538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x10E (17x10E.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 0.0926 0.0376 0.004 0.267 0.244 3.161 0.030 1.083 34.943 0.07 26771. 0.5969
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0.41 0.0253 0.0606 0.0913 0.0381 0.004 0.271 0.240 3.201 0.031 1.068 34.036 0.07 26789. 0.5774
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0.81 0.0506 0.1181 0.0899 0.0386 0.004 0.274 0.237 3.239 0.031 1.052 33.128 0.07 26809. 0.5578
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1.22 0.0760 0.1722 0.0884 0.0390 0.004 0.277 0.233 3.275 0.031 1.035 32.222 0.07 26830. 0.5380
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1.63 0.1013 0.2232 0.0868 0.0394 0.004 0.280 0.228 3.308 0.032 1.016 31.321 0.07 26854. 0.5182
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2.03 0.1266 0.2711 0.0851 0.0397 0.004 0.282 0.224 3.336 0.032 0.995 30.428 0.07 26879. 0.4983
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2.44 0.1519 0.3158 0.0832 0.0400 0.005 0.284 0.219 3.359 0.032 0.973 29.544 0.07 26907. 0.4784
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2.85 0.1772 0.3576 0.0811 0.0402 0.005 0.285 0.213 3.375 0.032 0.949 28.670 0.07 26936. 0.4584
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3.25 0.2026 0.3964 0.0789 0.0403 0.005 0.286 0.208 3.385 0.032 0.923 27.808 0.07 26968. 0.4385
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3.66 0.2279 0.4323 0.0765 0.0403 0.005 0.286 0.201 3.386 0.032 0.895 26.957 0.07 27002. 0.4186
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4.06 0.2532 0.4653 0.0739 0.0402 0.005 0.285 0.194 3.378 0.032 0.865 26.117 0.07 27038. 0.3987
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4.47 0.2785 0.4956 0.0712 0.0400 0.005 0.284 0.187 3.359 0.032 0.833 25.286 0.07 27077. 0.3788
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4.88 0.3038 0.5230 0.0683 0.0397 0.004 0.281 0.180 3.330 0.032 0.799 24.463 0.07 27118. 0.3589
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5.28 0.3292 0.5476 0.0652 0.0392 0.004 0.278 0.171 3.289 0.031 0.762 23.643 0.07 27161. 0.3389
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5.69 0.3545 0.5693 0.0619 0.0385 0.004 0.273 0.163 3.235 0.031 0.724 22.823 0.07 27207. 0.3188
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6.10 0.3798 0.5879 0.0584 0.0377 0.004 0.268 0.154 3.168 0.030 0.683 21.998 0.07 27255. 0.2985
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6.50 0.4051 0.6032 0.0548 0.0368 0.004 0.261 0.144 3.088 0.029 0.641 21.160 0.07 27305. 0.2780
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6.91 0.4304 0.6150 0.0510 0.0357 0.004 0.253 0.134 2.995 0.029 0.596 20.304 0.07 27358. 0.2573
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7.32 0.4558 0.6228 0.0470 0.0344 0.004 0.244 0.124 2.889 0.028 0.550 19.419 0.07 27413. 0.2364
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7.72 0.4811 0.6261 0.0430 0.0330 0.004 0.234 0.113 2.771 0.026 0.503 18.494 0.07 27471. 0.2152
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8.13 0.5064 0.6242 0.0388 0.0315 0.004 0.223 0.102 2.643 0.025 0.454 17.517 0.07 27531. 0.1937
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8.54 0.5317 0.6163 0.0346 0.0298 0.003 0.212 0.091 2.503 0.024 0.404 16.470 0.07 27593. 0.1719
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8.94 0.5570 0.6010 0.0302 0.0280 0.003 0.199 0.080 2.354 0.022 0.354 15.332 0.07 27658. 0.1497
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9.35 0.5824 0.5768 0.0259 0.0261 0.003 0.185 0.068 2.194 0.021 0.303 14.074 0.07 27726. 0.1271
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9.75 0.6077 0.5412 0.0215 0.0241 0.003 0.171 0.057 2.026 0.019 0.251 12.657 0.07 27796. 0.1042
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10.16 0.6330 0.4911 0.0171 0.0220 0.002 0.156 0.045 1.850 0.018 0.200 11.025 0.07 27868. 0.0809
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10.57 0.6583 0.4215 0.0127 0.0198 0.002 0.141 0.033 1.666 0.016 0.149 9.098 0.07 27942. 0.0576
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10.97 0.6836 0.3248 0.0083 0.0176 0.002 0.125 0.022 1.475 0.014 0.098 6.751 0.07 28020. 0.0346
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11.38 0.7090 0.1889 0.0041 0.0152 0.002 0.108 0.011 1.280 0.012 0.048 3.786 0.07 28099. 0.0135
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11.79 0.7343 -0.0075 -0.0001 0.0129 0.001 0.091 0.000 1.081 0.010 -0.002 -0.146 0.07 28180. 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 0.0929 0.0347 0.031 0.984 0.977 23.292 0.111 4.348 19.035 0.13 53540. 0.6514
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0.82 0.0254 0.0662 0.0916 0.0352 0.032 0.999 0.964 23.642 0.113 4.289 18.500 0.13 53577. 0.6289
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1.63 0.0508 0.1285 0.0903 0.0357 0.032 1.013 0.950 23.980 0.114 4.225 17.967 0.13 53617. 0.6062
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2.45 0.0762 0.1871 0.0888 0.0362 0.033 1.027 0.934 24.297 0.116 4.156 17.440 0.13 53660. 0.5835
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3.26 0.1017 0.2421 0.0872 0.0366 0.033 1.039 0.917 24.588 0.117 4.080 16.919 0.13 53708. 0.5609
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4.08 0.1271 0.2934 0.0854 0.0370 0.033 1.050 0.899 24.845 0.119 3.997 16.406 0.13 53759. 0.5384
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4.90 0.1525 0.3413 0.0835 0.0373 0.034 1.059 0.879 25.059 0.120 3.908 15.902 0.13 53814. 0.5160
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5.71 0.1779 0.3858 0.0814 0.0375 0.034 1.066 0.857 25.223 0.120 3.811 15.407 0.13 53874. 0.4937
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6.53 0.2033 0.4270 0.0792 0.0377 0.034 1.070 0.833 25.327 0.121 3.707 14.923 0.13 53938. 0.4716
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7.34 0.2287 0.4652 0.0768 0.0378 0.034 1.072 0.808 25.364 0.121 3.594 14.450 0.13 54006. 0.4496
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8.16 0.2542 0.5003 0.0742 0.0377 0.034 1.070 0.781 25.325 0.121 3.474 13.987 0.13 54079. 0.4279
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8.98 0.2796 0.5325 0.0715 0.0375 0.034 1.065 0.752 25.201 0.120 3.345 13.533 0.14 54157. 0.4062
