033 364.470 0.316 4.597 1.286 0.55 176013. 0.0639
|
|
119.89 0.9591 0.4761 0.0063 0.0128 0.341 1.951 0.507 253.956 0.220 2.256 0.906 0.55 176885. 0.0315
|
|
124.17 0.9934 -0.0068 0.0000 0.0071 0.190 1.090 -0.004 141.843 0.123 -0.017 -0.012 0.55 177780. 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 0.1183 0.0505 1.746 9.172 11.257 1302.242 1.036 50.073 3.921 0.57 177393. 0.6433
|
|
4.67 0.0342 0.0780 0.1177 0.0517 1.789 9.394 11.201 1333.762 1.061 49.824 3.809 0.57 177562. 0.6234
|
|
9.34 0.0685 0.1512 0.1170 0.0530 1.833 9.630 11.138 1367.203 1.088 49.540 3.695 0.57 177752. 0.6030
|
|
14.00 0.1027 0.2197 0.1163 0.0543 1.880 9.876 11.064 1402.161 1.116 49.212 3.579 0.57 177967. 0.5821
|
|
18.67 0.1369 0.2834 0.1154 0.0557 1.929 10.129 10.978 1438.119 1.144 48.829 3.462 0.57 178206. 0.5609
|
|
23.34 0.1712 0.3424 0.1143 0.0571 1.977 10.385 10.876 1474.407 1.173 48.378 3.346 0.57 178472. 0.5396
|
|
28.01 0.2054 0.3967 0.1130 0.0585 2.025 10.637 10.757 1510.206 1.202 47.849 3.231 0.57 178765. 0.5181
|
|
32.68 0.2396 0.4466 0.1116 0.0599 2.071 10.879 10.617 1544.541 1.229 47.225 3.118 0.57 179087. 0.4967
|
|
37.34 0.2738 0.4924 0.1098 0.0611 2.114 11.103 10.453 1576.311 1.254 46.493 3.008 0.57 179439. 0.4755
|
|
42.01 0.3081 0.5343 0.1078 0.0622 2.151 11.300 10.260 1604.296 1.277 45.639 2.901 0.57 179822. 0.4544
|
|
46.68 0.3423 0.5726 0.1055 0.0631 2.182 11.461 10.038 1627.194 1.295 44.648 2.798 0.57 180237. 0.4335
|
|
51.35 0.3765 0.6076 0.1028 0.0637 2.204 11.577 9.781 1643.648 1.308 43.507 2.699 0.58 180683. 0.4128
|
|
56.01 0.4108 0.6396 0.0997 0.0640 2.216 11.638 9.489 1652.295 1.315 42.205 2.605 0.58 181161. 0.3923
|
|
60.68 0.4450 0.6689 0.0962 0.0640 2.215 11.635 9.157 1651.808 1.314 40.732 2.515 0.58 181671. 0.3721
|
|
65.35 0.4792 0.6958 0.0923 0.0636 2.201 11.558 8.786 1640.985 1.306 39.081 2.429 0.58 182213. 0.3520
|
|
70.02 0.5135 0.7202 0.0880 0.0627 2.171 11.402 8.374 1618.822 1.288 37.250 2.346 0.58 182786. 0.3320
|
|
74.69 0.5477 0.7425 0.0833 0.0614 2.125 11.161 7.922 1584.551 1.261 35.238 2.268 0.58 183391. 0.3121
|
|
79.35 0.5819 0.7625 0.0781 0.0596 2.062 10.830 7.430 1537.602 1.224 33.049 2.192 0.58 184027. 0.2921
|
|
84.02 0.6162 0.7802 0.0725 0.0573 1.981 10.407 6.900 1477.590 1.176 30.690 2.118 0.58 184694. 0.2720
|
|
88.69 0.6504 0.7953 0.0666 0.0544 1.884 9.895 6.335 1404.764 1.118 28.179 2.045 0.58 185390. 0.2517
|
|
93.36 0.6846 0.8076 0.0603 0.0512 1.770 9.298 5.743 1320.062 1.050 25.544 1.973 0.58 186116. 0.2312
|
|
98.03 0.7189 0.8164 0.0539 0.0475 1.642 8.625 5.129 1224.484 0.974 22.812 1.900 0.59 186871. 0.2104
|
|
102.69 0.7531 0.8209 0.0473 0.0434 1.501 7.881 4.498 1118.929 0.890 20.007 1.823 0.59 187655. 0.1891
|
|
107.36 0.7873 0.8195 0.0405 0.0389 1.347 7.073 3.855 1004.230 0.799 17.148 1.741 0.59 188468. 0.1672
|
|
112.03 0.8215 0.8101 0.0337 0.0342 1.182 6.207 3.205 881.225 0.701 14.254 1.649 0.59 189308. 0.1444
|
|
116.70 0.8558 0.7883 0.0268 0.0291 1.007 5.288 2.551 750.821 0.597 11.345 1.541 0.59 190177. 0.1203
|
