501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x12E (18x12E.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 0.0975 0.0408 0.006 0.391 0.326 4.630 0.044 1.451 31.959 0.07 29880. 0.5950
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0.48 0.0280 0.0651 0.0965 0.0415 0.006 0.398 0.323 4.707 0.045 1.435 31.098 0.07 29903. 0.5759
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0.96 0.0561 0.1266 0.0953 0.0422 0.006 0.404 0.319 4.782 0.046 1.418 30.232 0.07 29927. 0.5564
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1.43 0.0841 0.1845 0.0940 0.0428 0.007 0.410 0.314 4.856 0.046 1.399 29.367 0.07 29955. 0.5368
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1.91 0.1121 0.2388 0.0925 0.0434 0.007 0.416 0.310 4.926 0.047 1.377 28.505 0.07 29985. 0.5170
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2.39 0.1401 0.2896 0.0910 0.0440 0.007 0.422 0.304 4.991 0.048 1.354 27.651 0.07 30017. 0.4972
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2.87 0.1682 0.3369 0.0892 0.0445 0.007 0.427 0.298 5.050 0.048 1.327 26.807 0.07 30053. 0.4774
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3.34 0.1962 0.3809 0.0873 0.0450 0.007 0.431 0.292 5.099 0.049 1.299 25.977 0.07 30091. 0.4576
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3.82 0.2242 0.4216 0.0852 0.0453 0.007 0.434 0.285 5.137 0.049 1.268 25.160 0.07 30133. 0.4378
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4.30 0.2523 0.4592 0.0829 0.0455 0.007 0.436 0.277 5.162 0.049 1.233 24.360 0.07 30178. 0.4181
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4.78 0.2803 0.4938 0.0804 0.0456 0.007 0.437 0.269 5.172 0.049 1.196 23.576 0.07 30226. 0.3985
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5.26 0.3083 0.5255 0.0776 0.0456 0.007 0.437 0.260 5.165 0.049 1.155 22.808 0.07 30277. 0.3789
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5.73 0.3363 0.5543 0.0747 0.0453 0.007 0.434 0.250 5.139 0.049 1.111 22.055 0.07 30332. 0.3594
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6.21 0.3644 0.5804 0.0715 0.0449 0.007 0.430 0.239 5.091 0.049 1.064 21.314 0.07 30390. 0.3398
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6.69 0.3924 0.6036 0.0681 0.0443 0.007 0.424 0.228 5.021 0.048 1.014 20.583 0.07 30452. 0.3203
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7.17 0.4204 0.6238 0.0645 0.0435 0.007 0.416 0.216 4.927 0.047 0.959 19.856 0.07 30517. 0.3006
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7.64 0.4485 0.6410 0.0606 0.0424 0.006 0.406 0.203 4.809 0.046 0.902 19.129 0.07 30585. 0.2808
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8.12 0.4765 0.6549 0.0565 0.0411 0.006 0.394 0.189 4.664 0.045 0.841 18.394 0.07 30657. 0.2608
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8.60 0.5045 0.6651 0.0523 0.0396 0.006 0.380 0.175 4.495 0.043 0.778 17.643 0.07 30732. 0.2405
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9.08 0.5325 0.6712 0.0478 0.0380 0.006 0.364 0.160 4.303 0.041 0.712 16.865 0.07 30810. 0.2199
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9.56 0.5606 0.6723 0.0433 0.0361 0.005 0.346 0.145 4.089 0.039 0.644 16.049 0.07 30892. 0.1990
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10.03 0.5886 0.6676 0.0386 0.0340 0.005 0.326 0.129 3.855 0.037 0.574 15.179 0.07 30977. 0.1777
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10.51 0.6166 0.6558 0.0338 0.0318 0.005 0.304 0.113 3.602 0.034 0.503 14.233 0.07 31066. 0.1560
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10.99 0.6447 0.6351 0.0289 0.0294 0.004 0.282 0.097 3.332 0.032 0.431 13.184 0.07 31158. 0.1338
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11.47 0.6727 0.6029 0.0241 0.0269 0.004 0.257 0.081 3.045 0.029 0.358 11.994 0.07 31253. 0.1109
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11.94 0.7007 0.5553 0.0192 0.0242 0.004 0.232 0.064 2.744 0.026 0.285 10.604 0.07 31351. 0.0876
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12.42 0.7288 0.4861 0.0143 0.0214 0.003 0.205 0.048 2.429 0.023 0.213 8.927 0.07 31453. 0.0636
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12.90 0.7568 0.3856 0.0095 0.0186 0.003 0.178 0.032 2.104 0.020 0.141 6.818 0.07 31558. 0.0395
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13.38 0.7848 0.2361 0.0047 0.0156 0.002 0.150 0.016 1.771 0.017 0.070 4.026 0.07 31666. 0.0165
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13.86 0.8128 0.0037 0.0001 0.0126 0.002 0.121 0.000 1.432 0.014 0.001 0.061 0.07 31778. 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 0.0979 0.0379 0.046 1.452 1.309 34.363 0.164 5.824 17.284 0.14 59760. 0.6447
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0.96 0.0282 0.0707 0.0968 0.0386 0.047 1.480 1.295 35.014 0.167 5.762 16.780 0.14 59805. 0.6226
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1.92 0.0564 0.1371 0.0956 0.0393 0.048 1.507 1.280 35.663 0.170 5.692 16.276 0.14 59855. 0.6002
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2.88 0.0845 0.1993 0.0943 0.0400 0.049 1.534 1.262 36.297 0.173 5.615 15.774 0.14 59910. 0.5777
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3.84 0.1127 0.2574 0.0929 0.0407 0.049 1.560 1.243 36.905 0.176 5.529 15.278 0.14 59970. 0.5553
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4.80 0.1409 0.3114 0.0913 0.0413 0.050 1.584 1.222 37.473 0.179 5.435 14.790 0.14 60036. 0.5329
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5.76 0.1691 0.3616 0.0896 0.0419 0.051 1.605 1.198 37.986 0.181 5.331 14.310 0.14 60107. 0.5107
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6.72 0.1972 0.4080 0.0876 0.0424 0.052 1.624 1.173 38.428 0.183 5.216 13.840 0.14 60185. 0.4886
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7.68 0.2254 0.4509 0.0855 0.0428 0.052 1.639 1.144 38.781 0.185 5.090 13.382 0.14 60269. 0.4666