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9.79 0.3050 0.5618 0.0685 0.0372 0.034 1.056 0.721 24.987 0.119 3.207 13.088 0.14 54239. 0.3847
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10.61 0.3304 0.5882 0.0654 0.0367 0.033 1.043 0.688 24.674 0.118 3.061 12.650 0.14 54326. 0.3632
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11.42 0.3558 0.6118 0.0621 0.0361 0.033 1.025 0.653 24.256 0.116 2.906 12.217 0.14 54418. 0.3418
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12.24 0.3812 0.6324 0.0586 0.0353 0.032 1.003 0.617 23.727 0.113 2.742 11.786 0.14 54515. 0.3204
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13.05 0.4067 0.6499 0.0549 0.0344 0.031 0.976 0.578 23.083 0.110 2.570 11.355 0.14 54616. 0.2988
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13.87 0.4321 0.6640 0.0511 0.0332 0.030 0.944 0.538 22.329 0.107 2.391 10.920 0.14 54723. 0.2772
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14.69 0.4575 0.6746 0.0471 0.0320 0.029 0.907 0.496 21.469 0.103 2.206 10.477 0.14 54834. 0.2554
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15.50 0.4829 0.6809 0.0430 0.0305 0.027 0.867 0.453 20.506 0.098 2.015 10.019 0.14 54950. 0.2334
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16.32 0.5083 0.6826 0.0389 0.0289 0.026 0.822 0.409 19.444 0.093 1.819 9.541 0.14 55071. 0.2112
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17.13 0.5337 0.6785 0.0346 0.0272 0.025 0.773 0.364 18.289 0.087 1.620 9.033 0.14 55197. 0.1887
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17.95 0.5591 0.6676 0.0303 0.0254 0.023 0.720 0.319 17.042 0.081 1.418 8.484 0.14 55328. 0.1658
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18.77 0.5846 0.6480 0.0259 0.0234 0.021 0.664 0.273 15.710 0.075 1.214 7.877 0.14 55463. 0.1424
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19.58 0.6100 0.6171 0.0215 0.0213 0.019 0.604 0.227 14.298 0.068 1.008 7.189 0.14 55604. 0.1185
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20.40 0.6354 0.5709 0.0171 0.0191 0.017 0.541 0.180 12.812 0.061 0.802 6.385 0.14 55749. 0.0939
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21.21 0.6608 0.5030 0.0128 0.0168 0.015 0.476 0.134 11.260 0.054 0.597 5.409 0.14 55900. 0.0686
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22.03 0.6862 0.4024 0.0084 0.0144 0.013 0.408 0.089 9.652 0.046 0.394 4.167 0.14 56055. 0.0429
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22.85 0.7116 0.2489 0.0042 0.0119 0.011 0.338 0.044 7.999 0.038 0.195 2.485 0.14 56215. 0.0180
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23.66 0.7371 0.0002 0.0000 0.0094 0.008 0.267 0.000 6.312 0.030 0.000 0.002 0.14 56379. 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 0.0932 0.0334 0.102 2.136 2.207 75.816 0.241 9.816 13.202 0.20 80309. 0.6789
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1.23 0.0255 0.0689 0.0920 0.0340 0.103 2.171 2.177 77.047 0.245 9.684 12.817 0.20 80364. 0.6547
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2.45 0.0510 0.1338 0.0906 0.0345 0.105 2.204 2.145 78.235 0.249 9.541 12.435 0.20 80424. 0.6304
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3.68 0.0764 0.1946 0.0891 0.0350 0.106 2.236 2.110 79.357 0.253 9.384 12.058 0.20 80490. 0.6063
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4.91 0.1019 0.2514 0.0875 0.0355 0.108 2.265 2.071 80.389 0.256 9.213 11.686 0.20 80561. 0.5822
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6.13 0.1274 0.3045 0.0857 0.0359 0.109 2.291 2.029 81.306 0.259 9.027 11.322 0.20 80638. 0.5583
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7.36 0.1529 0.3538 0.0838 0.0362 0.110 2.312 1.984 82.078 0.261 8.825 10.964 0.20 80722. 0.5346
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8.59 0.1783 0.3997 0.0817 0.0365 0.111 2.329 1.935 82.678 0.263 8.607 10.616 0.20 80811. 0.5112
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9.81 0.2038 0.4421 0.0795 0.0366 0.111 2.341 1.882 83.076 0.264 8.371 10.275 0.20 80908. 0.4880
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11.04 0.2293 0.4813 0.0771 0.0367 0.112 2.345 1.825 83.242 0.265 8.117 9.944 0.20 81011. 0.4650
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12.27 0.2548 0.5174 0.0745 0.0367 0.111 2.343 1.764 83.145 0.265 7.845 9.621 0.20 81121. 0.4423
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13.50 0.2802 0.5506 0.0717 0.0365 0.111 2.332 1.698 82.759 0.263 7.553 9.306 0.20 81238. 0.4198
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14.72 0.3057 0.5808 0.0688 0.0362 0.110 2.312 1.628 82.058 0.261 7.242 8.999 0.20 81362. 0.3975
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15.95 0.3312 0.6082 0.0656 0.0357 0.109 2.283 1.554 81.016 0.258 6.911 8.698 0.20 81493. 0.3753
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17.18 0.3567 0.6327 0.0623 0.0351 0.107 2.243 1.475 79.613 0.253 6.560 8.403 0.20 81631. 0.3532
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18.40 0.3822 0.6543 0.0588 0.0343 0.104 2.193 1.392 77.821 0.248 6.190 8.111 0.20 81777. 0.3312
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19.63 0.4076 0.6730 0.0551 0.0334 0.101 2.131 1.304 75.633 0.241 5.800 7.820 0.20 81930. 0.3091
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20.86 0.4331 0.6884 0.0512 0.0322 0.098 2.058 1.213 73.058 0.233 5.395 7.530 0.20 82090. 0.2870
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22.08 0.4586 0.7005 0.0472 0.0309 0.094 1.975 1.118 70.111 0.223 4.975 7.235 0.20 82258. 0.2649
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23.31 0.4841 0.7086 0.0431 0.0295 0.090 1.882 1.021 66.805 0.213 4.543 6.934 0.20 82433. 0.2426
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24.54 0.5095 0.7122 0.0389 0.0279 0.085 1.779 0.922 63.152 0.201 4.100 6.621 0.20 82615. 0.2201
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25.76 0.5350 0.7105 0.0347 0.0261 0.079 1.667 0.821 59.164 0.188 3.650 6.290 0.20 82805. 0.1972
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26.99 0.5605 0.7022 0.0303 0.0242 0.074 1.546 0.718 54.857 0.175 3.193 5.935 0.20 83002. 0.1740
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28.22 0.5860 0.6856 0.0259 0.0222 0.067 1.416 0.614 50.246 0.160 2.731 5.542 0.21 83206. 0.1503
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29.44 0.6114 0.6579 0.0215 0.0200 0.061 1.278 0.510 45.350 0.144 2.267 5.097 0.21 83418. 0.1260