|
121.36 0.8900 0.7460 0.0199 0.0238 0.823 4.325 1.898 614.055 0.489 8.443 1.402 0.59 191073. 0.0945
|
|
126.03 0.9242 0.6647 0.0132 0.0183 0.633 3.326 1.252 472.141 0.376 5.570 1.203 0.60 191997. 0.0658
|
|
130.70 0.9585 0.4924 0.0065 0.0127 0.438 2.300 0.619 326.518 0.260 2.752 0.859 0.60 192948. 0.0331
|
|
135.37 0.9927 0.0051 0.0000 0.0069 0.240 1.259 0.003 178.770 0.142 0.015 0.009 0.60 193923. 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 0.1187 0.0507 2.229 10.808 13.257 1662.392 1.221 58.966 3.617 0.62 192168. 0.6440
|
|
5.06 0.0342 0.0779 0.1182 0.0519 2.284 11.071 13.195 1702.837 1.251 58.692 3.515 0.62 192351. 0.6243
|
|
10.11 0.0685 0.1512 0.1175 0.0532 2.341 11.351 13.124 1745.846 1.282 58.377 3.410 0.62 192557. 0.6040
|
|
15.17 0.1027 0.2197 0.1168 0.0546 2.402 11.644 13.042 1790.917 1.316 58.012 3.303 0.62 192789. 0.5833
|
|
20.23 0.1369 0.2834 0.1159 0.0560 2.464 11.946 12.946 1837.388 1.350 57.584 3.196 0.62 193048. 0.5623
|
|
25.28 0.1711 0.3423 0.1149 0.0574 2.527 12.252 12.832 1884.404 1.384 57.079 3.089 0.62 193335. 0.5410
|
|
30.34 0.2054 0.3967 0.1137 0.0589 2.589 12.554 12.698 1930.906 1.418 56.480 2.983 0.62 193653. 0.5197
|
|
35.39 0.2396 0.4467 0.1123 0.0602 2.649 12.845 12.538 1975.633 1.451 55.771 2.879 0.62 194002. 0.4984
|
|
40.45 0.2738 0.4925 0.1106 0.0615 2.705 13.115 12.350 2017.147 1.482 54.934 2.777 0.62 194383. 0.4772
|
|
45.51 0.3080 0.5344 0.1086 0.0626 2.754 13.354 12.129 2053.861 1.509 53.952 2.679 0.62 194798. 0.4562
|
|
50.56 0.3423 0.5727 0.1063 0.0635 2.795 13.550 11.872 2084.070 1.531 52.807 2.584 0.62 195247. 0.4353
|
|
55.62 0.3765 0.6078 0.1036 0.0642 2.824 13.693 11.574 2106.004 1.547 51.483 2.493 0.62 195730. 0.4147
|
|
60.68 0.4107 0.6399 0.1006 0.0646 2.840 13.770 11.233 2117.878 1.556 49.966 2.406 0.62 196249. 0.3943
|
|
65.73 0.4450 0.6694 0.0971 0.0646 2.840 13.770 10.846 2117.962 1.556 48.244 2.323 0.62 196802. 0.3741
|
|
70.79 0.4792 0.6963 0.0932 0.0642 2.822 13.684 10.411 2104.677 1.546 46.309 2.244 0.63 197389. 0.3540
|
|
75.84 0.5134 0.7209 0.0889 0.0633 2.785 13.502 9.927 2076.701 1.525 44.156 2.168 0.63 198011. 0.3340
|
|
80.90 0.5476 0.7434 0.0841 0.0620 2.726 13.218 9.395 2033.028 1.493 41.787 2.096 0.63 198667. 0.3141
|
|
85.96 0.5819 0.7636 0.0789 0.0601 2.646 12.827 8.814 1972.917 1.449 39.205 2.026 0.63 199357. 0.2942
|
|
91.01 0.6161 0.7816 0.0733 0.0578 2.542 12.326 8.188 1895.867 1.393 36.418 1.959 0.63 200079. 0.2741
|
|
96.07 0.6503 0.7971 0.0673 0.0549 2.417 11.717 7.520 1802.176 1.324 33.447 1.893 0.63 200834. 0.2538
|
|
101.13 0.6845 0.8098 0.0611 0.0516 2.270 11.008 6.818 1693.039 1.244 30.327 1.827 0.63 201621. 0.2332
|
|
106.18 0.7188 0.8191 0.0545 0.0479 2.105 10.206 6.090 1569.758 1.153 27.089 1.760 0.63 202440. 0.2123
|
|
111.24 0.7530 0.8243 0.0478 0.0437 1.922 9.320 5.342 1433.499 1.053 23.761 1.690 0.64 203289. 0.1910
|
|
116.30 0.7872 0.8238 0.0410 0.0392 1.724 8.357 4.579 1285.344 0.944 20.367 1.616 0.64 204170. 0.1691
|
|