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8.65 0.2536 0.4903 0.0832 0.0430 0.052 1.649 1.113 39.028 0.186 4.951 12.937 0.14 60360. 0.4449
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9.61 0.2818 0.5266 0.0807 0.0432 0.053 1.655 1.079 39.151 0.187 4.801 12.504 0.14 60457. 0.4235
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10.57 0.3100 0.5598 0.0779 0.0431 0.052 1.654 1.043 39.133 0.187 4.637 12.083 0.14 60561. 0.4022
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11.53 0.3381 0.5900 0.0749 0.0429 0.052 1.646 1.003 38.955 0.186 4.460 11.675 0.14 60671. 0.3811
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12.49 0.3663 0.6174 0.0717 0.0426 0.052 1.631 0.960 38.603 0.184 4.269 11.277 0.14 60788. 0.3601
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13.45 0.3945 0.6420 0.0683 0.0420 0.051 1.609 0.914 38.064 0.182 4.064 10.888 0.14 60913. 0.3393
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14.41 0.4227 0.6637 0.0646 0.0411 0.050 1.577 0.865 37.326 0.178 3.846 10.507 0.14 61044. 0.3185
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15.37 0.4508 0.6826 0.0607 0.0401 0.049 1.537 0.812 36.379 0.174 3.614 10.130 0.14 61182. 0.2976
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16.33 0.4790 0.6983 0.0566 0.0388 0.047 1.488 0.757 35.214 0.168 3.368 9.754 0.14 61326. 0.2767
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17.29 0.5072 0.7107 0.0523 0.0373 0.045 1.430 0.700 33.840 0.162 3.112 9.376 0.14 61478. 0.2556
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18.25 0.5354 0.7193 0.0478 0.0356 0.043 1.364 0.640 32.268 0.154 2.845 8.990 0.14 61636. 0.2344
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19.21 0.5636 0.7236 0.0432 0.0336 0.041 1.289 0.578 30.511 0.146 2.570 8.591 0.15 61802. 0.2129
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20.17 0.5917 0.7225 0.0385 0.0315 0.038 1.208 0.515 28.578 0.136 2.290 8.170 0.15 61974. 0.1911
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21.13 0.6199 0.7149 0.0337 0.0292 0.036 1.119 0.451 26.480 0.126 2.004 7.717 0.15 62152. 0.1688
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22.09 0.6481 0.6990 0.0288 0.0267 0.032 1.024 0.385 24.227 0.116 1.715 7.217 0.15 62338. 0.1461
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23.05 0.6763 0.6719 0.0239 0.0241 0.029 0.923 0.320 21.832 0.104 1.423 6.648 0.15 62530. 0.1226
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24.02 0.7044 0.6293 0.0190 0.0213 0.026 0.816 0.254 19.307 0.092 1.132 5.977 0.15 62729. 0.0983
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24.98 0.7326 0.5636 0.0141 0.0184 0.022 0.704 0.189 16.669 0.080 0.841 5.148 0.15 62935. 0.0730
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25.94 0.7608 0.4613 0.0093 0.0154 0.019 0.589 0.125 13.938 0.067 0.554 4.057 0.15 63147. 0.0467
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26.90 0.7890 0.2947 0.0046 0.0123 0.015 0.471 0.061 11.134 0.053 0.273 2.499 0.15 63366. 0.0202
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27.86 0.8172 -0.0021 0.0000 0.0091 0.011 0.350 0.000 8.282 0.040 -0.001 -0.017 0.15 63590. 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 0.0982 0.0367 0.151 3.163 2.956 112.267 0.357 13.148 11.942 0.21 89638. 0.6693
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1.44 0.0282 0.0733 0.0971 0.0374 0.154 3.227 2.924 114.531 0.365 13.008 11.582 0.21 89706. 0.6456
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2.89 0.0565 0.1420 0.0960 0.0381 0.157 3.290 2.890 116.791 0.372 12.853 11.222 0.21 89781. 0.6218
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4.33 0.0847 0.2063 0.0947 0.0389 0.160 3.353 2.851 119.007 0.379 12.680 10.865 0.21 89863. 0.5980
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5.77 0.1129 0.2661 0.0932 0.0396 0.162 3.413 2.808 121.136 0.386 12.488 10.512 0.21 89954. 0.5742
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7.22 0.1412 0.3217 0.0917 0.0402 0.165 3.469 2.760 123.133 0.392 12.276 10.166 0.21 90053. 0.5505
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8.66 0.1694 0.3732 0.0899 0.0408 0.168 3.520 2.707 124.945 0.398 12.041 9.827 0.21 90161. 0.5271
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10.11 0.1976 0.4208 0.0880 0.0413 0.170 3.564 2.649 126.515 0.403 11.783 9.497 0.21 90278. 0.5039
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11.55 0.2259 0.4646 0.0859 0.0417 0.171 3.600 2.585 127.786 0.407 11.499 9.176 0.21 90405. 0.4809
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12.99 0.2541 0.5049 0.0835 0.0420 0.173 3.626 2.515 128.695 0.410 11.187 8.864 0.21 90541. 0.4583
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14.44 0.2823 0.5420 0.0810 0.0422 0.173 3.640 2.439 129.180 0.411 10.848 8.563 0.22 90687. 0.4359
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15.88 0.3106 0.5758 0.0782 0.0422 0.173 3.639 2.356 129.178 0.411 10.478 8.271 0.22 90843. 0.4138
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17.32 0.3388 0.6067 0.0752 0.0420 0.172 3.624 2.266 128.632 0.409 10.078 7.989 0.22 91010. 0.3920
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18.77 0.3670 0.6348 0.0720 0.0416 0.171 3.592 2.169 127.486 0.406 9.646 7.715 0.22 91186. 0.3704
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20.21 0.3953 0.6601 0.0686 0.0411 0.169 3.541 2.064 125.694 0.400 9.183 7.450 0.22 91373. 0.3489
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21.66 0.4235 0.6826 0.0649 0.0402 0.165 3.472 1.953 123.216 0.392 8.689 7.191 0.22 91571. 0.3276
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23.10 0.4517 0.7024 0.0610 0.0392 0.161 3.381 1.835 120.012 0.382 8.163 6.936 0.22 91778. 0.3063
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24.54 0.4799 0.7192 0.0568 0.0379 0.156 3.270 1.710 116.056 0.369 7.607 6.684 0.22 91996. 0.2850
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25.99 0.5082 0.7328 0.0525 0.0364 0.149 3.138 1.580 111.372 0.355 7.026 6.433 0.22 92225. 0.2635
