464 lines
82 KiB
Plaintext
464 lines
82 KiB
Plaintext
17x10 (17x10.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 0.1048 0.0461 0.005 0.327 0.276 3.867 0.037 1.226 32.332 0.07 34428. 0.5876
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0.42 0.0259 0.0573 0.1033 0.0466 0.005 0.331 0.272 3.912 0.037 1.208 31.491 0.07 34454. 0.5681
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0.83 0.0517 0.1116 0.1016 0.0471 0.005 0.334 0.267 3.955 0.038 1.189 30.650 0.07 34482. 0.5485
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1.25 0.0776 0.1628 0.0998 0.0476 0.005 0.338 0.262 3.993 0.038 1.168 29.813 0.07 34513. 0.5287
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1.66 0.1035 0.2110 0.0978 0.0480 0.005 0.340 0.257 4.027 0.038 1.145 28.981 0.07 34546. 0.5089
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2.08 0.1293 0.2562 0.0957 0.0483 0.005 0.343 0.252 4.055 0.039 1.120 28.156 0.07 34581. 0.4890
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2.49 0.1552 0.2985 0.0934 0.0486 0.005 0.345 0.246 4.077 0.039 1.093 27.339 0.07 34620. 0.4691
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2.91 0.1810 0.3380 0.0909 0.0487 0.005 0.346 0.239 4.090 0.039 1.064 26.530 0.07 34661. 0.4492
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3.32 0.2069 0.3746 0.0883 0.0488 0.005 0.346 0.232 4.095 0.039 1.033 25.730 0.07 34705. 0.4293
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3.74 0.2328 0.4085 0.0855 0.0487 0.005 0.346 0.225 4.090 0.039 1.000 24.939 0.07 34752. 0.4094
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4.15 0.2586 0.4396 0.0825 0.0485 0.005 0.344 0.217 4.073 0.039 0.965 24.154 0.07 34802. 0.3894
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4.57 0.2845 0.4680 0.0792 0.0482 0.005 0.342 0.208 4.045 0.039 0.927 23.376 0.07 34854. 0.3695
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4.98 0.3104 0.4937 0.0758 0.0477 0.005 0.338 0.199 4.003 0.038 0.887 22.603 0.07 34910. 0.3495
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5.40 0.3362 0.5165 0.0722 0.0470 0.005 0.334 0.190 3.948 0.038 0.845 21.832 0.07 34969. 0.3294
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5.81 0.3621 0.5366 0.0685 0.0462 0.005 0.328 0.180 3.879 0.037 0.801 21.060 0.07 35031. 0.3094
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6.23 0.3880 0.5538 0.0645 0.0452 0.005 0.321 0.170 3.797 0.036 0.755 20.284 0.07 35096. 0.2893
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6.64 0.4138 0.5678 0.0605 0.0441 0.005 0.313 0.159 3.701 0.035 0.708 19.500 0.07 35165. 0.2692
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7.06 0.4397 0.5786 0.0563 0.0428 0.005 0.304 0.148 3.591 0.034 0.659 18.701 0.07 35236. 0.2491
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7.47 0.4655 0.5858 0.0520 0.0413 0.005 0.293 0.137 3.468 0.033 0.608 17.882 0.07 35311. 0.2289
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7.89 0.4914 0.5890 0.0476 0.0397 0.004 0.282 0.125 3.332 0.032 0.557 17.034 0.07 35389. 0.2086
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8.30 0.5173 0.5877 0.0431 0.0379 0.004 0.269 0.113 3.182 0.030 0.504 16.146 0.07 35469. 0.1881
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8.72 0.5431 0.5811 0.0385 0.0359 0.004 0.255 0.101 3.018 0.029 0.450 15.204 0.07 35554. 0.1674
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9.13 0.5690 0.5681 0.0338 0.0338 0.004 0.240 0.089 2.842 0.027 0.395 14.189 0.07 35641. 0.1465
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9.55 0.5949 0.5474 0.0291 0.0316 0.004 0.224 0.076 2.652 0.025 0.340 13.076 0.07 35731. 0.1252
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9.96 0.6207 0.5166 0.0243 0.0292 0.003 0.207 0.064 2.448 0.023 0.284 11.827 0.07 35825. 0.1035
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10.38 0.6466 0.4727 0.0194 0.0266 0.003 0.189 0.051 2.232 0.021 0.227 10.390 0.07 35922. 0.0813
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10.79 0.6725 0.4107 0.0146 0.0239 0.003 0.169 0.038 2.004 0.019 0.171 8.680 0.07 36022. 0.0588
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11.21 0.6983 0.3226 0.0097 0.0210 0.002 0.149 0.026 1.763 0.017 0.114 6.565 0.07 36126. 0.0363
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11.62 0.7242 0.1943 0.0048 0.0180 0.002 0.128 0.013 1.511 0.014 0.057 3.812 0.07 36232. 0.0149
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12.04 0.7501 -0.0014 0.0000 0.0149 0.002 0.106 0.000 1.249 0.012 0.000 -0.027 0.07 36340. 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 0.1053 0.0415 0.037 1.179 1.108 27.891 0.133 4.927 18.014 0.13 68855. 0.6563
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0.84 0.0260 0.0641 0.1037 0.0421 0.038 1.196 1.092 28.288 0.135 4.856 17.503 0.13 68907. 0.6330
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1.67 0.0520 0.1244 0.1021 0.0427 0.038 1.211 1.074 28.665 0.137 4.778 16.996 0.13 68964. 0.6098
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2.51 0.0780 0.1812 0.1003 0.0432 0.039 1.226 1.055 29.011 0.139 4.693 16.496 0.13 69025. 0.5866
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3.34 0.1040 0.2343 0.0983 0.0436 0.039 1.239 1.034 29.320 0.140 4.601 16.003 0.13 69092. 0.5634
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4.18 0.1301 0.2840 0.0962 0.0440 0.040 1.250 1.012 29.583 0.141 4.502 15.518 0.13 69164. 0.5404
