501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x10 (18x10.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 0.0810 0.0332 0.005 0.318 0.271 3.768 0.036 1.205 32.606 0.07 25362. 0.5532
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0.43 0.0253 0.0599 0.0800 0.0338 0.005 0.324 0.268 3.830 0.037 1.190 31.683 0.07 25378. 0.5342
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0.86 0.0506 0.1164 0.0789 0.0343 0.005 0.329 0.264 3.889 0.037 1.173 30.762 0.07 25395. 0.5150
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1.29 0.0760 0.1694 0.0776 0.0348 0.005 0.333 0.260 3.946 0.038 1.155 29.846 0.07 25414. 0.4957
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1.73 0.1013 0.2190 0.0762 0.0352 0.005 0.338 0.255 3.997 0.038 1.134 28.938 0.07 25435. 0.4764
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2.16 0.1266 0.2653 0.0747 0.0356 0.005 0.342 0.250 4.042 0.039 1.112 28.042 0.07 25458. 0.4570
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2.59 0.1519 0.3083 0.0730 0.0360 0.005 0.345 0.244 4.079 0.039 1.086 27.157 0.07 25482. 0.4375
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3.02 0.1772 0.3481 0.0712 0.0362 0.006 0.347 0.238 4.108 0.039 1.059 26.287 0.07 25509. 0.4181
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3.45 0.2026 0.3849 0.0691 0.0364 0.006 0.349 0.231 4.125 0.039 1.029 25.430 0.07 25537. 0.3987
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3.88 0.2279 0.4187 0.0669 0.0364 0.006 0.349 0.224 4.131 0.039 0.996 24.588 0.07 25568. 0.3793
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4.32 0.2532 0.4495 0.0646 0.0364 0.006 0.349 0.216 4.124 0.039 0.961 23.758 0.07 25601. 0.3600
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4.75 0.2785 0.4774 0.0621 0.0362 0.006 0.347 0.208 4.104 0.039 0.923 22.940 0.07 25636. 0.3407
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5.18 0.3038 0.5025 0.0594 0.0359 0.005 0.344 0.199 4.071 0.039 0.883 22.131 0.07 25673. 0.3215
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5.61 0.3291 0.5246 0.0566 0.0355 0.005 0.340 0.189 4.023 0.038 0.842 21.329 0.07 25712. 0.3024
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6.04 0.3545 0.5438 0.0536 0.0349 0.005 0.335 0.179 3.962 0.038 0.798 20.529 0.07 25754. 0.2834
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6.47 0.3798 0.5599 0.0505 0.0343 0.005 0.329 0.169 3.887 0.037 0.752 19.729 0.07 25798. 0.2644
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6.91 0.4051 0.5728 0.0474 0.0335 0.005 0.321 0.158 3.797 0.036 0.705 18.923 0.07 25844. 0.2455
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7.34 0.4304 0.5823 0.0441 0.0326 0.005 0.312 0.147 3.693 0.035 0.656 18.105 0.07 25892. 0.2266
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7.77 0.4557 0.5882 0.0407 0.0315 0.005 0.302 0.136 3.575 0.034 0.606 17.271 0.07 25943. 0.2077
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8.20 0.4811 0.5899 0.0372 0.0304 0.005 0.291 0.125 3.443 0.033 0.554 16.410 0.07 25996. 0.1888
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8.63 0.5064 0.5870 0.0337 0.0291 0.004 0.279 0.113 3.296 0.031 0.501 15.514 0.07 26051. 0.1698
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9.06 0.5317 0.5788 0.0301 0.0276 0.004 0.265 0.101 3.135 0.030 0.448 14.568 0.07 26109. 0.1507
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9.49 0.5570 0.5642 0.0264 0.0261 0.004 0.250 0.088 2.960 0.028 0.393 13.554 0.07 26169. 0.1314
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9.93 0.5823 0.5417 0.0227 0.0244 0.004 0.234 0.076 2.770 0.026 0.338 12.449 0.07 26231. 0.1119
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10.36 0.6077 0.5094 0.0190 0.0226 0.003 0.217 0.063 2.567 0.025 0.282 11.218 0.07 26296. 0.0921
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10.79 0.6330 0.4641 0.0152 0.0207 0.003 0.199 0.051 2.350 0.022 0.226 9.813 0.07 26363. 0.0721
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11.22 0.6583 0.4013 0.0114 0.0187 0.003 0.179 0.038 2.120 0.020 0.170 8.158 0.07 26432. 0.0519
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11.65 0.6836 0.3134 0.0076 0.0166 0.003 0.159 0.025 1.877 0.018 0.113 6.135 0.07 26503. 0.0319
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12.08 0.7089 0.1878 0.0038 0.0143 0.002 0.137 0.013 1.622 0.015 0.056 3.545 0.07 26577. 0.0130
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12.52 0.7342 0.0002 0.0000 0.0120 0.002 0.115 0.000 1.356 0.013 0.000 0.004 0.07 26652. 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 0.0813 0.0294 0.036 1.126 1.088 26.650 0.127 4.842 18.525 0.14 50724. 0.6300
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0.87 0.0255 0.0682 0.0803 0.0300 0.036 1.149 1.075 27.186 0.130 4.783 17.939 0.14 50756. 0.6064
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1.74 0.0509 0.1321 0.0792 0.0305 0.037 1.171 1.060 27.707 0.132 4.716 17.358 0.14 50791. 0.5827
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2.60 0.0764 0.1916 0.0780 0.0311 0.038 1.192 1.044 28.203 0.135 4.643 16.787 0.14 50829. 0.5591
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3.47 0.1018 0.2469 0.0766 0.0316 0.038 1.211 1.025 28.661 0.137 4.561 16.226 0.14 50871. 0.5356
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4.34 0.1273 0.2982 0.0751 0.0320 0.039 1.229 1.005 29.071 0.139 4.470 15.678 0.14 50916. 0.5123
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5.21 0.1527 0.3457 0.0734 0.0324 0.039 1.243 0.982 29.420 0.140 4.369 15.143 0.14 50965. 0.4892
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6.07 0.1782 0.3894 0.0715 0.0327 0.040 1.255 0.957 29.696 0.142 4.258 14.623 0.14 51019. 0.4664
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6.94 0.2037 0.4297 0.0695 0.0329 0.040 1.263 0.930 29.886 0.143 4.137 14.116 0.14 51077. 0.4438