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27.43 0.5364 0.7430 0.0480 0.0346 0.142 2.986 1.444 105.998 0.337 6.422 6.178 0.22 92463. 0.2420
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28.87 0.5646 0.7490 0.0433 0.0327 0.134 2.817 1.304 99.974 0.318 5.801 5.917 0.22 92712. 0.2203
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30.32 0.5929 0.7501 0.0386 0.0305 0.125 2.630 1.161 93.334 0.297 5.166 5.644 0.22 92971. 0.1983
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31.76 0.6211 0.7452 0.0337 0.0281 0.115 2.426 1.016 86.113 0.274 4.520 5.352 0.22 93240. 0.1759
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33.21 0.6493 0.7325 0.0289 0.0256 0.105 2.207 0.869 78.347 0.249 3.866 5.032 0.22 93519. 0.1529
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34.65 0.6776 0.7091 0.0240 0.0229 0.094 1.974 0.721 70.078 0.223 3.208 4.669 0.22 93809. 0.1293
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36.09 0.7058 0.6706 0.0190 0.0200 0.082 1.729 0.573 61.353 0.195 2.550 4.238 0.22 94108. 0.1046
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37.54 0.7340 0.6089 0.0142 0.0171 0.070 1.471 0.426 52.228 0.166 1.895 3.701 0.22 94418. 0.0787
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38.98 0.7623 0.5086 0.0093 0.0140 0.057 1.205 0.281 42.773 0.136 1.249 2.977 0.22 94737. 0.0514
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40.42 0.7905 0.3358 0.0046 0.0108 0.044 0.932 0.138 33.065 0.105 0.614 1.895 0.22 95066. 0.0230
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41.87 0.8187 -0.0021 0.0000 0.0076 0.031 0.653 -0.001 23.186 0.074 -0.003 -0.011 0.22 95403. 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 0.0986 0.0361 0.351 5.529 5.276 261.674 0.625 23.466 9.144 0.29 119514. 0.6847
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1.93 0.0283 0.0749 0.0975 0.0368 0.358 5.645 5.220 267.159 0.638 23.220 8.863 0.29 119605. 0.6601
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3.85 0.0565 0.1450 0.0964 0.0376 0.366 5.761 5.159 272.641 0.651 22.945 8.582 0.29 119705. 0.6354
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5.78 0.0848 0.2104 0.0951 0.0383 0.373 5.875 5.090 278.024 0.664 22.641 8.304 0.29 119815. 0.6107
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7.71 0.1130 0.2713 0.0937 0.0390 0.380 5.984 5.014 283.207 0.676 22.302 8.030 0.29 119936. 0.5861
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9.63 0.1413 0.3278 0.0921 0.0397 0.386 6.087 4.929 288.077 0.688 21.926 7.761 0.29 120068. 0.5617
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11.56 0.1696 0.3801 0.0903 0.0403 0.392 6.181 4.836 292.508 0.698 21.511 7.499 0.29 120213. 0.5376
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13.49 0.1978 0.4283 0.0884 0.0408 0.397 6.262 4.733 296.366 0.708 21.052 7.243 0.29 120369. 0.5137
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15.42 0.2261 0.4728 0.0863 0.0413 0.402 6.329 4.619 299.507 0.715 20.547 6.995 0.29 120538. 0.4901
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17.34 0.2544 0.5136 0.0840 0.0416 0.405 6.377 4.495 301.781 0.720 19.993 6.756 0.29 120720. 0.4669
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19.27 0.2826 0.5511 0.0814 0.0418 0.406 6.403 4.359 303.038 0.723 19.388 6.524 0.29 120916. 0.4440
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21.20 0.3109 0.5854 0.0787 0.0418 0.407 6.405 4.211 303.128 0.724 18.729 6.300 0.29 121125. 0.4214
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23.12 0.3391 0.6168 0.0757 0.0416 0.405 6.379 4.050 301.906 0.721 18.014 6.084 0.29 121347. 0.3992
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25.05 0.3674 0.6453 0.0724 0.0412 0.401 6.323 3.877 299.240 0.714 17.244 5.876 0.29 121583. 0.3771
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26.98 0.3957 0.6711 0.0690 0.0407 0.396 6.234 3.691 295.017 0.704 16.416 5.674 0.29 121833. 0.3554
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28.90 0.4239 0.6941 0.0652 0.0398 0.388 6.110 3.492 289.136 0.690 15.533 5.478 0.29 122097. 0.3337
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30.83 0.4522 0.7145 0.0613 0.0388 0.378 5.948 3.281 281.502 0.672 14.593 5.286 0.29 122375. 0.3121
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32.76 0.4804 0.7320 0.0571 0.0375 0.365 5.749 3.057 272.049 0.649 13.599 5.097 0.29 122666. 0.2905
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34.68 0.5087 0.7465 0.0527 0.0359 0.350 5.512 2.823 260.830 0.623 12.558 4.910 0.29 122971. 0.2689
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36.61 0.5370 0.7577 0.0482 0.0342 0.332 5.239 2.581 247.938 0.592 11.479 4.721 0.29 123290. 0.2472
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38.54 0.5652 0.7651 0.0435 0.0322 0.313 4.933 2.331 233.462 0.557 10.367 4.528 0.29 123623. 0.2254
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40.47 0.5935 0.7678 0.0388 0.0300 0.292 4.596 2.075 217.484 0.519 9.231 4.328 0.29 123969. 0.2032
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42.39 0.6218 0.7648 0.0339 0.0276 0.268 4.228 1.815 200.088 0.478 8.075 4.115 0.29 124328. 0.1807
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44.32 0.6500 0.7544 0.0290 0.0250 0.243 3.832 1.553 181.362 0.433 6.906 3.883 0.29 124701. 0.1577
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46.25 0.6783 0.7339 0.0241 0.0222 0.216 3.411 1.288 161.404 0.385 5.729 3.620 0.29 125088. 0.1339
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48.17 0.7065 0.6986 0.0191 0.0193 0.188 2.965 1.024 140.333 0.335 4.553 3.308 0.29 125488. 0.1091
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50.10 0.7348 0.6404 0.0142 0.0163 0.159 2.499 0.760 118.287 0.282 3.382 2.916 0.29 125901. 0.0829
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52.03 0.7631 0.5427 0.0094 0.0132 0.128 2.017 0.501 95.433 0.228 2.227 2.379 0.29 126328. 0.0549
