538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x8 (17x8.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 0.0906 0.0377 0.004 0.268 0.238 3.165 0.030 1.060 34.142 0.07 34471. 0.5769
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0.35 0.0216 0.0506 0.0889 0.0379 0.004 0.269 0.234 3.184 0.030 1.040 33.312 0.07 34493. 0.5576
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0.69 0.0432 0.0987 0.0871 0.0381 0.004 0.270 0.229 3.200 0.031 1.019 32.480 0.07 34515. 0.5382
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1.04 0.0648 0.1443 0.0852 0.0383 0.004 0.272 0.224 3.213 0.031 0.997 31.648 0.07 34539. 0.5187
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1.39 0.0864 0.1874 0.0832 0.0384 0.004 0.272 0.219 3.222 0.031 0.974 30.817 0.07 34565. 0.4991
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1.73 0.1080 0.2279 0.0811 0.0384 0.004 0.273 0.213 3.226 0.031 0.949 29.986 0.07 34593. 0.4794
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2.08 0.1296 0.2659 0.0788 0.0384 0.004 0.273 0.207 3.226 0.031 0.922 29.157 0.07 34622. 0.4596
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2.43 0.1512 0.3014 0.0765 0.0384 0.004 0.272 0.201 3.220 0.031 0.895 28.329 0.07 34653. 0.4398
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2.77 0.1728 0.3344 0.0740 0.0382 0.004 0.271 0.195 3.209 0.031 0.865 27.502 0.07 34686. 0.4199
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3.12 0.1944 0.3649 0.0713 0.0380 0.004 0.270 0.188 3.191 0.030 0.835 26.674 0.07 34721. 0.4000
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3.47 0.2160 0.3928 0.0686 0.0377 0.004 0.268 0.180 3.166 0.030 0.802 25.844 0.07 34757. 0.3800
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3.81 0.2376 0.4182 0.0657 0.0373 0.004 0.265 0.173 3.135 0.030 0.769 25.012 0.07 34796. 0.3600
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4.16 0.2592 0.4410 0.0627 0.0369 0.004 0.262 0.165 3.095 0.030 0.734 24.175 0.07 34836. 0.3399
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4.51 0.2808 0.4610 0.0596 0.0363 0.004 0.258 0.157 3.049 0.029 0.698 23.331 0.07 34879. 0.3198
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4.85 0.3024 0.4783 0.0564 0.0357 0.004 0.253 0.148 2.995 0.029 0.660 22.476 0.07 34924. 0.2997
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5.20 0.3240 0.4927 0.0531 0.0349 0.004 0.248 0.140 2.933 0.028 0.622 21.608 0.07 34970. 0.2796
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5.55 0.3456 0.5039 0.0497 0.0341 0.004 0.242 0.131 2.864 0.027 0.582 20.721 0.07 35019. 0.2594
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5.89 0.3672 0.5119 0.0463 0.0332 0.004 0.235 0.122 2.786 0.027 0.541 19.809 0.07 35070. 0.2392
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6.24 0.3888 0.5162 0.0427 0.0322 0.004 0.228 0.112 2.700 0.026 0.500 18.867 0.07 35123. 0.2189
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6.59 0.4104 0.5165 0.0391 0.0310 0.003 0.220 0.103 2.606 0.025 0.457 17.886 0.07 35178. 0.1985
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6.93 0.4320 0.5124 0.0354 0.0298 0.003 0.212 0.093 2.504 0.024 0.414 16.853 0.07 35235. 0.1779
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7.28 0.4536 0.5030 0.0316 0.0285 0.003 0.202 0.083 2.393 0.023 0.370 15.757 0.07 35295. 0.1573
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7.63 0.4752 0.4875 0.0278 0.0271 0.003 0.192 0.073 2.273 0.022 0.325 14.578 0.07 35357. 0.1364
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7.97 0.4968 0.4647 0.0239 0.0255 0.003 0.181 0.063 2.144 0.020 0.280 13.292 0.07 35421. 0.1153
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8.32 0.5184 0.4329 0.0200 0.0239 0.003 0.170 0.053 2.007 0.019 0.234 11.866 0.07 35487. 0.0941