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5.01 0.1561 0.3304 0.0939 0.0444 0.040 1.259 0.988 29.791 0.142 4.394 15.041 0.13 69241. 0.5175
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5.85 0.1821 0.3735 0.0914 0.0446 0.040 1.265 0.962 29.936 0.143 4.279 14.574 0.13 69324. 0.4948
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6.68 0.2081 0.4134 0.0888 0.0447 0.040 1.268 0.934 30.008 0.143 4.154 14.117 0.13 69413. 0.4723
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7.52 0.2341 0.4504 0.0859 0.0447 0.040 1.268 0.904 29.998 0.143 4.021 13.669 0.13 69508. 0.4499
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8.35 0.2601 0.4843 0.0829 0.0445 0.040 1.263 0.872 29.896 0.143 3.879 13.230 0.13 69608. 0.4276
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9.19 0.2861 0.5154 0.0796 0.0442 0.040 1.255 0.838 29.694 0.142 3.727 12.799 0.14 69715. 0.4056
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10.02 0.3121 0.5437 0.0762 0.0437 0.039 1.242 0.802 29.384 0.140 3.566 12.375 0.14 69828. 0.3836
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10.86 0.3382 0.5691 0.0726 0.0431 0.039 1.224 0.764 28.960 0.138 3.396 11.959 0.14 69947. 0.3617
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11.69 0.3642 0.5918 0.0688 0.0423 0.038 1.201 0.724 28.422 0.136 3.218 11.547 0.14 70072. 0.3400
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12.53 0.3902 0.6117 0.0648 0.0413 0.037 1.174 0.682 27.768 0.133 3.033 11.139 0.14 70204. 0.3184
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13.36 0.4162 0.6286 0.0607 0.0402 0.036 1.141 0.639 27.000 0.129 2.841 10.731 0.14 70342. 0.2969
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14.20 0.4422 0.6424 0.0565 0.0389 0.035 1.104 0.594 26.116 0.125 2.644 10.322 0.14 70486. 0.2755
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15.03 0.4682 0.6529 0.0521 0.0374 0.034 1.061 0.549 25.117 0.120 2.440 9.908 0.14 70637. 0.2541
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15.87 0.4942 0.6597 0.0477 0.0357 0.032 1.014 0.502 24.002 0.115 2.232 9.485 0.14 70794. 0.2326
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16.70 0.5202 0.6624 0.0432 0.0339 0.031 0.962 0.454 22.771 0.109 2.020 9.046 0.14 70958. 0.2110
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17.54 0.5463 0.6601 0.0385 0.0319 0.029 0.905 0.406 21.425 0.102 1.804 8.586 0.14 71128. 0.1893
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18.37 0.5723 0.6518 0.0338 0.0297 0.027 0.844 0.356 19.963 0.095 1.584 8.093 0.14 71304. 0.1672
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19.21 0.5983 0.6360 0.0291 0.0274 0.025 0.777 0.306 18.385 0.088 1.362 7.553 0.14 71487. 0.1447
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20.04 0.6243 0.6101 0.0243 0.0249 0.022 0.705 0.256 16.694 0.080 1.137 6.944 0.14 71677. 0.1215
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20.88 0.6503 0.5703 0.0194 0.0222 0.020 0.629 0.205 14.891 0.071 0.910 6.232 0.14 71873. 0.0976
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21.71 0.6763 0.5100 0.0146 0.0193 0.017 0.549 0.153 12.980 0.062 0.682 5.358 0.14 72075. 0.0726
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22.55 0.7023 0.4170 0.0097 0.0163 0.015 0.463 0.102 10.966 0.052 0.454 4.219 0.14 72284. 0.0466
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23.38 0.7283 0.2665 0.0048 0.0132 0.012 0.374 0.051 8.856 0.042 0.226 2.600 0.14 72499. 0.0203
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24.22 0.7544 -0.0025 0.0000 0.0099 0.009 0.281 0.000 6.648 0.032 -0.002 -0.023 0.14 72715. 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 0.1057 0.0397 0.121 2.539 2.502 90.105 0.287 11.130 12.596 0.20 103280. 0.6898
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1.26 0.0261 0.0673 0.1042 0.0404 0.123 2.578 2.466 91.504 0.291 10.970 12.225 0.20 103358. 0.6646
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2.51 0.0522 0.1306 0.1025 0.0409 0.124 2.615 2.427 92.832 0.295 10.795 11.858 0.20 103444. 0.6395
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3.77 0.0783 0.1900 0.1007 0.0415 0.126 2.650 2.384 94.059 0.299 10.605 11.497 0.20 103536. 0.6145
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5.03 0.1044 0.2455 0.0987 0.0420 0.128 2.681 2.338 95.160 0.303 10.398 11.142 0.20 103637. 0.5897
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6.28 0.1304 0.2973 0.0966 0.0424 0.129 2.708 2.287 96.105 0.306 10.174 10.795 0.20 103745. 0.5652
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7.54 0.1565 0.3455 0.0943 0.0427 0.130 2.729 2.233 96.863 0.308 9.932 10.455 0.20 103862. 0.5408
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8.79 0.1826 0.3903 0.0918 0.0430 0.131 2.744 2.174 97.404 0.310 9.670 10.124 0.20 103987. 0.5167
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10.05 0.2087 0.4318 0.0892 0.0431 0.131 2.752 2.111 97.695 0.311 9.389 9.800 0.20 104121. 0.4929
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11.31 0.2348 0.4702 0.0863 0.0431 0.131 2.753 2.043 97.704 0.311 9.088 9.485 0.20 104264. 0.4693
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12.56 0.2609 0.5055 0.0832 0.0430 0.131 2.744 1.971 97.399 0.310 8.766 9.178 0.20 104416. 0.4460
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13.82 0.2870 0.5378 0.0800 0.0427 0.130 2.726 1.894 96.748 0.308 8.423 8.878 0.20 104577. 0.4229
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15.08 0.3131 0.5674 0.0765 0.0422 0.128 2.697 1.812 95.724 0.305 8.058 8.584 0.20 104747. 0.4000