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53.95 0.7913 0.3669 0.0046 0.0099 0.097 1.521 0.246 71.967 0.172 1.095 1.551 0.29 126768. 0.0251
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55.88 0.8196 -0.0034 0.0000 0.0066 0.064 1.016 -0.001 48.078 0.115 -0.007 -0.014 0.30 127218. 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 0.0990 0.0358 0.680 8.568 8.282 506.869 0.968 36.840 7.411 0.36 149388. 0.6953
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2.41 0.0283 0.0758 0.0980 0.0365 0.694 8.753 8.197 517.788 0.989 36.460 7.180 0.36 149501. 0.6701
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4.82 0.0565 0.1468 0.0969 0.0373 0.709 8.938 8.102 528.712 1.010 36.037 6.950 0.36 149626. 0.6449
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7.23 0.0848 0.2130 0.0956 0.0381 0.723 9.119 7.996 539.454 1.030 35.566 6.723 0.36 149764. 0.6197
|
|
9.64 0.1131 0.2746 0.0942 0.0388 0.737 9.294 7.878 549.812 1.050 35.042 6.499 0.36 149915. 0.5946
|
|
12.05 0.1413 0.3316 0.0926 0.0395 0.750 9.459 7.747 559.559 1.069 34.459 6.280 0.36 150081. 0.5698
|
|
14.45 0.1696 0.3844 0.0909 0.0401 0.762 9.609 7.602 568.449 1.086 33.813 6.066 0.36 150261. 0.5452
|
|
16.86 0.1979 0.4330 0.0890 0.0407 0.773 9.741 7.441 576.211 1.100 33.098 5.857 0.36 150457. 0.5209
|
|
19.27 0.2261 0.4779 0.0869 0.0411 0.781 9.848 7.264 582.560 1.113 32.311 5.656 0.36 150669. 0.4969
|
|
21.68 0.2544 0.5191 0.0845 0.0414 0.787 9.926 7.070 587.202 1.121 31.446 5.461 0.36 150897. 0.4733
|
|
24.09 0.2827 0.5569 0.0820 0.0416 0.791 9.971 6.857 589.832 1.126 30.500 5.273 0.36 151142. 0.4501
|
|
26.50 0.3109 0.5916 0.0792 0.0416 0.791 9.976 6.625 590.153 1.127 29.469 5.092 0.36 151403. 0.4272
|
|
28.91 0.3392 0.6232 0.0762 0.0415 0.788 9.938 6.374 587.876 1.123 28.350 4.917 0.36 151682. 0.4047
|
|
31.32 0.3675 0.6521 0.0730 0.0411 0.781 9.851 6.102 582.738 1.113 27.141 4.749 0.36 151977. 0.3824
|
|
33.73 0.3957 0.6782 0.0695 0.0405 0.770 9.712 5.810 574.508 1.097 25.843 4.587 0.36 152290. 0.3604
|
|
36.14 0.4240 0.7017 0.0657 0.0397 0.755 9.517 5.498 562.989 1.075 24.455 4.429 0.36 152620. 0.3386
|
|
38.55 0.4523 0.7226 0.0618 0.0387 0.735 9.263 5.166 547.987 1.047 22.979 4.276 0.36 152968. 0.3168
|
|
40.96 0.4805 0.7407 0.0576 0.0373 0.710 8.949 4.815 529.369 1.011 21.416 4.125 0.36 153332. 0.2951
|
|
43.36 0.5088 0.7559 0.0532 0.0358 0.680 8.574 4.447 507.229 0.969 19.779 3.976 0.36 153714. 0.2733
|
|
45.77 0.5371 0.7680 0.0486 0.0340 0.646 8.144 4.065 481.751 0.920 18.080 3.827 0.36 154113. 0.2515
|
|
48.18 0.5653 0.7763 0.0439 0.0320 0.608 7.660 3.672 453.106 0.865 16.331 3.675 0.36 154529. 0.2296
|
|
50.59 0.5936 0.7804 0.0391 0.0297 0.565 7.125 3.269 421.459 0.805 14.542 3.518 0.36 154962. 0.2074
|
|
53.00 0.6219 0.7790 0.0342 0.0273 0.519 6.542 2.860 386.973 0.739 12.722 3.352 0.36 155412. 0.1848
|
|
55.41 0.6502 0.7705 0.0293 0.0247 0.469 5.914 2.446 349.822 0.668 10.881 3.172 0.36 155878. 0.1617
|
|
57.82 0.6784 0.7524 0.0243 0.0219 0.416 5.244 2.030 310.205 0.592 9.029 2.968 0.37 156362. 0.1379
|
|
60.23 0.7067 0.7200 0.0193 0.0189 0.360 4.536 1.613 268.355 0.513 7.177 2.727 0.37 156862. 0.1129
|
|
62.64 0.7350 0.6652 0.0143 0.0158 0.301 3.796 1.199 224.552 0.429 5.334 2.422 0.37 157379. 0.0865
|
|
65.05 0.7632 0.5707 0.0094 0.0126 0.240 3.028 0.790 179.130 0.342 3.515 2.001 0.37 157913. 0.0580
|
|
67.46 0.7915 0.3946 0.0047 0.0093 0.178 2.240 0.390 132.485 0.253 1.734 1.334 0.37 158463. 0.0272
|
|
69.87 0.8198 0.0003 0.0000 0.0060 0.114 1.437 0.000 84.993 0.162 0.001 0.001 0.37 159025. 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 0.0996 0.0357 1.172 12.308 11.995 873.683 1.391 53.352 6.227 0.43 179257. 0.7030
|
|
2.89 0.0283 0.0765 0.0986 0.0365 1.197 12.579 11.874 892.924 1.421 52.816 6.032 0.43 179393. 0.6775
|
|
5.78 0.0566 0.1480 0.0975 0.0372 1.223 12.850 11.739 912.193 1.452 52.217 5.837 0.43 179543. 0.6520
|
|
8.68 0.0848 0.2147 0.0962 0.0380 1.249 13.117 11.589 931.164 1.482 51.547 5.645 0.43 179709. 0.6264
|
|
11.57 0.1131 0.2767 0.0948 0.0388 1.273 13.375 11.421 949.479 1.511 50.800 5.456 0.43 179891. 0.6010
|
|
14.46 0.1414 0.3341 0.0933 0.0395 1.296 13.619 11.234 966.741 1.539 49.968 5.271 0.43 180090. 0.5759
|
|
17.35 0.1697 0.3872 0.0916 0.0401 1.318 13.841 11.026 982.511 1.564 49.044 5.090 0.43 180307. 0.5510
|
|
20.24 0.1979 0.4362 0.0896 0.0407 1.336 14.035 10.796 996.313 1.586 48.020 4.915 0.43 180543. 0.5264
|
|
23.14 0.2262 0.4813 0.0875 0.0411 1.351 14.195 10.542 1007.644 1.604 46.890 4.745 0.43 180797. 0.5022
|
|
26.03 0.2545 0.5228 0.0852 0.0415 1.362 14.312 10.262 1015.983 1.617 45.645 4.581 0.43 181072. 0.4784
|
|
28.92 0.2828 0.5608 0.0827 0.0417 1.369 14.380 9.955 1020.794 1.625 44.282 4.423 0.43 181366. 0.4550
|
|
31.81 0.3111 0.5958 0.0799 0.0417 1.370 14.391 9.621 1021.548 1.626 42.793 4.272 0.43 181680. 0.4319
|
|
34.71 0.3393 0.6277 0.0769 0.0416 1.365 14.337 9.257 1017.738 1.620 41.176 4.126 0.43 182015. 0.4092
|
|
37.60 0.3676 0.6568 0.0736 0.0412 1.353 14.212 8.864 1008.896 1.606 39.427 3.985 0.43 182370. 0.3868
|
|
40.49 0.3959 0.6833 0.0701 0.0406 1.334 14.011 8.441 994.614 1.583 37.547 3.849 0.43 182746. 0.3646
|
|
43.38 0.4242 0.7072 0.0663 0.0398 1.307 13.728 7.989 974.540 1.551 35.536 3.718 0.43 183143. 0.3426
|
|
46.27 0.4525 0.7284 0.0623 0.0387 1.272 13.359 7.508 948.337 1.509 33.394 3.591 0.43 183561. 0.3207
|
|
49.17 0.4807 0.7470 0.0581 0.0374 1.228 12.900 6.998 915.761 1.457 31.125 3.466 0.43 183999. 0.2989
|
|
52.06 0.5090 0.7629 0.0537 0.0358 1.176 12.354 6.463 876.970 1.396 28.747 3.343 0.43 184458. 0.2770
|
|
54.95 0.5373 0.7756 0.0491 0.0340 1.116 11.724 5.908 832.278 1.325 26.279 3.220 0.43 184938. 0.2551
|
|
57.84 0.5656 0.7849 0.0443 0.0319 1.049 11.016 5.336 781.989 1.245 23.736 3.095 0.44 185437. 0.2331
|
|
60.73 0.5938 0.7899 0.0395 0.0297 0.974 10.233 4.751 726.388 1.156 21.134 2.967 0.44 185958. 0.2108
