686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13x8E (13x8E.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 0.1001 0.0452 0.001 0.083 0.090 0.987 0.009 0.399 41.220 0.05 16618. 0.5594
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0.32 0.0260 0.0563 0.0988 0.0457 0.001 0.084 0.089 0.998 0.010 0.394 40.247 0.05 16630. 0.5427
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0.64 0.0520 0.1099 0.0974 0.0462 0.001 0.085 0.087 1.009 0.010 0.388 39.266 0.05 16643. 0.5258
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0.96 0.0781 0.1607 0.0959 0.0466 0.001 0.086 0.086 1.019 0.010 0.382 38.279 0.05 16658. 0.5086
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1.28 0.1041 0.2087 0.0943 0.0470 0.001 0.087 0.085 1.028 0.010 0.376 37.292 0.05 16674. 0.4912
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1.60 0.1301 0.2540 0.0925 0.0474 0.001 0.088 0.083 1.036 0.010 0.369 36.306 0.05 16691. 0.4737
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1.91 0.1561 0.2965 0.0906 0.0477 0.001 0.088 0.081 1.042 0.010 0.361 35.324 0.05 16709. 0.4560
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2.23 0.1822 0.3364 0.0885 0.0479 0.001 0.089 0.079 1.047 0.010 0.353 34.347 0.05 16729. 0.4383
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2.55 0.2082 0.3736 0.0862 0.0480 0.001 0.089 0.077 1.050 0.010 0.344 33.377 0.05 16750. 0.4204
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2.87 0.2342 0.4081 0.0837 0.0481 0.001 0.089 0.075 1.050 0.010 0.334 32.414 0.05 16773. 0.4023
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3.19 0.2602 0.4401 0.0811 0.0479 0.001 0.089 0.073 1.048 0.010 0.323 31.457 0.05 16797. 0.3842
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3.51 0.2863 0.4694 0.0782 0.0477 0.001 0.088 0.070 1.042 0.010 0.312 30.504 0.05 16823. 0.3660
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3.83 0.3123 0.4962 0.0752 0.0473 0.001 0.087 0.067 1.034 0.010 0.300 29.554 0.05 16851. 0.3476
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4.15 0.3383 0.5202 0.0719 0.0468 0.001 0.086 0.064 1.022 0.010 0.287 28.601 0.05 16880. 0.3290
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4.47 0.3643 0.5414 0.0684 0.0461 0.001 0.085 0.061 1.006 0.010 0.273 27.641 0.05 16911. 0.3102
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4.79 0.3904 0.5596 0.0648 0.0452 0.001 0.083 0.058 0.987 0.009 0.258 26.667 0.05 16943. 0.2911
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5.11 0.4164 0.5746 0.0609 0.0441 0.001 0.081 0.055 0.964 0.009 0.243 25.671 0.05 16977. 0.2717
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5.43 0.4424 0.5861 0.0568 0.0429 0.001 0.079 0.051 0.937 0.009 0.227 24.642 0.05 17012. 0.2520
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5.74 0.4684 0.5935 0.0526 0.0415 0.001 0.077 0.047 0.907 0.009 0.210 23.570 0.05 17049. 0.2318
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6.06 0.4944 0.5964 0.0482 0.0399 0.001 0.074 0.043 0.872 0.008 0.192 22.439 0.05 17088. 0.2112
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6.38 0.5205 0.5941 0.0436 0.0382 0.001 0.071 0.039 0.835 0.008 0.174 21.233 0.05 17128. 0.1902
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6.70 0.5465 0.5856 0.0390 0.0364 0.001 0.067 0.035 0.795 0.008 0.155 19.932 0.05 17170. 0.1688
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7.02 0.5725 0.5697 0.0342 0.0344 0.001 0.064 0.031 0.751 0.007 0.136 18.510 0.05 17214. 0.1469
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7.34 0.5985 0.5450 0.0294 0.0323 0.001 0.060 0.026 0.706 0.007 0.117 16.936 0.05 17259. 0.1246
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7.66 0.6246 0.5092 0.0245 0.0301 0.001 0.056 0.022 0.657 0.006 0.098 15.167 0.05 17306. 0.1019
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7.98 0.6506 0.4597 0.0196 0.0278 0.001 0.051 0.018 0.607 0.006 0.078 13.144 0.05 17354. 0.0790
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8.30 0.6766 0.3924 0.0147 0.0254 0.001 0.047 0.013 0.554 0.005 0.059 10.788 0.05 17404. 0.0561
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8.62 0.7026 0.3016 0.0098 0.0229 0.001 0.042 0.009 0.500 0.005 0.039 7.985 0.05 17456. 0.0340
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8.94 0.7287 0.1788 0.0050 0.0203 0.001 0.038 0.004 0.445 0.004 0.020 4.565 0.05 17509. 0.0138
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9.25 0.7547 0.0106 0.0002 0.0178 0.001 0.033 0.000 0.388 0.004 0.001 0.261 0.05 17563. 0.0002
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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 0.1004 0.0411 0.010 0.304 0.360 7.187 0.034 1.601 22.722 0.10 33236. 0.6178
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0.66 0.0268 0.0636 0.0991 0.0417 0.010 0.308 0.355 7.288 0.035 1.581 22.120 0.10 33261. 0.5975
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1.31 0.0535 0.1238 0.0977 0.0422 0.010 0.312 0.350 7.385 0.035 1.558 21.516 0.10 33288. 0.5771
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1.97 0.0803 0.1805 0.0962 0.0428 0.010 0.316 0.345 7.478 0.036 1.534 20.914 0.10 33318. 0.5565
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2.62 0.1070 0.2338 0.0945 0.0433 0.010 0.320 0.339 7.564 0.036 1.507 20.316 0.10 33351. 0.5358
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3.28 0.1338 0.2837 0.0927 0.0437 0.010 0.323 0.332 7.639 0.036 1.478 19.723 0.10 33386. 0.5151
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3.94 0.1605 0.3303 0.0907 0.0441 0.010 0.326 0.325 7.702 0.037 1.446 19.138 0.10 33424. 0.4943
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4.59 0.1873 0.3737 0.0885 0.0443 0.010 0.328 0.317 7.750 0.037 1.411 18.561 0.10 33466. 0.4736
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5.25 0.2140 0.4141 0.0861 0.0445 0.010 0.329 0.309 7.780 0.037 1.373 17.993 0.10 33510. 0.4529
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5.91 0.2408 0.4514 0.0835 0.0446 0.010 0.329 0.299 7.789 0.037 1.332 17.435 0.10 33558. 0.4323
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6.56 0.2675 0.4858 0.0807 0.0445 0.010 0.329 0.289 7.775 0.037 1.287 16.886 0.10 33609. 0.4116
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7.22 0.2943 0.5172 0.0778 0.0442 0.010 0.327 0.279 7.734 0.037 1.240 16.346 0.10 33663. 0.3910
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7.87 0.3211 0.5459 0.0745 0.0438 0.010 0.324 0.267 7.665 0.037 1.189 15.813 0.10 33721. 0.3704
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8.53 0.3478 0.5716 0.0711 0.0433 0.010 0.320 0.255 7.565 0.036 1.134 15.285 0.10 33782. 0.3497
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9.19 0.3746 0.5944 0.0675 0.0425 0.010 0.314 0.242 7.433 0.035 1.076 14.759 0.10 33846. 0.3289
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9.84 0.4013 0.6141 0.0636 0.0416 0.010 0.307 0.228 7.268 0.035 1.014 14.231 0.10 33914. 0.3079
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10.50 0.4281 0.6305 0.0596 0.0404 0.009 0.299 0.213 7.069 0.034 0.950 13.698 0.10 33985. 0.2868
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11.16 0.4548 0.6432 0.0553 0.0391 0.009 0.289 0.198 6.834 0.033 0.881 13.152 0.10 34059. 0.2653
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11.81 0.4816 0.6518 0.0508 0.0376 0.009 0.277 0.182 6.566 0.031 0.811 12.588 0.10 34137. 0.2435
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12.47 0.5083 0.6558 0.0462 0.0358 0.008 0.265 0.166 6.266 0.030 0.737 11.998 0.10 34219. 0.2213
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13.12 0.5351 0.6542 0.0415 0.0340 0.008 0.251 0.149 5.937 0.028 0.662 11.370 0.10 34303. 0.1988
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13.78 0.5619 0.6459 0.0367 0.0319 0.007 0.236 0.132 5.580 0.027 0.585 10.692 0.10 34391. 0.1757
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14.44 0.5886 0.6295 0.0318 0.0297 0.007 0.220 0.114 5.197 0.025 0.507 9.946 0.10 34483. 0.1521