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7.81 0.2291 0.4665 0.0673 0.0331 0.040 1.267 0.901 29.981 0.143 4.006 13.625 0.14 51138. 0.4215
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8.68 0.2546 0.5002 0.0649 0.0330 0.040 1.267 0.869 29.972 0.143 3.864 13.147 0.14 51205. 0.3994
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9.55 0.2800 0.5307 0.0624 0.0329 0.040 1.262 0.835 29.854 0.143 3.713 12.681 0.14 51275. 0.3777
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10.41 0.3055 0.5583 0.0597 0.0327 0.040 1.252 0.799 29.622 0.141 3.552 12.228 0.14 51350. 0.3562
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11.28 0.3309 0.5828 0.0568 0.0323 0.039 1.237 0.761 29.275 0.140 3.383 11.784 0.14 51430. 0.3350
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12.15 0.3564 0.6044 0.0539 0.0318 0.039 1.218 0.721 28.810 0.138 3.206 11.347 0.14 51514. 0.3140
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13.02 0.3819 0.6230 0.0508 0.0311 0.038 1.193 0.679 28.225 0.135 3.022 10.917 0.14 51602. 0.2933
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13.89 0.4073 0.6386 0.0476 0.0303 0.037 1.163 0.636 27.519 0.131 2.831 10.490 0.14 51696. 0.2728
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14.75 0.4328 0.6509 0.0443 0.0294 0.036 1.128 0.592 26.691 0.127 2.634 10.063 0.14 51793. 0.2524
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15.62 0.4582 0.6597 0.0409 0.0284 0.035 1.088 0.547 25.739 0.123 2.432 9.634 0.14 51896. 0.2322
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16.49 0.4837 0.6648 0.0374 0.0272 0.033 1.042 0.500 24.664 0.118 2.224 9.197 0.14 52003. 0.2120
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17.36 0.5091 0.6656 0.0338 0.0259 0.031 0.992 0.453 23.465 0.112 2.013 8.747 0.14 52114. 0.1918
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18.22 0.5346 0.6613 0.0302 0.0244 0.030 0.936 0.404 22.140 0.106 1.797 8.278 0.14 52231. 0.1715
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19.09 0.5600 0.6510 0.0265 0.0228 0.028 0.874 0.355 20.691 0.099 1.578 7.778 0.15 52352. 0.1510
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19.96 0.5855 0.6331 0.0228 0.0211 0.026 0.808 0.305 19.119 0.091 1.356 7.235 0.15 52478. 0.1302
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20.83 0.6110 0.6051 0.0190 0.0192 0.023 0.736 0.255 17.424 0.083 1.132 6.627 0.15 52608. 0.1090
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21.70 0.6364 0.5634 0.0152 0.0172 0.021 0.660 0.204 15.611 0.075 0.907 5.923 0.15 52744. 0.0872
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22.56 0.6619 0.5014 0.0114 0.0151 0.018 0.578 0.153 13.683 0.065 0.680 5.069 0.15 52883. 0.0646
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23.43 0.6873 0.4079 0.0076 0.0128 0.016 0.492 0.102 11.645 0.056 0.453 3.971 0.15 53028. 0.0413
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24.30 0.7128 0.2600 0.0038 0.0105 0.013 0.402 0.051 9.505 0.045 0.228 2.441 0.15 53177. 0.0180
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25.17 0.7382 0.0030 0.0000 0.0080 0.010 0.307 0.000 7.257 0.035 0.002 0.027 0.15 53326. 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 0.0817 0.0279 0.114 2.402 2.459 85.269 0.271 10.938 13.080 0.21 76085. 0.6687
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1.31 0.0255 0.0724 0.0807 0.0285 0.117 2.455 2.429 87.150 0.277 10.806 12.644 0.21 76133. 0.6425
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2.61 0.0511 0.1398 0.0796 0.0291 0.119 2.507 2.396 88.983 0.283 10.659 12.214 0.21 76185. 0.6164
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3.92 0.0766 0.2025 0.0784 0.0296 0.122 2.556 2.359 90.732 0.289 10.494 11.794 0.21 76242. 0.5905
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5.22 0.1021 0.2606 0.0770 0.0302 0.124 2.602 2.318 92.358 0.294 10.309 11.383 0.21 76305. 0.5649
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6.53 0.1277 0.3143 0.0755 0.0306 0.126 2.643 2.272 93.821 0.299 10.105 10.983 0.21 76374. 0.5396
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7.83 0.1532 0.3638 0.0738 0.0311 0.128 2.679 2.221 95.079 0.303 9.878 10.594 0.21 76448. 0.5147
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9.14 0.1787 0.4094 0.0719 0.0314 0.129 2.707 2.165 96.087 0.306 9.629 10.219 0.21 76529. 0.4901
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10.44 0.2042 0.4512 0.0699 0.0316 0.130 2.727 2.103 96.805 0.308 9.356 9.855 0.21 76616. 0.4659
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11.75 0.2298 0.4896 0.0676 0.0317 0.130 2.738 2.037 97.195 0.309 9.059 9.504 0.21 76709. 0.4421
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13.06 0.2553 0.5245 0.0653 0.0318 0.130 2.739 1.965 97.229 0.309 8.739 9.165 0.21 76809. 0.4187
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14.36 0.2808 0.5563 0.0627 0.0316 0.130 2.730 1.888 96.887 0.308 8.396 8.837 0.22 76916. 0.3958
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15.67 0.3064 0.5851 0.0600 0.0314 0.129 2.709 1.806 96.153 0.306 8.032 8.519 0.22 77029. 0.3732
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16.97 0.3319 0.6108 0.0571 0.0310 0.127 2.677 1.720 95.017 0.302 7.650 8.209 0.22 77149. 0.3509
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18.28 0.3574 0.6336 0.0541 0.0305 0.125 2.633 1.630 93.470 0.298 7.249 7.908 0.22 77275. 0.3291
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19.58 0.3830 0.6535 0.0510 0.0299 0.123 2.578 1.536 91.507 0.291 6.831 7.613 0.22 77409. 0.3075
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20.89 0.4085 0.6705 0.0478 0.0291 0.120 2.511 1.439 89.122 0.284 6.399 7.322 0.22 77550. 0.2863
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22.19 0.4340 0.6843 0.0445 0.0282 0.116 2.432 1.338 86.311 0.275 5.953 7.033 0.22 77697. 0.2652