121.35 0.8215 0.8154 0.0341 0.0343 1.511 7.323 3.806 1126.382 0.827 16.930 1.533 0.64 205081. 0.1462
|
|
126.41 0.8557 0.7949 0.0271 0.0292 1.284 6.227 3.029 957.788 0.704 13.473 1.434 0.64 206022. 0.1221
|
|
131.46 0.8899 0.7543 0.0202 0.0238 1.047 5.077 2.253 780.915 0.574 10.023 1.309 0.64 206993. 0.0961
|
|
136.52 0.9241 0.6750 0.0133 0.0182 0.801 3.884 1.485 597.345 0.439 6.606 1.128 0.65 207993. 0.0672
|
|
141.58 0.9584 0.5036 0.0066 0.0125 0.548 2.659 0.732 408.957 0.300 3.254 0.811 0.65 209024. 0.0339
|
|
146.63 0.9926 -0.0004 0.0000 0.0066 0.292 1.416 0.000 217.827 0.160 -0.001 -0.001 0.65 210079. 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 0.1191 0.0510 2.804 12.624 15.430 2091.012 1.426 68.632 3.347 0.67 206941. 0.6429
|
|
5.44 0.0342 0.0776 0.1186 0.0523 2.872 12.929 15.363 2141.494 1.461 68.336 3.254 0.67 207137. 0.6236
|
|
10.89 0.0684 0.1507 0.1180 0.0536 2.944 13.254 15.287 2195.349 1.497 67.996 3.158 0.67 207359. 0.6038
|
|
16.33 0.1026 0.2191 0.1173 0.0550 3.020 13.596 15.198 2251.973 1.536 67.600 3.061 0.67 207608. 0.5835
|
|
21.77 0.1369 0.2828 0.1165 0.0564 3.099 13.950 15.093 2310.576 1.576 67.134 2.963 0.67 207887. 0.5628
|
|
27.22 0.1711 0.3418 0.1156 0.0578 3.178 14.309 14.968 2370.097 1.617 66.579 2.864 0.67 208196. 0.5419
|
|
32.66 0.2053 0.3962 0.1144 0.0593 3.258 14.666 14.819 2429.216 1.657 65.917 2.767 0.67 208538. 0.5208
|
|
38.10 0.2395 0.4462 0.1130 0.0607 3.334 15.011 14.642 2486.332 1.696 65.127 2.671 0.67 208913. 0.4998
|
|
43.55 0.2737 0.4920 0.1114 0.0620 3.406 15.332 14.431 2539.610 1.732 64.187 2.577 0.67 209324. 0.4787
|
|
48.99 0.3079 0.5340 0.1095 0.0631 3.469 15.619 14.181 2586.999 1.765 63.077 2.486 0.67 209770. 0.4578
|
|
54.43 0.3421 0.5724 0.1072 0.0641 3.522 15.856 13.888 2626.285 1.791 61.775 2.399 0.67 210254. 0.4371
|
|
59.88 0.3764 0.6075 0.1046 0.0648 3.561 16.030 13.548 2655.153 1.811 60.262 2.314 0.67 210774. 0.4165
|
|
65.32 0.4106 0.6397 0.1016 0.0652 3.582 16.127 13.157 2671.287 1.822 58.521 2.234 0.67 211332. 0.3962
|
|
70.76 0.4448 0.6692 0.0981 0.0652 3.584 16.134 12.710 2672.453 1.823 56.535 2.157 0.67 211928. 0.3761
|
|
76.21 0.4790 0.6963 0.0942 0.0648 3.563 16.039 12.207 2656.612 1.812 54.297 2.084 0.67 212561. 0.3560
|
|
81.65 0.5132 0.7211 0.0899 0.0640 3.516 15.830 11.645 2622.052 1.788 51.799 2.014 0.68 213231. 0.3361
|
|
87.09 0.5474 0.7437 0.0851 0.0627 3.443 15.501 11.026 2567.462 1.751 49.043 1.948 0.68 213938. 0.3163
|
|
92.53 0.5816 0.7642 0.0799 0.0608 3.342 15.044 10.349 2491.896 1.700 46.034 1.884 0.68 214681. 0.2963
|
|
97.98 0.6159 0.7824 0.0743 0.0584 3.211 14.458 9.618 2394.710 1.633 42.779 1.822 0.68 215459. 0.2762
|
|
103.42 0.6501 0.7983 0.0682 0.0556 3.052 13.742 8.836 2276.244 1.553 39.305 1.761 0.68 216273. 0.2559
|
|
108.86 0.6843 0.8115 0.0619 0.0522 2.867 12.908 8.015 2138.004 1.458 35.650 1.700 0.68 217120. 0.2354
|
|
114.31 0.7185 0.8214 0.0553 0.0484 2.657 11.964 7.161 1981.654 1.352 31.854 1.639 0.68 218002. 0.2145
|
|
119.75 0.7527 0.8272 0.0485 0.0441 2.425 10.920 6.283 1808.685 1.234 27.949 1.576 0.69 218917. 0.1931