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15.09 0.6154 0.6027 0.0268 0.0274 0.006 0.202 0.096 4.790 0.023 0.428 9.109 0.10 34578. 0.1280
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15.75 0.6421 0.5623 0.0218 0.0249 0.006 0.184 0.078 4.360 0.021 0.348 8.145 0.10 34676. 0.1033
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16.40 0.6689 0.5036 0.0168 0.0224 0.005 0.165 0.060 3.909 0.019 0.268 7.003 0.11 34778. 0.0780
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17.06 0.6956 0.4190 0.0119 0.0197 0.005 0.145 0.043 3.441 0.016 0.189 5.602 0.11 34883. 0.0523
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17.72 0.7224 0.2958 0.0069 0.0169 0.004 0.125 0.025 2.959 0.014 0.110 3.808 0.11 34991. 0.0272
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18.37 0.7491 0.1113 0.0021 0.0141 0.003 0.104 0.008 2.465 0.012 0.033 1.382 0.11 35103. 0.0054
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19.03 0.7759
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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 0.1007 0.0394 0.031 0.654 0.812 23.222 0.074 3.612 15.862 0.15 49853. 0.6477
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0.97 0.0263 0.0655 0.0994 0.0400 0.032 0.664 0.802 23.572 0.075 3.567 15.431 0.15 49890. 0.6262
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1.94 0.0526 0.1273 0.0981 0.0405 0.032 0.674 0.791 23.913 0.076 3.518 15.000 0.15 49930. 0.6045
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2.90 0.0789 0.1855 0.0966 0.0411 0.033 0.683 0.779 24.238 0.077 3.464 14.572 0.15 49974. 0.5827
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3.87 0.1052 0.2401 0.0949 0.0416 0.033 0.691 0.765 24.540 0.078 3.405 14.148 0.15 50022. 0.5609
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4.84 0.1315 0.2913 0.0931 0.0421 0.033 0.699 0.751 24.811 0.079 3.340 13.729 0.15 50074. 0.5391
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5.81 0.1579 0.3390 0.0912 0.0424 0.034 0.706 0.735 25.042 0.080 3.270 13.317 0.15 50130. 0.5174
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6.78 0.1842 0.3835 0.0890 0.0428 0.034 0.711 0.718 25.225 0.080 3.194 12.912 0.15 50191. 0.4958
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7.74 0.2105 0.4248 0.0867 0.0430 0.034 0.714 0.699 25.351 0.081 3.111 12.515 0.15 50256. 0.4743
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8.71 0.2368 0.4631 0.0842 0.0431 0.034 0.716 0.679 25.409 0.081 3.022 12.127 0.15 50326. 0.4529
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9.68 0.2631 0.4984 0.0815 0.0430 0.034 0.715 0.658 25.390 0.081 2.925 11.746 0.15 50400. 0.4316
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10.65 0.2894 0.5309 0.0786 0.0429 0.034 0.712 0.634 25.287 0.080 2.821 11.374 0.15 50479. 0.4104
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11.61 0.3157 0.5606 0.0755 0.0425 0.034 0.707 0.609 25.090 0.080 2.709 11.009 0.15 50563. 0.3893
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12.58 0.3420 0.5875 0.0722 0.0420 0.033 0.699 0.582 24.793 0.079 2.589 10.650 0.16 50652. 0.3682
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13.55 0.3683 0.6116 0.0686 0.0413 0.033 0.687 0.554 24.391 0.078 2.463 10.295 0.16 50746. 0.3471
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14.52 0.3946 0.6328 0.0649 0.0405 0.032 0.673 0.523 23.877 0.076 2.328 9.943 0.16 50844. 0.3259
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15.49 0.4210 0.6511 0.0609 0.0394 0.031 0.655 0.492 23.249 0.074 2.186 9.590 0.16 50948. 0.3047
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16.45 0.4473 0.6660 0.0568 0.0381 0.030 0.634 0.458 22.503 0.072 2.038 9.233 0.16 51057. 0.2832
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17.42 0.4736 0.6774 0.0525 0.0367 0.029 0.610 0.423 21.641 0.069 1.882 8.869 0.16 51170. 0.2614
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18.39 0.4999 0.6847 0.0480 0.0350 0.028 0.582 0.387 20.670 0.066 1.722 8.493 0.16 51289. 0.2394
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19.36 0.5262 0.6873 0.0434 0.0332 0.026 0.552 0.350 19.597 0.062 1.556 8.099 0.16 51412. 0.2171
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20.33 0.5525 0.6842 0.0387 0.0312 0.025 0.519 0.312 18.426 0.059 1.387 7.678 0.16 51540. 0.1943
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21.29 0.5788 0.6742 0.0339 0.0291 0.023 0.484 0.273 17.163 0.055 1.216 7.222 0.16 51674. 0.1711
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22.26 0.6051 0.6554 0.0290 0.0268 0.021 0.446 0.234 15.813 0.050 1.041 6.716 0.16 51812. 0.1472
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23.23 0.6314 0.6252 0.0241 0.0244 0.019 0.405 0.195 14.382 0.046 0.866 6.140 0.16 51955. 0.1227
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24.20 0.6577 0.5795 0.0192 0.0218 0.017 0.363 0.155 12.877 0.041 0.690 5.463 0.16 52103. 0.0975
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25.17 0.6841 0.5116 0.0143 0.0192 0.015 0.319 0.116 11.306 0.036 0.514 4.638 0.16 52256. 0.0714
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26.13 0.7104 0.4104 0.0095 0.0164 0.013 0.273 0.076 9.679 0.031 0.340 3.582 0.16 52413. 0.0449
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27.10 0.7367 0.2550 0.0047 0.0136 0.011 0.226 0.038 8.008 0.025 0.169 2.146 0.16 52576. 0.0189
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28.07 0.7630 0.0017 0.0000 0.0107 0.008 0.178 0.000 6.304 0.020 0.001 0.014 0.16 52743. 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 0.1010 0.0384 0.072 1.134 1.448 53.667 0.128 6.439 12.234 0.21 66470. 0.6669
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1.29 0.0264 0.0674 0.0997 0.0390 0.073 1.152 1.430 54.521 0.130 6.359 11.893 0.21 66519. 0.6443
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2.59 0.0527 0.1309 0.0983 0.0396 0.074 1.170 1.410 55.355 0.132 6.271 11.552 0.21 66573. 0.6215
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3.88 0.0791 0.1906 0.0968 0.0402 0.075 1.187 1.388 56.151 0.134 6.175 11.214 0.21 66632. 0.5987
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5.17 0.1054 0.2466 0.0952 0.0407 0.076 1.202 1.365 56.893 0.136 6.070 10.880 0.21 66696. 0.5759
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6.46 0.1318 0.2990 0.0934 0.0412 0.077 1.216 1.339 57.561 0.137 5.956 10.551 0.21 66765. 0.5532
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7.76 0.1581 0.3478 0.0914 0.0416 0.078 1.228 1.311 58.136 0.139 5.831 10.228 0.21 66840. 0.5307
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9.05 0.1845 0.3932 0.0893 0.0419 0.079 1.238 1.280 58.595 0.140 5.696 9.912 0.21 66921. 0.5082
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10.34 0.2108 0.4353 0.0870 0.0421 0.079 1.245 1.247 58.917 0.141 5.548 9.603 0.21 67008. 0.4859
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11.63 0.2372 0.4743 0.0845 0.0422 0.079 1.248 1.211 59.077 0.141 5.388 9.301 0.21 67101. 0.4638
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12.93 0.2635 0.5103 0.0818 0.0422 0.079 1.248 1.173 59.054 0.141 5.216 9.006 0.21 67201. 0.4419
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14.22 0.2899 0.5435 0.0789 0.0421 0.079 1.243 1.131 58.827 0.140 5.030 8.719 0.21 67307. 0.4201
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15.51 0.3162 0.5738 0.0757 0.0417 0.078 1.233 1.086 58.375 0.139 4.830 8.438 0.21 67419. 0.3984
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16.80 0.3426 0.6013 0.0724 0.0412 0.077 1.219 1.038 57.681 0.138 4.617 8.163 0.21 67538. 0.3768
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18.10 0.3689 0.6261 0.0688 0.0406 0.076 1.199 0.987 56.731 0.135 4.391 7.892 0.21 67663. 0.3553
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19.39 0.3953 0.6481 0.0651 0.0397 0.074 1.173 0.933 55.513 0.133 4.151 7.624 0.21 67795. 0.3337
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20.68 0.4216 0.6671 0.0611 0.0386 0.072 1.141 0.876 54.018 0.129 3.898 7.357 0.21 67934. 0.3121