|
|
63.63 0.6221 0.7898 0.0345 0.0272 0.893 9.379 4.156 665.762 1.060 18.487 2.832 0.44 186498. 0.1882
|
|
66.52 0.6504 0.7830 0.0295 0.0245 0.805 8.458 3.554 600.420 0.956 15.809 2.685 0.44 187059. 0.1650
|
|
69.41 0.6787 0.7668 0.0245 0.0217 0.712 7.476 2.948 530.713 0.845 13.115 2.520 0.44 187639. 0.1410
|
|
72.30 0.7070 0.7368 0.0194 0.0187 0.613 6.439 2.342 457.054 0.727 10.418 2.324 0.44 188240. 0.1160
|
|
75.19 0.7352 0.6846 0.0144 0.0155 0.510 5.352 1.740 379.939 0.605 7.738 2.077 0.44 188861. 0.0893
|
|
78.09 0.7635 0.5925 0.0095 0.0122 0.402 4.226 1.145 299.966 0.477 5.091 1.731 0.44 189502. 0.0604
|
|
80.98 0.7918 0.4153 0.0047 0.0089 0.292 3.069 0.562 217.839 0.347 2.499 1.170 0.44 190163. 0.0286
|
|
83.87 0.8201 -0.0060 0.0000 0.0055 0.180 1.891 -0.005 134.209 0.214 -0.022 -0.016 0.44 190837. 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 0.1003 0.0357 1.864 16.786 16.436 1390.158 1.896 73.108 5.363 0.50 209122. 0.7087
|
|
3.37 0.0283 0.0768 0.0993 0.0365 1.906 17.162 16.276 1421.353 1.939 72.396 5.194 0.50 209280. 0.6831
|
|
6.75 0.0566 0.1487 0.0982 0.0374 1.948 17.540 16.097 1452.633 1.982 71.598 5.026 0.50 209456. 0.6573
|
|
10.12 0.0848 0.2157 0.0970 0.0381 1.989 17.912 15.896 1483.464 2.024 70.704 4.860 0.50 209649. 0.6316
|
|
13.50 0.1131 0.2779 0.0956 0.0389 2.029 18.272 15.671 1513.275 2.064 69.703 4.697 0.50 209862. 0.6061
|
|
16.87 0.1414 0.3356 0.0941 0.0396 2.067 18.612 15.419 1541.411 2.103 68.585 4.537 0.50 210095. 0.5808
|
|
20.24 0.1697 0.3889 0.0924 0.0403 2.102 18.923 15.139 1567.159 2.138 67.339 4.382 0.50 210348. 0.5557
|
|
23.62 0.1979 0.4380 0.0905 0.0409 2.132 19.196 14.828 1589.748 2.169 65.955 4.231 0.50 210623. 0.5310
|
|
26.99 0.2262 0.4833 0.0884 0.0414 2.157 19.420 14.484 1608.358 2.194 64.423 4.085 0.50 210921. 0.5067
|
|
30.37 0.2545 0.5250 0.0860 0.0417 2.175 19.587 14.104 1622.139 2.213 62.734 3.944 0.50 211241. 0.4828
|
|
33.74 0.2828 0.5632 0.0835 0.0419 2.186 19.684 13.687 1630.224 2.224 60.878 3.808 0.50 211585. 0.4592
|
|
37.11 0.3110 0.5984 0.0807 0.0420 2.188 19.703 13.230 1631.751 2.226 58.849 3.678 0.50 211952. 0.4361
|
|
40.49 0.3393 0.6305 0.0777 0.0418 2.180 19.632 12.734 1625.894 2.218 56.641 3.552 0.50 212343. 0.4132
|
|
43.86 0.3676 0.6599 0.0744 0.0414 2.162 19.463 12.196 1611.890 2.199 54.250 3.432 0.50 212759. 0.3907
|
|
47.24 0.3959 0.6867 0.0709 0.0409 2.131 19.187 11.618 1589.074 2.168 51.675 3.316 0.50 213198. 0.3684
|
|
50.61 0.4242 0.7109 0.0671 0.0400 2.088 18.799 10.998 1556.878 2.124 48.918 3.204 0.50 213662. 0.3464
|
|
53.98 0.4524 0.7325 0.0631 0.0389 2.031 18.290 10.337 1514.756 2.066 45.979 3.095 0.50 214150. 0.3244
|
|
57.36 0.4807 0.7516 0.0588 0.0376 1.961 17.657 9.637 1462.301 1.995 42.864 2.989 0.51 214662. 0.3025
|
|
60.73 0.5090 0.7680 0.0543 0.0360 1.877 16.901 8.902 1399.749 1.910 39.595 2.885 0.51 215198. 0.2805
|
|
64.11 0.5373 0.7814 0.0496 0.0341 1.780 16.030 8.138 1327.602 1.811 36.200 2.780 0.51 215757. 0.2586
|
|
67.48 0.5655 0.7915 0.0448 0.0320 1.671 15.049 7.352 1246.351 1.700 32.700 2.675 0.51 216341. 0.2365
|
|
70.85 0.5938 0.7975 0.0399 0.0297 1.551 13.964 6.546 1156.459 1.578 29.118 2.567 0.51 216948. 0.2141
|
|
74.23 0.6221 0.7986 0.0349 0.0272 1.419 12.780 5.727 1058.391 1.444 25.472 2.454 0.51 217579. 0.1914
|
|
77.60 0.6504 0.7932 0.0299 0.0245 1.278 11.503 4.897 952.647 1.300 21.781 2.331 0.51 218233. 0.1682
|
|
80.97 0.6786 0.7788 0.0248 0.0216 1.126 10.140 4.062 839.799 1.146 18.067 2.194 0.51 218911. 0.1441
|
|
84.35 0.7069 0.7510 0.0197 0.0185 0.966 8.700 3.226 720.520 0.983 14.350 2.031 0.51 219613. 0.1189
|
|
87.72 0.7352 0.7014 0.0146 0.0153 0.799 7.192 2.395 595.618 0.813 10.654 1.824 0.51 220337. 0.0920
|
|
91.10 0.7635 0.6120 0.0096 0.0120 0.625 5.628 1.575 466.070 0.636 7.004 1.532 0.51 221085. 0.0627
|
|
94.47 0.7918 0.4349 0.0047 0.0086 0.447 4.021 0.771 333.033 0.454 3.429 1.050 0.52 221856. 0.0301
|
|
97.84 0.8200 -0.0104 -0.0001 0.0051 0.265 2.385 -0.011 197.547 0.269 -0.047 -0.024 0.52 222641. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1011 0.0360 2.799 22.054 21.636 2087.376 2.492 96.238 4.701 0.57 238981. 0.7129
|
|
3.85 0.0282 0.0769 0.1001 0.0368 2.863 22.557 21.434 2135.005 2.548 95.340 4.554 0.57 239162. 0.6872
|
|
7.70 0.0565 0.1488 0.0990 0.0376 2.927 23.062 21.207 2182.838 2.606 94.328 4.407 0.57 239362. 0.6615
|
|
11.56 0.0848 0.2159 0.0979 0.0384 2.991 23.561 20.951 2230.058 2.662 93.190 4.261 0.57 239583. 0.6358
|
|
15.41 0.1130 0.2782 0.0965 0.0392 3.052 24.044 20.664 2275.788 2.717 91.911 4.118 0.57 239826. 0.6103
|
|
19.26 0.1412 0.3359 0.0950 0.0399 3.110 24.501 20.341 2319.026 2.768 90.478 3.978 0.57 240092. 0.5849
|
|
23.11 0.1695 0.3893 0.0933 0.0406 3.163 24.920 19.981 2358.677 2.815 88.874 3.842 0.57 240382. 0.5599
|
|
26.97 0.1978 0.4386 0.0914 0.0412 3.210 25.289 19.579 2393.559 2.857 87.087 3.710 0.57 240696. 0.5351
|
|
30.82 0.2260 0.4840 0.0894 0.0417 3.249 25.594 19.133 2422.418 2.892 85.102 3.582 0.57 241037. 0.5108
|
|
34.67 0.2542 0.5258 0.0871 0.0421 3.277 25.821 18.639 2443.946 2.917 82.907 3.459 0.57 241403. 0.4868
|
|
38.52 0.2825 0.5642 0.0845 0.0423 3.295 25.957 18.096 2456.817 2.933 80.490 3.341 0.57 241796. 0.4633
|
|
42.38 0.3108 0.5995 0.0817 0.0424 3.299 25.988 17.500 2459.718 2.936 77.841 3.227 0.57 242216. 0.4401
|
|
46.23 0.3390 0.6319 0.0787 0.0422 3.287 25.900 16.851 2451.376 2.926 74.952 3.118 0.57 242663. 0.4172
|
|
50.08 0.3672 0.6615 0.0754 0.0419 3.260 25.680 16.146 2430.624 2.901 71.818 3.013 0.58 243138. 0.3947
|
|
53.93 0.3955 0.6885 0.0719 0.0413 3.214 25.319 15.386 2396.444 2.861 68.437 2.912 0.58 243640. 0.3724
|
|
57.78 0.4238 0.7130 0.0681 0.0404 3.149 24.807 14.571 2347.966 2.803 64.812 2.815 0.58 244170. 0.3503
|
|
61.64 0.4520 0.7351 0.0640 0.0393 3.063 24.135 13.701 2284.370 2.727 60.944 2.720 0.58 244728. 0.3283
|
|