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23.50 0.4596 0.6949 0.0410 0.0271 0.111 2.340 1.235 83.068 0.264 5.495 6.745 0.22 77851. 0.2444
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24.81 0.4851 0.7019 0.0375 0.0259 0.106 2.237 1.130 79.391 0.253 5.025 6.455 0.22 78013. 0.2237
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26.11 0.5106 0.7049 0.0339 0.0246 0.101 2.121 1.022 75.277 0.240 4.546 6.158 0.22 78181. 0.2029
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27.42 0.5361 0.7032 0.0303 0.0231 0.095 1.993 0.912 70.726 0.225 4.058 5.851 0.22 78357. 0.1822
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28.72 0.5617 0.6958 0.0266 0.0215 0.088 1.852 0.801 65.738 0.209 3.562 5.526 0.22 78540. 0.1612
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30.03 0.5872 0.6811 0.0229 0.0197 0.081 1.699 0.688 60.315 0.192 3.060 5.174 0.22 78730. 0.1399
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31.33 0.6127 0.6567 0.0191 0.0178 0.073 1.535 0.574 54.465 0.173 2.553 4.781 0.22 78926. 0.1181
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32.64 0.6383 0.6184 0.0153 0.0157 0.065 1.358 0.459 48.197 0.153 2.043 4.322 0.22 79130. 0.0955
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33.94 0.6638 0.5593 0.0114 0.0136 0.056 1.170 0.344 41.526 0.132 1.531 3.758 0.22 79341. 0.0719
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35.25 0.6893 0.4654 0.0076 0.0113 0.046 0.971 0.229 34.473 0.110 1.018 3.012 0.22 79559. 0.0470
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36.56 0.7149 0.3067 0.0038 0.0088 0.036 0.762 0.114 27.062 0.086 0.508 1.914 0.22 79783. 0.0211
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37.86 0.7404 -0.0028 0.0000 0.0063 0.026 0.542 -0.001 19.242 0.061 -0.003 -0.017 0.22 80006. 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 0.0821 0.0271 0.263 4.151 4.392 196.433 0.469 19.538 10.142 0.29 101444. 0.6929
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1.74 0.0256 0.0749 0.0811 0.0277 0.270 4.248 4.340 201.018 0.480 19.307 9.794 0.29 101508. 0.6651
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3.49 0.0512 0.1445 0.0800 0.0283 0.276 4.342 4.282 205.494 0.491 19.046 9.451 0.29 101578. 0.6375
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5.23 0.0767 0.2091 0.0788 0.0289 0.281 4.433 4.217 209.774 0.501 18.755 9.117 0.29 101655. 0.6103
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6.98 0.1023 0.2689 0.0774 0.0295 0.287 4.517 4.143 213.767 0.510 18.429 8.791 0.29 101739. 0.5833
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8.72 0.1279 0.3240 0.0759 0.0300 0.292 4.593 4.062 217.372 0.519 18.067 8.475 0.29 101830. 0.5568
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10.46 0.1535 0.3748 0.0742 0.0304 0.296 4.659 3.971 220.488 0.526 17.665 8.170 0.29 101930. 0.5307
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12.21 0.1791 0.4215 0.0723 0.0307 0.299 4.712 3.872 223.007 0.532 17.221 7.875 0.29 102038. 0.5051
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13.95 0.2046 0.4643 0.0703 0.0310 0.301 4.751 3.762 224.827 0.537 16.735 7.590 0.29 102154. 0.4799
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15.70 0.2302 0.5035 0.0681 0.0311 0.303 4.773 3.643 225.859 0.539 16.205 7.316 0.29 102279. 0.4552
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17.44 0.2558 0.5393 0.0657 0.0311 0.303 4.776 3.515 226.032 0.540 15.634 7.053 0.29 102413. 0.4310
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19.18 0.2814 0.5718 0.0631 0.0310 0.302 4.761 3.377 225.294 0.538 15.022 6.799 0.29 102556. 0.4073
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20.93 0.3070 0.6013 0.0604 0.0308 0.300 4.725 3.231 223.609 0.534 14.372 6.554 0.29 102707. 0.3840
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22.67 0.3325 0.6278 0.0575 0.0304 0.296 4.669 3.077 220.950 0.527 13.687 6.317 0.29 102868. 0.3612
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24.42 0.3581 0.6515 0.0545 0.0299 0.291 4.592 2.916 217.296 0.519 12.969 6.086 0.29 103037. 0.3388
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26.16 0.3837 0.6722 0.0513 0.0293 0.285 4.493 2.748 212.630 0.508 12.222 5.861 0.29 103216. 0.3167
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27.90 0.4093 0.6901 0.0481 0.0285 0.278 4.373 2.574 206.940 0.494 11.448 5.641 0.29 103404. 0.2950
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29.65 0.4348 0.7050 0.0447 0.0276 0.268 4.231 2.394 200.211 0.478 10.650 5.424 0.29 103602. 0.2736
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31.39 0.4604 0.7168 0.0413 0.0265 0.258 4.066 2.210 192.435 0.459 9.829 5.208 0.29 103808. 0.2524
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33.14 0.4860 0.7252 0.0378 0.0253 0.246 3.880 2.021 183.602 0.438 8.988 4.992 0.29 104025. 0.2313
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34.88 0.5116 0.7298 0.0341 0.0239 0.233 3.671 1.828 173.706 0.415 8.130 4.772 0.29 104250. 0.2103
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36.63 0.5372 0.7299 0.0305 0.0224 0.218 3.439 1.631 162.745 0.389 7.255 4.546 0.29 104485. 0.1893
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38.37 0.5627 0.7246 0.0267 0.0208 0.202 3.185 1.432 150.719 0.360 6.367 4.308 0.29 104730. 0.1680
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40.11 0.5883 0.7124 0.0230 0.0190 0.185 2.908 1.229 137.636 0.329 5.468 4.051 0.29 104984. 0.1464
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41.86 0.6139 0.6909 0.0192 0.0170 0.166 2.610 1.025 123.511 0.295 4.560 3.765 0.29 105247. 0.1243
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43.60 0.6395 0.6558 0.0153 0.0149 0.145 2.290 0.820 108.370 0.259 3.646 3.431 0.29 105520. 0.1013
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45.35 0.6651 0.5996 0.0115 0.0127 0.124 1.949 0.613 92.248 0.220 2.729 3.016 0.29 105802. 0.0770