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21.97 0.4480 0.6829 0.0569 0.0374 0.070 1.104 0.816 52.237 0.125 3.632 7.089 0.21 68079. 0.2903
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23.27 0.4743 0.6954 0.0526 0.0359 0.067 1.060 0.754 50.174 0.120 3.354 6.817 0.21 68231. 0.2682
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24.56 0.5007 0.7039 0.0481 0.0342 0.064 1.011 0.690 47.844 0.114 3.067 6.537 0.21 68390. 0.2460
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25.85 0.5270 0.7079 0.0435 0.0324 0.061 0.956 0.623 45.263 0.108 2.772 6.246 0.21 68555. 0.2234
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27.14 0.5534 0.7064 0.0387 0.0303 0.057 0.897 0.556 42.444 0.101 2.471 5.936 0.21 68726. 0.2005
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28.44 0.5797 0.6983 0.0339 0.0282 0.053 0.833 0.487 39.398 0.094 2.164 5.602 0.21 68904. 0.1771
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29.73 0.6061 0.6818 0.0291 0.0258 0.048 0.764 0.417 36.139 0.086 1.854 5.231 0.21 69089. 0.1530
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31.02 0.6324 0.6540 0.0242 0.0234 0.044 0.691 0.346 32.680 0.078 1.541 4.809 0.21 69280. 0.1282
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32.31 0.6588 0.6106 0.0192 0.0208 0.039 0.614 0.276 29.039 0.069 1.227 4.310 0.21 69478. 0.1026
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33.61 0.6851 0.5446 0.0143 0.0180 0.034 0.533 0.206 25.236 0.060 0.915 3.696 0.21 69683. 0.0760
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34.90 0.7115 0.4432 0.0095 0.0152 0.029 0.450 0.136 21.295 0.051 0.605 2.896 0.21 69894. 0.0484
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36.19 0.7378 0.2814 0.0047 0.0123 0.023 0.364 0.067 17.245 0.041 0.300 1.774 0.21 70111. 0.0209
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37.49 0.7642 0.0026 0.0000 0.0094 0.018 0.277 0.000 13.114 0.031 0.002 0.016 0.21 70334. 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 0.1013 0.0378 0.138 1.744 2.268 103.156 0.197 10.090 9.974 0.26 83086. 0.6807
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1.62 0.0264 0.0687 0.1000 0.0384 0.141 1.773 2.240 104.860 0.200 9.965 9.691 0.26 83147. 0.6573
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3.24 0.0528 0.1335 0.0986 0.0390 0.143 1.801 2.210 106.525 0.203 9.829 9.409 0.26 83215. 0.6337
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4.85 0.0792 0.1942 0.0971 0.0396 0.145 1.828 2.176 108.119 0.206 9.680 9.129 0.26 83288. 0.6102
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6.47 0.1055 0.2511 0.0955 0.0401 0.147 1.853 2.139 109.607 0.209 9.516 8.853 0.26 83369. 0.5868
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8.09 0.1319 0.3043 0.0937 0.0406 0.149 1.876 2.099 110.952 0.212 9.337 8.582 0.26 83456. 0.5634
|
|
9.71 0.1583 0.3538 0.0917 0.0410 0.150 1.895 2.055 112.112 0.214 9.143 8.316 0.26 83550. 0.5402
|
|
11.32 0.1847 0.3999 0.0896 0.0414 0.152 1.911 2.008 113.046 0.216 8.930 8.055 0.26 83651. 0.5172
|
|
12.94 0.2111 0.4426 0.0873 0.0416 0.152 1.922 1.956 113.707 0.217 8.699 7.801 0.26 83760. 0.4944
|
|
14.56 0.2375 0.4822 0.0848 0.0418 0.153 1.928 1.900 114.051 0.218 8.449 7.554 0.26 83877. 0.4718
|
|
16.18 0.2638 0.5187 0.0821 0.0417 0.153 1.928 1.839 114.033 0.218 8.178 7.313 0.26 84002. 0.4493
|
|
17.79 0.2902 0.5522 0.0791 0.0416 0.152 1.921 1.773 113.610 0.217 7.887 7.079 0.26 84134. 0.4271
|
|
19.41 0.3166 0.5830 0.0760 0.0413 0.151 1.906 1.703 112.743 0.215 7.574 6.851 0.26 84275. 0.4051
|
|
21.03 0.3430 0.6110 0.0727 0.0408 0.149 1.883 1.628 111.396 0.213 7.240 6.627 0.26 84424. 0.3831
|
|
22.65 0.3694 0.6363 0.0691 0.0401 0.147 1.852 1.548 109.541 0.209 6.884 6.409 0.26 84581. 0.3613
|
|
24.27 0.3958 0.6588 0.0653 0.0392 0.144 1.811 1.463 107.154 0.205 6.507 6.193 0.26 84747. 0.3394
|
|
25.88 0.4221 0.6784 0.0613 0.0382 0.140 1.762 1.374 104.215 0.199 6.110 5.979 0.26 84921. 0.3175
|
|
27.50 0.4485 0.6949 0.0571 0.0369 0.135 1.702 1.280 100.707 0.192 5.693 5.764 0.26 85103. 0.2955
|
|
29.12 0.4749 0.7082 0.0528 0.0354 0.130 1.634 1.182 96.637 0.185 5.257 5.547 0.26 85293. 0.2733
|
|
30.74 0.5013 0.7176 0.0482 0.0337 0.123 1.556 1.081 92.035 0.176 4.807 5.326 0.26 85491. 0.2508
|
|
32.35 0.5277 0.7227 0.0436 0.0318 0.117 1.470 0.977 86.930 0.166 4.344 5.095 0.26 85698. 0.2281
|
|
33.97 0.5541 0.7226 0.0388 0.0298 0.109 1.375 0.870 81.348 0.155 3.870 4.852 0.26 85913. 0.2051
|
|
35.59 0.5804 0.7160 0.0340 0.0276 0.101 1.273 0.762 75.312 0.144 3.389 4.589 0.26 86136. 0.1815
|
|
37.21 0.6068 0.7012 0.0291 0.0252 0.092 1.164 0.652 68.847 0.131 2.902 4.299 0.26 86368. 0.1573
|
|
38.82 0.6332 0.6753 0.0242 0.0227 0.083 1.048 0.542 61.982 0.118 2.412 3.968 0.26 86608. 0.1324
|
|
40.44 0.6596 0.6340 0.0193 0.0200 0.073 0.926 0.432 54.751 0.105 1.920 3.576 0.26 86856. 0.1065
|
|
42.06 0.6860 0.5697 0.0143 0.0173 0.063 0.798 0.321 47.194 0.090 1.430 3.090 0.26 87112. 0.0794
|
|
43.68 0.7124 0.4685 0.0095 0.0144 0.053 0.665 0.212 39.361 0.075 0.945 2.447 0.26 87376. 0.0511
|
|
45.30 0.7387 0.3021 0.0047 0.0115 0.042 0.529 0.105 31.311 0.060 0.467 1.521 0.26 87649. 0.0223
|
|
46.91 0.7651 0.0007 0.0000 0.0085 0.031 0.390 0.000 23.097 0.044 0.001 0.004 0.26 87927. 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 0.1016 0.0374 0.237 2.486 3.278 176.450 0.281 14.579 8.425 0.31 99700. 0.6911
|
|
1.94 0.0264 0.0697 0.1004 0.0380 0.241 2.528 3.237 179.450 0.286 14.400 8.183 0.31 99774. 0.6671
|
|
3.89 0.0528 0.1353 0.0990 0.0386 0.245 2.569 3.193 182.383 0.290 14.204 7.942 0.31 99855. 0.6431
|
|
5.83 0.0792 0.1968 0.0975 0.0392 0.248 2.609 3.145 185.193 0.295 13.990 7.703 0.31 99944. 0.6190
|
|
7.77 0.1056 0.2544 0.0959 0.0398 0.252 2.646 3.092 187.821 0.299 13.755 7.468 0.31 100040. 0.5950
|
|
9.71 0.1320 0.3082 0.0941 0.0403 0.255 2.679 3.035 190.200 0.303 13.498 7.237 0.31 100145. 0.5712
|
|
11.66 0.1584 0.3583 0.0921 0.0407 0.258 2.708 2.972 192.259 0.306 13.217 7.010 0.31 100258. 0.5476
|
|
13.60 0.1848 0.4048 0.0900 0.0411 0.260 2.732 2.903 193.923 0.309 12.911 6.789 0.31 100380. 0.5241
|
|
15.54 0.2112 0.4479 0.0877 0.0413 0.262 2.749 2.828 195.113 0.311 12.579 6.574 0.31 100511. 0.5009
|
|
17.49 0.2376 0.4879 0.0851 0.0415 0.263 2.758 2.747 195.749 0.312 12.218 6.365 0.31 100652. 0.4779
|
|
19.43 0.2640 0.5247 0.0824 0.0415 0.263 2.758 2.659 195.752 0.312 11.827 6.161 0.31 100802. 0.4552
|
|
21.37 0.2905 0.5587 0.0795 0.0413 0.262 2.748 2.564 195.047 0.310 11.406 5.963 0.31 100961. 0.4327
|
|
23.31 0.3169 0.5898 0.0763 0.0410 0.260 2.727 2.463 193.564 0.308 10.954 5.771 0.31 101131. 0.4103
|
|
25.26 0.3433 0.6182 0.0730 0.0405 0.256 2.694 2.354 191.241 0.304 10.471 5.583 0.31 101310. 0.3881
|
|
27.20 0.3697 0.6438 0.0694 0.0398 0.252 2.649 2.238 188.028 0.299 9.956 5.400 0.31 101499. 0.3660
|
|
29.14 0.3961 0.6668 0.0656 0.0390 0.247 2.590 2.116 183.880 0.293 9.411 5.219 0.31 101698. 0.3440
|
|
31.08 0.4225 0.6869 0.0616 0.0379 0.240 2.518 1.987 178.766 0.285 8.836 5.040 0.31 101907. 0.3219
|
|
33.03 0.4489 0.7040 0.0574 0.0366 0.232 2.432 1.851 172.651 0.275 8.232 4.862 0.31 102125. 0.2997
|
|
34.97 0.4753 0.7179 0.0530 0.0351 0.222 2.332 1.709 165.548 0.263 7.602 4.682 0.31 102354. 0.2774
|
|
36.91 0.5017 0.7281 0.0484 0.0334 0.211 2.219 1.562 157.510 0.251 6.950 4.499 0.31 102593. 0.2548
|
|
38.86 0.5281 0.7341 0.0438 0.0315 0.199 2.093 1.412 148.585 0.236 6.279 4.310 0.31 102841. 0.2320
|
|
40.80 0.5545 0.7351 0.0390 0.0294 0.186 1.956 1.258 138.817 0.221 5.595 4.110 0.31 103100. 0.2088
|
|
42.74 0.5809 0.7298 0.0341 0.0272 0.172 1.807 1.101 128.248 0.204 4.898 3.895 0.31 103368. 0.1852
|
|
44.68 0.6073 0.7165 0.0292 0.0248 0.157 1.647 0.943 116.921 0.186 4.194 3.658 0.31 103646. 0.1609
|
|
46.63 0.6337 0.6924 0.0243 0.0222 0.141 1.478 0.783 104.887 0.167 3.484 3.387 0.31 103935. 0.1358
|
|
48.57 0.6601 0.6529 0.0193 0.0195 0.124 1.299 0.623 92.207 0.147 2.773 3.066 0.31 104233. 0.1097
|
|
50.51 0.6865 0.5903 0.0144 0.0167 0.106 1.112 0.464 78.951 0.126 2.064 2.666 0.32 104541. 0.0823