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16.33 0.3392 0.5941 0.0729 0.0416 0.126 2.657 1.725 94.310 0.300 7.674 8.298 0.20 104927. 0.3773
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17.59 0.3653 0.6181 0.0690 0.0408 0.124 2.606 1.635 92.498 0.294 7.271 8.016 0.20 105116. 0.3548
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18.84 0.3913 0.6393 0.0651 0.0398 0.121 2.544 1.540 90.286 0.287 6.852 7.739 0.20 105314. 0.3325
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20.10 0.4174 0.6577 0.0609 0.0387 0.118 2.470 1.443 87.674 0.279 6.417 7.464 0.20 105522. 0.3103
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21.36 0.4435 0.6732 0.0567 0.0373 0.114 2.385 1.342 84.661 0.269 5.970 7.190 0.20 105740. 0.2883
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22.61 0.4696 0.6855 0.0523 0.0358 0.109 2.289 1.239 81.246 0.259 5.510 6.915 0.20 105967. 0.2664
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23.87 0.4957 0.6944 0.0478 0.0342 0.104 2.181 1.133 77.428 0.246 5.039 6.636 0.20 106204. 0.2445
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25.13 0.5218 0.6994 0.0433 0.0323 0.098 2.063 1.025 73.206 0.233 4.558 6.349 0.20 106451. 0.2225
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26.38 0.5479 0.6998 0.0386 0.0302 0.092 1.932 0.915 68.578 0.218 4.069 6.050 0.20 106708. 0.2003
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27.64 0.5740 0.6945 0.0339 0.0280 0.085 1.790 0.803 63.546 0.202 3.572 5.732 0.21 106974. 0.1778
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28.90 0.6001 0.6821 0.0291 0.0256 0.078 1.637 0.690 58.110 0.185 3.068 5.384 0.21 107250. 0.1548
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30.15 0.6261 0.6600 0.0243 0.0231 0.070 1.473 0.575 52.277 0.166 2.560 4.993 0.21 107536. 0.1311
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31.41 0.6522 0.6241 0.0194 0.0203 0.062 1.298 0.460 46.054 0.147 2.047 4.532 0.21 107831. 0.1064
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32.66 0.6783 0.5670 0.0145 0.0174 0.053 1.112 0.344 39.455 0.126 1.532 3.959 0.21 108137. 0.0804
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33.92 0.7044 0.4742 0.0096 0.0143 0.044 0.916 0.228 32.496 0.103 1.016 3.189 0.21 108452. 0.0528
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35.18 0.7305 0.3131 0.0048 0.0111 0.034 0.710 0.113 25.201 0.080 0.502 2.030 0.21 108775. 0.0236
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36.43 0.7566 -0.0113 -0.0001 0.0077 0.024 0.494 -0.003 17.549 0.056 -0.012 -0.071 0.21 109096. 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 0.1062 0.0389 0.280 4.413 4.469 208.821 0.499 19.880 9.708 0.27 137702. 0.7105
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1.68 0.0261 0.0692 0.1047 0.0395 0.285 4.485 4.406 212.229 0.507 19.596 9.416 0.27 137806. 0.6841
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3.35 0.0522 0.1341 0.1030 0.0401 0.289 4.553 4.336 215.467 0.514 19.287 9.128 0.27 137920. 0.6579
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5.03 0.0783 0.1949 0.1012 0.0407 0.293 4.616 4.260 218.468 0.522 18.949 8.845 0.27 138044. 0.6319
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6.70 0.1044 0.2518 0.0992 0.0412 0.297 4.673 4.178 221.167 0.528 18.582 8.567 0.27 138178. 0.6062
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8.38 0.1305 0.3048 0.0971 0.0416 0.300 4.723 4.088 223.494 0.534 18.184 8.297 0.27 138323. 0.5807
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10.06 0.1566 0.3541 0.0948 0.0419 0.302 4.762 3.991 225.376 0.538 17.753 8.032 0.27 138479. 0.5555
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11.73 0.1827 0.3999 0.0923 0.0422 0.304 4.791 3.887 226.737 0.541 17.288 7.775 0.27 138646. 0.5306
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13.41 0.2088 0.4423 0.0897 0.0423 0.305 4.807 3.774 227.500 0.543 16.788 7.525 0.27 138825. 0.5061
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15.08 0.2349 0.4815 0.0868 0.0424 0.305 4.809 3.654 227.586 0.543 16.251 7.282 0.27 139016. 0.4818
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16.76 0.2610 0.5176 0.0837 0.0422 0.304 4.795 3.525 226.917 0.542 15.677 7.045 0.27 139219. 0.4578
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18.44 0.2871 0.5508 0.0805 0.0419 0.302 4.763 3.387 225.420 0.538 15.065 6.815 0.27 139434. 0.4342
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20.11 0.3132 0.5811 0.0770 0.0415 0.299 4.713 3.241 223.029 0.532 14.415 6.591 0.27 139662. 0.4107
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21.79 0.3393 0.6087 0.0733 0.0409 0.295 4.642 3.087 219.697 0.524 13.729 6.372 0.27 139902. 0.3876
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23.46 0.3654 0.6335 0.0695 0.0401 0.289 4.552 2.925 215.406 0.514 13.010 6.159 0.27 140154. 0.3646
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25.14 0.3915 0.6557 0.0655 0.0391 0.282 4.441 2.757 210.152 0.502 12.261 5.950 0.27 140419. 0.3419
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26.81 0.4176 0.6751 0.0613 0.0379 0.273 4.309 2.582 203.931 0.487 11.486 5.743 0.27 140697. 0.3195
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28.49 0.4437 0.6918 0.0571 0.0366 0.264 4.157 2.402 196.743 0.470 10.686 5.538 0.27 140988. 0.2972
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30.17 0.4698 0.7054 0.0527 0.0351 0.253 3.985 2.218 188.584 0.450 9.864 5.334 0.27 141291. 0.2750