65.49 0.4803 0.7546 0.0597 0.0380 2.957 23.297 12.778 2205.010 2.632 56.838 2.628 0.58 245313. 0.3063
|
|
69.34 0.5085 0.7716 0.0552 0.0363 2.830 22.295 11.809 2110.198 2.519 52.525 2.538 0.58 245925. 0.2843
|
|
73.19 0.5368 0.7857 0.0504 0.0345 2.683 21.138 10.800 2000.694 2.388 48.039 2.448 0.58 246564. 0.2623
|
|
77.05 0.5650 0.7965 0.0456 0.0323 2.517 19.834 9.760 1877.247 2.241 43.413 2.358 0.58 247231. 0.2402
|
|
80.90 0.5932 0.8035 0.0406 0.0300 2.334 18.390 8.695 1740.567 2.078 38.673 2.266 0.58 247924. 0.2178
|
|
84.75 0.6215 0.8058 0.0355 0.0274 2.134 16.813 7.609 1591.361 1.900 33.847 2.169 0.58 248645. 0.1950
|
|
88.60 0.6497 0.8019 0.0304 0.0246 1.918 15.113 6.510 1430.396 1.707 28.959 2.064 0.58 249392. 0.1717
|
|
92.45 0.6780 0.7893 0.0252 0.0217 1.688 13.297 5.404 1258.540 1.502 24.036 1.947 0.58 250165. 0.1476
|
|
96.31 0.7063 0.7639 0.0201 0.0185 1.444 11.377 4.296 1076.823 1.285 19.107 1.809 0.59 250966. 0.1222
|
|
100.16 0.7345 0.7174 0.0149 0.0153 1.189 9.366 3.193 886.480 1.058 14.204 1.634 0.59 251793. 0.0952
|
|
104.01 0.7628 0.6317 0.0098 0.0119 0.924 7.280 2.104 689.006 0.822 9.361 1.385 0.59 252646. 0.0655
|
|
107.86 0.7910 0.4578 0.0048 0.0084 0.652 5.137 1.038 486.181 0.580 4.616 0.968 0.59 253526. 0.0321
|
|
111.72 0.8193 0.0002 0.0000 0.0048 0.375 2.954 0.000 279.632 0.334 0.001 0.000 0.59 254422. 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 0.1020 0.0363 4.024 28.182 27.631 3000.805 3.184 122.902 4.176 0.64 268833. 0.7156
|
|
4.33 0.0282 0.0768 0.1011 0.0371 4.117 28.835 27.386 3070.409 3.258 121.815 4.046 0.64 269036. 0.6901
|
|
8.66 0.0565 0.1487 0.1000 0.0380 4.211 29.493 27.110 3140.474 3.332 120.584 3.915 0.64 269261. 0.6646
|
|
12.99 0.0847 0.2157 0.0989 0.0388 4.304 30.144 26.797 3209.788 3.406 119.192 3.787 0.64 269510. 0.6390
|
|
17.33 0.1129 0.2780 0.0976 0.0396 4.395 30.776 26.443 3277.044 3.477 117.621 3.660 0.64 269783. 0.6135
|
|
21.66 0.1412 0.3357 0.0961 0.0404 4.480 31.374 26.045 3340.773 3.545 115.849 3.536 0.64 270083. 0.5883
|
|
25.99 0.1694 0.3891 0.0945 0.0411 4.559 31.925 25.598 3399.354 3.607 113.859 3.415 0.64 270409. 0.5633
|
|
30.32 0.1976 0.4385 0.0926 0.0417 4.628 32.410 25.097 3451.035 3.662 111.630 3.298 0.64 270763. 0.5387
|
|
34.65 0.2259 0.4839 0.0906 0.0423 4.685 32.813 24.538 3493.965 3.707 109.144 3.185 0.64 271147. 0.5144
|
|
38.98 0.2541 0.5258 0.0883 0.0427 4.729 33.116 23.917 3526.226 3.741 106.384 3.076 0.64 271559. 0.4904
|
|
43.32 0.2824 0.5643 0.0857 0.0429 4.755 33.301 23.232 3545.859 3.762 103.335 2.972 0.65 272002. 0.4669
|
|
47.65 0.3106 0.5997 0.0830 0.0430 4.762 33.348 22.478 3550.934 3.768 99.982 2.871 0.65 272475. 0.4437
|
|
51.98 0.3388 0.6323 0.0799 0.0428 4.747 33.242 21.654 3539.588 3.756 96.317 2.775 0.65 272979. 0.4209
|
|
56.31 0.3671 0.6622 0.0766 0.0425 4.707 32.965 20.758 3510.104 3.724 92.331 2.682 0.65 273514. 0.3984
|
|
60.64 0.3953 0.6895 0.0730 0.0419 4.641 32.503 19.789 3460.983 3.672 88.022 2.593 0.65 274080. 0.3761
|
|
64.97 0.4235 0.7143 0.0692 0.0410 4.547 31.846 18.748 3390.955 3.598 83.393 2.508 0.65 274677. 0.3540
|
|
69.31 0.4518 0.7368 0.0651 0.0399 4.424 30.981 17.636 3298.842 3.500 78.446 2.425 0.65 275305. 0.3320
|
|
73.64 0.4800 0.7567 0.0607 0.0385 4.269 29.899 16.454 3183.675 3.378 73.188 2.344 0.65 275963. 0.3100
|
|
77.97 0.5082 0.7742 0.0561 0.0368 4.085 28.605 15.210 3045.853 3.232 67.656 2.265 0.65 276653. 0.2880
|
|
82.30 0.5365 0.7889 0.0514 0.0349 3.871 27.108 13.916 2886.471 3.063 61.896 2.187 0.65 277373. 0.2659
|
|
86.63 0.5647 0.8006 0.0464 0.0327 3.630 25.419 12.579 2706.641 2.872 55.950 2.108 0.65 278123. 0.2437
|
|
90.96 0.5929 0.8085 0.0414 0.0303 3.362 23.548 11.208 2507.401 2.660 49.852 2.027 0.65 278903. 0.2213
|
|
95.29 0.6212 0.8118 0.0362 0.0277 3.071 21.504 9.811 2289.793 2.430 43.637 1.943 0.66 279713. 0.1984
|
|
99.63 0.6494 0.8093 0.0310 0.0249 2.756 19.299 8.395 2054.941 2.180 37.339 1.853 0.66 280554. 0.1750
|
|
103.96 0.6777 0.7984 0.0257 0.0218 2.419 16.943 6.968 1804.117 1.914 30.993 1.752 0.66 281424. 0.1507
|
|
108.29 0.7059 0.7750 0.0204 0.0186 2.064 14.452 5.538 1538.831 1.633 24.635 1.632 0.66 282324. 0.1252
|
|
112.62 0.7341 0.7310 0.0152 0.0153 1.691 11.842 4.116 1260.898 1.338 18.307 1.481 0.66 283254. 0.0979
|
|
116.95 0.7624 0.6481 0.0100 0.0118 1.304 9.133 2.710 972.521 1.032 12.055 1.264 0.66 284213. 0.0678
|
|
121.28 0.7906 0.4752 0.0049 0.0082 0.907 6.352 1.333 676.346 0.718 5.928 0.894 0.66 285202. 0.0336
|
|
125.62 0.8188 -0.0049 0.0000 0.0045 0.503 3.520 -0.007 374.793 0.398 -0.033 -0.009 0.66 286208. 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 0.1030 0.0370 5.634 35.507 34.459 4200.932 4.012 153.273 3.720 0.71 298676. 0.7119
|
|
4.81 0.0282 0.0761 0.1022 0.0379 5.760 36.304 34.176 4295.134 4.102 152.014 3.609 0.71 298901. 0.6878
|
|
9.62 0.0564 0.1474 0.1012 0.0387 5.888 37.108 33.853 4390.324 4.192 150.578 3.497 0.71 299151. 0.6633
|
|
14.42 0.0846 0.2141 0.1001 0.0396 6.014 37.907 33.485 4484.896 4.283 148.942 3.386 0.71 299427. 0.6388
|
|
19.23 0.1128 0.2763 0.0988 0.0404 6.138 38.687 33.067 4577.094 4.371 147.083 3.277 0.71 299731. 0.6142
|
|
24.04 0.1410 0.3340 0.0974 0.0411 6.256 39.429 32.593 4664.909 4.455 144.972 3.169 0.71 300063. 0.5898
|
|
28.85 0.1692 0.3875 0.0958 0.0419 6.365 40.115 32.056 4746.088 4.532 142.584 3.063 0.72 300426. 0.5654
|
|
33.66 0.1975 0.4369 0.0940 0.0425 6.461 40.724 31.451 4818.177 4.601 139.893 2.961 0.72 300820. 0.5413
|
|
38.47 0.2257 0.4825 0.0920 0.0430 6.542 41.235 30.772 4878.538 4.659 136.875 2.861 0.72 301246. 0.5174
|
|
43.27 0.2539 0.5245 0.0897 0.0434 6.604 41.622 30.015 4924.416 4.702 133.506 2.765 0.72 301705. 0.4937
|
|
48.08 0.2821 0.5632 0.0872 0.0437 6.642 41.864 29.174 4952.954 4.730 129.767 2.672 0.72 302197. 0.4704
|
|
52.89 0.3103 0.5988 0.0844 0.0438 6.653 41.934 28.246 4961.287 4.738 125.638 2.582 0.72 302724. 0.4474
|
|