|
|
52.46 0.7129 0.4899 0.0095 0.0138 0.087 0.919 0.306 65.208 0.104 1.362 2.130 0.32 104858. 0.0534
|
|
54.40 0.7393 0.3201 0.0047 0.0108 0.069 0.720 0.151 51.082 0.081 0.672 1.342 0.32 105186. 0.0236
|
|
56.34 0.7657 -0.0010 0.0000 0.0078 0.049 0.517 0.000 36.668 0.058 -0.002 -0.004 0.32 105520. 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 0.1020 0.0372 0.373 3.363 4.479 278.508 0.380 19.921 7.294 0.36 116314. 0.6994
|
|
2.27 0.0264 0.0704 0.1008 0.0378 0.380 3.421 4.424 283.350 0.387 19.679 7.082 0.36 116400. 0.6750
|
|
4.54 0.0528 0.1366 0.0994 0.0384 0.386 3.479 4.365 288.089 0.393 19.414 6.872 0.36 116495. 0.6505
|
|
6.80 0.0793 0.1987 0.0979 0.0390 0.392 3.533 4.299 292.634 0.399 19.123 6.664 0.36 116598. 0.6261
|
|
9.07 0.1057 0.2568 0.0963 0.0396 0.398 3.585 4.228 296.888 0.405 18.804 6.459 0.36 116711. 0.6017
|
|
11.34 0.1321 0.3110 0.0945 0.0401 0.403 3.631 4.149 300.746 0.410 18.455 6.257 0.36 116833. 0.5775
|
|
13.61 0.1585 0.3615 0.0925 0.0406 0.408 3.672 4.063 304.092 0.415 18.073 6.061 0.36 116965. 0.5536
|
|
15.87 0.1849 0.4084 0.0904 0.0409 0.411 3.705 3.970 306.806 0.419 17.657 5.869 0.36 117108. 0.5298
|
|
18.14 0.2113 0.4519 0.0881 0.0412 0.414 3.728 3.868 308.759 0.421 17.203 5.682 0.36 117261. 0.5063
|
|
20.41 0.2378 0.4921 0.0856 0.0413 0.415 3.741 3.757 309.823 0.423 16.711 5.500 0.36 117425. 0.4831
|
|
22.68 0.2642 0.5293 0.0828 0.0413 0.416 3.742 3.637 309.872 0.423 16.178 5.324 0.36 117601. 0.4601
|
|
24.95 0.2906 0.5635 0.0799 0.0412 0.414 3.728 3.508 308.782 0.421 15.604 5.153 0.36 117787. 0.4373
|
|
27.21 0.3170 0.5949 0.0767 0.0409 0.411 3.700 3.369 306.441 0.418 14.986 4.987 0.36 117985. 0.4148
|
|
29.48 0.3434 0.6236 0.0733 0.0404 0.406 3.656 3.221 302.749 0.413 14.326 4.825 0.36 118194. 0.3924
|
|
31.75 0.3699 0.6496 0.0697 0.0397 0.399 3.594 3.063 297.622 0.406 13.622 4.667 0.36 118415. 0.3701
|
|
34.02 0.3963 0.6729 0.0659 0.0388 0.390 3.514 2.895 290.992 0.397 12.877 4.512 0.36 118648. 0.3479
|
|
36.28 0.4227 0.6935 0.0619 0.0377 0.379 3.415 2.718 282.804 0.386 12.090 4.359 0.36 118892. 0.3257
|
|
38.55 0.4491 0.7111 0.0577 0.0364 0.366 3.296 2.532 273.003 0.372 11.264 4.207 0.36 119148. 0.3034
|
|
40.82 0.4755 0.7255 0.0533 0.0349 0.351 3.159 2.338 261.608 0.357 10.401 4.054 0.36 119415. 0.2809
|
|
43.09 0.5019 0.7364 0.0487 0.0332 0.334 3.003 2.138 248.703 0.339 9.508 3.899 0.36 119694. 0.2583
|
|
45.36 0.5284 0.7432 0.0440 0.0313 0.314 2.830 1.931 234.364 0.320 8.591 3.738 0.36 119984. 0.2354
|
|
47.62 0.5548 0.7452 0.0392 0.0292 0.293 2.640 1.721 218.662 0.298 7.653 3.569 0.37 120286. 0.2121
|
|
49.89 0.5812 0.7410 0.0343 0.0269 0.270 2.435 1.506 201.662 0.275 6.700 3.388 0.37 120600. 0.1884
|
|
52.16 0.6076 0.7291 0.0294 0.0245 0.246 2.215 1.289 183.436 0.250 5.736 3.188 0.37 120925. 0.1641
|
|
54.43 0.6340 0.7065 0.0244 0.0219 0.220 1.981 1.071 164.065 0.224 4.764 2.961 0.37 121261. 0.1389
|
|
56.69 0.6605 0.6688 0.0194 0.0192 0.193 1.734 0.852 143.646 0.196 3.791 2.691 0.37 121609. 0.1126
|
|
58.96 0.6869 0.6079 0.0144 0.0163 0.164 1.477 0.634 122.296 0.167 2.821 2.352 0.37 121969. 0.0849
|
|
61.23 0.7133 0.5084 0.0095 0.0134 0.134 1.209 0.418 100.159 0.137 1.860 1.894 0.37 122340. 0.0555
|
|
63.50 0.7397 0.3361 0.0047 0.0103 0.104 0.935 0.206 77.404 0.106 0.917 1.207 0.37 122722. 0.0248
|
|
65.77 0.7661 -0.0028 0.0000 0.0072 0.073 0.654 -0.001 54.181 0.074 -0.005 -0.010 0.37 123112. 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 0.1024 0.0371 0.556 4.380 5.876 414.547 0.495 26.135 6.429 0.41 132925. 0.7061
|
|
2.59 0.0264 0.0709 0.1012 0.0377 0.566 4.457 5.805 421.892 0.504 25.822 6.241 0.41 133024. 0.6814
|
|
5.18 0.0529 0.1376 0.0999 0.0384 0.575 4.533 5.728 429.085 0.512 25.478 6.055 0.41 133132. 0.6566
|
|
7.78 0.0793 0.2002 0.0984 0.0390 0.585 4.606 5.643 435.988 0.520 25.099 5.870 0.41 133251. 0.6319
|
|
10.37 0.1057 0.2586 0.0968 0.0395 0.593 4.675 5.550 442.456 0.528 24.684 5.689 0.41 133380. 0.6073
|
|
12.96 0.1321 0.3132 0.0950 0.0401 0.601 4.737 5.447 448.329 0.535 24.230 5.511 0.41 133520. 0.5828
|
|
15.55 0.1586 0.3639 0.0930 0.0405 0.608 4.791 5.335 453.433 0.541 23.732 5.337 0.41 133671. 0.5586
|
|
18.15 0.1850 0.4111 0.0909 0.0409 0.614 4.835 5.213 457.583 0.546 23.188 5.167 0.41 133834. 0.5346
|
|
20.74 0.2114 0.4548 0.0886 0.0412 0.618 4.866 5.080 460.586 0.550 22.596 5.003 0.41 134010. 0.5109
|
|
23.33 0.2378 0.4953 0.0860 0.0413 0.620 4.884 4.935 462.248 0.552 21.952 4.843 0.41 134198. 0.4875
|
|
25.92 0.2643 0.5327 0.0833 0.0413 0.620 4.885 4.778 462.375 0.552 21.254 4.687 0.41 134398. 0.4643
|
|
28.52 0.2907 0.5672 0.0804 0.0412 0.618 4.868 4.609 460.782 0.550 20.502 4.537 0.41 134612. 0.4414
|
|
31.11 0.3171 0.5989 0.0772 0.0409 0.613 4.831 4.427 457.297 0.546 19.692 4.391 0.41 134838. 0.4187
|
|
33.70 0.3435 0.6278 0.0738 0.0404 0.606 4.773 4.232 451.768 0.539 18.826 4.249 0.41 135078. 0.3961
|
|
36.29 0.3700 0.6541 0.0702 0.0397 0.596 4.692 4.025 444.068 0.530 17.903 4.111 0.41 135331. 0.3737
|
|
38.89 0.3964 0.6778 0.0663 0.0388 0.582 4.586 3.805 434.094 0.518 16.925 3.976 0.41 135597. 0.3514
|
|
41.48 0.4228 0.6987 0.0623 0.0377 0.566 4.456 3.573 421.759 0.503 15.892 3.842 0.41 135876. 0.3291
|
|
44.07 0.4492 0.7167 0.0580 0.0364 0.546 4.300 3.329 406.982 0.486 14.806 3.710 0.42 136169. 0.3067
|
|
46.66 0.4757 0.7317 0.0536 0.0348 0.523 4.118 3.074 389.790 0.465 13.672 3.577 0.42 136475. 0.2841
|
|
49.26 0.5021 0.7432 0.0490 0.0331 0.497 3.912 2.810 370.305 0.442 12.499 3.442 0.42 136794. 0.2614
|
|
51.85 0.5285 0.7507 0.0443 0.0312 0.468 3.684 2.539 348.645 0.416 11.293 3.303 0.42 137126. 0.2385
|
|
54.44 0.5549 0.7535 0.0394 0.0290 0.436 3.433 2.262 324.912 0.388 10.060 3.157 0.42 137471. 0.2152
|
|
57.03 0.5814 0.7505 0.0345 0.0267 0.401 3.161 1.980 299.208 0.357 8.807 3.001 0.42 137830. 0.1914
|
|
59.62 0.6078 0.7397 0.0296 0.0243 0.364 2.870 1.695 271.640 0.324 7.539 2.830 0.42 138201. 0.1669
|
|
62.22 0.6342 0.7186 0.0245 0.0217 0.325 2.560 1.408 242.332 0.289 6.261 2.635 0.42 138586. 0.1416
|
|
64.81 0.6606 0.6826 0.0195 0.0189 0.284 2.234 1.120 211.431 0.252 4.981 2.402 0.42 138984. 0.1152
|
|
67.40 0.6871 0.6234 0.0145 0.0160 0.240 1.892 0.833 179.117 0.214 3.706 2.110 0.42 139396. 0.0873
|
|
69.99 0.7135 0.5251 0.0096 0.0130 0.195 1.538 0.549 145.606 0.174 2.443 1.711 0.42 139820. 0.0575
|
|
72.59 0.7399 0.3511 0.0047 0.0099 0.149 1.174 0.270 111.158 0.133 1.203 1.103 0.42 140257. 0.0260
|
|
75.18 0.7663 -0.0039 0.0000 0.0068 0.102 0.803 -0.002 75.998 0.091 -0.009 -0.012 0.42 140702. 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 0.1030 0.0370 0.791 5.542 7.474 590.127 0.626 33.245 5.745 0.46 149534. 0.7116
|
|
2.92 0.0264 0.0713 0.1017 0.0377 0.806 5.642 7.386 600.754 0.637 32.852 5.576 0.46 149646. 0.6867
|
|
5.83 0.0529 0.1383 0.1004 0.0384 0.820 5.740 7.289 611.170 0.648 32.420 5.409 0.46 149768. 0.6617
|
|
8.75 0.0793 0.2012 0.0989 0.0390 0.833 5.834 7.182 621.173 0.659 31.944 5.244 0.46 149901. 0.6368
|
|
11.67 0.1057 0.2599 0.0973 0.0396 0.846 5.922 7.064 630.555 0.669 31.421 5.081 0.46 150047. 0.6120
|
|
14.58 0.1321 0.3147 0.0955 0.0401 0.857 6.002 6.935 639.082 0.678 30.848 4.922 0.46 150204. 0.5873
|
|
17.50 0.1586 0.3657 0.0936 0.0406 0.867 6.072 6.794 646.504 0.686 30.219 4.766 0.46 150375. 0.5629
|
|
20.42 0.1850 0.4130 0.0915 0.0410 0.875 6.128 6.639 652.553 0.692 29.532 4.615 0.46 150559. 0.5388
|
|
23.33 0.2114 0.4570 0.0891 0.0412 0.881 6.170 6.471 656.951 0.697 28.782 4.467 0.46 150756. 0.5149
|
|
26.25 0.2378 0.4977 0.0866 0.0414 0.884 6.193 6.287 659.416 0.700 27.966 4.325 0.46 150968. 0.4913
|
|
29.17 0.2643 0.5353 0.0839 0.0414 0.885 6.195 6.088 659.667 0.700 27.081 4.186 0.46 151194. 0.4680
|
|
32.08 0.2907 0.5700 0.0809 0.0413 0.882 6.174 5.874 657.435 0.698 26.126 4.052 0.46 151435. 0.4450
|
|
35.00 0.3171 0.6018 0.0777 0.0410 0.875 6.128 5.643 652.472 0.692 25.098 3.922 0.46 151690. 0.4222
|
|