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31.84 0.4959 0.7158 0.0482 0.0334 0.241 3.792 2.029 179.450 0.428 9.023 5.127 0.27 141608. 0.2528
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33.52 0.5220 0.7225 0.0436 0.0315 0.227 3.578 1.836 169.338 0.404 8.165 4.917 0.27 141937. 0.2306
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35.19 0.5482 0.7249 0.0389 0.0294 0.212 3.344 1.639 158.244 0.378 7.291 4.698 0.27 142280. 0.2082
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36.87 0.5743 0.7220 0.0342 0.0272 0.196 3.089 1.440 146.171 0.349 6.403 4.467 0.27 142635. 0.1855
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38.55 0.6004 0.7124 0.0294 0.0248 0.179 2.813 1.237 133.123 0.318 5.504 4.216 0.27 143004. 0.1623
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40.22 0.6265 0.6937 0.0245 0.0222 0.160 2.517 1.033 119.112 0.284 4.595 3.934 0.27 143385. 0.1384
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41.90 0.6526 0.6617 0.0197 0.0194 0.140 2.201 0.827 104.158 0.249 3.680 3.603 0.27 143780. 0.1134
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43.57 0.6787 0.6089 0.0147 0.0164 0.118 1.866 0.620 88.292 0.211 2.760 3.188 0.28 144187. 0.0869
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45.25 0.7048 0.5199 0.0098 0.0133 0.096 1.512 0.413 71.556 0.171 1.839 2.621 0.28 144608. 0.0583
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46.93 0.7309 0.3576 0.0049 0.0100 0.072 1.141 0.207 54.007 0.129 0.921 1.738 0.28 145040. 0.0274
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48.60 0.7570 0.0015 0.0000 0.0066 0.048 0.752 0.001 35.585 0.085 0.002 0.007 0.28 145467. 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 0.1068 0.0384 0.541 6.816 7.023 403.221 0.770 31.238 7.900 0.34 172119. 0.7247
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2.11 0.0263 0.0708 0.1053 0.0391 0.550 6.932 6.923 410.079 0.783 30.795 7.657 0.34 172251. 0.6975
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4.22 0.0526 0.1372 0.1036 0.0397 0.559 7.042 6.814 416.596 0.796 30.309 7.419 0.34 172395. 0.6704
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6.33 0.0789 0.1994 0.1018 0.0403 0.567 7.145 6.695 422.641 0.807 29.779 7.185 0.34 172551. 0.6435
|
|
8.44 0.1051 0.2573 0.0998 0.0408 0.574 7.236 6.565 428.078 0.818 29.201 6.956 0.34 172720. 0.6170
|
|
10.55 0.1314 0.3114 0.0977 0.0412 0.580 7.316 6.424 432.768 0.827 28.574 6.733 0.34 172904. 0.5907
|
|
12.66 0.1577 0.3616 0.0954 0.0416 0.585 7.380 6.271 436.560 0.834 27.894 6.516 0.34 173101. 0.5648
|
|
14.77 0.1840 0.4082 0.0928 0.0419 0.589 7.426 6.106 439.302 0.839 27.160 6.304 0.34 173312. 0.5393
|
|
16.88 0.2103 0.4513 0.0901 0.0420 0.591 7.452 5.928 440.837 0.842 26.369 6.099 0.34 173539. 0.5141
|
|
18.99 0.2366 0.4912 0.0872 0.0420 0.591 7.455 5.737 441.006 0.842 25.519 5.901 0.34 173780. 0.4892
|
|
21.10 0.2629 0.5279 0.0841 0.0419 0.590 7.432 5.533 439.653 0.840 24.609 5.708 0.34 174037. 0.4647
|
|
23.21 0.2892 0.5617 0.0808 0.0416 0.586 7.381 5.314 436.628 0.834 23.638 5.521 0.34 174310. 0.4405
|
|
25.32 0.3154 0.5925 0.0773 0.0411 0.579 7.299 5.082 431.799 0.825 22.607 5.339 0.34 174598. 0.4166
|
|
27.43 0.3417 0.6207 0.0736 0.0405 0.570 7.186 4.838 425.077 0.812 21.518 5.162 0.34 174902. 0.3930
|
|
29.54 0.3680 0.6461 0.0697 0.0397 0.558 7.039 4.581 416.426 0.795 20.376 4.990 0.34 175221. 0.3697
|
|
31.65 0.3943 0.6689 0.0656 0.0387 0.544 6.860 4.314 405.836 0.775 19.187 4.821 0.34 175557. 0.3466
|
|
33.76 0.4206 0.6889 0.0614 0.0375 0.527 6.649 4.037 393.303 0.751 17.956 4.655 0.34 175909. 0.3238
|
|
35.87 0.4469 0.7062 0.0570 0.0361 0.508 6.404 3.751 378.821 0.723 16.686 4.492 0.34 176277. 0.3011
|
|
37.98 0.4732 0.7206 0.0526 0.0345 0.486 6.126 3.458 362.385 0.692 15.382 4.328 0.34 176662. 0.2786
|
|
40.09 0.4995 0.7318 0.0480 0.0328 0.461 5.815 3.158 343.985 0.657 14.047 4.164 0.34 177063. 0.2562
|
|
42.19 0.5257 0.7394 0.0434 0.0308 0.434 5.471 2.852 323.614 0.618 12.684 3.997 0.34 177480. 0.2336
|
|
44.30 0.5520 0.7427 0.0386 0.0287 0.404 5.093 2.540 301.268 0.575 11.298 3.824 0.34 177914. 0.2110
|
|
46.41 0.5783 0.7409 0.0338 0.0264 0.371 4.682 2.223 276.949 0.529 9.889 3.641 0.34 178364. 0.1879
|
|
48.52 0.6046 0.7324 0.0289 0.0239 0.336 4.237 1.903 250.670 0.479 8.463 3.443 0.34 178830. 0.1644
|
|
50.63 0.6309 0.7145 0.0240 0.0212 0.298 3.761 1.579 222.457 0.425 7.022 3.219 0.34 179314. 0.1400
|
|
52.74 0.6572 0.6829 0.0190 0.0183 0.258 3.252 1.253 192.352 0.367 5.571 2.953 0.34 179813. 0.1144
|
|
54.85 0.6835 0.6288 0.0141 0.0153 0.215 2.712 0.925 160.422 0.306 4.114 2.615 0.34 180329. 0.0871
|
|
56.96 0.7098 0.5335 0.0091 0.0121 0.170 2.143 0.597 126.761 0.242 2.656 2.136 0.34 180862. 0.0571
|
|
59.07 0.7360 0.3472 0.0041 0.0087 0.123 1.546 0.270 91.480 0.175 1.203 1.341 0.35 181408. 0.0241
|
|
61.18 0.7623
|
|
|
|
|
|
|
|
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 0.1075 0.0383 0.931 9.775 10.182 693.877 1.104 45.289 6.656 0.40 206531. 0.7352
|
|
2.52 0.0262 0.0712 0.1060 0.0389 0.947 9.945 10.040 705.939 1.124 44.658 6.451 0.40 206688. 0.7076
|
|
5.04 0.0523 0.1380 0.1044 0.0396 0.962 10.106 9.885 717.416 1.142 43.966 6.249 0.40 206860. 0.6801
|
|
7.56 0.0785 0.2005 0.1026 0.0401 0.976 10.256 9.715 728.075 1.159 43.211 6.052 0.40 207047. 0.6530
|
|
10.08 0.1046 0.2589 0.1006 0.0407 0.989 10.392 9.529 737.684 1.174 42.387 5.859 0.40 207250. 0.6261