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47.09 0.6906 0.5071 0.0076 0.0104 0.101 1.589 0.407 75.197 0.180 1.812 2.457 0.29 106094. 0.0511
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48.83 0.7162 0.3424 0.0038 0.0079 0.077 1.210 0.202 57.276 0.137 0.898 1.599 0.29 106394. 0.0234
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50.58 0.7418 -0.0116 -0.0001 0.0053 0.051 0.809 -0.004 38.284 0.091 -0.020 -0.052 0.29 106687. 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 0.0825 0.0266 0.507 6.385 6.903 377.724 0.721 30.703 8.289 0.36 126801. 0.7099
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2.18 0.0256 0.0765 0.0816 0.0273 0.519 6.540 6.823 386.901 0.739 30.347 7.998 0.36 126881. 0.6810
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4.36 0.0512 0.1476 0.0805 0.0279 0.531 6.692 6.733 395.878 0.756 29.947 7.714 0.36 126968. 0.6525
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6.55 0.0768 0.2134 0.0793 0.0285 0.542 6.837 6.631 404.478 0.772 29.496 7.436 0.36 127064. 0.6242
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8.73 0.1024 0.2742 0.0779 0.0291 0.553 6.973 6.518 412.517 0.788 28.992 7.167 0.36 127170. 0.5964
|
|
10.91 0.1280 0.3303 0.0764 0.0296 0.563 7.096 6.391 419.798 0.802 28.429 6.906 0.36 127285. 0.5691
|
|
13.09 0.1536 0.3818 0.0747 0.0301 0.571 7.203 6.251 426.114 0.814 27.804 6.654 0.36 127410. 0.5423
|
|
15.27 0.1792 0.4292 0.0729 0.0304 0.578 7.290 6.095 431.252 0.824 27.112 6.411 0.36 127545. 0.5160
|
|
17.45 0.2048 0.4727 0.0708 0.0307 0.583 7.354 5.925 435.007 0.831 26.353 6.177 0.36 127691. 0.4902
|
|
19.64 0.2304 0.5125 0.0686 0.0308 0.586 7.391 5.738 437.198 0.835 25.524 5.953 0.36 127847. 0.4649
|
|
21.82 0.2560 0.5488 0.0662 0.0309 0.587 7.399 5.537 437.681 0.836 24.629 5.738 0.36 128015. 0.4401
|
|
24.00 0.2816 0.5819 0.0636 0.0308 0.585 7.376 5.321 436.353 0.833 23.669 5.531 0.36 128193. 0.4159
|
|
26.18 0.3072 0.6120 0.0609 0.0306 0.581 7.322 5.092 433.137 0.827 22.648 5.332 0.36 128383. 0.3922
|
|
28.36 0.3328 0.6391 0.0580 0.0302 0.574 7.235 4.850 427.978 0.817 21.572 5.140 0.36 128584. 0.3690
|
|
30.54 0.3584 0.6633 0.0550 0.0297 0.564 7.114 4.596 420.837 0.804 20.444 4.954 0.36 128797. 0.3462
|
|
32.73 0.3840 0.6848 0.0518 0.0290 0.552 6.959 4.332 411.678 0.786 19.269 4.773 0.36 129021. 0.3238
|
|
34.91 0.4096 0.7034 0.0485 0.0283 0.537 6.770 4.058 400.474 0.765 18.051 4.596 0.36 129257. 0.3018
|
|
37.09 0.4352 0.7191 0.0451 0.0273 0.519 6.545 3.776 387.202 0.740 16.794 4.423 0.36 129504. 0.2801
|
|
39.27 0.4608 0.7319 0.0417 0.0262 0.499 6.286 3.485 371.840 0.710 15.501 4.251 0.36 129763. 0.2587
|
|
41.45 0.4864 0.7414 0.0381 0.0250 0.475 5.990 3.187 354.370 0.677 14.177 4.079 0.36 130034. 0.2374
|
|
43.64 0.5120 0.7472 0.0345 0.0236 0.449 5.659 2.883 334.779 0.639 12.824 3.906 0.36 130316. 0.2162
|
|
45.82 0.5376 0.7489 0.0308 0.0221 0.420 5.292 2.573 313.062 0.598 11.447 3.729 0.36 130611. 0.1950
|
|
48.00 0.5632 0.7454 0.0270 0.0204 0.388 4.889 2.259 289.220 0.552 10.048 3.543 0.36 130917. 0.1736
|
|
50.18 0.5888 0.7354 0.0232 0.0186 0.353 4.450 1.940 263.270 0.503 8.631 3.343 0.36 131235. 0.1518
|
|
52.36 0.6144 0.7164 0.0194 0.0166 0.315 3.977 1.619 235.240 0.449 7.200 3.121 0.36 131565. 0.1294
|
|
54.54 0.6400 0.6844 0.0155 0.0145 0.275 3.468 1.295 205.181 0.392 5.759 2.862 0.36 131907. 0.1062
|
|
56.73 0.6656 0.6316 0.0116 0.0122 0.232 2.927 0.970 173.166 0.331 4.313 2.540 0.36 132260. 0.0815
|
|
58.91 0.6912 0.5421 0.0077 0.0098 0.187 2.355 0.645 139.297 0.266 2.868 2.099 0.37 132625. 0.0549
|
|
61.09 0.7168 0.3761 0.0038 0.0073 0.139 1.753 0.321 103.692 0.198 1.428 1.404 0.37 133000. 0.0259
|
|
63.27 0.7424 -0.0094 -0.0001 0.0046 0.088 1.113 -0.005 65.870 0.126 -0.022 -0.034 0.37 133364. 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 0.0831 0.0265 0.869 9.128 10.008 647.980 1.031 44.514 7.005 0.43 152155. 0.7224
|
|
2.65 0.0259 0.0784 0.0822 0.0271 0.891 9.360 9.894 664.418 1.057 44.008 6.754 0.43 152252. 0.6925
|
|
5.30 0.0518 0.1511 0.0811 0.0278 0.913 9.586 9.765 680.516 1.083 43.435 6.508 0.43 152358. 0.6630
|
|
7.94 0.0777 0.2183 0.0799 0.0284 0.933 9.804 9.620 695.951 1.108 42.788 6.269 0.43 152475. 0.6339
|
|
10.59 0.1036 0.2803 0.0785 0.0290 0.953 10.007 9.456 710.387 1.131 42.059 6.037 0.43 152604. 0.6052
|
|
13.24 0.1294 0.3374 0.0770 0.0295 0.970 10.191 9.272 723.461 1.151 41.243 5.813 0.43 152744. 0.5770
|
|
15.89 0.1553 0.3898 0.0753 0.0300 0.985 10.351 9.068 734.789 1.169 40.333 5.597 0.43 152896. 0.5494
|
|
18.53 0.1812 0.4379 0.0734 0.0304 0.998 10.481 8.841 743.985 1.184 39.324 5.390 0.43 153062. 0.5224
|
|
21.18 0.2071 0.4820 0.0713 0.0306 1.007 10.575 8.591 750.671 1.195 38.212 5.191 0.43 153240. 0.4959
|
|
23.83 0.2330 0.5223 0.0691 0.0308 1.012 10.629 8.317 754.518 1.201 36.996 5.000 0.43 153432. 0.4701
|
|
26.48 0.2589 0.5591 0.0666 0.0308 1.013 10.639 8.021 755.267 1.202 35.679 4.817 0.43 153637. 0.4447
|
|
29.12 0.2848 0.5927 0.0640 0.0307 1.009 10.604 7.704 752.730 1.198 34.266 4.642 0.43 153855. 0.4200
|
|
31.77 0.3107 0.6231 0.0612 0.0305 1.001 10.520 7.366 746.773 1.189 32.762 4.474 0.43 154088. 0.3958
|
|
34.42 0.3365 0.6506 0.0582 0.0301 0.989 10.386 7.009 737.301 1.173 31.175 4.312 0.43 154335. 0.3721
|
|
37.07 0.3624 0.6752 0.0551 0.0296 0.971 10.202 6.635 724.240 1.153 29.510 4.155 0.43 154595. 0.3489
|
|
39.71 0.3883 0.6970 0.0519 0.0289 0.949 9.967 6.245 707.533 1.126 27.776 4.003 0.43 154870. 0.3261
|
|
42.36 0.4142 0.7159 0.0485 0.0281 0.921 9.680 5.840 687.132 1.094 25.978 3.855 0.43 155158. 0.3037
|
|
45.01 0.4401 0.7321 0.0450 0.0271 0.889 9.340 5.423 662.995 1.055 24.122 3.710 0.43 155461. 0.2816
|
|
47.66 0.4660 0.7452 0.0415 0.0259 0.852 8.946 4.994 635.086 1.011 22.214 3.567 0.43 155779. 0.2598
|
|
50.30 0.4919 0.7551 0.0378 0.0246 0.809 8.500 4.555 603.372 0.960 20.259 3.424 0.43 156111. 0.2382