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8.67 0.5400 0.3897 0.0160 0.0222 0.002 0.157 0.042 1.862 0.018 0.187 10.255 0.07 35555. 0.0728
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9.01 0.5616 0.3317 0.0120 0.0203 0.002 0.144 0.032 1.708 0.016 0.141 8.392 0.07 35626. 0.0516
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9.36 0.5832 0.2536 0.0080 0.0184 0.002 0.131 0.021 1.546 0.015 0.094 6.180 0.07 35699. 0.0310
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9.71 0.6048 0.1475 0.0040 0.0164 0.002 0.116 0.011 1.376 0.013 0.047 3.465 0.07 35774. 0.0123
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10.06 0.6264 -0.0009 0.0000 0.0143 0.002 0.101 0.000 1.198 0.011 0.000 -0.019 0.07 35849. 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 0.0910 0.0335 0.030 0.952 0.958 22.520 0.108 4.260 19.288 0.13 68942. 0.6534
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0.71 0.0220 0.0582 0.0893 0.0338 0.030 0.959 0.940 22.699 0.108 4.180 18.778 0.13 68985. 0.6302
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1.41 0.0441 0.1133 0.0875 0.0340 0.031 0.966 0.921 22.854 0.109 4.095 18.271 0.13 69031. 0.6069
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2.12 0.0661 0.1653 0.0856 0.0342 0.031 0.971 0.900 22.982 0.110 4.005 17.769 0.13 69081. 0.5836
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2.83 0.0881 0.2142 0.0835 0.0344 0.031 0.975 0.879 23.077 0.110 3.909 17.271 0.13 69134. 0.5605
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3.54 0.1101 0.2601 0.0813 0.0344 0.031 0.978 0.856 23.136 0.110 3.807 16.779 0.13 69191. 0.5373
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4.24 0.1322 0.3031 0.0790 0.0345 0.031 0.978 0.832 23.153 0.111 3.699 16.292 0.13 69251. 0.5143
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4.95 0.1542 0.3431 0.0766 0.0344 0.031 0.977 0.806 23.124 0.110 3.585 15.810 0.13 69315. 0.4914
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5.66 0.1762 0.3803 0.0740 0.0343 0.031 0.974 0.779 23.044 0.110 3.465 15.334 0.13 69382. 0.4685
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6.36 0.1983 0.4147 0.0713 0.0341 0.031 0.968 0.751 22.909 0.109 3.339 14.862 0.13 69454. 0.4458
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7.07 0.2203 0.4463 0.0685 0.0338 0.030 0.960 0.721 22.715 0.108 3.207 14.395 0.13 69529. 0.4231
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7.78 0.2423 0.4751 0.0656 0.0334 0.030 0.949 0.690 22.460 0.107 3.068 13.931 0.13 69609. 0.4005
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8.49 0.2643 0.5011 0.0625 0.0330 0.030 0.936 0.657 22.141 0.106 2.925 13.469 0.13 69692. 0.3781
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9.19 0.2864 0.5243 0.0593 0.0324 0.029 0.919 0.624 21.757 0.104 2.776 13.008 0.14 69780. 0.3557
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9.90 0.3084 0.5446 0.0560 0.0317 0.029 0.900 0.589 21.306 0.102 2.622 12.547 0.14 69872. 0.3334
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10.61 0.3304 0.5619 0.0526 0.0309 0.028 0.878 0.554 20.787 0.099 2.463 12.083 0.14 69969. 0.3112
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11.31 0.3524 0.5760 0.0491 0.0301 0.027 0.854 0.517 20.198 0.096 2.300 11.613 0.14 70070. 0.2891
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12.02 0.3745 0.5868 0.0456 0.0291 0.026 0.826 0.480 19.537 0.093 2.133 11.134 0.14 70175. 0.2669
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12.73 0.3965 0.5939 0.0419 0.0280 0.025 0.795 0.441 18.803 0.090 1.962 10.642 0.14 70284. 0.2447
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13.44 0.4185 0.5969 0.0382 0.0268 0.024 0.760 0.402 17.995 0.086 1.788 10.133 0.14 70399. 0.2224