|
|
12.60 0.1308 0.3132 0.0985 0.0411 1.000 10.509 9.328 745.999 1.187 41.491 5.671 0.40 207468. 0.5996
|
|
15.12 0.1570 0.3637 0.0962 0.0415 1.009 10.604 9.109 752.762 1.198 40.519 5.489 0.40 207704. 0.5735
|
|
17.64 0.1831 0.4107 0.0937 0.0418 1.016 10.674 8.873 757.708 1.206 39.468 5.312 0.40 207957. 0.5477
|
|
20.16 0.2093 0.4541 0.0910 0.0419 1.020 10.714 8.619 760.567 1.210 38.335 5.140 0.40 208227. 0.5223
|
|
22.67 0.2354 0.4944 0.0881 0.0420 1.021 10.721 8.345 761.064 1.211 37.117 4.973 0.40 208515. 0.4973
|
|
25.19 0.2616 0.5315 0.0850 0.0418 1.018 10.691 8.051 758.931 1.208 35.813 4.812 0.40 208822. 0.4726
|
|
27.71 0.2878 0.5656 0.0817 0.0416 1.011 10.620 7.738 753.908 1.200 34.420 4.656 0.41 209147. 0.4483
|
|
30.23 0.3139 0.5970 0.0782 0.0411 1.000 10.506 7.406 745.762 1.187 32.940 4.504 0.41 209490. 0.4243
|
|
32.75 0.3401 0.6256 0.0745 0.0405 0.985 10.345 7.054 734.333 1.169 31.375 4.357 0.41 209853. 0.4006
|
|
35.27 0.3662 0.6516 0.0706 0.0397 0.965 10.136 6.685 719.554 1.145 29.734 4.214 0.41 210234. 0.3771
|
|
37.79 0.3924 0.6750 0.0665 0.0387 0.941 9.881 6.300 701.403 1.116 28.024 4.074 0.41 210634. 0.3540
|
|
40.31 0.4186 0.6958 0.0623 0.0375 0.912 9.577 5.902 679.875 1.082 26.251 3.937 0.41 211054. 0.3311
|
|
42.83 0.4447 0.7140 0.0580 0.0361 0.878 9.226 5.491 654.961 1.042 24.423 3.802 0.41 211493. 0.3084
|
|
45.35 0.4709 0.7293 0.0535 0.0346 0.840 8.828 5.068 626.650 0.997 22.544 3.668 0.41 211950. 0.2859
|
|
47.87 0.4970 0.7417 0.0489 0.0328 0.798 8.381 4.636 594.927 0.947 20.620 3.534 0.41 212428. 0.2634
|
|
50.39 0.5232 0.7507 0.0443 0.0309 0.751 7.886 4.194 559.779 0.891 18.656 3.399 0.41 212925. 0.2409
|
|
52.91 0.5494 0.7559 0.0395 0.0287 0.699 7.342 3.745 521.200 0.830 16.657 3.259 0.41 213441. 0.2183
|
|
55.43 0.5755 0.7563 0.0347 0.0264 0.643 6.750 3.288 479.190 0.763 14.625 3.112 0.41 213977. 0.1954
|
|
57.95 0.6017 0.7505 0.0298 0.0239 0.582 6.111 2.825 433.769 0.690 12.568 2.954 0.41 214532. 0.1719
|
|
60.47 0.6278 0.7364 0.0249 0.0212 0.516 5.423 2.358 384.978 0.613 10.488 2.778 0.41 215107. 0.1477
|
|
62.99 0.6540 0.7098 0.0199 0.0184 0.446 4.689 1.887 332.888 0.530 8.392 2.571 0.41 215702. 0.1222
|
|
65.51 0.6802 0.6631 0.0149 0.0153 0.372 3.911 1.413 277.607 0.442 6.286 2.309 0.41 216316. 0.0950
|
|
68.02 0.7063 0.5794 0.0099 0.0121 0.294 3.089 0.939 219.292 0.349 4.178 1.943 0.41 216949. 0.0652
|
|
70.54 0.7325 0.4140 0.0049 0.0087 0.212 2.228 0.467 158.138 0.252 2.076 1.339 0.41 217600. 0.0317
|
|
73.06 0.7586 -0.0115 -0.0001 0.0052 0.126 1.320 -0.007 93.680 0.149 -0.033 -0.036 0.42 218227. 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 0.1084 0.0383 1.480 13.322 13.970 1103.334 1.505 62.140 5.743 0.47 240935. 0.7431
|
|
2.95 0.0263 0.0720 0.1069 0.0390 1.506 13.560 13.778 1123.031 1.532 61.286 5.565 0.47 241119. 0.7150
|
|
5.90 0.0525 0.1394 0.1053 0.0396 1.531 13.786 13.568 1141.773 1.558 60.348 5.390 0.47 241321. 0.6872
|
|
8.85 0.0788 0.2025 0.1035 0.0402 1.554 13.997 13.337 1159.184 1.581 59.321 5.218 0.47 241541. 0.6597
|
|
11.80 0.1050 0.2613 0.1015 0.0408 1.576 14.186 13.084 1174.881 1.603 58.198 5.051 0.47 241779. 0.6325
|
|
14.75 0.1313 0.3161 0.0994 0.0413 1.594 14.350 12.809 1188.459 1.621 56.975 4.889 0.47 242036. 0.6056
|
|
17.70 0.1575 0.3671 0.0970 0.0416 1.609 14.483 12.510 1199.498 1.636 55.646 4.731 0.47 242313. 0.5792
|
|
20.65 0.1838 0.4144 0.0945 0.0419 1.619 14.581 12.187 1207.566 1.647 54.206 4.577 0.47 242610. 0.5531
|
|
23.60 0.2101 0.4583 0.0918 0.0421 1.626 14.637 11.837 1212.220 1.654 52.651 4.429 0.47 242928. 0.5275
|
|
26.55 0.2363 0.4989 0.0889 0.0421 1.627 14.647 11.461 1213.012 1.655 50.978 4.285 0.47 243268. 0.5022
|
|
29.50 0.2626 0.5363 0.0858 0.0420 1.622 14.604 11.057 1209.509 1.650 49.184 4.147 0.47 243628. 0.4773
|
|
32.45 0.2888 0.5708 0.0824 0.0417 1.611 14.505 10.626 1201.288 1.639 47.266 4.012 0.47 244011. 0.4528
|
|
35.40 0.3151 0.6025 0.0789 0.0412 1.593 14.344 10.168 1187.972 1.621 45.226 3.882 0.47 244415. 0.4285
|
|
38.35 0.3414 0.6315 0.0751 0.0406 1.568 14.119 9.683 1169.303 1.595 43.069 3.756 0.47 244841. 0.4046
|
|
41.31 0.3676 0.6579 0.0712 0.0398 1.536 13.828 9.174 1145.175 1.562 40.805 3.633 0.47 245290. 0.3810
|
|
44.26 0.3939 0.6818 0.0670 0.0387 1.496 13.470 8.643 1115.557 1.522 38.444 3.514 0.47 245761. 0.3576
|
|
47.21 0.4201 0.7031 0.0628 0.0375 1.449 13.046 8.093 1080.442 1.474 35.997 3.397 0.47 246254. 0.3346
|
|
50.16 0.4464 0.7218 0.0584 0.0361 1.394 12.555 7.525 1039.818 1.419 33.472 3.283 0.48 246770. 0.3117
|
|
53.11 0.4726 0.7377 0.0539 0.0345 1.333 11.998 6.942 993.669 1.356 30.878 3.169 0.48 247308. 0.2890
|
|
56.06 0.4989 0.7508 0.0492 0.0327 1.263 11.374 6.345 941.971 1.285 28.221 3.055 0.48 247869. 0.2664
|
|
59.01 0.5252 0.7606 0.0445 0.0307 1.186 10.682 5.735 884.704 1.207 25.508 2.940 0.48 248453. 0.2437
|
|
61.96 0.5514 0.7665 0.0397 0.0285 1.102 9.924 5.114 821.856 1.121 22.745 2.822 0.48 249060. 0.2209
|
|
64.91 0.5777 0.7679 0.0348 0.0262 1.010 9.097 4.483 753.435 1.028 19.939 2.699 0.48 249690. 0.1978
|
|
67.86 0.6039 0.7633 0.0298 0.0236 0.911 8.204 3.843 679.472 0.927 17.096 2.566 0.48 250343. 0.1741
|
|
70.81 0.6302 0.7503 0.0248 0.0208 0.805 7.245 3.197 600.037 0.819 14.222 2.417 0.48 251019. 0.1496
|
|
73.76 0.6564 0.7248 0.0198 0.0179 0.691 6.221 2.546 515.250 0.703 11.327 2.242 0.48 251718. 0.1238
|
|
76.71 0.6827 0.6787 0.0147 0.0148 0.570 5.135 1.892 425.294 0.580 8.418 2.018 0.48 252439. 0.0961