57.70 0.3385 0.6315 0.0814 0.0436 6.634 41.810 27.227 4946.631 4.724 121.108 2.497 0.72 303284. 0.4247
|
|
62.51 0.3667 0.6616 0.0781 0.0433 6.580 41.470 26.116 4906.399 4.685 116.166 2.414 0.72 303879. 0.4022
|
|
67.31 0.3949 0.6892 0.0745 0.0427 6.488 40.895 24.912 4838.388 4.620 110.809 2.335 0.72 304509. 0.3800
|
|
72.12 0.4231 0.7144 0.0706 0.0418 6.358 40.070 23.615 4740.806 4.527 105.041 2.259 0.72 305173. 0.3579
|
|
76.93 0.4513 0.7372 0.0664 0.0407 6.185 38.982 22.227 4612.013 4.404 98.864 2.186 0.72 305871. 0.3359
|
|
81.74 0.4795 0.7577 0.0620 0.0393 5.968 37.618 20.748 4450.609 4.250 92.286 2.114 0.72 306603. 0.3140
|
|
86.55 0.5077 0.7757 0.0574 0.0375 5.709 35.982 19.189 4257.048 4.065 85.353 2.045 0.72 307369. 0.2919
|
|
91.36 0.5360 0.7911 0.0525 0.0356 5.408 34.087 17.564 4032.875 3.851 78.123 1.975 0.72 308169. 0.2699
|
|
96.16 0.5642 0.8035 0.0475 0.0333 5.069 31.947 15.883 3779.667 3.609 70.647 1.906 0.73 309003. 0.2476
|
|
100.97 0.5924 0.8124 0.0423 0.0309 4.692 29.574 14.158 3498.914 3.341 62.973 1.835 0.73 309870. 0.2251
|
|
105.78 0.6206 0.8169 0.0371 0.0282 4.281 26.981 12.398 3192.132 3.048 55.144 1.762 0.73 310770. 0.2022
|
|
110.59 0.6488 0.8157 0.0317 0.0252 3.837 24.182 10.612 2860.988 2.732 47.203 1.682 0.73 311703. 0.1787
|
|
115.40 0.6770 0.8063 0.0263 0.0221 3.363 21.193 8.811 2507.421 2.394 39.193 1.594 0.73 312669. 0.1542
|
|
120.21 0.7052 0.7848 0.0209 0.0188 2.861 18.035 7.006 2133.777 2.038 31.162 1.489 0.73 313668. 0.1285
|
|
125.01 0.7334 0.7427 0.0156 0.0154 2.337 14.732 5.207 1742.949 1.664 23.162 1.355 0.73 314700. 0.1008
|
|
129.82 0.7616 0.6612 0.0102 0.0118 1.795 11.314 3.429 1338.528 1.278 15.251 1.162 0.73 315764. 0.0701
|
|
134.63 0.7898 0.4876 0.0050 0.0082 1.240 7.817 1.684 924.865 0.883 7.493 0.826 0.74 316861. 0.0350
|
|
139.44 0.8180 -0.0074 0.0000 0.0045 0.679 4.277 -0.013 506.020 0.483 -0.060 -0.012 0.74 317977. 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 0.1041 0.0394 7.973 45.685 42.148 5945.518 5.161 187.474 3.215 0.79 328508. 0.6805
|
|
5.28 0.0282 0.0725 0.1033 0.0402 8.126 46.563 41.835 6059.798 5.261 186.081 3.131 0.79 328755. 0.6602
|
|
10.56 0.0563 0.1410 0.1025 0.0409 8.280 47.445 41.475 6174.605 5.360 184.481 3.047 0.79 329029. 0.6396
|
|
15.84 0.0845 0.2057 0.1014 0.0417 8.432 48.315 41.062 6287.830 5.459 182.642 2.962 0.79 329332. 0.6187
|
|
21.12 0.1126 0.2664 0.1003 0.0424 8.579 49.155 40.587 6397.177 5.554 180.532 2.878 0.79 329665. 0.5976
|
|
26.40 0.1408 0.3234 0.0989 0.0431 8.717 49.946 40.044 6500.064 5.643 178.115 2.794 0.79 330030. 0.5764
|
|
31.68 0.1689 0.3766 0.0974 0.0437 8.842 50.665 39.424 6593.646 5.724 175.356 2.712 0.79 330428. 0.5551
|
|
36.96 0.1971 0.4263 0.0956 0.0442 8.951 51.289 38.718 6674.854 5.795 172.219 2.631 0.79 330861. 0.5337
|
|
42.24 0.2253 0.4725 0.0937 0.0447 9.039 51.793 37.921 6740.470 5.852 168.672 2.552 0.79 331330. 0.5122
|
|
47.52 0.2534 0.5154 0.0915 0.0450 9.102 52.151 37.024 6787.149 5.892 164.684 2.474 0.79 331834. 0.4908
|
|
52.80 0.2816 0.5552 0.0890 0.0451 9.134 52.338 36.022 6811.439 5.913 160.226 2.399 0.79 332376. 0.4693
|
|
58.08 0.3097 0.5920 0.0862 0.0451 9.132 52.326 34.909 6809.841 5.912 155.276 2.325 0.79 332955. 0.4478
|
|
63.36 0.3379 0.6259 0.0832 0.0449 9.091 52.088 33.681 6778.883 5.885 149.814 2.254 0.79 333572. 0.4263
|
|
68.64 0.3661 0.6572 0.0799 0.0445 9.005 51.599 32.336 6715.233 5.830 143.829 2.184 0.79 334227. 0.4049
|
|
73.92 0.3942 0.6858 0.0763 0.0438 8.872 50.835 30.871 6615.848 5.743 137.316 2.116 0.79 334920. 0.3833
|
|
79.20 0.4224 0.7120 0.0724 0.0429 8.687 49.776 29.289 6478.021 5.624 130.277 2.051 0.79 335650. 0.3618
|
|
84.47 0.4505 0.7357 0.0682 0.0417 8.447 48.402 27.589 6299.202 5.468 122.718 1.987 0.79 336418. 0.3401
|
|
89.75 0.4787 0.7570 0.0637 0.0403 8.149 46.695 25.775 6076.988 5.276 114.648 1.924 0.79 337223. 0.3184
|
|
95.03 0.5068 0.7758 0.0589 0.0385 7.793 44.655 23.858 5811.556 5.045 106.118 1.862 0.80 338066. 0.2965
|
|
100.31 0.5350 0.7918 0.0540 0.0365 7.382 42.299 21.853 5504.915 4.779 97.203 1.801 0.80 338945. 0.2744
|
|
105.59 0.5632 0.8049 0.0489 0.0342 6.918 39.641 19.777 5158.974 4.479 87.969 1.739 0.80 339861. 0.2521
|
|
110.87 0.5913 0.8144 0.0436 0.0316 6.405 36.699 17.642 4776.058 4.146 78.472 1.675 0.80 340814. 0.2294
|
|
116.15 0.6195 0.8192 0.0382 0.0289 5.845 33.492 15.461 4358.713 3.784 68.769 1.609 0.80 341802. 0.2062
|
|
121.43 0.6476 0.8179 0.0327 0.0259 5.243 30.044 13.245 3909.995 3.394 58.912 1.536 0.80 342827. 0.1823
|
|
126.71 0.6758 0.8077 0.0272 0.0228 4.604 26.383 11.006 3433.498 2.981 48.955 1.454 0.80 343887. 0.1572
|
|
131.99 0.7040 0.7836 0.0216 0.0194 3.934 22.541 8.758 2933.521 2.547 38.956 1.354 0.80 344984. 0.1306
|
|
137.27 0.7321 0.7363 0.0161 0.0160 3.239 18.559 6.515 2415.354 2.097 28.979 1.223 0.81 346116. 0.1018
|
|
142.55 0.7603 0.6455 0.0106 0.0125 2.528 14.486 4.293 1885.288 1.637 19.097 1.033 0.81 347283. 0.0698
|
|
147.83 0.7884 0.4594 0.0052 0.0089 1.811 10.377 2.111 1350.537 1.172 9.388 0.709 0.81 348486. 0.0336
|
|
153.11 0.8166 -0.0066 0.0000 0.0054 1.097 6.283 -0.018 817.675 0.710 -0.079 -0.010 0.81 349712. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 12000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.1051 0.0450 11.824 62.106 50.652 8817.516 7.017 225.299 2.606 0.86 358331. 0.6045
|
|
5.76 0.0282 0.0645 0.1045 0.0457 11.998 63.019 50.324 8947.003 7.120 223.841 2.551 0.86 358599. 0.5900
|
|
11.53 0.0564 0.1262 0.1037 0.0463 12.168 63.912 49.944 9073.844 7.221 222.149 2.497 0.86 358897. 0.5751
|
|
17.29 0.0845 0.1851 0.1028 0.0469 12.330 64.764 49.501 9194.801 7.317 220.181 2.442 0.86 359226. 0.5600
|
|
23.05 0.1127 0.2413 0.1017 0.0475 12.480 65.549 48.987 9306.304 7.406 217.892 2.388 0.86 359589. 0.5447
|
|
28.82 0.1409 0.2948 0.1004 0.0480 12.612 66.245 48.390 9405.016 7.484 215.238 2.334 0.86 359987. 0.5292
|
|