|
|
125.19 0.7869 0.8276 0.0416 0.0396 2.173 9.783 5.387 1620.477 1.105 23.963 1.508 0.69 219865. 0.1711
|
|
130.64 0.8211 0.8203 0.0346 0.0346 1.902 8.563 4.479 1418.420 0.967 19.923 1.432 0.69 220846. 0.1482
|
|
136.08 0.8554 0.8013 0.0275 0.0294 1.615 7.269 3.565 1204.021 0.821 15.858 1.343 0.69 221859. 0.1240
|
|
141.52 0.8896 0.7624 0.0205 0.0239 1.313 5.911 2.653 979.025 0.668 11.798 1.229 0.69 222904. 0.0979
|
|
146.97 0.9238 0.6852 0.0135 0.0182 1.000 4.501 1.748 745.528 0.509 7.776 1.064 0.69 223982. 0.0688
|
|
152.41 0.9580 0.5153 0.0066 0.0124 0.679 3.055 0.861 506.074 0.345 3.828 0.771 0.70 225090. 0.0350
|
|
157.85 0.9922 -0.0023 0.0000 0.0064 0.353 1.591 -0.002 263.543 0.180 -0.008 -0.003 0.70 226227. 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 0.1196 0.0519 3.505 14.727 17.777 2613.551 1.664 79.073 3.085 0.71 221712. 0.6360
|
|
5.83 0.0342 0.0767 0.1191 0.0531 3.587 15.071 17.707 2674.615 1.703 78.761 3.003 0.71 221922. 0.6179
|
|
11.66 0.0684 0.1491 0.1186 0.0544 3.674 15.439 17.627 2739.898 1.744 78.404 2.918 0.71 222159. 0.5990
|
|
17.48 0.1026 0.2170 0.1179 0.0557 3.767 15.827 17.533 2808.694 1.788 77.985 2.831 0.71 222425. 0.5797
|
|
23.31 0.1368 0.2804 0.1172 0.0571 3.862 16.229 17.421 2880.050 1.833 77.489 2.744 0.71 222723. 0.5599
|
|
29.14 0.1709 0.3392 0.1163 0.0586 3.960 16.638 17.288 2952.697 1.880 76.895 2.656 0.72 223053. 0.5399
|
|
34.97 0.2051 0.3936 0.1152 0.0600 4.057 17.045 17.127 3025.016 1.926 76.180 2.568 0.72 223418. 0.5197
|
|
40.79 0.2393 0.4438 0.1139 0.0614 4.151 17.440 16.933 3095.079 1.970 75.319 2.481 0.72 223820. 0.4993
|
|
46.62 0.2735 0.4898 0.1123 0.0627 4.238 17.810 16.701 3160.643 2.012 74.286 2.397 0.72 224259. 0.4789
|
|
52.45 0.3077 0.5321 0.1105 0.0639 4.317 18.140 16.424 3219.208 2.049 73.055 2.314 0.72 224737. 0.4586
|
|
58.28 0.3419 0.5708 0.1083 0.0648 4.383 18.415 16.097 3268.071 2.081 71.600 2.234 0.72 225255. 0.4383
|
|
64.10 0.3761 0.6062 0.1057 0.0656 4.431 18.620 15.714 3304.379 2.104 69.897 2.157 0.72 225812. 0.4181
|
|
69.93 0.4103 0.6386 0.1027 0.0660 4.459 18.737 15.271 3325.216 2.117 67.926 2.083 0.72 226410. 0.3980
|
|
75.76 0.4445 0.6683 0.0993 0.0660 4.463 18.751 14.763 3327.711 2.118 65.667 2.012 0.72 227048. 0.3781
|
|
81.59 0.4786 0.6956 0.0954 0.0657 4.438 18.647 14.188 3309.172 2.107 63.109 1.945 0.72 227726. 0.3582
|
|
87.41 0.5128 0.7206 0.0911 0.0648 4.381 18.411 13.544 3267.280 2.080 60.245 1.880 0.72 228444. 0.3384
|
|
93.24 0.5470 0.7434 0.0863 0.0635 4.292 18.033 12.832 3200.233 2.037 57.076 1.819 0.72 229201. 0.3185
|
|
99.07 0.5812 0.7642 0.0811 0.0616 4.166 17.506 12.052 3106.778 1.978 53.606 1.759 0.73 229997. 0.2987
|
|
104.90 0.6154 0.7828 0.0754 0.0593 4.004 16.826 11.206 2986.094 1.901 49.845 1.702 0.73 230831. 0.2786
|
|
110.72 0.6496 0.7990 0.0693 0.0563 3.807 15.995 10.302 2838.551 1.807 45.822 1.646 0.73 231702. 0.2583
|
|
116.55 0.6838 0.8127 0.0629 0.0529 3.575 15.023 9.349 2666.010 1.697 41.584 1.591 0.73 232610. 0.2378
|
|