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30.67 0.6369 0.6148 0.0171 0.0177 0.054 1.132 0.405 40.193 0.128 1.802 4.573 0.21 83637. 0.1008
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31.90 0.6624 0.5491 0.0127 0.0154 0.047 0.981 0.301 34.804 0.111 1.340 3.927 0.21 83864. 0.0746
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33.12 0.6879 0.4476 0.0084 0.0129 0.039 0.823 0.199 29.216 0.093 0.883 3.082 0.21 84098. 0.0475
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34.35 0.7134 0.2841 0.0041 0.0104 0.031 0.661 0.098 23.471 0.075 0.434 1.887 0.21 84339. 0.0204
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35.58 0.7388 -0.0038 0.0000 0.0078 0.024 0.496 -0.001 17.603 0.056 -0.004 -0.024 0.21 84585. 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 0.0936 0.0328 0.236 3.725 3.939 176.283 0.421 17.521 10.135 0.27 107076. 0.6963
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1.65 0.0258 0.0713 0.0923 0.0334 0.240 3.789 3.886 179.307 0.428 17.286 9.830 0.27 107150. 0.6708
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3.31 0.0515 0.1382 0.0910 0.0339 0.244 3.851 3.828 182.229 0.435 17.028 9.529 0.27 107232. 0.6454
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4.96 0.0773 0.2008 0.0894 0.0344 0.248 3.909 3.765 184.991 0.442 16.746 9.231 0.27 107320. 0.6200
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6.61 0.1030 0.2592 0.0878 0.0349 0.251 3.963 3.696 187.534 0.448 16.439 8.939 0.27 107417. 0.5949
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8.27 0.1288 0.3136 0.0860 0.0353 0.255 4.010 3.621 189.793 0.453 16.104 8.652 0.27 107521. 0.5699
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9.92 0.1545 0.3642 0.0841 0.0357 0.257 4.051 3.539 191.698 0.458 15.740 8.373 0.27 107634. 0.5452
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11.58 0.1803 0.4111 0.0820 0.0359 0.259 4.082 3.450 193.179 0.461 15.346 8.100 0.27 107756. 0.5208
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13.23 0.2060 0.4544 0.0797 0.0361 0.260 4.103 3.354 194.159 0.464 14.919 7.835 0.27 107887. 0.4967
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14.88 0.2318 0.4944 0.0772 0.0362 0.261 4.111 3.251 194.565 0.464 14.459 7.578 0.27 108027. 0.4730
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16.54 0.2576 0.5313 0.0746 0.0362 0.261 4.106 3.140 194.322 0.464 13.965 7.328 0.27 108176. 0.4495
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18.19 0.2833 0.5650 0.0718 0.0360 0.259 4.086 3.020 193.362 0.462 13.435 7.085 0.27 108335. 0.4262
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19.84 0.3091 0.5958 0.0687 0.0357 0.257 4.049 2.893 191.619 0.457 12.869 6.849 0.27 108503. 0.4033
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21.50 0.3348 0.6237 0.0655 0.0352 0.253 3.994 2.758 189.035 0.451 12.268 6.618 0.27 108682. 0.3805
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23.15 0.3606 0.6487 0.0621 0.0345 0.249 3.921 2.615 185.548 0.443 11.631 6.392 0.27 108870. 0.3578
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24.81 0.3863 0.6709 0.0585 0.0337 0.243 3.827 2.463 181.100 0.432 10.957 6.170 0.27 109068. 0.3352
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26.46 0.4121 0.6901 0.0547 0.0327 0.236 3.712 2.304 175.673 0.419 10.249 5.949 0.27 109276. 0.3126
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28.11 0.4378 0.7061 0.0508 0.0315 0.227 3.577 2.139 169.296 0.404 9.512 5.729 0.27 109494. 0.2900
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29.77 0.4636 0.7187 0.0467 0.0301 0.217 3.423 1.967 162.001 0.387 8.750 5.508 0.27 109722. 0.2674
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31.42 0.4894 0.7274 0.0425 0.0286 0.206 3.250 1.791 153.818 0.367 7.966 5.281 0.27 109960. 0.2446
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33.07 0.5151 0.7317 0.0383 0.0269 0.194 3.059 1.611 144.777 0.346 7.164 5.046 0.27 110208. 0.2217
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34.73 0.5409 0.7305 0.0339 0.0251 0.181 2.851 1.427 134.911 0.322 6.348 4.798 0.27 110466. 0.1984
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36.38 0.5666 0.7227 0.0295 0.0231 0.167 2.626 1.241 124.255 0.297 5.521 4.531 0.27 110734. 0.1747
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38.03 0.5924 0.7061 0.0250 0.0210 0.151 2.385 1.054 112.851 0.269 4.687 4.235 0.27 111012. 0.1505
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39.69 0.6181 0.6778 0.0206 0.0187 0.135 2.129 0.865 100.749 0.241 3.849 3.895 0.27 111300. 0.1254
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41.34 0.6439 0.6324 0.0161 0.0164 0.118 1.860 0.677 88.011 0.210 3.011 3.489 0.27 111598. 0.0994
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43.00 0.6697 0.5609 0.0116 0.0139 0.100 1.579 0.490 74.712 0.178 2.180 2.975 0.27 111906. 0.0721
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44.65 0.6954 0.4453 0.0073 0.0113 0.082 1.288 0.306 60.946 0.145 1.360 2.275 0.28 112224. 0.0435
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46.30 0.7212 0.2458 0.0030 0.0087 0.063 0.989 0.125 46.817 0.112 0.556 1.211 0.28 112552. 0.0148
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47.96 0.7469
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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 0.0940 0.0325 0.457 5.762 6.185 340.836 0.651 27.512 8.231 0.34 133841. 0.7086
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2.05 0.0255 0.0717 0.0928 0.0330 0.465 5.863 6.104 346.811 0.662 27.150 7.983 0.34 133933. 0.6827
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4.10 0.0510 0.1389 0.0915 0.0336 0.473 5.960 6.015 352.594 0.673 26.754 7.737 0.34 134033. 0.6569
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6.14 0.0766 0.2019 0.0900 0.0341 0.480 6.053 5.917 358.074 0.684 26.320 7.495 0.34 134143. 0.6311
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8.19 0.1021 0.2607 0.0884 0.0346 0.487 6.139 5.811 363.135 0.694 25.846 7.258 0.34 134262. 0.6056
|
|
10.24 0.1276 0.3154 0.0866 0.0350 0.493 6.215 5.695 367.654 0.702 25.331 7.026 0.34 134392. 0.5804
|
|
12.29 0.1531 0.3663 0.0847 0.0354 0.498 6.280 5.569 371.496 0.710 24.770 6.799 0.34 134531. 0.5554
|
|
14.34 0.1786 0.4135 0.0826 0.0357 0.502 6.331 5.432 374.524 0.715 24.162 6.579 0.34 134681. 0.5308
|
|