|
|
79.66 0.7090 0.5934 0.0096 0.0115 0.443 3.990 1.238 330.432 0.451 5.506 1.699 0.48 253183. 0.0654
|
|
82.61 0.7352 0.4162 0.0045 0.0080 0.310 2.789 0.585 230.985 0.315 2.603 1.149 0.48 253947. 0.0304
|
|
85.56 0.7615
|
|
|
|
|
|
|
|
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 0.1094 0.0385 2.222 17.505 18.419 1656.851 1.978 81.929 5.042 0.54 275329. 0.7491
|
|
3.36 0.0262 0.0720 0.1079 0.0392 2.262 17.824 18.173 1686.989 2.014 80.832 4.886 0.54 275540. 0.7210
|
|
6.72 0.0524 0.1395 0.1063 0.0399 2.301 18.127 17.901 1715.689 2.048 79.624 4.732 0.54 275771. 0.6931
|
|
10.09 0.0786 0.2026 0.1045 0.0405 2.337 18.409 17.603 1742.368 2.080 78.297 4.582 0.54 276021. 0.6655
|
|
13.45 0.1047 0.2616 0.1026 0.0411 2.369 18.663 17.276 1766.447 2.109 76.844 4.436 0.54 276293. 0.6383
|
|
16.81 0.1309 0.3165 0.1005 0.0416 2.397 18.884 16.919 1787.314 2.133 75.257 4.294 0.54 276587. 0.6114
|
|
20.17 0.1571 0.3675 0.0982 0.0420 2.420 19.063 16.531 1804.332 2.154 73.530 4.156 0.54 276904. 0.5849
|
|
23.54 0.1833 0.4150 0.0957 0.0423 2.436 19.195 16.110 1816.842 2.169 71.656 4.022 0.54 277243. 0.5588
|
|
26.90 0.2095 0.4590 0.0930 0.0424 2.446 19.273 15.654 1824.181 2.177 69.630 3.892 0.54 277606. 0.5331
|
|
30.26 0.2357 0.4998 0.0901 0.0425 2.448 19.289 15.163 1825.680 2.179 67.446 3.767 0.54 277993. 0.5078
|
|
33.62 0.2618 0.5375 0.0869 0.0424 2.442 19.236 14.636 1820.678 2.173 65.101 3.646 0.54 278405. 0.4829
|
|
36.99 0.2880 0.5722 0.0836 0.0421 2.425 19.108 14.072 1808.548 2.159 62.593 3.529 0.54 278841. 0.4583
|
|
40.35 0.3142 0.6042 0.0800 0.0416 2.399 18.898 13.472 1788.720 2.135 59.922 3.416 0.54 279302. 0.4340
|
|
43.71 0.3404 0.6336 0.0762 0.0410 2.361 18.603 12.836 1760.794 2.102 57.095 3.306 0.54 279788. 0.4101
|
|
47.07 0.3666 0.6604 0.0723 0.0401 2.313 18.221 12.168 1724.599 2.059 54.124 3.200 0.54 280300. 0.3864
|
|
50.44 0.3928 0.6847 0.0681 0.0391 2.253 17.751 11.471 1680.090 2.005 51.024 3.097 0.54 280837. 0.3631
|
|
53.80 0.4189 0.7066 0.0638 0.0379 2.182 17.193 10.748 1627.263 1.942 47.809 2.996 0.54 281399. 0.3400
|
|
57.16 0.4451 0.7259 0.0594 0.0364 2.100 16.546 10.002 1566.110 1.869 44.490 2.897 0.54 281987. 0.3171
|
|
60.52 0.4713 0.7426 0.0549 0.0348 2.007 15.812 9.235 1496.610 1.786 41.078 2.799 0.54 282600. 0.2944
|
|
63.88 0.4975 0.7565 0.0502 0.0330 1.903 14.989 8.449 1418.730 1.693 37.582 2.701 0.54 283239. 0.2718
|
|
67.25 0.5237 0.7674 0.0454 0.0310 1.787 14.078 7.646 1332.440 1.590 34.011 2.603 0.55 283904. 0.2492
|
|
70.61 0.5499 0.7746 0.0406 0.0288 1.660 13.077 6.829 1237.725 1.477 30.373 2.502 0.55 284595. 0.2264
|
|
73.97 0.5760 0.7775 0.0356 0.0264 1.522 11.987 5.997 1134.590 1.354 26.677 2.398 0.55 285312. 0.2033
|
|
77.33 0.6022 0.7748 0.0306 0.0238 1.372 10.809 5.155 1023.083 1.221 22.930 2.285 0.55 286055. 0.1796
|
|
80.70 0.6284 0.7644 0.0256 0.0210 1.211 9.544 4.303 903.303 1.078 19.141 2.161 0.55 286824. 0.1552
|
|
84.06 0.6546 0.7425 0.0205 0.0180 1.040 8.193 3.445 775.423 0.926 15.322 2.015 0.55 287619. 0.1295
|
|
87.42 0.6808 0.7015 0.0153 0.0149 0.858 6.759 2.582 639.713 0.764 11.483 1.830 0.55 288440. 0.1018
|
|
90.78 0.7070 0.6243 0.0102 0.0116 0.666 5.246 1.717 496.559 0.593 7.639 1.569 0.55 289286. 0.0712
|
|
94.15 0.7332 0.4621 0.0051 0.0081 0.465 3.660 0.855 346.443 0.414 3.804 1.120 0.55 290155. 0.0358
|
|
97.51 0.7593 -0.0129 -0.0001 0.0044 0.252 1.984 -0.012 187.767 0.224 -0.056 -0.030 0.55 290976. 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 0.1106 0.0389 3.196 22.384 23.567 2383.421 2.529 104.827 4.485 0.61 309712. 0.7537
|
|
3.79 0.0262 0.0721 0.1092 0.0397 3.256 22.800 23.261 2427.787 2.576 103.464 4.346 0.61 309950. 0.7255
|
|
7.57 0.0524 0.1397 0.1076 0.0404 3.312 23.197 22.922 2470.048 2.621 101.955 4.209 0.61 310210. 0.6976
|
|
11.36 0.0786 0.2029 0.1058 0.0410 3.365 23.566 22.548 2509.345 2.662 100.293 4.076 0.61 310493. 0.6699
|
|
15.14 0.1048 0.2619 0.1039 0.0416 3.413 23.899 22.137 2544.823 2.700 98.467 3.946 0.61 310801. 0.6426
|
|
18.93 0.1310 0.3169 0.1018 0.0421 3.454 24.188 21.688 2575.579 2.733 96.468 3.819 0.61 311133. 0.6157
|
|
22.71 0.1572 0.3681 0.0995 0.0425 3.488 24.424 21.197 2600.680 2.759 94.285 3.697 0.61 311490. 0.5892
|
|
26.50 0.1834 0.4157 0.0970 0.0428 3.512 24.598 20.663 2619.163 2.779 91.910 3.578 0.61 311874. 0.5631
|
|
30.28 0.2096 0.4598 0.0943 0.0430 3.527 24.700 20.085 2630.059 2.791 89.337 3.464 0.61 312285. 0.5374
|
|
34.07 0.2358 0.5008 0.0913 0.0430 3.530 24.722 19.460 2632.388 2.793 86.559 3.353 0.61 312722. 0.5120
|
|
37.85 0.2620 0.5387 0.0882 0.0429 3.520 24.654 18.788 2625.207 2.785 83.570 3.246 0.61 313187. 0.4871
|
|
41.64 0.2882 0.5737 0.0848 0.0426 3.497 24.489 18.069 2607.600 2.767 80.369 3.143 0.61 313681. 0.4625
|
|
45.42 0.3144 0.6060 0.0812 0.0421 3.458 24.218 17.301 2578.748 2.736 76.956 3.043 0.61 314202. 0.4382
|
|
49.21 0.3406 0.6357 0.0774 0.0415 3.404 23.836 16.488 2538.066 2.693 73.339 2.947 0.61 314751. 0.4142
|
|
52.99 0.3668 0.6628 0.0734 0.0406 3.333 23.340 15.633 2485.302 2.637 69.535 2.853 0.61 315329. 0.3905
|
|
56.78 0.3930 0.6876 0.0692 0.0395 3.246 22.731 14.740 2420.406 2.568 65.562 2.762 0.61 315935. 0.3671
|
|
60.57 0.4192 0.7098 0.0648 0.0383 3.143 22.008 13.813 2343.386 2.486 61.438 2.673 0.61 316570. 0.3440
|
|
64.35 0.4454 0.7297 0.0603 0.0368 3.023 21.170 12.855 2254.237 2.392 57.180 2.587 0.61 317233. 0.3210
|
|