122.38 0.7180 0.8232 0.0562 0.0490 3.313 13.921 8.358 2470.568 1.573 37.175 1.534 0.73 233555. 0.2169
|
|
128.21 0.7521 0.8298 0.0493 0.0447 3.023 12.702 7.337 2254.124 1.435 32.634 1.476 0.73 234535. 0.1955
|
|
134.03 0.7863 0.8310 0.0423 0.0401 2.707 11.374 6.294 2018.455 1.285 27.995 1.414 0.74 235550. 0.1735
|
|
139.86 0.8205 0.8248 0.0352 0.0350 2.367 9.948 5.236 1765.403 1.124 23.289 1.345 0.74 236600. 0.1505
|
|
145.69 0.8547 0.8070 0.0280 0.0297 2.008 8.436 4.170 1497.034 0.953 18.549 1.263 0.74 237684. 0.1262
|
|
151.52 0.8889 0.7694 0.0209 0.0241 1.630 6.851 3.105 1215.802 0.774 13.810 1.158 0.74 238803. 0.0998
|
|
157.35 0.9231 0.6930 0.0138 0.0183 1.240 5.211 2.048 924.697 0.589 9.110 1.005 0.74 239956. 0.0703
|
|
163.17 0.9573 0.5223 0.0068 0.0124 0.841 3.535 1.010 627.368 0.399 4.492 0.730 0.75 241143. 0.0359
|
|
169.00 0.9915 0.0002 0.0000 0.0065 0.440 1.848 0.000 327.935 0.209 0.001 0.000 0.75 242359. 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 0.1200 0.0536 4.397 17.320 20.296 3278.667 1.957 90.278 2.808 0.76 236481. 0.6185
|
|
6.21 0.0342 0.0745 0.1196 0.0548 4.493 17.700 20.225 3350.629 2.000 89.959 2.738 0.76 236704. 0.6020
|
|
12.42 0.0683 0.1451 0.1191 0.0560 4.597 18.107 20.142 3427.633 2.046 89.592 2.665 0.76 236956. 0.5849
|
|
18.63 0.1025 0.2116 0.1185 0.0574 4.705 18.536 20.045 3508.820 2.094 89.162 2.591 0.76 237239. 0.5673
|
|
24.84 0.1366 0.2739 0.1178 0.0587 4.818 18.981 19.930 3593.026 2.144 88.649 2.516 0.76 237555. 0.5492
|
|
31.05 0.1708 0.3321 0.1170 0.0601 4.933 19.433 19.791 3678.685 2.196 88.029 2.440 0.76 237906. 0.5308
|
|
37.26 0.2049 0.3862 0.1160 0.0615 5.047 19.883 19.622 3763.811 2.246 87.277 2.365 0.76 238295. 0.5122
|
|
43.46 0.2391 0.4363 0.1148 0.0629 5.158 20.317 19.416 3846.026 2.295 86.360 2.290 0.76 238722. 0.4933
|
|
49.67 0.2732 0.4826 0.1133 0.0641 5.260 20.722 19.166 3922.595 2.341 85.250 2.216 0.76 239189. 0.4744
|
|
55.88 0.3074 0.5253 0.1115 0.0652 5.351 21.081 18.865 3990.515 2.382 83.912 2.144 0.77 239698. 0.4554
|
|
62.09 0.3415 0.5647 0.1094 0.0662 5.427 21.377 18.506 4046.555 2.415 82.316 2.074 0.77 240249. 0.4363
|
|
68.30 0.3757 0.6008 0.1069 0.0668 5.481 21.592 18.083 4087.364 2.439 80.433 2.007 0.77 240843. 0.4172
|
|
74.51 0.4098 0.6341 0.1040 0.0672 5.511 21.709 17.589 4109.523 2.453 78.235 1.941 0.77 241480. 0.3981
|
|
80.72 0.4440 0.6647 0.1006 0.0672 5.511 21.710 17.019 4109.676 2.453 75.702 1.878 0.77 242159. 0.3789
|
|
86.93 0.4781 0.6928 0.0968 0.0668 5.478 21.578 16.371 4084.661 2.438 72.817 1.818 0.77 242882. 0.3596
|
|
93.14 0.5123 0.7185 0.0925 0.0659 5.407 21.298 15.641 4031.681 2.406 69.571 1.760 0.77 243648. 0.3403
|
|
99.35 0.5464 0.7420 0.0877 0.0646 5.295 20.858 14.830 3948.460 2.357 65.964 1.704 0.77 244455. 0.3208
|
|
105.56 0.5806 0.7633 0.0824 0.0627 5.140 20.250 13.939 3833.260 2.288 62.003 1.649 0.77 245304. 0.3011
|
|
111.77 0.6147 0.7823 0.0767 0.0602 4.941 19.465 12.971 3684.789 2.199 57.697 1.597 0.78 246193. 0.2812
|
|