34.58 0.1691 0.3457 0.0990 0.0484 12.722 66.823 47.700 9487.098 7.550 212.171 2.281 0.86 360422. 0.5134
|
|
40.34 0.1972 0.3941 0.0974 0.0487 12.805 67.257 46.907 9548.706 7.599 208.643 2.228 0.86 360896. 0.4975
|
|
46.11 0.2254 0.4400 0.0955 0.0489 12.855 67.519 46.000 9585.958 7.628 204.610 2.177 0.86 361408. 0.4812
|
|
51.87 0.2536 0.4834 0.0933 0.0490 12.867 67.583 44.970 9595.065 7.636 200.026 2.126 0.86 361961. 0.4647
|
|
57.63 0.2818 0.5245 0.0909 0.0489 12.837 67.422 43.807 9572.250 7.617 194.855 2.076 0.86 362554. 0.4479
|
|
63.40 0.3099 0.5632 0.0882 0.0486 12.758 67.011 42.505 9513.885 7.571 189.061 2.026 0.86 363189. 0.4307
|
|
69.16 0.3381 0.5996 0.0852 0.0481 12.628 66.326 41.056 9416.533 7.493 182.619 1.978 0.86 363865. 0.4131
|
|
74.93 0.3663 0.6337 0.0819 0.0473 12.441 65.343 39.459 9277.025 7.382 175.512 1.929 0.86 364583. 0.3950
|
|
80.69 0.3945 0.6654 0.0783 0.0464 12.193 64.044 37.709 9092.543 7.236 167.731 1.881 0.86 365342. 0.3766
|
|
86.45 0.4227 0.6947 0.0743 0.0452 11.882 62.410 35.810 8860.565 7.051 159.281 1.833 0.86 366143. 0.3576
|
|
92.22 0.4508 0.7216 0.0701 0.0438 11.504 60.423 33.761 8578.460 6.827 150.168 1.785 0.87 366985. 0.3381
|
|
97.98 0.4790 0.7460 0.0655 0.0421 11.055 58.066 31.566 8243.818 6.560 140.405 1.737 0.87 367868. 0.3181
|
|
103.74 0.5072 0.7677 0.0607 0.0401 10.536 55.339 29.239 7856.648 6.252 130.055 1.688 0.87 368791. 0.2975
|
|
109.51 0.5354 0.7860 0.0556 0.0379 9.956 52.291 26.800 7423.973 5.908 119.205 1.637 0.87 369754. 0.2763
|
|
115.27 0.5635 0.8001 0.0504 0.0355 9.322 48.965 24.266 6951.739 5.532 107.937 1.583 0.87 370757. 0.2542
|
|
121.03 0.5917 0.8087 0.0450 0.0329 8.642 45.390 21.655 6444.143 5.128 96.322 1.524 0.87 371800. 0.2312
|
|
126.80 0.6199 0.8104 0.0394 0.0301 7.920 41.597 18.982 5905.729 4.700 84.430 1.458 0.87 372882. 0.2070
|
|
132.56 0.6481 0.8036 0.0338 0.0272 7.153 37.568 16.262 5333.754 4.244 72.333 1.383 0.87 374003. 0.1818
|
|
138.32 0.6762 0.7848 0.0280 0.0242 6.350 33.355 13.512 4735.492 3.768 60.102 1.294 0.88 375163. 0.1551
|
|
144.09 0.7044 0.7476 0.0223 0.0210 5.524 29.013 10.749 4119.077 3.278 47.809 1.184 0.88 376361. 0.1265
|
|
149.85 0.7326 0.6815 0.0166 0.0178 4.685 24.605 7.990 3493.278 2.780 35.539 1.037 0.88 377599. 0.0956
|
|
155.61 0.7608 0.5672 0.0109 0.0146 3.846 20.201 5.257 2868.084 2.282 23.385 0.831 0.88 378875. 0.0621
|
|
161.38 0.7890 0.3667 0.0053 0.0115 3.023 15.878 2.576 2254.259 1.794 11.458 0.518 0.88 380189. 0.0271
|
|
167.14 0.8171 -0.0069 -0.0001 0.0085 2.224 11.683 -0.035 1658.616 1.320 -0.154 -0.009 0.89 381532. 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 0.1044 0.0518 17.290 83.826 59.006 12892.854 9.471 262.459 2.076 0.93 388220. 0.5198
|
|
6.29 0.0284 0.0561 0.1038 0.0525 17.539 85.034 58.706 13078.683 9.607 261.123 2.036 0.93 388505. 0.5085
|
|
12.57 0.0567 0.1100 0.1032 0.0532 17.784 86.225 58.352 13261.848 9.742 259.552 1.996 0.93 388823. 0.4970
|
|
18.86 0.0851 0.1617 0.1025 0.0539 18.019 87.362 57.935 13436.755 9.870 257.694 1.956 0.93 389176. 0.4852
|
|
25.15 0.1135 0.2112 0.1016 0.0546 18.234 88.404 57.440 13597.034 9.988 255.494 1.916 0.93 389565. 0.4734
|
|
31.44 0.1419 0.2587 0.1006 0.0551 18.420 89.304 56.855 13735.493 10.090 252.889 1.877 0.93 389994. 0.4615
|
|
37.72 0.1702 0.3043 0.0993 0.0556 18.566 90.013 56.163 13844.446 10.170 249.811 1.840 0.93 390463. 0.4495
|
|
44.01 0.1986 0.3481 0.0979 0.0559 18.662 90.478 55.349 13916.013 10.222 246.191 1.804 0.93 390976. 0.4375
|
|
50.30 0.2270 0.3902 0.0962 0.0560 18.697 90.651 54.397 13942.627 10.242 241.959 1.770 0.93 391532. 0.4255
|
|
56.58 0.2554 0.4308 0.0943 0.0559 18.664 90.488 53.293 13917.468 10.223 237.049 1.737 0.93 392133. 0.4133
|
|
62.87 0.2837 0.4701 0.0920 0.0555 18.553 89.950 52.023 13834.806 10.163 231.400 1.706 0.93 392780. 0.4010
|
|
69.16 0.3121 0.5080 0.0895 0.0550 18.359 89.010 50.576 13690.267 10.056 224.962 1.676 0.93 393474. 0.3885
|
|
75.45 0.3405 0.5446 0.0866 0.0541 18.078 87.649 48.941 13480.831 9.902 217.691 1.647 0.93 394214. 0.3755
|
|
81.73 0.3688 0.5799 0.0833 0.0530 17.708 85.853 47.114 13204.712 9.700 209.561 1.618 0.93 395002. 0.3621
|
|
88.02 0.3972 0.6136 0.0798 0.0516 17.247 83.620 45.090 12861.182 9.447 200.560 1.590 0.94 395835. 0.3481
|
|
94.31 0.4256 0.6457 0.0758 0.0500 16.696 80.948 42.870 12450.267 9.145 190.688 1.562 0.94 396715. 0.3333
|
|
100.59 0.4540 0.6760 0.0716 0.0481 16.055 77.839 40.458 11972.006 8.794 179.957 1.533 0.94 397640. 0.3178
|
|
106.88 0.4823 0.7041 0.0670 0.0459 15.322 74.288 37.856 11425.938 8.393 168.381 1.503 0.94 398611. 0.3014
|
|
113.17 0.5107 0.7300 0.0620 0.0434 14.502 70.311 35.081 10814.234 7.944 156.039 1.471 0.94 399626. 0.2841
|
|
119.46 0.5391 0.7531 0.0569 0.0407 13.604 65.955 32.162 10144.198 7.452 143.054 1.438 0.94 400685. 0.2658
|
|
125.74 0.5675 0.7709 0.0515 0.0379 12.665 61.404 29.119 9444.299 6.937 129.520 1.398 0.94 401789. 0.2460
|
|
132.03 0.5958 0.7813 0.0459 0.0350 11.704 56.743 25.975 8727.403 6.411 115.535 1.350 0.94 402935. 0.2243
|
|
138.32 0.6242 0.7769 0.0402 0.0323 10.796 52.344 22.740 8050.718 5.914 101.149 1.281 0.95 404124. 0.1992
|
|
144.60 0.6526 0.7567 0.0344 0.0297 9.908 48.037 19.443 7388.339 5.427 86.484 1.194 0.95 405355. 0.1716
|
|
150.89 0.6809 0.7202 0.0285 0.0269 9.003 43.649 16.114 6713.413 4.931 71.675 1.089 0.95 406629. 0.1425
|
|
157.18 0.7093 0.6613 0.0226 0.0242 8.098 39.263 12.778 6038.860 4.436 56.835 0.960 0.95 407945. 0.1118
|
|
163.47 0.7377 0.5721 0.0167 0.0216 7.211 34.962 9.465 5377.347 3.950 42.099 0.798 0.95 409303. 0.0801
|
|
169.75 0.7661 0.4422 0.0110 0.0190 6.355 30.814 6.209 4739.285 3.481 27.619 0.594 0.96 410704. 0.0483
|
|
176.04 0.7944 0.2582 0.0054 0.0166 5.544 26.879 3.050 4134.152 3.037 13.566 0.335 0.96 412149. 0.0190
|
|
182.33 0.8228 0.0004 0.0000 0.0143 4.771 23.129 0.004 3557.374 2.613 0.018 0.001 0.96 413650. 0.0000
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