16.38 0.2041 0.4571 0.0803 0.0359 0.505 6.366 5.284 376.592 0.719 23.504 6.364 0.34 134843. 0.5064
|
|
18.43 0.2297 0.4975 0.0779 0.0360 0.506 6.382 5.125 377.556 0.721 22.795 6.157 0.34 135015. 0.4825
|
|
20.48 0.2552 0.5347 0.0753 0.0359 0.506 6.378 4.953 377.275 0.721 22.032 5.955 0.34 135199. 0.4588
|
|
22.53 0.2807 0.5688 0.0725 0.0358 0.504 6.350 4.770 375.611 0.717 21.215 5.760 0.34 135395. 0.4354
|
|
24.58 0.3062 0.6001 0.0695 0.0355 0.499 6.296 4.573 372.437 0.711 20.343 5.570 0.34 135603. 0.4123
|
|
26.62 0.3317 0.6285 0.0664 0.0350 0.493 6.215 4.365 367.639 0.702 19.414 5.385 0.34 135823. 0.3894
|
|
28.67 0.3573 0.6542 0.0630 0.0344 0.484 6.104 4.144 361.100 0.690 18.430 5.205 0.34 136054. 0.3667
|
|
30.72 0.3828 0.6771 0.0594 0.0336 0.473 5.962 3.910 352.701 0.674 17.390 5.028 0.34 136298. 0.3441
|
|
32.77 0.4083 0.6972 0.0557 0.0326 0.459 5.788 3.664 342.391 0.654 16.296 4.853 0.34 136554. 0.3216
|
|
34.82 0.4338 0.7143 0.0518 0.0315 0.443 5.582 3.407 330.213 0.631 15.155 4.680 0.34 136823. 0.2990
|
|
36.86 0.4593 0.7282 0.0478 0.0301 0.424 5.346 3.142 316.227 0.604 13.974 4.506 0.34 137103. 0.2765
|
|
38.91 0.4848 0.7386 0.0436 0.0286 0.403 5.080 2.868 300.493 0.574 12.758 4.330 0.34 137396. 0.2538
|
|
40.96 0.5104 0.7448 0.0394 0.0270 0.380 4.785 2.589 283.067 0.541 11.514 4.148 0.34 137701. 0.2310
|
|
43.01 0.5359 0.7462 0.0350 0.0252 0.354 4.463 2.304 264.008 0.504 10.247 3.958 0.34 138018. 0.2080
|
|
45.06 0.5614 0.7416 0.0306 0.0232 0.326 4.114 2.015 243.384 0.465 8.961 3.755 0.34 138348. 0.1845
|
|
47.10 0.5869 0.7293 0.0262 0.0211 0.297 3.740 1.723 221.271 0.423 7.663 3.532 0.34 138690. 0.1605
|
|
49.15 0.6124 0.7065 0.0217 0.0188 0.265 3.343 1.430 197.764 0.378 6.359 3.279 0.34 139044. 0.1357
|
|
51.20 0.6380 0.6687 0.0173 0.0165 0.232 2.924 1.136 172.978 0.330 5.054 2.979 0.34 139410. 0.1099
|
|
53.25 0.6635 0.6080 0.0128 0.0140 0.197 2.486 0.844 147.053 0.281 3.756 2.605 0.34 139789. 0.0829
|
|
55.30 0.6890 0.5089 0.0085 0.0114 0.161 2.031 0.556 120.161 0.229 2.473 2.099 0.34 140180. 0.0542
|
|
57.34 0.7145 0.3366 0.0042 0.0088 0.124 1.564 0.273 92.504 0.177 1.215 1.339 0.34 140583. 0.0242
|
|
59.39 0.7400 -0.0061 -0.0001 0.0061 0.086 1.086 -0.003 64.234 0.123 -0.015 -0.023 0.35 140993. 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 0.0946 0.0323 0.787 8.264 8.960 586.610 0.934 39.855 6.928 0.40 160602. 0.7179
|
|
2.46 0.0255 0.0724 0.0934 0.0329 0.801 8.412 8.844 597.141 0.950 39.337 6.717 0.40 160712. 0.6915
|
|
4.92 0.0510 0.1403 0.0920 0.0335 0.814 8.556 8.716 607.342 0.967 38.769 6.509 0.40 160833. 0.6652
|
|
7.37 0.0766 0.2038 0.0906 0.0340 0.827 8.692 8.576 617.017 0.982 38.147 6.304 0.40 160965. 0.6391
|
|
9.83 0.1021 0.2631 0.0889 0.0345 0.839 8.818 8.423 625.963 0.996 37.467 6.104 0.40 161109. 0.6132
|
|
12.29 0.1276 0.3182 0.0872 0.0350 0.850 8.931 8.257 633.964 1.009 36.726 5.907 0.40 161264. 0.5876
|
|
14.75 0.1531 0.3695 0.0853 0.0353 0.859 9.027 8.075 640.783 1.020 35.919 5.716 0.40 161432. 0.5623
|
|
17.20 0.1786 0.4171 0.0832 0.0356 0.867 9.103 7.878 646.176 1.028 35.043 5.530 0.40 161613. 0.5373
|
|
19.66 0.2042 0.4611 0.0809 0.0358 0.872 9.155 7.665 649.891 1.034 34.095 5.350 0.40 161806. 0.5127
|
|
22.12 0.2297 0.5018 0.0785 0.0359 0.874 9.180 7.435 651.672 1.037 33.071 5.175 0.40 162014. 0.4885
|
|
24.58 0.2552 0.5393 0.0759 0.0359 0.873 9.174 7.187 651.268 1.037 31.970 5.006 0.40 162235. 0.4645
|
|
27.03 0.2807 0.5738 0.0731 0.0358 0.870 9.135 6.922 648.440 1.032 30.788 4.842 0.41 162471. 0.4409
|
|
29.49 0.3062 0.6054 0.0701 0.0355 0.862 9.057 6.638 642.964 1.023 29.526 4.683 0.41 162720. 0.4176
|
|
31.95 0.3317 0.6343 0.0669 0.0350 0.851 8.940 6.336 634.633 1.010 28.182 4.528 0.41 162984. 0.3946
|
|
34.41 0.3573 0.6604 0.0635 0.0344 0.836 8.780 6.016 623.249 0.992 26.757 4.378 0.41 163263. 0.3717
|
|
36.87 0.3828 0.6837 0.0599 0.0336 0.816 8.573 5.677 608.598 0.969 25.249 4.231 0.41 163556. 0.3489
|
|
39.32 0.4083 0.7043 0.0562 0.0326 0.792 8.320 5.320 590.587 0.940 23.663 4.086 0.41 163863. 0.3262
|
|
41.78 0.4338 0.7221 0.0522 0.0314 0.763 8.020 4.948 569.285 0.906 22.008 3.942 0.41 164186. 0.3036
|
|
44.24 0.4593 0.7367 0.0482 0.0300 0.731 7.675 4.563 544.795 0.867 20.295 3.799 0.41 164523. 0.2809
|
|
46.70 0.4849 0.7479 0.0440 0.0285 0.694 7.286 4.166 517.221 0.823 18.531 3.654 0.41 164874. 0.2581
|
|
49.15 0.5104 0.7552 0.0397 0.0268 0.653 6.856 3.760 486.661 0.775 16.726 3.505 0.41 165241. 0.2353
|
|
51.61 0.5359 0.7578 0.0353 0.0250 0.608 6.385 3.347 453.219 0.721 14.886 3.349 0.41 165622. 0.2121
|
|
54.07 0.5614 0.7546 0.0309 0.0230 0.559 5.874 2.927 417.011 0.664 13.019 3.184 0.41 166017. 0.1885
|
|
56.53 0.5869 0.7440 0.0264 0.0209 0.507 5.327 2.503 378.173 0.602 11.134 3.002 0.41 166428. 0.1644
|
|
58.98 0.6125 0.7232 0.0219 0.0186 0.452 4.746 2.077 336.872 0.536 9.240 2.797 0.41 166853. 0.1395
|
|
61.44 0.6380 0.6878 0.0174 0.0162 0.393 4.132 1.651 293.310 0.467 7.345 2.553 0.41 167293. 0.1136
|
|
63.90 0.6635 0.6296 0.0130 0.0137 0.332 3.490 1.228 247.736 0.394 5.460 2.247 0.41 167747. 0.0862
|
|
66.36 0.6890 0.5324 0.0085 0.0111 0.269 2.824 0.809 200.455 0.319 3.597 1.830 0.41 168217. 0.0570
|
|
68.82 0.7145 0.3585 0.0042 0.0084 0.204 2.139 0.398 151.827 0.242 1.769 1.188 0.41 168700. 0.0259
|
|
71.27 0.7400 -0.0049 0.0000 0.0056 0.137 1.438 -0.004 102.110 0.163 -0.016 -0.016 0.41 169191. 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 0.0953 0.0324 1.250 11.256 12.283 932.176 1.272 54.633 5.976 0.47 187359. 0.7250
|
|
2.90 0.0258 0.0735 0.0941 0.0330 1.273 11.464 12.124 949.406 1.295 53.927 5.792 0.47 187490. 0.6981
|
|
5.79 0.0515 0.1424 0.0927 0.0335 1.296 11.665 11.949 966.098 1.318 53.151 5.610 0.47 187633. 0.6713
|
|
8.69 0.0773 0.2068 0.0912 0.0341 1.317 11.856 11.758 981.927 1.340 52.300 5.431 0.47 187789. 0.6447
|
|
11.58 0.1031 0.2668 0.0896 0.0346 1.336 12.033 11.548 996.553 1.359 51.367 5.256 0.47 187958. 0.6183
|
|
14.48 0.1288 0.3227 0.0878 0.0351 1.354 12.191 11.319 1009.614 1.377 50.347 5.085 0.47 188142. 0.5922
|
|
17.37 0.1546 0.3745 0.0859 0.0354 1.369 12.325 11.069 1020.717 1.392 49.234 4.919 0.47 188341. 0.5665
|
|
20.27 0.1804 0.4226 0.0838 0.0357 1.381 12.430 10.797 1029.453 1.404 48.024 4.757 0.47 188555. 0.5411
|
|
23.16 0.2061 0.4671 0.0815 0.0360 1.388 12.502 10.502 1035.399 1.412 46.711 4.600 0.47 188785. 0.5161