117.97 0.6489 0.7991 0.0705 0.0573 4.698 18.506 11.933 3503.150 2.091 53.080 1.545 0.78 247122. 0.2610
|
|
124.18 0.6830 0.8133 0.0641 0.0538 4.413 17.382 10.837 3290.427 1.964 48.204 1.494 0.78 248090. 0.2405
|
|
130.39 0.7172 0.8244 0.0573 0.0499 4.089 16.108 9.695 3049.247 1.820 43.124 1.442 0.78 249096. 0.2196
|
|
136.60 0.7513 0.8315 0.0503 0.0455 3.731 14.697 8.517 2782.155 1.660 37.884 1.389 0.78 250140. 0.1981
|
|
142.81 0.7855 0.8333 0.0432 0.0407 3.341 13.162 7.312 2491.617 1.487 32.522 1.331 0.79 251222. 0.1760
|
|
149.02 0.8196 0.8273 0.0360 0.0356 2.924 11.518 6.087 2180.271 1.301 27.077 1.266 0.79 252341. 0.1528
|
|
155.23 0.8538 0.8091 0.0287 0.0303 2.482 9.779 4.852 1851.150 1.105 21.583 1.189 0.79 253496. 0.1281
|
|
161.44 0.8879 0.7697 0.0214 0.0247 2.022 7.966 3.616 1507.937 0.900 16.083 1.088 0.79 254688. 0.1011
|
|
167.65 0.9221 0.6890 0.0141 0.0189 1.549 6.102 2.387 1155.069 0.689 10.619 0.937 0.79 255915. 0.0708
|
|
173.86 0.9562 0.5105 0.0070 0.0130 1.070 4.215 1.178 797.815 0.476 5.240 0.670 0.80 257179. 0.0355
|
|
180.07 0.9904 -0.0001 0.0000 0.0072 0.593 2.335 0.000 441.958 0.264 -0.001 0.000 0.80 258474. 0.0000
|
|
|
|
|
|
|
|
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 0.1203 0.0568 5.588 20.718 22.982 4166.971 2.341 102.223 2.502 0.81 251246. 0.5864
|
|
6.59 0.0341 0.0707 0.1200 0.0579 5.700 21.132 22.910 4250.352 2.388 101.902 2.445 0.81 251483. 0.5722
|
|
13.18 0.0683 0.1379 0.1195 0.0592 5.819 21.576 22.827 4339.550 2.438 101.534 2.386 0.81 251749. 0.5574
|
|
19.78 0.1024 0.2016 0.1190 0.0604 5.945 22.043 22.730 4433.498 2.490 101.104 2.325 0.81 252049. 0.5421
|
|
26.37 0.1365 0.2617 0.1184 0.0618 6.076 22.526 22.614 4530.718 2.545 100.587 2.264 0.81 252384. 0.5264
|
|
32.96 0.1706 0.3182 0.1177 0.0631 6.208 23.016 22.473 4629.215 2.600 99.959 2.202 0.81 252756. 0.5104
|
|
39.55 0.2048 0.3711 0.1168 0.0644 6.338 23.500 22.299 4726.459 2.655 99.187 2.140 0.81 253167. 0.4941
|
|
46.15 0.2389 0.4205 0.1156 0.0657 6.463 23.962 22.086 4819.404 2.707 98.236 2.079 0.81 253620. 0.4776
|
|
52.74 0.2730 0.4666 0.1143 0.0669 6.577 24.385 21.823 4904.602 2.755 97.069 2.018 0.81 254116. 0.4610
|
|
59.33 0.3071 0.5096 0.1126 0.0679 6.676 24.752 21.503 4978.316 2.796 95.646 1.959 0.81 254656. 0.4442
|
|
65.92 0.3413 0.5496 0.1106 0.0687 6.754 25.042 21.117 5036.661 2.829 93.929 1.902 0.81 255240. 0.4273
|
|
72.52 0.3754 0.5868 0.1082 0.0692 6.807 25.236 20.656 5075.705 2.851 91.880 1.846 0.81 255870. 0.4102
|
|
79.11 0.4095 0.6214 0.1053 0.0694 6.828 25.315 20.114 5091.583 2.860 89.467 1.792 0.82 256547. 0.3929
|
|
85.70 0.4436 0.6535 0.1020 0.0693 6.813 25.260 19.484 5080.551 2.854 86.663 1.739 0.82 257269. 0.3754
|
|
92.29 0.4778 0.6832 0.0982 0.0687 6.758 25.054 18.761 5039.165 2.831 83.447 1.689 0.82 258037. 0.3576
|
|
98.89 0.5119 0.7106 0.0940 0.0677 6.657 24.683 17.942 4964.426 2.789 79.808 1.639 0.82 258851. 0.3395
|
|
105.48 0.5460 0.7358 0.0892 0.0662 6.509 24.133 17.029 4853.895 2.727 75.743 1.591 0.82 259709. 0.3211
|
|