|
|
52.95 0.5178 0.7613 0.0341 0.0232 0.761 7.999 4.106 567.835 0.904 18.262 3.279 0.43 156457. 0.2166
|
|
55.60 0.5436 0.7633 0.0303 0.0216 0.709 7.445 3.649 528.466 0.841 16.229 3.132 0.43 156818. 0.1950
|
|
58.25 0.5695 0.7601 0.0264 0.0198 0.651 6.836 3.185 485.273 0.772 14.165 2.977 0.44 157193. 0.1731
|
|
60.90 0.5954 0.7500 0.0225 0.0179 0.588 6.174 2.715 438.290 0.698 12.075 2.809 0.44 157583. 0.1509
|
|
63.54 0.6213 0.7303 0.0186 0.0158 0.520 5.460 2.240 387.578 0.617 9.965 2.622 0.44 157987. 0.1279
|
|
66.19 0.6472 0.6963 0.0146 0.0136 0.447 4.694 1.763 333.238 0.530 7.842 2.400 0.44 158406. 0.1039
|
|
68.84 0.6731 0.6383 0.0107 0.0112 0.369 3.880 1.284 275.419 0.438 5.713 2.115 0.44 158839. 0.0781
|
|
71.49 0.6990 0.5349 0.0067 0.0088 0.287 3.019 0.806 214.320 0.341 3.587 1.707 0.44 159286. 0.0500
|
|
74.13 0.7249 0.3248 0.0027 0.0061 0.201 2.115 0.331 150.133 0.239 1.471 0.999 0.44 159744. 0.0187
|
|
76.78 0.7507
|
|
|
|
|
|
|
|
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 0.0838 0.0264 1.378 12.410 13.731 1027.812 1.402 61.073 6.059 0.50 177506. 0.7319
|
|
3.07 0.0257 0.0785 0.0829 0.0271 1.414 12.732 13.582 1054.435 1.438 60.412 5.842 0.50 177617. 0.7019
|
|
6.13 0.0514 0.1513 0.0818 0.0278 1.449 13.047 13.413 1080.565 1.474 59.659 5.630 0.50 177740. 0.6721
|
|
9.20 0.0771 0.2186 0.0807 0.0284 1.483 13.351 13.221 1105.685 1.508 58.806 5.423 0.50 177876. 0.6428
|
|
12.26 0.1028 0.2808 0.0793 0.0290 1.514 13.635 13.004 1129.258 1.541 57.843 5.223 0.50 178024. 0.6140
|
|
15.33 0.1285 0.3380 0.0778 0.0296 1.543 13.894 12.761 1150.703 1.570 56.759 5.030 0.50 178186. 0.5857
|
|
18.39 0.1541 0.3905 0.0762 0.0301 1.568 14.120 12.488 1169.405 1.595 55.548 4.844 0.50 178363. 0.5580
|
|
21.46 0.1798 0.4388 0.0743 0.0305 1.589 14.305 12.185 1184.745 1.616 54.200 4.665 0.50 178553. 0.5308
|
|
24.52 0.2055 0.4831 0.0723 0.0308 1.604 14.443 11.851 1196.114 1.632 52.711 4.494 0.50 178759. 0.5043
|
|
27.59 0.2312 0.5237 0.0701 0.0309 1.613 14.525 11.484 1202.973 1.641 51.080 4.330 0.50 178981. 0.4783
|
|
30.65 0.2569 0.5608 0.0676 0.0310 1.616 14.549 11.085 1204.899 1.644 49.308 4.173 0.50 179217. 0.4529
|
|
33.72 0.2826 0.5946 0.0650 0.0309 1.611 14.509 10.657 1201.577 1.639 47.402 4.023 0.50 179470. 0.4281
|
|
36.78 0.3083 0.6255 0.0622 0.0307 1.600 14.402 10.200 1192.790 1.627 45.371 3.879 0.50 179738. 0.4038
|
|
39.85 0.3340 0.6534 0.0593 0.0303 1.580 14.228 9.717 1178.379 1.608 43.223 3.740 0.50 180023. 0.3801
|
|
42.91 0.3597 0.6786 0.0562 0.0298 1.553 13.985 9.210 1158.232 1.580 40.967 3.607 0.50 180323. 0.3568
|
|
45.98 0.3854 0.7010 0.0530 0.0291 1.518 13.672 8.681 1132.259 1.545 38.614 3.478 0.50 180640. 0.3340
|
|
49.04 0.4110 0.7207 0.0496 0.0283 1.476 13.287 8.132 1100.385 1.501 36.171 3.352 0.50 180973. 0.3116
|
|
52.11 0.4367 0.7377 0.0461 0.0273 1.425 12.830 7.565 1062.549 1.450 33.648 3.229 0.50 181322. 0.2895
|
|
55.18 0.4624 0.7519 0.0426 0.0262 1.366 12.300 6.981 1018.694 1.390 31.052 3.108 0.51 181688. 0.2677
|
|
58.24 0.4881 0.7630 0.0389 0.0249 1.299 11.698 6.383 968.773 1.322 28.391 2.988 0.51 182070. 0.2461
|
|
61.31 0.5138 0.7708 0.0352 0.0235 1.224 11.021 5.771 912.751 1.245 25.671 2.868 0.51 182468. 0.2246
|
|
64.37 0.5395 0.7747 0.0314 0.0219 1.141 10.271 5.148 850.613 1.160 22.899 2.745 0.51 182884. 0.2030
|
|
67.44 0.5652 0.7738 0.0275 0.0201 1.049 9.447 4.515 782.368 1.067 20.083 2.618 0.51 183316. 0.1813
|
|
70.50 0.5909 0.7669 0.0236 0.0182 0.950 8.550 3.874 708.059 0.966 17.229 2.481 0.51 183764. 0.1592
|
|
73.57 0.6166 0.7516 0.0197 0.0161 0.842 7.580 3.225 627.776 0.856 14.347 2.330 0.51 184230. 0.1364
|
|
76.63 0.6423 0.7238 0.0157 0.0139 0.726 6.540 2.573 541.665 0.739 11.444 2.154 0.51 184711. 0.1126
|
|
79.70 0.6679 0.6754 0.0117 0.0116 0.603 5.433 1.918 449.945 0.614 8.530 1.933 0.51 185210. 0.0873
|
|
82.76 0.6936 0.5888 0.0077 0.0091 0.473 4.261 1.263 352.918 0.481 5.617 1.623 0.51 185724. 0.0594
|
|
85.83 0.7193 0.4153 0.0037 0.0065 0.336 3.030 0.611 250.922 0.342 2.716 1.104 0.51 186253. 0.0281
|
|
88.89 0.7450
|
|
|
|
|
|
|
|
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 0.0845 0.0265 2.065 16.273 18.099 1540.221 1.839 80.506 5.330 0.57 202851. 0.7392
|
|
3.50 0.0257 0.0789 0.0837 0.0272 2.120 16.706 17.913 1581.192 1.887 79.678 5.138 0.57 202978. 0.7089
|
|
7.00 0.0513 0.1520 0.0827 0.0279 2.174 17.132 17.700 1621.498 1.936 78.731 4.951 0.57 203119. 0.6790
|
|
10.50 0.0770 0.2195 0.0815 0.0286 2.227 17.542 17.458 1660.346 1.982 77.651 4.769 0.57 203274. 0.6495
|
|
14.00 0.1027 0.2819 0.0802 0.0292 2.276 17.928 17.182 1696.895 2.026 76.425 4.593 0.57 203443. 0.6206
|
|
17.50 0.1283 0.3393 0.0788 0.0298 2.320 18.281 16.870 1730.246 2.065 75.039 4.422 0.57 203629. 0.5921
|
|
21.00 0.1540 0.3921 0.0772 0.0303 2.359 18.589 16.520 1759.448 2.100 73.480 4.259 0.57 203830. 0.5642
|
|
24.50 0.1797 0.4406 0.0753 0.0307 2.392 18.844 16.129 1783.534 2.129 71.740 4.102 0.57 204049. 0.5370
|
|
28.00 0.2054 0.4851 0.0733 0.0310 2.416 19.034 15.694 1801.563 2.150 69.809 3.951 0.57 204284. 0.5103
|
|
31.50 0.2310 0.5259 0.0711 0.0312 2.431 19.152 15.217 1812.696 2.164 67.685 3.808 0.57 204538. 0.4842
|
|
35.00 0.2567 0.5632 0.0686 0.0313 2.436 19.189 14.697 1816.263 2.168 65.372 3.670 0.57 204808. 0.4587
|
|
38.50 0.2824 0.5974 0.0660 0.0312 2.430 19.142 14.136 1811.781 2.163 62.877 3.539 0.57 205097. 0.4337
|
|
42.00 0.3080 0.6285 0.0632 0.0310 2.412 19.006 13.537 1798.908 2.147 60.212 3.413 0.57 205404. 0.4094
|
|
45.50 0.3337 0.6568 0.0603 0.0306 2.384 18.779 12.902 1777.409 2.122 57.388 3.292 0.57 205730. 0.3855
|
|
49.01 0.3594 0.6824 0.0571 0.0301 2.343 18.459 12.234 1747.116 2.085 54.418 3.176 0.57 206073. 0.3621
|
|
52.51 0.3850 0.7053 0.0539 0.0294 2.290 18.045 11.537 1707.902 2.039 51.316 3.064 0.58 206435. 0.3392