|
|
26.06 0.2319 0.5082 0.0790 0.0360 1.392 12.535 10.182 1038.132 1.416 45.291 4.449 0.47 189032. 0.4914
|
|
28.95 0.2577 0.5460 0.0763 0.0360 1.391 12.524 9.839 1037.232 1.415 43.762 4.302 0.47 189294. 0.4671
|
|
31.85 0.2834 0.5808 0.0735 0.0358 1.384 12.465 9.469 1032.303 1.408 42.119 4.161 0.47 189574. 0.4432
|
|
34.74 0.3092 0.6128 0.0704 0.0355 1.372 12.352 9.074 1022.974 1.396 40.362 4.023 0.47 189870. 0.4195
|
|
37.64 0.3350 0.6419 0.0671 0.0350 1.353 12.182 8.653 1008.905 1.376 38.490 3.890 0.47 190184. 0.3961
|
|
40.53 0.3607 0.6682 0.0637 0.0344 1.327 11.951 8.207 989.764 1.350 36.503 3.761 0.47 190514. 0.3729
|
|
43.43 0.3865 0.6919 0.0600 0.0335 1.294 11.654 7.734 965.202 1.317 34.399 3.634 0.47 190862. 0.3498
|
|
46.32 0.4122 0.7127 0.0561 0.0325 1.254 11.291 7.236 935.100 1.276 32.186 3.510 0.47 191228. 0.3268
|
|
49.22 0.4380 0.7307 0.0521 0.0312 1.206 10.862 6.717 899.586 1.227 29.878 3.387 0.48 191611. 0.3039
|
|
52.11 0.4638 0.7456 0.0479 0.0298 1.152 10.370 6.180 858.833 1.172 27.489 3.264 0.48 192011. 0.2809
|
|
55.01 0.4895 0.7571 0.0437 0.0282 1.090 9.817 5.627 813.009 1.109 25.031 3.139 0.48 192429. 0.2578
|
|
57.90 0.5153 0.7645 0.0393 0.0265 1.022 9.204 5.062 762.277 1.040 22.515 3.012 0.48 192864. 0.2346
|
|
60.80 0.5411 0.7672 0.0348 0.0245 0.948 8.535 4.486 706.814 0.964 19.952 2.878 0.48 193316. 0.2110
|
|
63.69 0.5668 0.7639 0.0303 0.0225 0.867 7.810 3.902 646.818 0.882 17.354 2.736 0.48 193786. 0.1871
|
|
66.59 0.5926 0.7528 0.0257 0.0202 0.781 7.034 3.312 582.526 0.795 14.732 2.579 0.48 194274. 0.1625
|
|
69.48 0.6184 0.7308 0.0211 0.0179 0.690 6.209 2.720 514.227 0.702 12.099 2.399 0.48 194779. 0.1370
|
|
72.38 0.6441 0.6926 0.0165 0.0154 0.593 5.340 2.129 442.277 0.603 9.468 2.183 0.48 195301. 0.1103
|
|
75.27 0.6699 0.6284 0.0120 0.0127 0.492 4.433 1.541 367.114 0.501 6.856 1.904 0.48 195841. 0.0818
|
|
78.17 0.6957 0.5168 0.0075 0.0100 0.388 3.493 0.962 289.274 0.395 4.278 1.508 0.48 196398. 0.0512
|
|
81.06 0.7214 0.3037 0.0031 0.0073 0.281 2.528 0.395 209.382 0.286 1.755 0.855 0.48 196972. 0.0186
|
|
83.96 0.7472
|
|
|
|
|
|
|
|
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 0.0961 0.0325 1.875 14.771 16.177 1398.090 1.669 71.954 5.248 0.54 214111. 0.7307
|
|
3.27 0.0255 0.0730 0.0949 0.0331 1.910 15.046 15.974 1424.118 1.700 71.053 5.088 0.54 214259. 0.7039
|
|
6.55 0.0510 0.1415 0.0936 0.0337 1.944 15.313 15.751 1449.365 1.730 70.061 4.929 0.54 214421. 0.6772
|
|
9.82 0.0765 0.2056 0.0921 0.0343 1.976 15.566 15.506 1473.348 1.759 68.972 4.774 0.54 214597. 0.6507
|
|
13.10 0.1020 0.2653 0.0905 0.0348 2.006 15.801 15.238 1495.563 1.785 67.777 4.621 0.54 214789. 0.6244
|
|
16.37 0.1275 0.3210 0.0888 0.0353 2.032 16.011 14.943 1515.475 1.809 66.468 4.472 0.54 214997. 0.5985
|
|
19.64 0.1530 0.3727 0.0868 0.0356 2.055 16.191 14.622 1532.507 1.829 65.040 4.328 0.54 215221. 0.5729
|
|
22.92 0.1785 0.4207 0.0848 0.0360 2.073 16.335 14.273 1546.051 1.845 63.485 4.187 0.54 215463. 0.5476
|
|
26.19 0.2040 0.4652 0.0825 0.0362 2.086 16.434 13.893 1555.486 1.857 61.796 4.051 0.54 215722. 0.5227
|
|
29.47 0.2295 0.5063 0.0801 0.0363 2.092 16.484 13.482 1560.182 1.862 59.969 3.919 0.54 216000. 0.4982
|
|
32.74 0.2550 0.5443 0.0774 0.0363 2.091 16.477 13.039 1559.519 1.862 57.997 3.792 0.54 216296. 0.4740
|
|
36.02 0.2805 0.5793 0.0746 0.0361 2.082 16.407 12.563 1552.907 1.854 55.879 3.669 0.54 216610. 0.4502
|
|
39.29 0.3060 0.6115 0.0716 0.0358 2.065 16.268 12.053 1539.791 1.838 53.611 3.550 0.54 216944. 0.4267
|
|
42.56 0.3315 0.6410 0.0684 0.0353 2.038 16.056 11.509 1519.668 1.814 51.193 3.435 0.54 217297. 0.4034
|
|
45.84 0.3570 0.6678 0.0649 0.0347 2.001 15.764 10.932 1492.053 1.781 48.624 3.323 0.54 217669. 0.3803
|
|
49.11 0.3825 0.6920 0.0613 0.0339 1.953 15.388 10.320 1456.427 1.738 45.903 3.214 0.54 218060. 0.3574
|
|
52.39 0.4079 0.7135 0.0575 0.0329 1.894 14.924 9.675 1412.522 1.686 43.036 3.107 0.54 218471. 0.3345
|
|
55.66 0.4334 0.7323 0.0535 0.0316 1.824 14.374 9.002 1360.486 1.624 40.042 3.001 0.54 218901. 0.3117
|
|
58.93 0.4589 0.7482 0.0493 0.0303 1.744 13.741 8.304 1300.573 1.552 36.938 2.896 0.54 219351. 0.2889
|
|
62.21 0.4844 0.7610 0.0451 0.0287 1.654 13.027 7.585 1233.031 1.472 33.740 2.790 0.54 219820. 0.2660
|
|
65.48 0.5099 0.7700 0.0407 0.0269 1.553 12.236 6.849 1158.103 1.382 30.463 2.682 0.54 220308. 0.2430
|
|
68.76 0.5354 0.7747 0.0362 0.0250 1.443 11.369 6.097 1076.045 1.284 27.121 2.570 0.55 220817. 0.2197
|
|
72.03 0.5609 0.7740 0.0317 0.0230 1.324 10.429 5.335 987.141 1.178 23.729 2.451 0.55 221344. 0.1960
|
|
75.30 0.5864 0.7664 0.0271 0.0207 1.196 9.421 4.564 891.727 1.064 20.302 2.322 0.55 221891. 0.1717
|
|
78.58 0.6119 0.7493 0.0225 0.0184 1.060 8.349 3.789 790.211 0.943 16.855 2.175 0.55 222457. 0.1466
|
|
81.85 0.6374 0.7182 0.0179 0.0159 0.916 7.217 3.014 683.094 0.815 13.407 2.001 0.55 223043. 0.1203
|
|
85.13 0.6629 0.6648 0.0133 0.0133 0.766 6.033 2.243 570.997 0.682 9.976 1.782 0.55 223649. 0.0924
|
|
88.40 0.6884 0.5722 0.0088 0.0106 0.610 4.804 1.480 454.676 0.543 6.584 1.477 0.55 224274. 0.0622
|
|
91.67 0.7139 0.3981 0.0043 0.0078 0.449 3.540 0.732 335.035 0.400 3.255 0.991 0.55 224918. 0.0293
|
|
94.95 0.7394 0.0007 0.0000 0.0049 0.285 2.247 0.001 212.696 0.254 0.003 0.002 0.55 225570. 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 0.0970 0.0328 2.692 18.855 20.673 2007.668 2.130 91.952 4.670 0.61 240857. 0.7351
|
|
3.68 0.0255 0.0731 0.0958 0.0334 2.743 19.212 20.421 2045.670 2.171 90.832 4.528 0.61 241023. 0.7083
|
|
7.37 0.0510 0.1416 0.0945 0.0340 2.793 19.558 20.142 2082.564 2.210 89.593 4.387 0.61 241206. 0.6815
|
|
11.05 0.0765 0.2058 0.0931 0.0346 2.840 19.887 19.836 2117.632 2.247 88.229 4.249 0.61 241405. 0.6550
|
|
14.73 0.1020 0.2656 0.0915 0.0351 2.883 20.193 19.498 2150.145 2.281 86.729 4.113 0.61 241621. 0.6287
|
|
18.41 0.1275 0.3214 0.0898 0.0356 2.923 20.467 19.128 2179.317 2.312 85.083 3.981 0.61 241855. 0.6027
|
|
22.10 0.1530 0.3732 0.0879 0.0360 2.956 20.701 18.723 2204.297 2.339 83.281 3.853 0.61 242109. 0.5771
|
|
25.78 0.1784 0.4213 0.0858 0.0363 2.983 20.888 18.281 2224.202 2.360 81.315 3.728 0.61 242381. 0.5518
|
|
29.46 0.2039 0.4659 0.0835 0.0366 3.001 21.019 17.800 2238.121 2.375 79.176 3.607 0.61 242674. 0.5269
|
|