68.14 0.4716 0.7470 0.0557 0.0352 2.887 20.219 11.870 2152.946 2.284 52.800 2.501 0.61 317926. 0.2983
|
|
71.92 0.4979 0.7616 0.0510 0.0333 2.735 19.153 10.861 2039.472 2.164 48.310 2.415 0.61 318647. 0.2756
|
|
75.71 0.5241 0.7732 0.0461 0.0313 2.566 17.973 9.830 1913.772 2.031 43.723 2.330 0.61 319397. 0.2528
|
|
79.49 0.5503 0.7814 0.0412 0.0290 2.381 16.677 8.779 1775.827 1.884 39.048 2.242 0.61 320177. 0.2300
|
|
83.28 0.5765 0.7854 0.0362 0.0266 2.180 15.267 7.710 1625.648 1.725 34.295 2.151 0.62 320985. 0.2068
|
|
87.06 0.6027 0.7840 0.0311 0.0239 1.962 13.742 6.627 1463.302 1.553 29.476 2.054 0.62 321823. 0.1830
|
|
90.85 0.6289 0.7752 0.0260 0.0211 1.728 12.105 5.531 1288.935 1.368 24.603 1.946 0.62 322690. 0.1585
|
|
94.63 0.6551 0.7553 0.0208 0.0180 1.479 10.357 4.426 1102.799 1.170 19.688 1.821 0.62 323586. 0.1326
|
|
98.42 0.6813 0.7167 0.0156 0.0148 1.214 8.502 3.316 905.288 0.961 14.748 1.661 0.62 324511. 0.1047
|
|
102.20 0.7075 0.6423 0.0103 0.0114 0.935 6.545 2.203 696.965 0.740 9.798 1.434 0.62 325464. 0.0737
|
|
105.99 0.7337 0.4812 0.0051 0.0078 0.642 4.494 1.093 478.540 0.508 4.860 1.036 0.62 326444. 0.0375
|
|
109.77 0.7599 -0.0255 -0.0001 0.0040 0.331 2.318 -0.029 246.866 0.262 -0.128 -0.053 0.62 327347. 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 0.1120 0.0396 4.454 28.075 29.461 3321.585 3.172 131.044 4.023 0.67 344081. 0.7559
|
|
4.21 0.0262 0.0720 0.1106 0.0403 4.538 28.601 29.093 3383.880 3.231 129.404 3.900 0.67 344346. 0.7281
|
|
8.42 0.0525 0.1395 0.1090 0.0410 4.618 29.104 28.682 3443.359 3.288 127.579 3.778 0.67 344636. 0.7004
|
|
12.63 0.0787 0.2027 0.1073 0.0417 4.692 29.573 28.228 3498.796 3.341 125.559 3.659 0.67 344952. 0.6730
|
|
16.84 0.1049 0.2617 0.1054 0.0423 4.759 29.997 27.727 3548.967 3.389 123.328 3.544 0.67 345295. 0.6459
|
|
21.05 0.1312 0.3167 0.1033 0.0428 4.818 30.365 27.175 3592.573 3.431 120.875 3.431 0.67 345666. 0.6191
|
|
25.27 0.1574 0.3679 0.1010 0.0432 4.866 30.667 26.571 3628.255 3.465 118.188 3.322 0.67 346066. 0.5927
|
|
29.48 0.1836 0.4156 0.0985 0.0435 4.901 30.890 25.912 3654.613 3.490 115.256 3.216 0.67 346495. 0.5667
|
|
33.69 0.2099 0.4598 0.0958 0.0437 4.922 31.022 25.195 3670.226 3.505 112.068 3.114 0.67 346953. 0.5410
|
|
37.90 0.2361 0.5009 0.0928 0.0438 4.927 31.051 24.419 3673.691 3.508 108.618 3.015 0.67 347443. 0.5157
|
|
42.11 0.2623 0.5390 0.0896 0.0436 4.913 30.966 23.583 3663.647 3.499 104.898 2.920 0.67 347963. 0.4908
|
|
46.32 0.2886 0.5742 0.0862 0.0433 4.880 30.756 22.686 3638.817 3.475 100.906 2.828 0.68 348514. 0.4662
|
|
50.53 0.3148 0.6067 0.0826 0.0429 4.825 30.412 21.727 3598.064 3.436 96.643 2.739 0.68 349097. 0.4419
|
|
54.74 0.3410 0.6367 0.0787 0.0422 4.748 29.926 20.710 3540.564 3.381 92.119 2.653 0.68 349711. 0.4180
|
|
58.95 0.3673 0.6642 0.0747 0.0413 4.648 29.295 19.639 3465.974 3.310 87.354 2.570 0.68 350356. 0.3943
|
|
63.16 0.3935 0.6893 0.0704 0.0402 4.525 28.520 18.519 3374.243 3.222 82.373 2.489 0.68 351033. 0.3708
|
|
67.37 0.4197 0.7121 0.0660 0.0389 4.379 27.600 17.356 3265.401 3.118 77.200 2.411 0.68 351742. 0.3477
|
|
71.59 0.4460 0.7324 0.0614 0.0374 4.210 26.536 16.154 3139.477 2.998 71.853 2.334 0.68 352483. 0.3247
|
|
75.80 0.4722 0.7503 0.0567 0.0357 4.018 25.327 14.917 2996.465 2.861 66.351 2.258 0.68 353256. 0.3019
|
|
80.01 0.4984 0.7655 0.0519 0.0338 3.804 23.973 13.649 2836.327 2.708 60.709 2.183 0.68 354061. 0.2791
|
|
84.22 0.5247 0.7779 0.0470 0.0317 3.566 22.475 12.352 2659.009 2.539 54.941 2.107 0.68 354898. 0.2563
|
|
88.43 0.5509 0.7870 0.0419 0.0294 3.305 20.830 11.030 2464.481 2.353 49.060 2.030 0.68 355767. 0.2334
|
|
92.64 0.5771 0.7920 0.0368 0.0268 3.021 19.041 9.685 2252.763 2.151 43.080 1.950 0.68 356669. 0.2101
|
|
96.85 0.6034 0.7918 0.0316 0.0241 2.714 17.107 8.322 2023.957 1.933 37.014 1.865 0.68 357603. 0.1862
|
|
101.06 0.6296 0.7845 0.0264 0.0212 2.385 15.030 6.942 1778.269 1.698 30.877 1.771 0.69 358569. 0.1615
|
|
105.27 0.6558 0.7663 0.0211 0.0181 2.033 12.814 5.550 1516.057 1.448 24.685 1.660 0.69 359568. 0.1354
|
|
109.48 0.6821 0.7298 0.0158 0.0147 1.660 10.463 4.150 1237.875 1.182 18.459 1.521 0.69 360598. 0.1072
|
|
113.69 0.7083 0.6576 0.0104 0.0112 1.267 7.983 2.747 944.524 0.902 12.220 1.319 0.69 361660. 0.0757
|
|
117.91 0.7345 0.4959 0.0051 0.0076 0.854 5.384 1.347 637.035 0.608 5.993 0.959 0.69 362751. 0.0385
|
|
122.12 0.7608 -0.0692 -0.0003 0.0036 0.411 2.588 -0.087 306.197 0.292 -0.388 -0.129 0.69 363641. 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 0.1136 0.0410 6.149 35.235 36.151 4585.595 3.981 160.801 3.576 0.74 378432. 0.7442
|
|
4.64 0.0263 0.0706 0.1122 0.0417 6.254 35.836 35.723 4663.789 4.049 158.894 3.474 0.74 378724. 0.7188
|
|
9.28 0.0525 0.1372 0.1107 0.0424 6.354 36.406 35.242 4738.028 4.113 156.757 3.374 0.74 379044. 0.6933
|
|
13.92 0.0788 0.1998 0.1090 0.0430 6.446 36.935 34.706 4806.788 4.173 154.373 3.275 0.74 379393. 0.6679
|
|
18.55 0.1051 0.2585 0.1072 0.0436 6.529 37.409 34.111 4868.527 4.226 151.724 3.178 0.74 379772. 0.6425
|
|
23.19 0.1314 0.3135 0.1051 0.0440 6.600 37.817 33.452 4921.599 4.273 148.793 3.083 0.74 380182. 0.6172
|
|
27.83 0.1576 0.3648 0.1028 0.0444 6.657 38.145 32.726 4964.312 4.310 145.566 2.990 0.74 380625. 0.5921
|
|
32.47 0.1839 0.4127 0.1003 0.0447 6.698 38.380 31.931 4994.860 4.336 142.027 2.900 0.74 381100. 0.5672
|
|
37.11 0.2102 0.4574 0.0976 0.0448 6.720 38.507 31.062 5011.383 4.350 138.166 2.811 0.74 381609. 0.5424