|
|
56.01 0.4107 0.7255 0.0505 0.0286 2.226 17.535 10.812 1659.666 1.981 48.093 2.955 0.58 206816. 0.3167
|
|
59.51 0.4364 0.7431 0.0470 0.0276 2.149 16.929 10.063 1602.317 1.913 44.761 2.849 0.58 207215. 0.2946
|
|
63.01 0.4621 0.7580 0.0434 0.0265 2.060 16.226 9.292 1535.783 1.833 41.330 2.744 0.58 207633. 0.2727
|
|
66.51 0.4877 0.7700 0.0397 0.0251 1.958 15.425 8.500 1459.995 1.743 37.810 2.641 0.58 208070. 0.2510
|
|
70.01 0.5134 0.7787 0.0359 0.0237 1.844 14.526 7.691 1374.909 1.641 34.211 2.537 0.58 208525. 0.2294
|
|
73.51 0.5391 0.7838 0.0321 0.0221 1.717 13.529 6.866 1280.498 1.528 30.542 2.432 0.58 209000. 0.2078
|
|
77.01 0.5647 0.7844 0.0282 0.0203 1.578 12.433 6.028 1176.777 1.405 26.812 2.323 0.58 209493. 0.1859
|
|
80.51 0.5904 0.7792 0.0242 0.0183 1.427 11.239 5.178 1063.811 1.270 23.031 2.208 0.58 210005. 0.1638
|
|
84.01 0.6161 0.7660 0.0202 0.0162 1.263 9.950 4.319 941.731 1.124 19.209 2.080 0.58 210537. 0.1409
|
|
87.51 0.6417 0.7411 0.0161 0.0140 1.087 8.566 3.453 810.759 0.968 15.358 1.932 0.58 211087. 0.1170
|
|
91.01 0.6674 0.6966 0.0121 0.0116 0.900 7.092 2.584 671.225 0.801 11.492 1.746 0.58 211656. 0.0915
|
|
94.51 0.6931 0.6153 0.0080 0.0090 0.702 5.532 1.714 523.585 0.625 7.625 1.485 0.58 212243. 0.0634
|
|
98.01 0.7187 0.4488 0.0040 0.0063 0.494 3.892 0.848 368.362 0.440 3.773 1.045 0.59 212847. 0.0314
|
|
101.51 0.7444 -0.0385 -0.0002 0.0035 0.269 2.120 -0.038 200.669 0.240 -0.170 -0.087 0.59 213389. 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 0.0854 0.0268 2.967 20.782 23.146 2212.860 2.348 102.953 4.744 0.64 228192. 0.7440
|
|
3.98 0.0259 0.0797 0.0846 0.0275 3.049 21.352 22.922 2273.607 2.412 101.956 4.573 0.64 228336. 0.7137
|
|
7.95 0.0518 0.1536 0.0836 0.0282 3.129 21.916 22.662 2333.588 2.476 100.802 4.405 0.64 228496. 0.6836
|
|
11.93 0.0778 0.2219 0.0825 0.0289 3.207 22.460 22.364 2391.585 2.538 99.475 4.241 0.64 228672. 0.6538
|
|
15.91 0.1037 0.2848 0.0813 0.0296 3.281 22.974 22.022 2446.308 2.596 97.955 4.083 0.64 228866. 0.6246
|
|
19.89 0.1296 0.3427 0.0798 0.0302 3.348 23.444 21.632 2496.336 2.649 96.221 3.930 0.64 229077. 0.5959
|
|
23.86 0.1555 0.3958 0.0782 0.0307 3.406 23.856 21.191 2540.196 2.695 94.257 3.784 0.64 229308. 0.5678
|
|
27.84 0.1815 0.4447 0.0764 0.0312 3.455 24.196 20.694 2576.374 2.734 92.049 3.643 0.64 229558. 0.5403
|
|
31.82 0.2074 0.4894 0.0743 0.0315 3.491 24.450 20.140 2603.407 2.762 89.584 3.509 0.64 229827. 0.5133
|
|
35.79 0.2333 0.5305 0.0721 0.0317 3.513 24.605 19.528 2620.004 2.780 86.860 3.381 0.64 230117. 0.4870
|
|
39.77 0.2592 0.5681 0.0696 0.0318 3.520 24.654 18.858 2625.147 2.785 83.881 3.258 0.64 230428. 0.4612
|
|
43.75 0.2852 0.6025 0.0669 0.0317 3.511 24.588 18.133 2618.112 2.778 80.657 3.141 0.65 230759. 0.4361
|
|
47.73 0.3111 0.6339 0.0641 0.0314 3.485 24.403 17.357 2598.400 2.757 77.203 3.030 0.65 231111. 0.4115
|
|
51.70 0.3370 0.6625 0.0610 0.0310 3.441 24.095 16.533 2565.676 2.722 73.537 2.923 0.65 231485. 0.3874
|
|
55.68 0.3629 0.6883 0.0578 0.0305 3.379 23.664 15.665 2519.712 2.673 69.676 2.820 0.65 231879. 0.3638
|
|
59.66 0.3889 0.7115 0.0545 0.0298 3.299 23.106 14.757 2460.341 2.611 65.638 2.720 0.65 232294. 0.3407
|
|
63.63 0.4148 0.7321 0.0510 0.0289 3.202 22.421 13.813 2387.437 2.533 61.438 2.624 0.65 232731. 0.3179
|
|
67.61 0.4407 0.7500 0.0474 0.0278 3.086 21.609 12.836 2300.891 2.441 57.093 2.530 0.65 233189. 0.2955
|
|
71.59 0.4666 0.7652 0.0437 0.0266 2.951 20.667 11.829 2200.612 2.335 52.617 2.438 0.65 233668. 0.2734
|
|
75.57 0.4926 0.7775 0.0398 0.0252 2.798 19.595 10.797 2086.517 2.214 48.024 2.347 0.65 234169. 0.2514
|
|
79.54 0.5185 0.7866 0.0359 0.0237 2.626 18.393 9.740 1958.549 2.078 43.325 2.256 0.65 234692. 0.2295
|
|
83.52 0.5444 0.7920 0.0320 0.0220 2.436 17.061 8.663 1816.683 1.928 38.534 2.163 0.65 235236. 0.2075
|
|
87.50 0.5703 0.7927 0.0279 0.0201 2.227 15.599 7.568 1660.959 1.762 33.663 2.067 0.65 235802. 0.1853
|
|
91.47 0.5963 0.7876 0.0238 0.0180 2.000 14.007 6.458 1491.491 1.583 28.725 1.964 0.65 236389. 0.1627
|
|
95.45 0.6222 0.7740 0.0197 0.0158 1.755 12.289 5.336 1308.505 1.388 23.735 1.850 0.66 236998. 0.1393
|
|
99.43 0.6481 0.7475 0.0155 0.0135 1.492 10.447 4.206 1112.364 1.180 18.707 1.715 0.66 237629. 0.1146
|
|
103.41 0.6740 0.6989 0.0113 0.0109 1.212 8.486 3.071 903.609 0.959 13.662 1.542 0.66 238281. 0.0881
|
|
107.38 0.7000 0.6058 0.0072 0.0083 0.916 6.414 1.938 682.973 0.725 8.619 1.287 0.66 238953. 0.0584
|
|
111.36 0.7259 0.3968 0.0030 0.0055 0.605 4.237 0.809 451.168 0.479 3.596 0.813 0.66 239643. 0.0238
|
|
115.34 0.7518
|
|
|
|
|
|
|
|
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 0.0864 0.0275 4.187 26.389 28.901 3122.082 2.981 128.554 4.199 0.71 253526. 0.7358
|
|
4.42 0.0259 0.0786 0.0856 0.0283 4.297 27.083 28.647 3204.271 3.060 127.421 4.055 0.71 253686. 0.7075
|
|
8.84 0.0519 0.1517 0.0847 0.0290 4.406 27.770 28.349 3285.513 3.137 126.098 3.914 0.71 253863. 0.6793
|
|
13.26 0.0778 0.2195 0.0837 0.0297 4.511 28.435 28.003 3364.143 3.213 124.558 3.776 0.71 254059. 0.6513
|
|
17.68 0.1037 0.2823 0.0825 0.0303 4.611 29.062 27.602 3438.396 3.283 122.774 3.641 0.71 254274. 0.6236
|
|
22.10 0.1297 0.3402 0.0811 0.0309 4.702 29.636 27.140 3506.343 3.348 120.720 3.511 0.71 254509. 0.5962
|
|
26.53 0.1556 0.3936 0.0795 0.0314 4.782 30.140 26.612 3565.949 3.405 118.370 3.385 0.71 254766. 0.5692
|
|
30.95 0.1816 0.4428 0.0778 0.0319 4.848 30.556 26.012 3615.142 3.452 115.703 3.264 0.72 255044. 0.5426
|
|
35.37 0.2075 0.4880 0.0757 0.0322 4.897 30.867 25.338 3651.884 3.487 112.705 3.147 0.72 255345. 0.5164
|
|
39.79 0.2334 0.5294 0.0735 0.0324 4.927 31.056 24.588 3674.336 3.509 109.368 3.035 0.72 255668. 0.4906
|
|
44.21 0.2594 0.5675 0.0710 0.0325 4.936 31.113 23.763 3681.013 3.515 105.697 2.928 0.72 256015. 0.4653
|
|