37.92 0.3436 0.6310 0.0743 0.0405 0.864 6.053 5.395 644.559 0.684 23.997 3.796 0.47 151960. 0.3995
|
|
40.83 0.3700 0.6576 0.0707 0.0398 0.850 5.950 5.131 633.511 0.672 22.823 3.674 0.47 152245. 0.3771
|
|
43.75 0.3964 0.6816 0.0668 0.0389 0.830 5.815 4.851 619.175 0.657 21.577 3.554 0.47 152544. 0.3546
|
|
46.67 0.4228 0.7028 0.0628 0.0378 0.807 5.648 4.555 601.432 0.638 20.262 3.435 0.47 152859. 0.3322
|
|
49.58 0.4493 0.7213 0.0585 0.0364 0.778 5.449 4.244 580.161 0.616 18.879 3.318 0.47 153188. 0.3098
|
|
52.50 0.4757 0.7367 0.0540 0.0349 0.745 5.216 3.920 555.396 0.589 17.434 3.201 0.47 153533. 0.2872
|
|
55.42 0.5021 0.7488 0.0494 0.0331 0.707 4.952 3.583 527.313 0.559 15.939 3.082 0.47 153892. 0.2644
|
|
58.33 0.5285 0.7571 0.0446 0.0311 0.665 4.659 3.238 496.079 0.526 14.402 2.960 0.47 154266. 0.2414
|
|
61.25 0.5550 0.7607 0.0397 0.0290 0.619 4.337 2.885 461.843 0.490 12.830 2.833 0.47 154655. 0.2180
|
|
64.17 0.5814 0.7585 0.0348 0.0267 0.570 3.989 2.525 424.752 0.451 11.232 2.697 0.47 155058. 0.1942
|
|
67.08 0.6078 0.7490 0.0298 0.0242 0.516 3.615 2.162 384.960 0.408 9.614 2.547 0.47 155477. 0.1697
|
|
70.00 0.6343 0.7292 0.0247 0.0215 0.459 3.218 1.795 342.647 0.364 7.985 2.376 0.47 155910. 0.1443
|
|
72.92 0.6607 0.6948 0.0197 0.0187 0.400 2.799 1.428 298.024 0.316 6.352 2.173 0.47 156358. 0.1177
|
|
75.83 0.6871 0.6373 0.0146 0.0158 0.337 2.361 1.062 251.354 0.267 4.725 1.917 0.47 156821. 0.0895
|
|
78.75 0.7135 0.5403 0.0096 0.0127 0.272 1.906 0.700 202.952 0.215 3.115 1.565 0.47 157298. 0.0593
|
|
81.67 0.7400 0.3651 0.0047 0.0096 0.205 1.439 0.344 153.197 0.163 1.532 1.020 0.47 157790. 0.0271
|
|
84.58 0.7664 -0.0049 0.0000 0.0064 0.137 0.962 -0.003 102.408 0.109 -0.013 -0.013 0.48 158291. 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 0.1036 0.0371 1.088 6.857 9.280 811.235 0.775 41.279 5.189 0.51 166141. 0.7162
|
|
3.24 0.0264 0.0715 0.1024 0.0378 1.108 6.982 9.172 826.064 0.789 40.799 5.036 0.51 166265. 0.6911
|
|
6.48 0.0528 0.1388 0.1010 0.0385 1.127 7.105 9.053 840.608 0.803 40.270 4.885 0.51 166401. 0.6660
|
|
9.72 0.0793 0.2018 0.0996 0.0391 1.146 7.223 8.922 854.584 0.816 39.687 4.736 0.51 166549. 0.6409
|
|
12.96 0.1057 0.2607 0.0980 0.0397 1.164 7.334 8.778 867.703 0.829 39.046 4.589 0.51 166711. 0.6160
|
|
16.20 0.1321 0.3157 0.0962 0.0403 1.180 7.435 8.620 879.640 0.840 38.341 4.445 0.51 166887. 0.5913
|
|
19.44 0.1585 0.3669 0.0942 0.0407 1.194 7.523 8.446 890.043 0.850 37.567 4.304 0.51 167076. 0.5668
|
|
22.68 0.1850 0.4144 0.0921 0.0411 1.205 7.595 8.255 898.541 0.858 36.720 4.167 0.51 167281. 0.5425
|
|
25.92 0.2114 0.4585 0.0898 0.0414 1.213 7.647 8.047 904.747 0.864 35.794 4.034 0.51 167501. 0.5186
|
|
29.16 0.2378 0.4993 0.0873 0.0416 1.218 7.677 7.821 908.263 0.867 34.786 3.905 0.52 167737. 0.4949
|
|
32.40 0.2642 0.5371 0.0845 0.0416 1.219 7.681 7.575 908.698 0.868 33.692 3.781 0.52 167988. 0.4715
|
|
35.64 0.2907 0.5720 0.0816 0.0414 1.215 7.655 7.309 905.678 0.865 32.509 3.660 0.52 168256. 0.4484
|
|
38.89 0.3171 0.6041 0.0784 0.0411 1.205 7.597 7.022 898.857 0.858 31.235 3.543 0.52 168540. 0.4255
|
|
42.13 0.3435 0.6335 0.0749 0.0406 1.191 7.505 6.715 887.926 0.848 29.869 3.430 0.52 168840. 0.4028
|
|
45.37 0.3699 0.6603 0.0713 0.0399 1.170 7.376 6.388 872.628 0.833 28.412 3.320 0.52 169157. 0.3802
|
|
48.61 0.3964 0.6845 0.0674 0.0390 1.144 7.208 6.040 852.754 0.814 26.865 3.212 0.52 169490. 0.3577
|
|
51.85 0.4228 0.7061 0.0633 0.0379 1.111 7.000 5.672 828.131 0.791 25.230 3.107 0.52 169840. 0.3353
|
|
55.09 0.4492 0.7250 0.0590 0.0365 1.071 6.750 5.286 798.597 0.763 23.511 3.002 0.52 170207. 0.3127
|
|
58.33 0.4756 0.7409 0.0545 0.0350 1.025 6.459 4.882 764.193 0.730 21.714 2.897 0.52 170590. 0.2901
|
|
61.57 0.5021 0.7535 0.0498 0.0332 0.972 6.129 4.463 725.157 0.692 19.853 2.792 0.52 170989. 0.2673
|
|
64.81 0.5285 0.7624 0.0450 0.0312 0.914 5.762 4.033 681.724 0.651 17.940 2.683 0.52 171405. 0.2442
|
|
68.05 0.5549 0.7668 0.0401 0.0290 0.850 5.360 3.593 634.101 0.606 15.983 2.570 0.52 171837. 0.2208
|
|
71.29 0.5813 0.7656 0.0351 0.0267 0.781 4.923 3.146 582.492 0.556 13.993 2.450 0.52 172286. 0.1969
|
|
74.53 0.6078 0.7571 0.0300 0.0241 0.707 4.455 2.693 527.112 0.503 11.978 2.317 0.52 172751. 0.1723
|
|
77.77 0.6342 0.7387 0.0250 0.0214 0.628 3.957 2.237 468.212 0.447 9.948 2.167 0.52 173232. 0.1468
|
|
81.01 0.6606 0.7058 0.0199 0.0186 0.545 3.432 1.779 406.089 0.388 7.914 1.987 0.52 173730. 0.1201
|
|
84.25 0.6870 0.6500 0.0148 0.0156 0.457 2.883 1.323 341.107 0.326 5.887 1.760 0.53 174244. 0.0917
|
|
87.49 0.7135 0.5544 0.0097 0.0125 0.367 2.313 0.872 273.709 0.261 3.880 1.445 0.53 174775. 0.0612
|
|
90.73 0.7399 0.3785 0.0048 0.0094 0.274 1.728 0.429 204.426 0.195 1.908 0.952 0.53 175321. 0.0282
|
|
93.97 0.7663 -0.0058 0.0000 0.0061 0.179 1.130 -0.004 133.699 0.128 -0.018 -0.014 0.53 175877. 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 0.1042 0.0373 1.454 8.332 11.301 1084.412 0.941 50.268 4.727 0.57 182746. 0.7200
|
|
3.56 0.0264 0.0717 0.1030 0.0380 1.481 8.487 11.173 1104.519 0.959 49.695 4.588 0.57 182882. 0.6949
|
|
7.13 0.0528 0.1390 0.1017 0.0387 1.508 8.639 11.030 1124.249 0.976 49.063 4.450 0.57 183031. 0.6697
|
|
10.69 0.0793 0.2022 0.1003 0.0393 1.533 8.784 10.873 1143.227 0.992 48.364 4.314 0.57 183195. 0.6446
|
|
14.25 0.1057 0.2612 0.0987 0.0399 1.557 8.921 10.700 1161.053 1.008 47.594 4.180 0.57 183373. 0.6196
|
|
17.82 0.1321 0.3163 0.0969 0.0405 1.579 9.046 10.509 1177.288 1.022 46.746 4.049 0.57 183566. 0.5948
|
|
21.38 0.1585 0.3675 0.0950 0.0410 1.598 9.155 10.300 1191.459 1.034 45.814 3.921 0.57 183775. 0.5702
|
|
24.95 0.1849 0.4152 0.0929 0.0414 1.613 9.244 10.070 1203.059 1.044 44.791 3.797 0.57 184001. 0.5459
|
|
28.51 0.2114 0.4594 0.0905 0.0417 1.625 9.309 9.818 1211.563 1.052 43.673 3.676 0.57 184243. 0.5219
|
|
32.07 0.2378 0.5004 0.0880 0.0418 1.631 9.347 9.544 1216.433 1.056 42.452 3.559 0.57 184503. 0.4982
|
|
35.64 0.2642 0.5383 0.0853 0.0418 1.632 9.352 9.246 1217.138 1.057 41.126 3.446 0.57 184780. 0.4747
|
|
39.20 0.2906 0.5733 0.0823 0.0417 1.627 9.322 8.923 1213.170 1.053 39.690 3.336 0.57 185074. 0.4516
|
|
42.76 0.3170 0.6056 0.0791 0.0414 1.615 9.252 8.575 1204.056 1.045 38.142 3.230 0.57 185387. 0.4286
|
|
46.33 0.3434 0.6352 0.0756 0.0409 1.595 9.139 8.202 1189.383 1.033 36.481 3.128 0.57 185718. 0.4059
|
|
49.89 0.3699 0.6623 0.0720 0.0402 1.567 8.981 7.803 1168.798 1.015 34.708 3.028 0.57 186067. 0.3833
|
|
53.46 0.3963 0.6868 0.0681 0.0393 1.531 8.775 7.379 1142.021 0.991 32.823 2.931 0.57 186434. 0.3607
|
|
57.02 0.4227 0.7088 0.0639 0.0381 1.487 8.520 6.932 1108.821 0.963 30.831 2.835 0.57 186819. 0.3382
|
|
60.58 0.4491 0.7280 0.0596 0.0368 1.434 8.214 6.460 1068.979 0.928 28.734 2.741 0.57 187223. 0.3157
|
|
64.15 0.4755 0.7444 0.0550 0.0352 1.371 7.857 5.967 1022.541 0.888 26.542 2.647 0.57 187644. 0.2930
|
|
67.71 0.5020 0.7575 0.0503 0.0333 1.301 7.452 5.457 969.826 0.842 24.271 2.552 0.57 188084. 0.2701
|
|
71.27 0.5284 0.7670 0.0455 0.0313 1.222 7.001 4.931 911.152 0.791 21.934 2.455 0.57 188541. 0.2470
|
|
74.84 0.5548 0.7721 0.0405 0.0291 1.136 6.507 4.394 846.799 0.735 19.544 2.353 0.57 189017. 0.2235
|
|
78.40 0.5812 0.7718 0.0355 0.0267 1.042 5.971 3.847 777.042 0.675 17.112 2.246 0.57 189511. 0.1996
|
|
81.96 0.6076 0.7644 0.0304 0.0241 0.942 5.395 3.293 702.175 0.610 14.649 2.127 0.58 190022. 0.1749
|
|
85.53 0.6341 0.7473 0.0252 0.0214 0.835 4.783 2.735 622.535 0.540 12.167 1.993 0.58 190552. 0.1494
|
|
89.09 0.6605 0.7158 0.0201 0.0185 0.722 4.138 2.176 538.527 0.468 9.679 1.833 0.58 191099. 0.1225
|
|
92.66 0.6869 0.6618 0.0149 0.0155 0.604 3.463 1.619 450.645 0.391 7.200 1.629 0.58 191665. 0.0939
|
|
96.22 0.7133 0.5677 0.0098 0.0124 0.482 2.762 1.067 359.490 0.312 4.745 1.346 0.58 192248. 0.0630
|
|
99.78 0.7397 0.3915 0.0048 0.0091 0.356 2.042 0.524 265.788 0.231 2.332 0.895 0.58 192849. 0.0294
|
|