|
|
41.75 0.2364 0.4989 0.0946 0.0448 6.721 38.511 30.119 5011.975 4.351 133.970 2.726 0.74 382151. 0.5178
|
|
46.39 0.2627 0.5374 0.0914 0.0447 6.698 38.379 29.099 4994.743 4.336 129.433 2.642 0.74 382727. 0.4934
|
|
51.03 0.2890 0.5730 0.0880 0.0444 6.649 38.096 28.002 4957.900 4.304 124.551 2.562 0.74 383338. 0.4692
|
|
55.66 0.3153 0.6060 0.0843 0.0438 6.571 37.649 26.827 4899.777 4.254 119.325 2.483 0.74 383984. 0.4452
|
|
60.30 0.3415 0.6364 0.0804 0.0431 6.463 37.030 25.577 4819.134 4.184 113.767 2.407 0.74 384664. 0.4214
|
|
64.94 0.3678 0.6643 0.0762 0.0422 6.323 36.232 24.259 4715.373 4.093 107.905 2.333 0.74 385379. 0.3979
|
|
69.58 0.3941 0.6899 0.0719 0.0411 6.153 35.256 22.880 4588.320 3.983 101.768 2.262 0.75 386128. 0.3745
|
|
74.22 0.4203 0.7131 0.0674 0.0397 5.951 34.100 21.445 4437.940 3.853 95.387 2.192 0.75 386913. 0.3513
|
|
78.86 0.4466 0.7340 0.0627 0.0382 5.718 32.766 19.961 4264.214 3.702 88.787 2.123 0.75 387733. 0.3284
|
|
83.50 0.4729 0.7525 0.0579 0.0364 5.454 31.251 18.433 4067.094 3.531 81.990 2.056 0.75 388588. 0.3055
|
|
88.13 0.4992 0.7684 0.0530 0.0344 5.158 29.556 16.865 3846.538 3.339 75.017 1.989 0.75 389478. 0.2827
|
|
92.77 0.5254 0.7815 0.0479 0.0322 4.831 27.681 15.262 3602.488 3.127 67.884 1.922 0.75 390403. 0.2599
|
|
97.41 0.5517 0.7914 0.0428 0.0298 4.472 25.625 13.626 3334.902 2.895 60.608 1.853 0.75 391364. 0.2368
|
|
102.05 0.5780 0.7974 0.0376 0.0272 4.082 23.388 11.962 3043.810 2.642 53.205 1.782 0.75 392360. 0.2134
|
|
106.69 0.6042 0.7984 0.0323 0.0244 3.660 20.973 10.273 2729.424 2.369 45.692 1.707 0.75 393392. 0.1894
|
|
111.33 0.6305 0.7924 0.0269 0.0214 3.208 18.381 8.563 2392.190 2.077 38.087 1.624 0.75 394459. 0.1645
|
|
115.97 0.6568 0.7755 0.0215 0.0182 2.726 15.620 6.837 2032.894 1.765 30.410 1.525 0.76 395561. 0.1381
|
|
120.61 0.6831 0.7400 0.0160 0.0148 2.216 12.700 5.100 1652.751 1.435 22.685 1.400 0.76 396699. 0.1094
|
|
125.24 0.7093 0.6673 0.0106 0.0112 1.681 9.632 3.359 1253.479 1.088 14.940 1.215 0.76 397871. 0.0771
|
|
129.88 0.7356 0.4996 0.0051 0.0075 1.123 6.433 1.620 837.236 0.727 7.205 0.877 0.76 399074. 0.0387
|
|
134.52 0.7619
|
|
|
|
|
|
|
|
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 0.1153 0.0448 8.721 45.806 43.673 6503.312 5.175 194.259 3.046 0.81 412761. 0.6968
|
|
5.05 0.0262 0.0658 0.1140 0.0454 8.834 46.397 43.197 6587.217 5.242 192.140 2.974 0.81 413078. 0.6767
|
|
10.10 0.0524 0.1285 0.1126 0.0459 8.936 46.937 42.657 6663.840 5.303 189.740 2.903 0.81 413425. 0.6564
|
|
15.15 0.0786 0.1881 0.1110 0.0464 9.027 47.412 42.049 6731.345 5.357 187.035 2.833 0.81 413805. 0.6360
|
|
20.20 0.1048 0.2447 0.1092 0.0468 9.103 47.812 41.367 6788.014 5.402 184.002 2.764 0.81 414219. 0.6154
|
|
25.24 0.1311 0.2983 0.1072 0.0471 9.162 48.122 40.607 6832.098 5.437 180.618 2.696 0.81 414667. 0.5947
|
|
30.29 0.1573 0.3491 0.1050 0.0473 9.202 48.331 39.762 6861.685 5.460 176.862 2.628 0.81 415150. 0.5737
|
|
35.34 0.1835 0.3969 0.1025 0.0474 9.220 48.425 38.830 6875.059 5.471 172.718 2.562 0.81 415670. 0.5526
|
|
40.39 0.2097 0.4420 0.0998 0.0474 9.213 48.391 37.808 6870.330 5.467 168.170 2.496 0.81 416226. 0.5313
|
|
45.44 0.2359 0.4843 0.0969 0.0472 9.180 48.217 36.692 6845.498 5.447 163.205 2.431 0.81 416819. 0.5098
|
|
50.49 0.2621 0.5239 0.0937 0.0469 9.117 47.885 35.480 6798.458 5.410 157.813 2.367 0.81 417450. 0.4881
|
|
55.54 0.2883 0.5609 0.0902 0.0464 9.021 47.383 34.170 6727.126 5.353 151.990 2.304 0.81 418118. 0.4662
|
|
60.59 0.3145 0.5954 0.0865 0.0457 8.890 46.696 32.764 6629.583 5.276 145.736 2.242 0.81 418824. 0.4442
|
|
65.64 0.3408 0.6273 0.0825 0.0448 8.722 45.814 31.265 6504.334 5.176 139.065 2.180 0.81 419567. 0.4220
|
|
70.68 0.3670 0.6568 0.0783 0.0438 8.516 44.731 29.678 6350.651 5.054 132.009 2.120 0.81 420348. 0.3997
|
|
75.73 0.3932 0.6839 0.0739 0.0425 8.272 43.447 28.014 6168.335 4.909 124.607 2.060 0.81 421167. 0.3774
|
|
80.78 0.4194 0.7086 0.0694 0.0411 7.989 41.960 26.280 5957.261 4.741 116.895 2.001 0.81 422024. 0.3551
|
|
85.83 0.4456 0.7309 0.0646 0.0394 7.667 40.270 24.485 5717.285 4.550 108.907 1.942 0.81 422919. 0.3327
|
|
90.88 0.4718 0.7507 0.0597 0.0375 7.306 38.374 22.633 5448.123 4.335 100.671 1.884 0.82 423851. 0.3103
|
|
95.93 0.4980 0.7679 0.0547 0.0355 6.905 36.270 20.731 5149.420 4.098 92.212 1.826 0.82 424822. 0.2878
|
|
100.98 0.5242 0.7824 0.0496 0.0332 6.465 33.956 18.784 4820.896 3.836 83.552 1.767 0.82 425831. 0.2652
|
|
106.03 0.5505 0.7933 0.0443 0.0308 5.986 31.443 16.796 4464.107 3.552 74.710 1.707 0.82 426878. 0.2421
|
|
111.08 0.5767 0.7999 0.0390 0.0281 5.470 28.730 14.772 4078.927 3.246 65.705 1.643 0.82 427963. 0.2185
|
|
116.13 0.6029 0.8010 0.0336 0.0253 4.915 25.817 12.715 3665.398 2.917 56.556 1.573 0.82 429086. 0.1942
|
|
121.17 0.6291 0.7943 0.0281 0.0222 4.325 22.715 10.631 3224.930 2.566 47.285 1.495 0.82 430247. 0.1687
|
|
126.22 0.6553 0.7752 0.0225 0.0190 3.701 19.438 8.524 2759.710 2.196 37.914 1.401 0.82 431447. 0.1416
|
|
131.27 0.6815 0.7352 0.0169 0.0157 3.048 16.007 6.401 2272.571 1.808 28.472 1.278 0.83 432684. 0.1119
|
|
136.32 0.7077 0.6550 0.0113 0.0122 2.370 12.446 4.269 1766.944 1.406 18.991 1.096 0.83 433959. 0.0784
|
|
141.37 0.7339 0.4818 0.0056 0.0086 1.672 8.783 2.137 1246.988 0.992 9.506 0.777 0.83 435268. 0.0393
|
|
146.42 0.7602 -0.0078 0.0000 0.0049 0.946 4.970 -0.019 705.642 0.562 -0.084 -0.012 0.83 436489. 0.0000
|
|
|
|
|
|
|