48.63 0.2853 0.6023 0.0683 0.0324 4.923 31.027 22.865 3670.818 3.505 101.705 2.825 0.72 256384. 0.4404
|
|
53.05 0.3112 0.6342 0.0655 0.0321 4.885 30.791 21.900 3642.963 3.479 97.412 2.727 0.72 256777. 0.4160
|
|
57.47 0.3372 0.6632 0.0624 0.0317 4.823 30.402 20.872 3596.880 3.435 92.840 2.632 0.72 257194. 0.3920
|
|
61.89 0.3631 0.6894 0.0591 0.0312 4.737 29.855 19.787 3532.141 3.373 88.011 2.541 0.72 257633. 0.3684
|
|
66.31 0.3890 0.7131 0.0557 0.0304 4.624 29.147 18.649 3448.439 3.293 82.950 2.453 0.72 258096. 0.3453
|
|
70.74 0.4150 0.7342 0.0522 0.0295 4.486 28.277 17.464 3345.540 3.195 77.678 2.368 0.72 258583. 0.3225
|
|
75.16 0.4409 0.7527 0.0485 0.0284 4.322 27.244 16.236 3223.270 3.078 72.216 2.285 0.72 259094. 0.3001
|
|
79.58 0.4669 0.7686 0.0447 0.0272 4.132 26.046 14.969 3081.524 2.943 66.582 2.203 0.72 259628. 0.2779
|
|
84.00 0.4928 0.7817 0.0409 0.0258 3.916 24.682 13.668 2920.219 2.789 60.794 2.123 0.72 260186. 0.2558
|
|
88.42 0.5187 0.7917 0.0369 0.0242 3.673 23.153 12.336 2739.289 2.616 54.869 2.043 0.72 260769. 0.2339
|
|
92.84 0.5447 0.7982 0.0328 0.0224 3.404 21.458 10.976 2538.715 2.424 48.823 1.961 0.72 261375. 0.2118
|
|
97.26 0.5706 0.8002 0.0287 0.0204 3.109 19.597 9.594 2318.541 2.214 42.672 1.877 0.73 262005. 0.1895
|
|
101.68 0.5965 0.7966 0.0245 0.0183 2.788 17.572 8.191 2078.931 1.985 36.432 1.787 0.73 262659. 0.1667
|
|
106.10 0.6225 0.7849 0.0202 0.0161 2.441 15.385 6.772 1820.200 1.738 30.121 1.687 0.73 263336. 0.1431
|
|
110.52 0.6484 0.7609 0.0160 0.0136 2.069 13.041 5.342 1542.863 1.473 23.760 1.570 0.73 264038. 0.1183
|
|
114.95 0.6743 0.7154 0.0117 0.0110 1.673 10.546 3.905 1247.725 1.191 17.371 1.420 0.73 264764. 0.0915
|
|
119.37 0.7003 0.6262 0.0074 0.0083 1.255 7.911 2.469 935.949 0.894 10.983 1.197 0.73 265512. 0.0613
|
|
123.79 0.7262 0.4197 0.0031 0.0054 0.816 5.146 1.038 608.818 0.581 4.617 0.773 0.73 266280. 0.0257
|
|
128.21 0.7522
|
|
|
|
|
|
|
|
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 0.0874 0.0299 6.059 34.715 35.380 4517.900 3.922 157.370 3.552 0.79 278853. 0.6887
|
|
4.83 0.0258 0.0731 0.0867 0.0306 6.195 35.497 35.109 4619.655 4.010 156.163 3.447 0.79 279027. 0.6658
|
|
9.67 0.0516 0.1417 0.0859 0.0313 6.328 36.261 34.788 4719.132 4.097 154.736 3.344 0.79 279220. 0.6429
|
|
14.50 0.0773 0.2061 0.0850 0.0319 6.456 36.990 34.409 4813.992 4.179 153.053 3.242 0.79 279433. 0.6199
|
|
19.34 0.1031 0.2664 0.0839 0.0325 6.573 37.665 33.965 4901.811 4.255 151.078 3.143 0.79 279667. 0.5971
|
|
24.17 0.1289 0.3228 0.0826 0.0330 6.678 38.266 33.447 4979.988 4.323 148.772 3.046 0.79 279924. 0.5743
|
|
29.01 0.1547 0.3754 0.0811 0.0334 6.767 38.772 32.846 5045.874 4.380 146.101 2.953 0.79 280204. 0.5516
|
|
33.84 0.1805 0.4245 0.0794 0.0338 6.835 39.164 32.157 5096.867 4.425 143.035 2.862 0.79 280507. 0.5290
|
|
38.67 0.2063 0.4703 0.0775 0.0340 6.880 39.422 31.373 5130.530 4.454 139.549 2.774 0.79 280836. 0.5064
|
|
43.51 0.2320 0.5128 0.0753 0.0341 6.899 39.532 30.493 5144.759 4.466 135.631 2.688 0.79 281189. 0.4839
|
|
48.34 0.2578 0.5522 0.0729 0.0340 6.890 39.479 29.515 5137.965 4.460 131.284 2.606 0.79 281568. 0.4614
|
|
53.18 0.2836 0.5887 0.0703 0.0339 6.851 39.258 28.445 5109.100 4.435 126.521 2.525 0.79 281972. 0.4390
|
|
58.01 0.3094 0.6223 0.0674 0.0335 6.782 38.861 27.286 5057.533 4.391 121.368 2.447 0.79 282402. 0.4167
|
|
62.85 0.3352 0.6532 0.0643 0.0330 6.682 38.287 26.046 4982.837 4.326 115.851 2.371 0.79 282857. 0.3944
|
|
67.68 0.3610 0.6813 0.0611 0.0324 6.550 37.533 24.730 4884.660 4.240 110.001 2.296 0.79 283337. 0.3723
|
|
72.51 0.3867 0.7068 0.0577 0.0316 6.387 36.596 23.347 4762.655 4.135 103.847 2.223 0.79 283843. 0.3502
|
|
77.35 0.4125 0.7297 0.0541 0.0306 6.191 35.472 21.901 4616.447 4.008 97.417 2.152 0.79 284375. 0.3283
|
|
82.18 0.4383 0.7499 0.0504 0.0295 5.962 34.160 20.400 4445.661 3.859 90.737 2.081 0.79 284933. 0.3064
|
|
87.02 0.4641 0.7673 0.0466 0.0282 5.699 32.656 18.848 4249.911 3.689 83.834 2.011 0.79 285516. 0.2847
|
|
91.85 0.4899 0.7820 0.0426 0.0267 5.403 30.957 17.250 4028.810 3.497 76.729 1.942 0.79 286125. 0.2629
|
|
96.69 0.5157 0.7936 0.0386 0.0251 5.072 29.060 15.613 3782.004 3.283 69.445 1.872 0.80 286760. 0.2412
|
|
101.52 0.5414 0.8019 0.0344 0.0233 4.706 26.964 13.939 3509.193 3.046 62.002 1.802 0.80 287421. 0.2193
|
|
106.35 0.5672 0.8059 0.0302 0.0213 4.305 24.669 12.235 3210.472 2.787 54.420 1.728 0.80 288108. 0.1971
|
|
111.19 0.5930 0.8046 0.0259 0.0191 3.870 22.177 10.503 2886.155 2.506 46.718 1.651 0.80 288820. 0.1744
|
|
116.02 0.6188 0.7957 0.0216 0.0168 3.402 19.492 8.749 2536.771 2.202 38.918 1.564 0.80 289559. 0.1508
|
|
120.86 0.6446 0.7752 0.0172 0.0143 2.901 16.625 6.979 2163.612 1.878 31.044 1.463 0.80 290323. 0.1260
|
|
125.69 0.6704 0.7346 0.0128 0.0117 2.372 13.590 5.198 1768.635 1.535 23.123 1.333 0.80 291113. 0.0991
|
|
130.53 0.6961 0.6542 0.0084 0.0090 1.816 10.408 3.414 1354.498 1.176 15.186 1.143 0.80 291928. 0.0689
|
|
135.36 0.7219 0.4756 0.0040 0.0061 1.239 7.102 1.633 924.254 0.802 7.264 0.801 0.81 292766. 0.0334
|
|
140.19 0.7477
|
|
|
|
|
|
|
|
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 0.0882 0.0352 9.241 48.540 42.491 6891.373 5.484 188.999 2.797 0.86 304178. 0.5943
|
|
5.27 0.0258 0.0630 0.0876 0.0358 9.411 49.428 42.220 7017.474 5.584 187.796 2.729 0.86 304365. 0.5780
|
|
10.53 0.0515 0.1229 0.0870 0.0364 9.573 50.279 41.896 7138.344 5.681 186.352 2.662 0.86 304573. 0.5617
|
|
15.80 0.0773 0.1799 0.0862 0.0370 9.722 51.066 41.507 7250.006 5.769 184.621 2.597 0.86 304804. 0.5453
|
|
21.07 0.1030 0.2340 0.0852 0.0375 9.854 51.758 41.041 7348.285 5.848 182.552 2.533 0.86 305057. 0.5290
|
|
26.34 0.1288 0.2854 0.0840 0.0379 9.962 52.326 40.488 7428.927 5.912 180.092 2.472 0.86 305335. 0.5127
|
|
31.60 0.1545 0.3343 0.0827 0.0382 10.041 52.741 39.836 7487.810 5.959 177.191 2.413 0.86 305639. 0.4965