103.35 0.7661 -0.0065 0.0000 0.0058 0.228 1.307 -0.005 170.129 0.148 -0.024 -0.014 0.58 193460. 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 0.1050 0.0375 1.900 9.980 13.546 1416.948 1.128 60.252 4.336 0.62 199346. 0.7231
|
|
3.89 0.0264 0.0717 0.1038 0.0382 1.936 10.168 13.395 1443.588 1.149 59.582 4.209 0.62 199495. 0.6980
|
|
7.77 0.0528 0.1391 0.1025 0.0389 1.971 10.352 13.228 1469.746 1.170 58.840 4.082 0.62 199658. 0.6728
|
|
11.66 0.0792 0.2023 0.1011 0.0396 2.005 10.530 13.044 1494.929 1.190 58.019 3.958 0.62 199837. 0.6477
|
|
15.55 0.1056 0.2614 0.0995 0.0402 2.036 10.696 12.840 1518.602 1.208 57.112 3.835 0.62 200031. 0.6227
|
|
19.43 0.1320 0.3165 0.0978 0.0408 2.065 10.848 12.615 1540.187 1.226 56.111 3.715 0.62 200242. 0.5979
|
|
23.32 0.1585 0.3678 0.0958 0.0413 2.091 10.981 12.367 1559.055 1.241 55.008 3.598 0.62 200471. 0.5733
|
|
27.20 0.1849 0.4155 0.0937 0.0417 2.111 11.090 12.094 1574.532 1.253 53.795 3.484 0.62 200717. 0.5490
|
|
31.09 0.2113 0.4598 0.0914 0.0420 2.127 11.171 11.795 1585.924 1.262 52.466 3.373 0.62 200982. 0.5250
|
|
34.98 0.2377 0.5009 0.0889 0.0422 2.136 11.217 11.469 1592.519 1.267 51.014 3.267 0.62 201266. 0.5012
|
|
38.86 0.2641 0.5389 0.0861 0.0422 2.137 11.225 11.114 1593.609 1.268 49.433 3.163 0.62 201568. 0.4778
|
|
42.75 0.2905 0.5741 0.0831 0.0421 2.130 11.189 10.728 1588.520 1.264 47.719 3.063 0.62 201890. 0.4546
|
|
46.64 0.3169 0.6065 0.0799 0.0418 2.114 11.105 10.312 1576.630 1.255 45.869 2.967 0.62 202232. 0.4317
|
|
50.52 0.3433 0.6364 0.0764 0.0412 2.088 10.969 9.865 1557.385 1.239 43.882 2.873 0.62 202593. 0.4089
|
|
54.41 0.3697 0.6637 0.0727 0.0405 2.052 10.779 9.388 1530.323 1.218 41.757 2.782 0.62 202974. 0.3863
|
|
58.29 0.3961 0.6885 0.0688 0.0396 2.005 10.531 8.880 1495.076 1.190 39.498 2.694 0.62 203375. 0.3638
|
|
62.18 0.4226 0.7107 0.0646 0.0384 1.946 10.223 8.343 1451.342 1.155 37.109 2.607 0.62 203796. 0.3412
|
|
66.07 0.4490 0.7304 0.0603 0.0370 1.876 9.853 7.777 1398.834 1.113 34.591 2.522 0.62 204237. 0.3186
|
|
69.95 0.4754 0.7472 0.0557 0.0354 1.794 9.421 7.185 1337.599 1.064 31.958 2.436 0.62 204697. 0.2959
|
|
73.84 0.5018 0.7608 0.0509 0.0336 1.700 8.932 6.571 1268.056 1.009 29.228 2.350 0.62 205176. 0.2730
|
|
77.73 0.5282 0.7710 0.0460 0.0315 1.597 8.386 5.939 1190.623 0.947 26.418 2.263 0.63 205676. 0.2499
|
|
81.61 0.5546 0.7768 0.0410 0.0293 1.483 7.788 5.293 1105.675 0.880 23.543 2.171 0.63 206195. 0.2263
|
|
85.50 0.5810 0.7774 0.0359 0.0268 1.359 7.139 4.635 1013.574 0.807 20.615 2.074 0.63 206733. 0.2023
|
|
89.38 0.6074 0.7710 0.0307 0.0242 1.227 6.443 3.968 914.710 0.728 17.650 1.968 0.63 207291. 0.1776
|
|
93.27 0.6338 0.7551 0.0255 0.0214 1.086 5.702 3.296 809.530 0.644 14.661 1.847 0.63 207869. 0.1519
|
|
97.16 0.6602 0.7252 0.0203 0.0185 0.937 4.920 2.622 698.568 0.556 11.664 1.703 0.63 208466. 0.1249
|
|
101.04 0.6866 0.6729 0.0151 0.0154 0.781 4.103 1.951 582.479 0.464 8.677 1.519 0.63 209083. 0.0961
|
|
104.93 0.7131 0.5805 0.0100 0.0122 0.620 3.255 1.286 462.064 0.368 5.718 1.262 0.63 209719. 0.0648
|
|
108.82 0.7395 0.4041 0.0049 0.0090 0.454 2.383 0.632 338.285 0.269 2.810 0.847 0.63 210375. 0.0305
|
|
112.70 0.7659 -0.0072 -0.0001 0.0056 0.284 1.493 -0.007 211.920 0.169 -0.030 -0.015 0.63 211040. 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 0.1058 0.0379 2.437 11.817 16.024 1817.524 1.335 71.276 3.999 0.67 215943. 0.7253
|
|
4.21 0.0264 0.0716 0.1047 0.0386 2.484 12.042 15.851 1852.059 1.360 70.507 3.882 0.67 216104. 0.7003
|
|
8.42 0.0528 0.1389 0.1034 0.0393 2.529 12.262 15.659 1886.036 1.385 69.653 3.766 0.67 216281. 0.6752
|
|
12.62 0.0792 0.2021 0.1020 0.0400 2.573 12.475 15.446 1918.792 1.409 68.705 3.651 0.67 216475. 0.6502
|
|
16.83 0.1056 0.2611 0.1004 0.0406 2.615 12.676 15.210 1949.633 1.432 67.654 3.538 0.67 216686. 0.6253
|
|
21.04 0.1320 0.3162 0.0987 0.0412 2.652 12.859 14.948 1977.788 1.453 66.490 3.428 0.67 216915. 0.6006
|
|
25.25 0.1584 0.3675 0.0968 0.0417 2.685 13.019 14.660 2002.437 1.471 65.205 3.321 0.67 217163. 0.5761
|
|
29.46 0.1848 0.4153 0.0947 0.0421 2.712 13.151 14.341 2022.705 1.486 63.790 3.216 0.67 217430. 0.5518
|
|
33.66 0.2112 0.4596 0.0924 0.0424 2.733 13.248 13.992 2037.683 1.497 62.234 3.114 0.67 217717. 0.5279
|
|
37.87 0.2376 0.5008 0.0899 0.0426 2.744 13.305 13.609 2046.448 1.503 60.532 3.016 0.67 218025. 0.5042
|
|
42.08 0.2640 0.5389 0.0871 0.0427 2.747 13.316 13.191 2048.073 1.504 58.674 2.921 0.67 218353. 0.4808
|
|
46.29 0.2904 0.5742 0.0841 0.0425 2.738 13.274 12.738 2041.685 1.500 56.657 2.830 0.67 218703. 0.4576
|
|
50.50 0.3168 0.6068 0.0809 0.0422 2.718 13.176 12.247 2026.466 1.489 54.477 2.741 0.67 219073. 0.4347
|
|
54.70 0.3432 0.6369 0.0774 0.0417 2.684 13.015 11.720 2001.707 1.470 52.131 2.656 0.67 219465. 0.4119
|
|
58.91 0.3695 0.6644 0.0737 0.0410 2.638 12.788 11.156 1966.804 1.445 49.620 2.573 0.67 219879. 0.3893
|
|
63.12 0.3959 0.6895 0.0697 0.0400 2.576 12.492 10.555 1921.279 1.411 46.948 2.492 0.67 220314. 0.3668
|
|
67.33 0.4223 0.7121 0.0655 0.0388 2.501 12.124 9.919 1864.754 1.370 44.118 2.413 0.67 220770. 0.3443
|
|
71.54 0.4487 0.7321 0.0611 0.0374 2.410 11.683 9.248 1796.860 1.320 41.135 2.334 0.67 221247. 0.3217
|
|
75.74 0.4751 0.7494 0.0564 0.0358 2.303 11.168 8.546 1717.641 1.262 38.013 2.257 0.68 221746. 0.2989
|
|
79.95 0.5015 0.7636 0.0516 0.0339 2.183 10.582 7.818 1627.633 1.196 34.773 2.179 0.68 222266. 0.2760
|
|
84.16 0.5279 0.7743 0.0467 0.0318 2.048 9.931 7.067 1527.380 1.122 31.436 2.099 0.68 222807. 0.2528
|
|
88.37 0.5543 0.7809 0.0416 0.0295 1.901 9.215 6.299 1417.370 1.041 28.019 2.016 0.68 223370. 0.2292
|
|
92.58 0.5807 0.7824 0.0364 0.0270 1.741 8.440 5.517 1298.077 0.954 24.540 1.928 0.68 223953. 0.2052
|
|
96.78 0.6071 0.7771 0.0312 0.0244 1.569 7.607 4.724 1170.004 0.859 21.014 1.831 0.68 224558. 0.1804
|
|
100.99 0.6335 0.7625 0.0259 0.0215 1.386 6.721 3.925 1033.734 0.759 17.458 1.722 0.68 225183. 0.1546
|
|
105.20 0.6599 0.7341 0.0206 0.0185 1.193 5.786 3.123 889.959 0.654 13.891 1.592 0.68 225830. 0.1274
|
|
109.41 0.6863 0.6835 0.0153 0.0154 0.992 4.808 2.323 739.535 0.543 10.334 1.425 0.68 226498. 0.0984
|
|
113.62 0.7127 0.5928 0.0101 0.0122 0.783 3.794 1.531 583.535 0.429 6.811 1.190 0.68 227186. 0.0667
|
|
117.82 0.7391 0.4166 0.0050 0.0088 0.568 2.752 0.753 423.265 0.311 3.348 0.806 0.69 227896. 0.0317
|
|
122.03 0.7655 -0.0077 -0.0001 0.0054 0.348 1.689 -0.008 259.808 0.191 -0.037 -0.014 0.69 228616. 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 0.1067 0.0385 3.092 13.920 18.747 2305.698 1.573 83.388 3.688 0.72 232535. 0.7235
|
|
4.53 0.0264 0.0711 0.1056 0.0392 3.149 14.176 18.553 2348.128 1.602 82.523 3.584 0.72 232709. 0.6994
|
|
9.06 0.0528 0.1382 0.1044 0.0399 3.205 14.429 18.336 2389.990 1.630 81.557 3.480 0.72 232899. 0.6751
|
|
13.59 0.0791 0.2011 0.1030 0.0405 3.259 14.674 18.094 2430.485 1.658 80.481 3.377 0.72 233108. 0.6508
|
|
18.11 0.1055 0.2601 0.1015 0.0412 3.311 14.905 17.825 2468.745 1.684 79.283 3.275 0.72 233335. 0.6265
|
|
22.64 0.1319 0.3151 0.0998 0.0418 3.358 15.116 17.525 2503.831 1.708 77.953 3.175 0.72 233582. 0.6022
|
|
27.17 0.1583 0.3665 0.0979 0.0423 3.399 15.303 17.194 2534.691 1.729 76.479 3.077 0.72 233849. 0.5781
|
|
31.70 0.1846 0.4143 0.0958 0.0427 3.433 15.457 16.828 2560.206 1.746 74.849 2.981 0.72 234138. 0.5541
|
|
36.23 0.2110 0.4587 0.0935 0.0430 3.459 15.571 16.424 2579.188 1.759 73.054 2.888 0.72 234448. 0.5304
|
|
40.76 0.2374 0.5000 0.0910 0.0432 3.474 15.639 15.981 2590.413 1.767 71.084 2.798 0.72 234779. 0.5069
|
|
45.28 0.2638 0.5382 0.0882 0.0432 3.477 15.653 15.497 2592.651 1.768 68.929 2.711 0.72 235134. 0.4836
|
|
49.81 0.2902 0.5737 0.0852 0.0431 3.466 15.605 14.970 2584.714 1.763 66.584 2.627 0.72 235510. 0.4605
|
|
54.34 0.3165 0.6064 0.0820 0.0428 3.440 15.489 14.399 2565.518 1.750 64.045 2.546 0.72 235910. 0.4377
|
|
58.87 0.3429 0.6367 0.0785 0.0423 3.398 15.299 13.783 2534.133 1.729 61.308 2.467 0.72 236333. 0.4150
|
|
63.40 0.3693 0.6645 0.0747 0.0415 3.339 15.032 13.124 2489.792 1.698 58.375 2.391 0.72 236779. 0.3924