33.14 0.2294 0.5072 0.0811 0.0367 3.011 21.085 17.279 2245.136 2.382 76.857 3.491 0.61 242987. 0.5023
|
|
36.83 0.2549 0.5454 0.0784 0.0367 3.010 21.077 16.716 2244.343 2.381 74.351 3.378 0.61 243320. 0.4781
|
|
40.51 0.2804 0.5806 0.0756 0.0365 2.997 20.989 16.109 2234.876 2.371 71.654 3.269 0.61 243675. 0.4542
|
|
44.19 0.3059 0.6130 0.0725 0.0362 2.972 20.811 15.459 2215.933 2.351 68.763 3.164 0.61 244051. 0.4307
|
|
47.87 0.3314 0.6428 0.0693 0.0357 2.933 20.537 14.765 2186.776 2.320 65.677 3.063 0.61 244449. 0.4074
|
|
51.56 0.3569 0.6699 0.0658 0.0351 2.879 20.161 14.028 2146.712 2.278 62.395 2.964 0.61 244868. 0.3843
|
|
55.24 0.3824 0.6945 0.0622 0.0342 2.809 19.675 13.245 2094.994 2.223 58.915 2.868 0.61 245310. 0.3613
|
|
58.92 0.4079 0.7164 0.0583 0.0332 2.724 19.076 12.420 2031.205 2.155 55.246 2.773 0.61 245772. 0.3384
|
|
62.61 0.4334 0.7358 0.0542 0.0319 2.622 18.365 11.558 1955.550 2.075 51.410 2.681 0.61 246257. 0.3155
|
|
66.29 0.4589 0.7523 0.0500 0.0305 2.506 17.547 10.663 1868.395 1.982 47.430 2.589 0.61 246764. 0.2926
|
|
69.97 0.4843 0.7656 0.0457 0.0289 2.374 16.624 9.741 1770.108 1.878 43.327 2.496 0.61 247292. 0.2697
|
|
73.65 0.5098 0.7755 0.0413 0.0271 2.227 15.600 8.795 1661.044 1.762 39.121 2.402 0.61 247842. 0.2466
|
|
77.34 0.5353 0.7811 0.0367 0.0252 2.067 14.478 7.830 1541.578 1.636 34.830 2.304 0.61 248414. 0.2232
|
|
81.02 0.5608 0.7815 0.0321 0.0231 1.894 13.262 6.851 1412.126 1.498 30.472 2.200 0.61 249008. 0.1994
|
|
84.70 0.5863 0.7752 0.0275 0.0208 1.707 11.957 5.860 1273.181 1.351 26.067 2.088 0.62 249623. 0.1750
|
|
88.38 0.6118 0.7596 0.0228 0.0184 1.509 10.568 4.864 1125.336 1.194 21.635 1.960 0.62 250261. 0.1497
|
|
92.07 0.6373 0.7303 0.0181 0.0158 1.300 9.103 3.867 969.327 1.028 17.200 1.809 0.62 250920. 0.1232
|
|
95.75 0.6628 0.6790 0.0135 0.0132 1.081 7.570 2.875 806.062 0.855 12.786 1.618 0.62 251601. 0.0949
|
|
99.43 0.6883 0.5880 0.0089 0.0104 0.854 5.979 1.893 636.653 0.676 8.422 1.349 0.62 252305. 0.0643
|
|
103.11 0.7138 0.4125 0.0044 0.0076 0.620 4.343 0.930 462.431 0.491 4.139 0.913 0.62 253029. 0.0305
|
|
106.80 0.7393 -0.0079 0.0000 0.0046 0.381 2.669 -0.011 284.235 0.302 -0.047 -0.017 0.62 253761. 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 0.0981 0.0332 3.740 23.571 25.809 2788.760 2.663 114.798 4.198 0.67 267594. 0.7382
|
|
4.09 0.0255 0.0730 0.0969 0.0338 3.811 24.023 25.505 2842.229 2.714 113.446 4.070 0.67 267780. 0.7116
|
|
8.18 0.0509 0.1414 0.0957 0.0345 3.881 24.463 25.168 2894.243 2.764 111.947 3.944 0.67 267983. 0.6850
|
|
12.27 0.0764 0.2054 0.0943 0.0351 3.948 24.882 24.795 2943.782 2.811 110.290 3.820 0.67 268204. 0.6585
|
|
16.36 0.1019 0.2652 0.0927 0.0356 4.009 25.270 24.384 2989.794 2.855 108.461 3.699 0.67 268445. 0.6323
|
|
20.44 0.1274 0.3210 0.0910 0.0361 4.065 25.620 23.932 3031.128 2.895 106.448 3.581 0.67 268706. 0.6064
|
|
24.53 0.1528 0.3728 0.0891 0.0365 4.112 25.919 23.435 3066.581 2.928 104.237 3.466 0.67 268988. 0.5808
|
|
28.62 0.1783 0.4209 0.0870 0.0369 4.150 26.159 22.891 3094.893 2.955 101.819 3.355 0.67 269292. 0.5556
|
|
32.71 0.2038 0.4656 0.0848 0.0371 4.177 26.327 22.298 3114.784 2.974 99.180 3.247 0.67 269617. 0.5308
|
|
36.80 0.2293 0.5070 0.0823 0.0372 4.191 26.413 21.653 3124.954 2.984 96.313 3.143 0.67 269966. 0.5062
|
|
40.89 0.2547 0.5453 0.0797 0.0372 4.190 26.406 20.955 3124.133 2.983 93.208 3.042 0.67 270337. 0.4821
|
|
44.98 0.2802 0.5807 0.0768 0.0371 4.172 26.296 20.202 3111.098 2.971 89.860 2.945 0.68 270732. 0.4583
|
|
49.07 0.3057 0.6134 0.0737 0.0367 4.137 26.073 19.394 3084.719 2.946 86.265 2.852 0.68 271151. 0.4347
|
|
53.15 0.3311 0.6434 0.0704 0.0363 4.082 25.728 18.530 3043.968 2.907 82.422 2.761 0.68 271594. 0.4114
|
|
57.24 0.3566 0.6709 0.0669 0.0356 4.007 25.254 17.610 2987.875 2.853 78.330 2.673 0.68 272060. 0.3883
|
|
61.33 0.3821 0.6958 0.0632 0.0347 3.910 24.642 16.634 2915.416 2.784 73.986 2.588 0.68 272551. 0.3653
|
|
65.42 0.4076 0.7182 0.0593 0.0337 3.790 23.886 15.603 2825.965 2.699 69.400 2.504 0.68 273066. 0.3424
|
|
69.51 0.4330 0.7381 0.0552 0.0324 3.647 22.988 14.523 2719.775 2.597 64.600 2.422 0.68 273605. 0.3195
|
|
73.60 0.4585 0.7552 0.0509 0.0309 3.483 21.954 13.403 2597.370 2.480 59.615 2.340 0.68 274168. 0.2966
|
|
77.69 0.4840 0.7692 0.0466 0.0293 3.298 20.786 12.246 2459.276 2.348 54.472 2.259 0.68 274756. 0.2736
|
|
81.78 0.5095 0.7799 0.0420 0.0275 3.092 19.491 11.060 2305.999 2.202 49.195 2.175 0.68 275367. 0.2504
|
|
85.86 0.5349 0.7865 0.0374 0.0255 2.867 18.071 9.849 2138.070 2.042 43.808 2.089 0.68 276002. 0.2270
|
|
89.95 0.5604 0.7881 0.0328 0.0233 2.623 16.533 8.618 1956.079 1.868 38.334 1.998 0.68 276662. 0.2031
|
|
94.04 0.5859 0.7831 0.0280 0.0210 2.361 14.882 7.374 1760.715 1.681 32.798 1.899 0.68 277346. 0.1786
|
|
98.13 0.6113 0.7691 0.0233 0.0185 2.082 13.125 6.121 1552.822 1.483 27.226 1.788 0.68 278054. 0.1531
|
|
102.22 0.6368 0.7418 0.0185 0.0159 1.788 11.271 4.866 1333.439 1.273 21.646 1.655 0.69 278786. 0.1264
|
|
106.31 0.6623 0.6927 0.0138 0.0131 1.480 9.330 3.617 1103.881 1.054 16.091 1.486 0.69 279542. 0.0979
|
|
110.40 0.6878 0.6040 0.0091 0.0103 1.161 7.318 2.382 865.779 0.827 10.596 1.248 0.69 280322. 0.0667
|
|
114.49 0.7132 0.4286 0.0044 0.0074 0.833 5.250 1.169 621.111 0.593 5.201 0.854 0.69 281126. 0.0320
|
|
118.57 0.7387 -0.0103 -0.0001 0.0044 0.498 3.137 -0.016 371.154 0.354 -0.072 -0.020 0.69 281937. 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 0.0994 0.0341 5.110 29.279 31.629 3810.487 3.308 140.685 3.765 0.74 294322. 0.7330
|
|
4.52 0.0256 0.0725 0.0982 0.0347 5.202 29.806 31.271 3879.069 3.367 139.093 3.656 0.74 294528. 0.7078
|
|
9.05 0.0513 0.1408 0.0970 0.0353 5.292 30.320 30.872 3945.923 3.426 137.317 3.549 0.74 294753. 0.6825
|
|
13.57 0.0769 0.2048 0.0956 0.0359 5.377 30.810 30.428 4009.721 3.481 135.343 3.442 0.74 294999. 0.6572
|
|
18.10 0.1025 0.2648 0.0940 0.0364 5.457 31.266 29.935 4069.082 3.532 133.152 3.337 0.74 295267. 0.6320
|
|
22.62 0.1281 0.3207 0.0923 0.0369 5.528 31.677 29.390 4122.479 3.579 130.728 3.234 0.74 295557. 0.6068
|
|
27.15 0.1538 0.3729 0.0904 0.0373 5.590 32.028 28.789 4168.267 3.619 128.054 3.133 0.74 295871. 0.5819
|
|
31.67 0.1794 0.4213 0.0884 0.0376 5.639 32.308 28.128 4204.697 3.650 125.115 3.034 0.74 296210. 0.5571
|
|
36.20 0.2050 0.4663 0.0861 0.0378 5.672 32.502 27.405 4229.948 3.672 121.896 2.939 0.74 296573. 0.5325