112.07 0.5801 0.7587 0.0839 0.0641 6.310 23.396 16.021 4705.650 2.643 71.260 1.544 0.82 260611. 0.3022
|
|
118.66 0.6143 0.7792 0.0781 0.0616 6.059 22.464 14.922 4518.240 2.538 66.371 1.498 0.82 261556. 0.2829
|
|
125.25 0.6484 0.7973 0.0719 0.0585 5.755 21.338 13.739 4291.673 2.411 61.110 1.452 0.83 262543. 0.2632
|
|
131.85 0.6825 0.8124 0.0654 0.0549 5.403 20.034 12.487 4029.348 2.263 55.540 1.406 0.83 263572. 0.2429
|
|
138.44 0.7166 0.8240 0.0585 0.0509 5.008 18.566 11.179 3734.263 2.098 49.722 1.358 0.83 264641. 0.2220
|
|
145.03 0.7508 0.8311 0.0515 0.0465 4.573 16.954 9.827 3409.889 1.915 43.709 1.307 0.83 265751. 0.2004
|
|
151.62 0.7849 0.8321 0.0442 0.0417 4.102 15.207 8.442 3058.648 1.718 37.549 1.252 0.83 266900. 0.1778
|
|
158.22 0.8190 0.8242 0.0368 0.0366 3.600 13.347 7.033 2684.561 1.508 31.282 1.188 0.84 268088. 0.1541
|
|
164.81 0.8531 0.8021 0.0294 0.0312 3.074 11.396 5.610 2292.093 1.288 24.952 1.110 0.84 269315. 0.1286
|
|
171.40 0.8873 0.7555 0.0219 0.0257 2.530 9.381 4.183 1886.856 1.060 18.604 1.005 0.84 270580. 0.1005
|
|
177.99 0.9214 0.6628 0.0145 0.0201 1.979 7.336 2.763 1475.487 0.829 12.291 0.849 0.84 271883. 0.0690
|
|
184.59 0.9555 0.4702 0.0071 0.0145 1.428 5.296 1.365 1065.117 0.598 6.069 0.581 0.85 273224. 0.0332
|
|
191.18 0.9896 0.0000 0.0000 0.0090 0.890 3.298 0.000 663.375 0.373 0.000 0.000 0.85 274599. 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 0.1205 0.0617 7.210 25.246 25.799 5376.363 2.852 114.756 2.177 0.86 266014. 0.5406
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6.99 0.0342 0.0653 0.1202 0.0629 7.340 25.702 25.728 5473.578 2.904 114.440 2.132 0.86 266263. 0.5288
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13.98 0.0683 0.1278 0.1198 0.0640 7.479 26.190 25.648 5577.436 2.959 114.082 2.086 0.86 266545. 0.5165
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20.97 0.1025 0.1874 0.1193 0.0653 7.626 26.702 25.553 5686.537 3.017 113.662 2.038 0.86 266861. 0.5038
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27.96 0.1367 0.2439 0.1188 0.0666 7.776 27.229 25.440 5798.759 3.076 113.156 1.990 0.86 267215. 0.4907
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34.95 0.1709 0.2974 0.1182 0.0679 7.928 27.759 25.300 5911.587 3.136 112.534 1.941 0.86 267609. 0.4774
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41.94 0.2050 0.3479 0.1174 0.0692 8.075 28.277 25.127 6021.840 3.195 111.763 1.893 0.86 268044. 0.4639
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48.93 0.2392 0.3956 0.1163 0.0703 8.214 28.764 24.910 6125.535 3.250 110.800 1.844 0.86 268523. 0.4501
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55.91 0.2734 0.4406 0.1151 0.0714 8.339 29.198 24.641 6218.114 3.299 109.602 1.797 0.86 269048. 0.4363
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62.90 0.3075 0.4830 0.1135 0.0723 8.441 29.558 24.308 6294.635 3.339 108.120 1.752 0.86 269620. 0.4222
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69.89 0.3417 0.5231 0.1116 0.0729 8.516 29.818 23.900 6350.026 3.369 106.305 1.707 0.86 270240. 0.4081