|
|
67.93 0.3957 0.6899 0.0707 0.0406 3.261 14.682 12.421 2431.892 1.659 55.249 2.317 0.72 237247. 0.3699
|
|
72.46 0.4220 0.7128 0.0665 0.0394 3.165 14.248 11.676 2359.956 1.610 51.935 2.244 0.73 237739. 0.3475
|
|
76.98 0.4484 0.7332 0.0620 0.0379 3.049 13.726 10.890 2273.530 1.551 48.439 2.173 0.73 238254. 0.3249
|
|
81.51 0.4748 0.7510 0.0573 0.0362 2.914 13.117 10.066 2172.643 1.482 44.775 2.101 0.73 238791. 0.3021
|
|
86.04 0.5012 0.7657 0.0524 0.0343 2.760 12.425 9.211 2057.966 1.404 40.970 2.030 0.73 239351. 0.2792
|
|
90.57 0.5275 0.7771 0.0474 0.0322 2.588 11.653 8.329 1930.197 1.317 37.049 1.957 0.73 239934. 0.2560
|
|
95.10 0.5539 0.7845 0.0423 0.0299 2.400 10.807 7.426 1789.965 1.221 33.031 1.882 0.73 240540. 0.2324
|
|
99.63 0.5803 0.7869 0.0370 0.0273 2.196 9.889 6.506 1637.898 1.117 28.937 1.802 0.73 241168. 0.2082
|
|
104.16 0.6067 0.7826 0.0317 0.0246 1.978 8.903 5.572 1474.694 1.006 24.786 1.714 0.73 241819. 0.1833
|
|
108.68 0.6331 0.7691 0.0264 0.0217 1.745 7.856 4.631 1301.172 0.888 20.597 1.614 0.73 242492. 0.1574
|
|
113.21 0.6594 0.7419 0.0210 0.0187 1.500 6.752 3.686 1118.331 0.763 16.394 1.495 0.73 243188. 0.1300
|
|
117.74 0.6858 0.6924 0.0156 0.0155 1.244 5.599 2.743 927.419 0.633 12.199 1.341 0.74 243907. 0.1007
|
|
122.27 0.7122 0.6022 0.0103 0.0122 0.979 4.407 1.808 729.992 0.498 8.042 1.123 0.74 244648. 0.0684
|
|
126.80 0.7386 0.4245 0.0051 0.0088 0.708 3.187 0.889 527.937 0.360 3.954 0.764 0.74 245411. 0.0326
|
|
131.33 0.7649 -0.0079 -0.0001 0.0054 0.433 1.949 -0.010 322.849 0.220 -0.044 -0.014 0.74 246185. 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 0.1077 0.0398 3.938 16.547 21.725 2936.606 1.870 96.631 3.355 0.77 249122. 0.7087
|
|
4.85 0.0263 0.0694 0.1067 0.0405 4.003 16.819 21.510 2984.777 1.900 95.676 3.269 0.77 249308. 0.6869
|
|
9.69 0.0527 0.1352 0.1055 0.0411 4.066 17.085 21.269 3032.112 1.930 94.605 3.182 0.77 249512. 0.6649
|
|
14.54 0.0790 0.1973 0.1041 0.0417 4.127 17.342 21.000 3077.664 1.959 93.407 3.095 0.77 249735. 0.6426
|
|
19.39 0.1054 0.2557 0.1027 0.0423 4.185 17.583 20.698 3120.425 1.987 92.067 3.009 0.77 249979. 0.6202
|
|
24.23 0.1317 0.3105 0.1010 0.0428 4.237 17.802 20.362 3159.301 2.011 90.571 2.923 0.77 250243. 0.5977
|
|
29.08 0.1581 0.3619 0.0991 0.0433 4.282 17.992 19.988 3193.076 2.033 88.906 2.839 0.77 250530. 0.5752
|
|
33.92 0.1844 0.4100 0.0971 0.0437 4.319 18.147 19.573 3220.459 2.050 87.059 2.757 0.77 250839. 0.5526
|
|
38.77 0.2108 0.4548 0.0948 0.0439 4.345 18.257 19.113 3240.073 2.063 85.016 2.676 0.77 251171. 0.5300
|
|
43.62 0.2371 0.4965 0.0923 0.0441 4.359 18.316 18.607 3250.488 2.069 82.766 2.596 0.77 251527. 0.5075
|
|
48.46 0.2635 0.5352 0.0895 0.0441 4.359 18.315 18.053 3250.236 2.069 80.299 2.519 0.77 251907. 0.4850
|
|
53.31 0.2898 0.5712 0.0865 0.0439 4.342 18.245 17.447 3237.864 2.061 77.606 2.444 0.77 252311. 0.4626
|
|
58.16 0.3162 0.6045 0.0833 0.0436 4.307 18.099 16.790 3211.995 2.045 74.681 2.371 0.77 252740. 0.4402
|
|
63.00 0.3425 0.6352 0.0797 0.0430 4.253 17.870 16.080 3171.375 2.019 71.523 2.300 0.78 253194. 0.4179
|
|
67.85 0.3689 0.6634 0.0760 0.0422 4.177 17.552 15.317 3114.924 1.983 68.132 2.230 0.78 253672. 0.3955
|
|
72.70 0.3952 0.6892 0.0719 0.0412 4.079 17.140 14.504 3041.755 1.936 64.512 2.163 0.78 254174. 0.3732
|
|
77.54 0.4216 0.7126 0.0676 0.0400 3.958 16.629 13.640 2951.161 1.879 60.669 2.096 0.78 254701. 0.3508
|
|
82.39 0.4479 0.7335 0.0631 0.0385 3.812 16.017 12.727 2842.481 1.810 56.609 2.031 0.78 255253. 0.3283
|
|
87.23 0.4742 0.7518 0.0584 0.0368 3.642 15.302 11.769 2715.668 1.729 52.350 1.966 0.78 255829. 0.3056
|
|
92.08 0.5006 0.7671 0.0534 0.0349 3.449 14.490 10.774 2571.591 1.637 47.923 1.900 0.78 256429. 0.2826
|
|
96.93 0.5269 0.7791 0.0483 0.0327 3.234 13.587 9.747 2411.228 1.535 43.355 1.834 0.78 257053. 0.2594
|
|
101.77 0.5533 0.7870 0.0431 0.0303 2.998 12.597 8.694 2235.495 1.423 38.671 1.764 0.78 257702. 0.2357
|
|
106.62 0.5796 0.7898 0.0378 0.0277 2.743 11.525 7.620 2045.343 1.302 33.894 1.690 0.78 258374. 0.2114
|
|
111.47 0.6060 0.7858 0.0324 0.0250 2.470 10.379 6.530 1841.865 1.173 29.045 1.608 0.78 259071. 0.1862
|
|
116.31 0.6323 0.7721 0.0269 0.0221 2.181 9.164 5.429 1626.332 1.035 24.150 1.514 0.79 259791. 0.1599
|
|
121.16 0.6587 0.7439 0.0214 0.0190 1.878 7.891 4.324 1400.321 0.891 19.232 1.400 0.79 260536. 0.1319
|
|
126.00 0.6850 0.6919 0.0160 0.0158 1.563 6.569 3.219 1165.742 0.742 14.320 1.253 0.79 261304. 0.1018
|
|
130.85 0.7114 0.5974 0.0105 0.0125 1.240 5.212 2.124 924.918 0.589 9.446 1.041 0.79 262097. 0.0688
|
|
135.70 0.7377 0.4142 0.0052 0.0092 0.913 3.835 1.045 680.580 0.433 4.648 0.696 0.79 262913. 0.0323
|
|
140.54 0.7641 -0.0070 -0.0001 0.0059 0.583 2.451 -0.011 435.014 0.277 -0.049 -0.011 0.79 263742. 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 0.1088 0.0427 5.121 20.174 24.961 3818.930 2.279 111.027 2.965 0.82 265702. 0.6711
|
|
5.17 0.0263 0.0657 0.1078 0.0432 5.188 20.438 24.729 3868.853 2.309 109.995 2.899 0.82 265899. 0.6533
|
|
10.33 0.0527 0.1283 0.1067 0.0438 5.253 20.692 24.468 3917.004 2.338 108.832 2.833 0.82 266117. 0.6350
|
|
15.50 0.0790 0.1880 0.1054 0.0443 5.313 20.931 24.173 3962.251 2.365 107.522 2.767 0.82 266355. 0.6165
|
|
20.66 0.1053 0.2447 0.1039 0.0447 5.369 21.149 23.842 4003.403 2.389 106.050 2.701 0.82 266615. 0.5976
|
|
25.83 0.1316 0.2984 0.1023 0.0451 5.417 21.338 23.470 4039.191 2.411 104.396 2.636 0.82 266898. 0.5785
|
|
31.00 0.1580 0.3493 0.1005 0.0455 5.456 21.491 23.054 4068.259 2.428 102.545 2.570 0.82 267204. 0.5592
|
|
36.16 0.1843 0.3972 0.0985 0.0457 5.484 21.602 22.590 4089.200 2.441 100.481 2.506 0.82 267534. 0.5396
|
|
41.33 0.2106 0.4424 0.0962 0.0458 5.499 21.662 22.074 4100.526 2.447 98.187 2.442 0.82 267889. 0.5198
|
|
46.49 0.2370 0.4848 0.0937 0.0458 5.499 21.663 21.504 4100.709 2.447 95.650 2.378 0.82 268270. 0.4998
|
|
51.66 0.2633 0.5245 0.0910 0.0457 5.482 21.596 20.876 4088.178 2.440 92.856 2.316 0.82 268676. 0.4795
|
|
56.83 0.2896 0.5617 0.0880 0.0454 5.446 21.455 20.188 4061.365 2.424 89.796 2.255 0.83 269108. 0.4590
|
|
61.99 0.3160 0.5962 0.0847 0.0449 5.389 21.230 19.439 4018.763 2.399 86.463 2.194 0.83 269567. 0.4383
|
|
67.16 0.3423 0.6283 0.0812 0.0442 5.309 20.914 18.627 3958.967 2.363 82.853 2.134 0.83 270052. 0.4173
|
|
72.32 0.3686 0.6579 0.0774 0.0434 5.204 20.501 17.753 3880.722 2.316 78.967 2.075 0.83 270562. 0.3962
|
|
77.49 0.3949 0.6850 0.0733 0.0423 5.073 19.984 16.819 3782.982 2.258 74.809 2.017 0.83 271100. 0.3747
|
|
82.66 0.4213 0.7097 0.0690 0.0409 4.915 19.360 15.824 3664.899 2.187 70.387 1.958 0.83 271663. 0.3530
|
|
87.82 0.4476 0.7317 0.0644 0.0394 4.728 18.625 14.773 3525.636 2.104 65.709 1.900 0.83 272252. 0.3310
|
|
92.99 0.4739 0.7508 0.0596 0.0376 4.514 17.782 13.667 3366.033 2.009 60.792 1.842 0.83 272867. 0.3085
|
|
98.15 0.5003 0.7665 0.0546 0.0356 4.274 16.836 12.517 3186.956 1.902 55.674 1.781 0.83 273508. 0.2856
|
|
103.32 0.5266 0.7785 0.0494 0.0334 4.009 15.791 11.328 2989.304 1.784 50.387 1.719 0.83 274175. 0.2621
|
|
108.49 0.5529 0.7860 0.0441 0.0310 3.720 14.655 10.108 2774.255 1.656 44.960 1.653 0.83 274867. 0.2381
|
|
113.65 0.5793 0.7876 0.0386 0.0284 3.410 13.433 8.862 2542.838 1.518 39.420 1.581 0.84 275585. 0.2132
|
|
118.82 0.6056 0.7814 0.0331 0.0257 3.080 12.134 7.597 2297.016 1.371 33.793 1.500 0.84 276328. 0.1874
|
|
123.99 0.6319 0.7641 0.0275 0.0228 2.734 10.770 6.319 2038.821 1.217 28.106 1.406 0.84 277096. 0.1601
|
|
129.15 0.6582 0.7300 0.0219 0.0198 2.375 9.354 5.033 1770.699 1.057 22.388 1.289 0.84 277890. 0.1311
|
|
134.32 0.6846 0.6693 0.0163 0.0167 2.006 7.901 3.748 1495.620 0.893 16.672 1.137 0.84 278709. 0.0997
|
|
139.48 0.7109 0.5635 0.0108 0.0136 1.632 6.428 2.472 1216.864 0.726 10.996 0.921 0.84 279554. 0.0657
|
|
144.65 0.7372 0.3726 0.0053 0.0105 1.258 4.957 1.215 938.265 0.560 5.406 0.588 0.84 280424. 0.0293
|
|