|
|
40.72 0.2306 0.5081 0.0836 0.0380 5.689 32.596 26.615 4242.155 3.683 118.385 2.846 0.74 296961. 0.5082
|
|
45.25 0.2563 0.5467 0.0809 0.0379 5.685 32.575 25.758 4239.449 3.680 114.571 2.756 0.74 297375. 0.4842
|
|
49.77 0.2819 0.5824 0.0780 0.0378 5.659 32.426 24.831 4220.032 3.663 110.446 2.669 0.74 297816. 0.4604
|
|
54.30 0.3075 0.6153 0.0749 0.0374 5.608 32.135 23.832 4182.201 3.631 106.007 2.585 0.74 298283. 0.4368
|
|
58.82 0.3332 0.6456 0.0715 0.0369 5.531 31.691 22.763 4124.399 3.580 101.251 2.503 0.74 298776. 0.4134
|
|
63.35 0.3588 0.6733 0.0679 0.0362 5.425 31.083 21.623 4045.202 3.512 96.178 2.424 0.74 299297. 0.3903
|
|
67.87 0.3844 0.6986 0.0641 0.0353 5.288 30.299 20.410 3943.170 3.423 90.785 2.348 0.75 299844. 0.3672
|
|
72.40 0.4100 0.7214 0.0601 0.0342 5.119 29.333 19.129 3817.492 3.314 85.085 2.273 0.75 300418. 0.3441
|
|
76.92 0.4357 0.7416 0.0559 0.0328 4.920 28.189 17.786 3668.570 3.185 79.114 2.199 0.75 301019. 0.3210
|
|
81.45 0.4613 0.7591 0.0515 0.0313 4.690 26.872 16.391 3497.155 3.036 72.909 2.126 0.75 301647. 0.2979
|
|
85.97 0.4869 0.7736 0.0470 0.0296 4.431 25.388 14.951 3304.018 2.868 66.504 2.053 0.75 302301. 0.2747
|
|
90.50 0.5125 0.7847 0.0423 0.0276 4.144 23.743 13.473 3089.945 2.682 59.930 1.978 0.75 302982. 0.2513
|
|
95.02 0.5382 0.7916 0.0376 0.0256 3.830 21.943 11.964 2855.771 2.479 53.216 1.900 0.75 303690. 0.2275
|
|
99.55 0.5638 0.7933 0.0328 0.0233 3.490 19.997 10.430 2602.466 2.259 46.392 1.818 0.75 304424. 0.2032
|
|
104.07 0.5894 0.7881 0.0279 0.0209 3.126 17.913 8.878 2331.201 2.024 39.490 1.727 0.75 305185. 0.1782
|
|
108.60 0.6151 0.7731 0.0230 0.0183 2.740 15.702 7.316 2043.447 1.774 32.542 1.624 0.75 305973. 0.1520
|
|
113.12 0.6407 0.7432 0.0181 0.0156 2.335 13.378 5.752 1741.058 1.511 25.586 1.499 0.75 306788. 0.1244
|
|
117.65 0.6663 0.6882 0.0132 0.0128 1.913 10.960 4.196 1426.358 1.238 18.663 1.334 0.76 307629. 0.0946
|
|
122.17 0.6919 0.5857 0.0083 0.0099 1.478 8.469 2.657 1102.206 0.957 11.820 1.094 0.76 308497. 0.0617
|
|
126.70 0.7176 0.3746 0.0036 0.0069 1.035 5.932 1.148 771.988 0.670 5.106 0.674 0.76 309391. 0.0250
|
|
131.22 0.7432
|
|
|
|
|
|
|
|
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 0.1008 0.0366 7.127 37.434 38.172 5314.712 4.229 169.791 3.258 0.81 321038. 0.6967
|
|
4.89 0.0254 0.0681 0.0997 0.0371 7.225 37.951 37.771 5388.021 4.288 168.006 3.180 0.81 321260. 0.6765
|
|
9.78 0.0508 0.1329 0.0985 0.0376 7.320 38.445 37.321 5458.248 4.344 166.004 3.101 0.81 321503. 0.6558
|
|
14.67 0.0761 0.1944 0.0972 0.0381 7.408 38.908 36.818 5523.864 4.396 163.765 3.023 0.81 321769. 0.6350
|
|
19.56 0.1015 0.2525 0.0957 0.0385 7.487 39.326 36.256 5583.283 4.443 161.268 2.945 0.81 322059. 0.6139
|
|
24.44 0.1269 0.3074 0.0941 0.0388 7.556 39.689 35.632 5634.771 4.484 158.490 2.868 0.81 322372. 0.5927
|
|
29.33 0.1523 0.3590 0.0922 0.0391 7.612 39.982 34.939 5676.476 4.517 155.411 2.792 0.81 322711. 0.5712
|
|
34.22 0.1777 0.4075 0.0902 0.0393 7.652 40.193 34.175 5706.437 4.541 152.010 2.716 0.81 323077. 0.5497
|
|
39.11 0.2031 0.4530 0.0880 0.0394 7.674 40.307 33.334 5722.616 4.554 148.268 2.642 0.81 323469. 0.5280
|
|
44.00 0.2284 0.4955 0.0856 0.0394 7.675 40.310 32.412 5722.926 4.554 144.170 2.569 0.81 323888. 0.5063
|
|
48.89 0.2538 0.5352 0.0829 0.0393 7.651 40.185 31.408 5705.268 4.540 139.702 2.497 0.81 324335. 0.4844
|
|
53.78 0.2792 0.5720 0.0800 0.0391 7.600 39.920 30.318 5667.557 4.510 134.854 2.426 0.81 324811. 0.4625
|
|
58.67 0.3046 0.6062 0.0769 0.0386 7.520 39.499 29.141 5607.782 4.463 129.618 2.357 0.81 325314. 0.4404
|
|
63.56 0.3300 0.6378 0.0736 0.0381 7.408 38.909 27.876 5524.008 4.396 123.994 2.289 0.81 325846. 0.4183
|
|
68.45 0.3553 0.6667 0.0700 0.0373 7.261 38.137 26.524 5414.405 4.309 117.980 2.222 0.81 326407. 0.3961
|
|
73.33 0.3807 0.6932 0.0662 0.0364 7.077 37.168 25.084 5276.962 4.199 111.575 2.156 0.81 326997. 0.3738
|
|
78.22 0.4061 0.7171 0.0622 0.0352 6.853 35.994 23.558 5110.202 4.067 104.786 2.091 0.81 327615. 0.3513
|
|
83.11 0.4315 0.7382 0.0580 0.0339 6.591 34.618 21.955 4914.796 3.911 97.654 2.026 0.81 328262. 0.3286
|
|
88.00 0.4569 0.7566 0.0535 0.0323 6.291 33.043 20.284 4691.220 3.733 90.225 1.961 0.82 328937. 0.3058
|
|
92.89 0.4823 0.7719 0.0490 0.0306 5.955 31.277 18.556 4440.540 3.534 82.539 1.895 0.82 329641. 0.2826
|
|
97.78 0.5076 0.7836 0.0443 0.0287 5.583 29.326 16.779 4163.514 3.313 74.635 1.828 0.82 330373. 0.2592
|
|
102.67 0.5330 0.7910 0.0395 0.0266 5.178 27.199 14.961 3861.566 3.073 66.548 1.757 0.82 331134. 0.2353
|
|
107.56 0.5584 0.7929 0.0346 0.0244 4.742 24.909 13.110 3536.371 2.814 58.313 1.681 0.82 331923. 0.2108
|
|
112.45 0.5838 0.7874 0.0297 0.0220 4.278 22.469 11.234 3190.063 2.539 49.968 1.597 0.82 332740. 0.1853
|
|
117.33 0.6092 0.7714 0.0247 0.0195 3.789 19.901 9.341 2825.416 2.248 41.551 1.500 0.82 333586. 0.1587
|
|
122.22 0.6345 0.7396 0.0196 0.0169 3.280 17.225 7.443 2445.548 1.946 33.105 1.380 0.82 334460. 0.1304
|
|
127.11 0.6599 0.6826 0.0146 0.0142 2.755 14.469 5.548 2054.239 1.635 24.677 1.225 0.82 335363. 0.0999
|
|
132.00 0.6853 0.5816 0.0097 0.0114 2.221 11.664 3.669 1655.944 1.318 16.322 1.005 0.83 336294. 0.0666
|
|
136.89 0.7107 0.3947 0.0048 0.0087 1.684 8.844 1.821 1255.681 0.999 8.099 0.658 0.83 337253. 0.0307
|
|
141.78 0.7361 0.0037 0.0000 0.0059 1.149 6.036 0.011 857.012 0.682 0.050 0.006 0.83 338226. 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 0.1020 0.0422 10.435 50.591 45.368 7781.210 5.716 201.796 2.645 0.87 347745. 0.6166
|
|
5.31 0.0254 0.0604 0.1011 0.0425 10.526 51.032 44.934 7848.968 5.766 199.868 2.597 0.87 347986. 0.6025
|
|
10.62 0.0509 0.1186 0.1000 0.0429 10.606 51.422 44.443 7909.040 5.810 197.683 2.549 0.87 348249. 0.5882
|
|
15.92 0.0763 0.1746 0.0987 0.0431 10.674 51.749 43.888 7959.336 5.847 195.214 2.501 0.87 348538. 0.5735
|
|
21.23 0.1017 0.2284 0.0973 0.0434 10.725 51.999 43.263 7997.785 5.875 192.432 2.454 0.87 348852. 0.5586
|
|
26.54 0.1272 0.2800 0.0957 0.0435 10.758 52.159 42.560 8022.353 5.893 189.309 2.406 0.87 349194. 0.5434
|
|
31.85 0.1526 0.3294 0.0940 0.0435 10.770 52.216 41.775 8031.030 5.899 185.815 2.359 0.88 349563. 0.5279
|
|
37.16 0.1781 0.3767 0.0920 0.0435 10.757 52.156 40.901 8021.826 5.893 181.926 2.313 0.88 349961. 0.5120
|
|