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76.88 0.3759 0.5609 0.1093 0.0733 8.555 29.955 23.407 6379.318 3.384 104.112 1.664 0.86 270909. 0.3937
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83.87 0.4100 0.5967 0.1066 0.0732 8.553 29.949 22.819 6377.941 3.384 101.499 1.623 0.86 271627. 0.3790
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90.86 0.4442 0.6304 0.1034 0.0728 8.505 29.779 22.129 6341.837 3.364 98.430 1.583 0.87 272394. 0.3640
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97.85 0.4784 0.6622 0.0996 0.0720 8.405 29.430 21.330 6267.353 3.325 94.877 1.544 0.87 273211. 0.3486
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104.84 0.5126 0.6920 0.0954 0.0706 8.250 28.888 20.420 6151.941 3.264 90.828 1.506 0.87 274076. 0.3327
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111.83 0.5467 0.7196 0.0906 0.0688 8.038 28.145 19.398 5993.734 3.180 86.280 1.468 0.87 274988. 0.3161
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118.82 0.5809 0.7451 0.0853 0.0665 7.766 27.194 18.264 5791.328 3.072 81.240 1.430 0.87 275947. 0.2989
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125.81 0.6151 0.7682 0.0795 0.0637 7.434 26.031 17.024 5543.652 2.941 75.724 1.393 0.87 276952. 0.2810
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132.80 0.6492 0.7888 0.0733 0.0603 7.042 24.657 15.685 5250.968 2.786 69.769 1.355 0.87 278002. 0.2624
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139.79 0.6834 0.8062 0.0666 0.0565 6.595 23.091 14.263 4917.573 2.609 63.444 1.316 0.88 279095. 0.2429
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146.78 0.7176 0.8192 0.0597 0.0523 6.103 21.371 12.774 4551.112 2.414 56.819 1.273 0.88 280232. 0.2225
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153.77 0.7517 0.8261 0.0525 0.0477 5.575 19.520 11.231 4156.921 2.205 49.956 1.225 0.88 281411. 0.2008
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160.76 0.7859 0.8240 0.0451 0.0430 5.018 17.571 9.646 3742.004 1.985 42.907 1.169 0.88 282632. 0.1776
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167.74 0.8201 0.8106 0.0375 0.0380 4.433 15.521 8.033 3305.426 1.754 35.731 1.102 0.89 283894. 0.1528
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174.73 0.8543 0.7795 0.0299 0.0328 3.827 13.400 6.403 2853.779 1.514 28.479 1.018 0.89 285197. 0.1259
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181.72 0.8884 0.7193 0.0223 0.0275 3.211 11.245 4.767 2394.771 1.270 21.205 0.903 0.89 286540. 0.0964
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188.71 0.9226 0.6084 0.0147 0.0222 2.598 9.098 3.141 1937.552 1.028 13.973 0.735 0.89 287924. 0.0637
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195.70 0.9568 0.4022 0.0072 0.0171 2.000 7.003 1.541 1491.412 0.791 6.856 0.469 0.90 289347. 0.0285
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202.69 0.9909 -0.0054 -0.0001 0.0122 1.428 5.002 -0.014 1065.137 0.565 -0.063 -0.006 0.90 290808. 0.0000
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