149.82 0.7636 -0.0068 -0.0001 0.0074 0.889 3.500 -0.015 662.589 0.395 -0.067 -0.010 0.85 281309. 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 0.1097 0.0474 6.827 25.310 28.399 5090.576 2.859 126.319 2.530 0.87 282280. 0.6110
|
|
5.49 0.0264 0.0599 0.1087 0.0479 6.893 25.555 28.156 5139.808 2.887 125.238 2.485 0.87 282490. 0.5974
|
|
10.99 0.0527 0.1175 0.1076 0.0483 6.953 25.780 27.880 5185.118 2.913 124.010 2.439 0.87 282721. 0.5835
|
|
16.48 0.0791 0.1729 0.1064 0.0487 7.007 25.978 27.567 5225.047 2.935 122.617 2.393 0.87 282973. 0.5693
|
|
21.98 0.1054 0.2262 0.1051 0.0490 7.051 26.143 27.212 5258.162 2.954 121.038 2.347 0.87 283250. 0.5548
|
|
27.47 0.1318 0.2772 0.1035 0.0492 7.085 26.266 26.810 5282.953 2.968 119.252 2.302 0.87 283550. 0.5400
|
|
32.97 0.1581 0.3261 0.1018 0.0493 7.105 26.341 26.357 5297.888 2.976 117.238 2.257 0.87 283876. 0.5249
|
|
38.46 0.1845 0.3729 0.0998 0.0494 7.109 26.358 25.849 5301.380 2.978 114.976 2.212 0.87 284228. 0.5095
|
|
43.96 0.2109 0.4175 0.0976 0.0493 7.096 26.310 25.280 5291.819 2.973 112.446 2.167 0.88 284607. 0.4936
|
|
49.45 0.2372 0.4601 0.0952 0.0491 7.064 26.190 24.647 5267.581 2.959 109.630 2.122 0.88 285013. 0.4774
|
|
54.95 0.2636 0.5005 0.0925 0.0487 7.010 25.989 23.946 5227.111 2.936 106.512 2.078 0.88 285446. 0.4607
|
|
60.44 0.2899 0.5388 0.0895 0.0481 6.932 25.700 23.174 5168.950 2.904 103.079 2.034 0.88 285908. 0.4436
|
|
65.93 0.3163 0.5750 0.0862 0.0474 6.828 25.316 22.330 5091.762 2.860 99.323 1.989 0.88 286398. 0.4259
|
|
71.43 0.3426 0.6089 0.0827 0.0465 6.698 24.831 21.412 4994.354 2.805 95.240 1.945 0.88 286915. 0.4077
|
|
76.92 0.3690 0.6406 0.0788 0.0454 6.538 24.241 20.420 4875.544 2.739 90.829 1.900 0.88 287461. 0.3890
|
|
82.42 0.3953 0.6700 0.0747 0.0441 6.349 23.540 19.356 4734.592 2.660 86.098 1.854 0.88 288035. 0.3697
|
|
87.91 0.4217 0.6969 0.0704 0.0426 6.129 22.725 18.223 4570.661 2.567 81.054 1.808 0.88 288636. 0.3498
|
|
93.41 0.4481 0.7213 0.0657 0.0408 5.877 21.791 17.020 4382.801 2.462 75.707 1.761 0.88 289265. 0.3293
|
|
98.90 0.4744 0.7426 0.0608 0.0389 5.595 20.745 15.755 4172.476 2.344 70.077 1.713 0.88 289922. 0.3080
|
|
104.40 0.5008 0.7597 0.0557 0.0367 5.289 19.610 14.434 3944.075 2.215 64.205 1.660 0.88 290606. 0.2858
|
|
109.89 0.5271 0.7720 0.0505 0.0345 4.960 18.391 13.069 3699.001 2.078 58.129 1.602 0.89 291317. 0.2625
|
|
115.39 0.5535 0.7773 0.0450 0.0321 4.617 17.118 11.664 3442.904 1.934 51.882 1.537 0.89 292055. 0.2378
|
|
120.88 0.5798 0.7751 0.0395 0.0295 4.254 15.772 10.229 3172.201 1.782 45.499 1.463 0.89 292820. 0.2120
|
|
126.37 0.6062 0.7632 0.0339 0.0269 3.873 14.358 8.771 2887.839 1.622 39.013 1.378 0.89 293612. 0.1849
|
|
131.87 0.6326 0.7377 0.0282 0.0242 3.478 12.895 7.297 2593.622 1.457 32.455 1.276 0.89 294431. 0.1562
|
|
137.36 0.6589 0.6927 0.0225 0.0214 3.075 11.399 5.814 2292.665 1.288 25.862 1.150 0.89 295277. 0.1257
|
|
142.86 0.6853 0.6188 0.0167 0.0185 2.668 9.890 4.333 1989.204 1.117 19.275 0.988 0.89 296149. 0.0932
|
|
148.35 0.7116 0.5007 0.0111 0.0157 2.263 8.391 2.864 1687.668 0.948 12.741 0.770 0.90 297049. 0.0590
|
|
153.85 0.7380 0.3118 0.0055 0.0130 1.867 6.924 1.419 1392.549 0.782 6.312 0.462 0.90 297975. 0.0250
|
|
159.34 0.7643 0.0019 0.0000 0.0103 1.484 5.500 0.007 1106.286 0.621 0.030 0.003 0.90 298921. 0.0000
|
|
|
|
|
|
|
|
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 0.1094 0.0528 9.015 31.567 31.764 6722.576 3.566 141.288 2.143 0.92 298889. 0.5473
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5.85 0.0265 0.0540 0.1086 0.0533 9.102 31.871 31.529 6787.374 3.601 140.243 2.107 0.92 299108. 0.5361
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11.70 0.0530 0.1063 0.1077 0.0537 9.180 32.146 31.259 6845.867 3.632 139.041 2.071 0.92 299349. 0.5247
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17.55 0.0795 0.1567 0.1066 0.0541 9.247 32.379 30.948 6895.553 3.658 137.658 2.036 0.92 299615. 0.5131
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23.40 0.1060 0.2053 0.1054 0.0544 9.299 32.559 30.591 6933.909 3.679 136.067 2.001 0.93 299906. 0.5015
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29.26 0.1325 0.2523 0.1039 0.0546 9.331 32.675 30.180 6958.405 3.692 134.241 1.967 0.93 300224. 0.4897
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35.11 0.1590 0.2977 0.1023 0.0547 9.342 32.713 29.711 6966.574 3.696 132.153 1.934 0.93 300569. 0.4777
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40.96 0.1856 0.3416 0.1005 0.0546 9.328 32.664 29.176 6956.117 3.690 129.775 1.902 0.93 300943. 0.4656
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46.81 0.2121 0.3840 0.0984 0.0543 9.287 32.518 28.571 6924.972 3.674 127.082 1.871 0.93 301346. 0.4532
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52.66 0.2386 0.4250 0.0960 0.0539 9.214 32.265 27.889 6871.209 3.645 124.048 1.841 0.93 301778. 0.4405
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58.51 0.2651 0.4646 0.0934 0.0533 9.110 31.899 27.125 6793.201 3.604 120.653 1.811 0.93 302241. 0.4274
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64.36 0.2916 0.5027 0.0905 0.0525 8.972 31.416 26.278 6690.318 3.549 116.883 1.781 0.93 302734. 0.4138
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70.21 0.3181 0.5392 0.0873 0.0515 8.799 30.812 25.343 6561.676 3.481 112.726 1.752 0.93 303258. 0.3996
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76.07 0.3446 0.5742 0.0838 0.0503 8.591 30.083 24.321 6406.571 3.399 108.178 1.722 0.93 303813. 0.3848
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81.92 0.3711 0.6074 0.0799 0.0488 8.347 29.228 23.210 6224.450 3.302 103.237 1.691 0.93 304397. 0.3692
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87.77 0.3976 0.6387 0.0758 0.0472 8.066 28.244 22.012 6014.947 3.191 97.909 1.660 0.93 305012. 0.3529
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93.62 0.4241 0.6679 0.0714 0.0453 7.748 27.131 20.730 5777.895 3.065 92.205 1.627 0.93 305657. 0.3357
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99.47 0.4506 0.6948 0.0667 0.0433 7.393 25.888 19.366 5513.127 2.925 86.138 1.593 0.93 306331. 0.3177
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105.32 0.4771 0.7190 0.0617 0.0410 7.002 24.517 17.927 5221.220 2.770 79.737 1.557 0.94 307035. 0.2988
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111.17 0.5037 0.7387 0.0566 0.0386 6.591 23.078 16.423 4914.771 2.607 73.048 1.516 0.94 307768. 0.2783
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117.02 0.5302 0.7522 0.0512 0.0361 6.166 21.590 14.864 4597.891 2.439 66.114 1.466 0.94 308530. 0.2561
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122.87 0.5567 0.7560 0.0457 0.0336 5.746 20.118 13.258 4284.426 2.273 58.969 1.404 0.94 309321. 0.2316
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128.73 0.5832 0.7462 0.0400 0.0313 5.341 18.703 11.611 3982.958 2.113 51.646 1.322 0.94 310140. 0.2042
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134.58 0.6097 0.7243 0.0342 0.0288 4.924 17.242 9.938 3671.885 1.948 44.205 1.228 0.94 310989. 0.1754
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140.43 0.6362 0.6863 0.0284 0.0263 4.501 15.760 8.249 3356.194 1.781 36.692 1.115 0.94 311866. 0.1451
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146.28 0.6627 0.6269 0.0226 0.0239 4.078 14.280 6.555 3041.150 1.613 29.155 0.978 0.94 312771. 0.1134
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152.13 0.6892 0.5392 0.0168 0.0214 3.662 12.824 4.868 2730.992 1.449 21.655 0.809 0.95 313705. 0.0808
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157.98 0.7157 0.4142 0.0110 0.0191 3.260 11.414 3.205 2430.794 1.290 14.257 0.598 0.95 314668. 0.0485
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163.83 0.7422 0.2402 0.0054 0.0168 2.876 10.071 1.582 2144.687 1.138 7.035 0.334 0.95 315661. 0.0191
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169.68 0.7687 0.0009 0.0000 0.0147 2.508 8.781 0.005 1870.052 0.992 0.022 0.001 0.95 316686. 0.0000
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