|
|
36.87 0.1803 0.3809 0.0811 0.0384 10.086 52.976 39.074 7521.265 5.985 173.802 2.356 0.86 305970. 0.4802
|
|
42.14 0.2060 0.4252 0.0793 0.0384 10.093 53.011 38.194 7526.228 5.989 169.888 2.302 0.86 306328. 0.4637
|
|
47.41 0.2318 0.4674 0.0772 0.0383 10.058 52.829 37.191 7500.336 5.969 165.426 2.249 0.86 306713. 0.4471
|
|
52.67 0.2575 0.5076 0.0749 0.0380 9.980 52.419 36.063 7442.122 5.922 160.410 2.198 0.86 307126. 0.4303
|
|
57.94 0.2833 0.5456 0.0723 0.0375 9.859 51.781 34.814 7351.571 5.850 154.854 2.148 0.86 307568. 0.4131
|
|
63.21 0.3090 0.5816 0.0694 0.0369 9.694 50.918 33.450 7229.048 5.753 148.786 2.099 0.86 308037. 0.3957
|
|
68.48 0.3348 0.6154 0.0664 0.0361 9.488 49.836 31.978 7075.386 5.630 142.239 2.050 0.86 308534. 0.3779
|
|
73.74 0.3605 0.6470 0.0631 0.0352 9.242 48.541 30.407 6891.603 5.484 135.252 2.001 0.86 309060. 0.3597
|
|
79.01 0.3863 0.6762 0.0597 0.0341 8.956 47.041 28.747 6678.594 5.315 127.865 1.952 0.86 309613. 0.3412
|
|
84.28 0.4120 0.7031 0.0561 0.0329 8.632 45.339 27.004 6436.944 5.122 120.115 1.903 0.86 310195. 0.3223
|
|
89.55 0.4378 0.7273 0.0523 0.0315 8.270 43.437 25.188 6166.881 4.907 112.038 1.853 0.87 310804. 0.3031
|
|
94.81 0.4635 0.7488 0.0484 0.0299 7.869 41.333 23.306 5868.218 4.670 103.666 1.801 0.87 311441. 0.2835
|
|
100.08 0.4893 0.7674 0.0443 0.0283 7.430 39.024 21.364 5540.402 4.409 95.028 1.749 0.87 312106. 0.2635
|
|
105.35 0.5150 0.7828 0.0402 0.0265 6.950 36.505 19.368 5182.742 4.124 86.151 1.695 0.87 312800. 0.2432
|
|
110.62 0.5408 0.7948 0.0360 0.0245 6.430 33.771 17.325 4794.634 3.815 77.061 1.639 0.87 313521. 0.2224
|
|
115.88 0.5665 0.8025 0.0316 0.0223 5.868 30.820 15.240 4375.606 3.482 67.786 1.580 0.87 314271. 0.2010
|
|
121.15 0.5923 0.8031 0.0272 0.0201 5.276 27.713 13.117 3934.538 3.131 58.345 1.512 0.87 315048. 0.1785
|
|
126.42 0.6180 0.7916 0.0228 0.0178 4.668 24.519 10.962 3481.115 2.770 48.758 1.428 0.87 315853. 0.1541
|
|
131.69 0.6438 0.7654 0.0182 0.0153 4.029 21.163 8.783 3004.603 2.391 39.065 1.326 0.87 316686. 0.1281
|
|
136.95 0.6696 0.7149 0.0137 0.0128 3.365 17.674 6.587 2509.279 1.997 29.299 1.191 0.88 317547. 0.0996
|
|
142.22 0.6953 0.6198 0.0091 0.0102 2.682 14.087 4.383 2000.041 1.592 19.498 0.994 0.88 318436. 0.0678
|
|
147.49 0.7211 0.4314 0.0045 0.0076 1.989 10.445 2.181 1482.963 1.180 9.702 0.667 0.88 319348. 0.0321
|
|
152.76 0.7468 -0.0283 -0.0002 0.0047 1.248 6.555 -0.087 930.570 0.741 -0.385 -0.042 0.88 320172. 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 0.0871 0.0406 13.553 65.712 49.264 10106.842 7.424 219.126 2.211 0.93 329554. 0.5058
|
|
5.74 0.0259 0.0544 0.0867 0.0412 13.776 66.793 49.007 10273.077 7.546 217.982 2.164 0.93 329754. 0.4938
|
|
11.47 0.0518 0.1064 0.0861 0.0419 13.996 67.859 48.698 10437.001 7.667 216.607 2.116 0.93 329977. 0.4814
|
|
17.21 0.0777 0.1561 0.0855 0.0425 14.206 68.877 48.325 10593.640 7.782 214.949 2.069 0.93 330224. 0.4689
|
|
22.94 0.1035 0.2034 0.0847 0.0431 14.399 69.811 47.876 10737.257 7.887 212.951 2.022 0.93 330496. 0.4562
|
|
28.68 0.1294 0.2485 0.0837 0.0436 14.565 70.618 47.336 10861.449 7.978 210.549 1.977 0.93 330794. 0.4433
|
|
34.42 0.1553 0.2916 0.0826 0.0440 14.697 71.254 46.690 10959.229 8.050 207.677 1.932 0.93 331121. 0.4304
|
|
40.15 0.1812 0.3326 0.0812 0.0443 14.783 71.671 45.923 11023.442 8.097 204.268 1.890 0.93 331477. 0.4174
|
|
45.89 0.2071 0.3719 0.0796 0.0443 14.814 71.825 45.023 11047.082 8.115 200.262 1.849 0.93 331863. 0.4043
|
|
51.63 0.2330 0.4095 0.0778 0.0443 14.783 71.673 43.977 11023.716 8.098 195.611 1.809 0.93 332279. 0.3912
|
|
57.36 0.2589 0.4457 0.0757 0.0439 14.682 71.181 42.780 10948.074 8.042 190.286 1.772 0.93 332727. 0.3779
|
|
63.10 0.2848 0.4806 0.0733 0.0434 14.505 70.323 41.429 10816.052 7.945 184.276 1.737 0.93 333206. 0.3645
|
|
68.83 0.3106 0.5143 0.0706 0.0427 14.250 69.089 39.926 10626.181 7.806 177.592 1.704 0.93 333716. 0.3510
|
|
74.57 0.3365 0.5469 0.0677 0.0417 13.919 67.482 38.278 10379.158 7.624 170.262 1.673 0.93 334258. 0.3374
|
|
80.31 0.3624 0.5783 0.0645 0.0405 13.514 65.518 36.493 10077.043 7.402 162.322 1.643 0.93 334832. 0.3235
|
|
86.04 0.3883 0.6085 0.0612 0.0390 13.039 63.219 34.581 9723.352 7.142 153.815 1.613 0.94 335437. 0.3092
|
|
91.78 0.4142 0.6373 0.0576 0.0374 12.501 60.610 32.552 9322.201 6.848 144.789 1.584 0.94 336074. 0.2946
|
|
97.52 0.4401 0.6644 0.0538 0.0356 11.905 57.720 30.417 8877.684 6.521 135.293 1.554 0.94 336741. 0.2794
|
|
103.25 0.4660 0.6895 0.0499 0.0337 11.255 54.569 28.186 8393.049 6.165 125.373 1.523 0.94 337440. 0.2636
|
|
108.99 0.4918 0.7123 0.0458 0.0316 10.554 51.171 25.870 7870.446 5.781 115.069 1.491 0.94 338169. 0.2472
|
|
114.72 0.5177 0.7325 0.0415 0.0293 9.805 47.537 23.476 7311.378 5.371 104.422 1.456 0.94 338929. 0.2300
|
|
120.46 0.5436 0.7494 0.0372 0.0270 9.008 43.673 21.015 6717.207 4.934 93.474 1.419 0.94 339720. 0.2120
|
|
126.20 0.5695 0.7622 0.0327 0.0244 8.165 39.589 18.495 6088.950 4.473 82.265 1.378 0.94 340542. 0.1931
|
|
131.93 0.5954 0.7689 0.0282 0.0218 7.286 35.327 15.924 5433.442 3.991 70.832 1.329 0.94 341394. 0.1729
|
|
137.67 0.6213 0.7523 0.0235 0.0194 6.488 31.457 13.297 4838.312 3.554 59.144 1.247 0.95 342276. 0.1482
|
|
143.41 0.6472 0.7076 0.0188 0.0172 5.743 27.843 10.626 4282.375 3.146 47.266 1.125 0.95 343189. 0.1196
|
|
149.14 0.6731 0.6317 0.0140 0.0150 4.995 24.219 7.934 3724.996 2.736 35.292 0.966 0.95 344132. 0.0887
|
|
154.88 0.6989 0.5079 0.0093 0.0127 4.258 20.644 5.236 3175.099 2.332 23.291 0.748 0.95 345105. 0.0558
|
|
160.61 0.7248 0.3084 0.0045 0.0106 3.539 17.156 2.548 2638.716 1.938 11.335 0.438 0.95 346105. 0.0228
|
|
166.35 0.7507 -0.0343 -0.0004 0.0083 2.765 13.407 -0.214 2062.024 1.515 -0.950 -0.047 0.95 347060. 0.0000
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