42.46 0.2035 0.4218 0.0898 0.0433 10.719 51.967 39.932 7992.819 5.871 177.616 2.266 0.88 350389. 0.4957
|
|
47.77 0.2289 0.4648 0.0874 0.0431 10.650 51.637 38.863 7942.048 5.834 172.865 2.219 0.88 350847. 0.4790
|
|
53.08 0.2544 0.5056 0.0848 0.0426 10.551 51.153 37.692 7867.598 5.779 167.653 2.173 0.88 351335. 0.4618
|
|
58.39 0.2798 0.5443 0.0819 0.0421 10.416 50.502 36.413 7767.431 5.706 161.966 2.126 0.88 351854. 0.4442
|
|
63.70 0.3052 0.5807 0.0788 0.0414 10.245 49.671 35.025 7639.697 5.612 155.793 2.079 0.88 352404. 0.4260
|
|
69.00 0.3307 0.6148 0.0754 0.0406 10.035 48.651 33.528 7482.750 5.497 149.134 2.032 0.88 352986. 0.4074
|
|
74.31 0.3561 0.6466 0.0718 0.0395 9.783 47.429 31.921 7294.876 5.359 141.987 1.985 0.88 353598. 0.3882
|
|
79.62 0.3816 0.6760 0.0679 0.0383 9.487 45.994 30.205 7074.122 5.196 134.351 1.937 0.88 354242. 0.3684
|
|
84.93 0.4070 0.7029 0.0638 0.0370 9.144 44.334 28.380 6818.815 5.009 126.236 1.888 0.88 354917. 0.3481
|
|
90.24 0.4324 0.7269 0.0595 0.0354 8.759 42.465 26.459 6531.363 4.798 117.691 1.837 0.88 355624. 0.3272
|
|
95.54 0.4579 0.7472 0.0550 0.0337 8.337 40.422 24.453 6217.111 4.567 108.768 1.784 0.88 356361. 0.3054
|
|
100.85 0.4833 0.7636 0.0503 0.0319 7.880 38.204 22.374 5875.958 4.316 99.520 1.727 0.88 357128. 0.2828
|
|
106.16 0.5087 0.7747 0.0455 0.0299 7.393 35.842 20.232 5512.675 4.049 89.992 1.665 0.89 357927. 0.2592
|
|
111.47 0.5342 0.7786 0.0406 0.0278 6.886 33.383 18.036 5134.556 3.772 80.225 1.593 0.89 358756. 0.2342
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|
116.78 0.5596 0.7749 0.0355 0.0257 6.349 30.782 15.799 4734.363 3.478 70.272 1.514 0.89 359616. 0.2083
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|
122.08 0.5851 0.7612 0.0304 0.0234 5.786 28.052 13.529 4314.541 3.169 60.179 1.422 0.89 360507. 0.1811
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|
127.39 0.6105 0.7338 0.0253 0.0210 5.203 25.227 11.240 3880.068 2.850 49.997 1.314 0.89 361428. 0.1525
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|
132.70 0.6359 0.6866 0.0201 0.0186 4.609 22.345 8.943 3436.793 2.525 39.780 1.180 0.89 362380. 0.1222
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|
138.01 0.6614 0.6106 0.0150 0.0162 4.010 19.442 6.653 2990.264 2.197 29.593 1.009 0.89 363362. 0.0901
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|
143.32 0.6868 0.4906 0.0099 0.0138 3.416 16.560 4.385 2546.957 1.871 19.505 0.781 0.89 364376. 0.0566
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|
148.62 0.7122 0.3017 0.0049 0.0115 2.834 13.741 2.158 2113.427 1.552 9.597 0.463 0.90 365419. 0.0235
|
|
153.93 0.7377 -0.0035 0.0000 0.0092 2.268 10.995 -0.019 1691.064 1.242 -0.085 -0.005 0.90 366482. 0.0000
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PROP RPM = 14000
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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 0.1015 0.0487 15.035 67.690 52.329 11211.869 7.648 232.759 2.117 0.94 374509. 0.5301
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|
5.87 0.0261 0.0535 0.1007 0.0491 15.175 68.320 51.908 11316.283 7.719 230.885 2.081 0.94 374768. 0.5189
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|
11.74 0.0522 0.1052 0.0997 0.0495 15.299 68.876 51.422 11408.383 7.782 228.724 2.044 0.94 375054. 0.5075
|
|
17.61 0.0784 0.1551 0.0986 0.0498 15.400 69.330 50.862 11483.519 7.833 226.234 2.009 0.94 375369. 0.4960
|
|
23.48 0.1045 0.2032 0.0974 0.0501 15.471 69.652 50.218 11536.888 7.869 223.372 1.974 0.94 375713. 0.4843
|
|
29.35 0.1306 0.2497 0.0960 0.0502 15.507 69.813 49.481 11563.659 7.887 220.091 1.941 0.94 376088. 0.4726
|
|
35.22 0.1567 0.2947 0.0943 0.0502 15.501 69.787 48.639 11559.242 7.884 216.346 1.909 0.94 376497. 0.4608
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|
41.09 0.1828 0.3382 0.0925 0.0500 15.448 69.547 47.683 11519.560 7.857 212.094 1.877 0.94 376938. 0.4488
|
|
46.96 0.2090 0.3804 0.0904 0.0497 15.342 69.069 46.603 11440.391 7.803 207.288 1.848 0.94 377415. 0.4366
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|
52.83 0.2351 0.4212 0.0880 0.0491 15.180 68.341 45.391 11319.763 7.721 201.899 1.819 0.94 377926. 0.4242
|
|
58.70 0.2612 0.4608 0.0854 0.0484 14.960 67.352 44.042 11155.961 7.609 195.898 1.791 0.94 378474. 0.4114
|
|
64.57 0.2873 0.4990 0.0825 0.0475 14.681 66.094 42.550 10947.613 7.467 189.264 1.763 0.95 379057. 0.3981
|
|
70.44 0.3134 0.5358 0.0793 0.0464 14.341 64.563 40.913 10693.940 7.294 181.982 1.735 0.95 379677. 0.3842
|
|
76.31 0.3396 0.5712 0.0759 0.0451 13.940 62.756 39.130 10394.751 7.090 174.049 1.707 0.95 380332. 0.3697
|
|
82.18 0.3657 0.6048 0.0721 0.0436 13.477 60.676 37.200 10050.165 6.855 165.465 1.679 0.95 381024. 0.3545
|
|
88.05 0.3918 0.6366 0.0681 0.0419 12.954 58.320 35.124 9659.903 6.589 156.231 1.649 0.95 381751. 0.3383
|
|
93.92 0.4179 0.6662 0.0638 0.0400 12.371 55.692 32.909 9224.694 6.292 146.378 1.618 0.95 382514. 0.3213
|
|
99.79 0.4440 0.6935 0.0593 0.0380 11.730 52.811 30.572 8747.403 5.967 135.982 1.585 0.95 383313. 0.3034
|
|
105.65 0.4702 0.7163 0.0545 0.0358 11.062 49.803 28.126 8249.196 5.627 125.105 1.546 0.95 384146. 0.2839
|
|
111.52 0.4963 0.7338 0.0496 0.0336 10.370 46.687 25.588 7733.139 5.275 113.815 1.501 0.95 385015. 0.2628
|
|
117.39 0.5224 0.7439 0.0446 0.0313 9.666 43.516 22.971 7207.790 4.916 102.176 1.446 0.95 385918. 0.2398
|
|
123.26 0.5485 0.7374 0.0393 0.0293 9.039 40.696 20.280 6740.711 4.598 90.207 1.365 0.96 386856. 0.2127
|
|
129.13 0.5746 0.7171 0.0340 0.0273 8.423 37.920 17.540 6280.896 4.284 78.016 1.267 0.96 387828. 0.1836
|
|
135.00 0.6008 0.6819 0.0286 0.0252 7.798 35.106 14.770 5814.853 3.966 65.697 1.152 0.96 388834. 0.1533
|
|
140.87 0.6269 0.6280 0.0233 0.0232 7.173 32.293 11.991 5348.867 3.648 53.335 1.017 0.96 389876. 0.1219
|
|
146.74 0.6530 0.5504 0.0179 0.0212 6.558 29.526 9.225 4890.592 3.336 41.031 0.856 0.96 390952. 0.0899
|
|
152.61 0.6791 0.4433 0.0126 0.0193 5.964 26.852 6.497 4447.634 3.034 28.897 0.663 0.96 392063. 0.0585
|
|
158.48 0.7052 0.3005 0.0074 0.0175 5.398 24.301 3.838 4025.063 2.745 17.072 0.432 0.96 393209. 0.0293
|
|
164.35 0.7314 0.1145 0.0025 0.0157 4.860 21.882 1.270 3624.391 2.472 5.648 0.159 0.97 394397. 0.0062
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|
170.22 0.7575
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