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14.14 0.4406 0.5951 0.0344 0.0255 0.023 0.723 0.362 17.111 0.082 1.610 9.598 0.14 70517. 0.1999
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14.85 0.4626 0.5878 0.0305 0.0240 0.022 0.683 0.321 16.150 0.077 1.430 9.028 0.14 70641. 0.1772
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15.56 0.4846 0.5737 0.0266 0.0225 0.020 0.639 0.280 15.112 0.072 1.247 8.412 0.14 70769. 0.1542
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16.26 0.5066 0.5512 0.0227 0.0208 0.019 0.592 0.239 13.997 0.067 1.061 7.730 0.14 70901. 0.1307
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16.97 0.5287 0.5176 0.0187 0.0191 0.017 0.541 0.196 12.805 0.061 0.874 6.956 0.14 71038. 0.1067
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17.68 0.5507 0.4689 0.0146 0.0172 0.015 0.488 0.154 11.537 0.055 0.684 6.050 0.14 71180. 0.0822
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18.39 0.5727 0.3986 0.0106 0.0152 0.014 0.431 0.111 10.195 0.049 0.494 4.945 0.14 71327. 0.0571
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19.09 0.5948 0.2955 0.0065 0.0131 0.012 0.371 0.068 8.781 0.042 0.304 3.530 0.14 71478. 0.0319
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19.80 0.6168 0.1378 0.0024 0.0109 0.010 0.308 0.026 7.298 0.035 0.114 1.588 0.14 71632. 0.0088
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20.51 0.6388
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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 0.0914 0.0319 0.097 2.036 2.164 72.282 0.230 9.627 13.582 0.20 103410. 0.6917
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1.06 0.0219 0.0611 0.0897 0.0322 0.098 2.054 2.124 72.918 0.232 9.449 13.214 0.20 103475. 0.6667
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2.11 0.0438 0.1189 0.0879 0.0324 0.099 2.070 2.082 73.476 0.234 9.259 12.850 0.20 103544. 0.6418
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3.17 0.0657 0.1733 0.0860 0.0326 0.099 2.083 2.036 73.941 0.235 9.057 12.490 0.20 103618. 0.6170
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4.22 0.0876 0.2245 0.0840 0.0328 0.100 2.093 1.988 74.297 0.236 8.842 12.136 0.20 103697. 0.5923
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5.28 0.1096 0.2726 0.0818 0.0329 0.100 2.100 1.937 74.530 0.237 8.615 11.786 0.20 103782. 0.5678
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6.33 0.1315 0.3176 0.0795 0.0329 0.100 2.102 1.883 74.623 0.238 8.374 11.442 0.20 103871. 0.5435
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7.39 0.1534 0.3595 0.0771 0.0329 0.100 2.101 1.825 74.561 0.237 8.119 11.104 0.20 103967. 0.5193
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8.44 0.1753 0.3986 0.0745 0.0328 0.100 2.094 1.765 74.328 0.237 7.850 10.770 0.20 104067. 0.4953
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9.50 0.1972 0.4347 0.0719 0.0326 0.099 2.082 1.701 73.908 0.235 7.568 10.442 0.20 104174. 0.4715
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10.55 0.2191 0.4680 0.0690 0.0323 0.098 2.065 1.635 73.288 0.233 7.272 10.118 0.20 104286. 0.4478
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11.61 0.2410 0.4986 0.0661 0.0320 0.097 2.041 1.565 72.460 0.231 6.962 9.798 0.20 104405. 0.4244
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12.66 0.2629 0.5263 0.0631 0.0315 0.096 2.012 1.493 71.415 0.227 6.641 9.482 0.20 104529. 0.4011
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13.72 0.2849 0.5514 0.0599 0.0309 0.094 1.976 1.418 70.148 0.223 6.307 9.169 0.20 104660. 0.3779
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14.77 0.3068 0.5736 0.0566 0.0303 0.092 1.934 1.341 68.652 0.219 5.963 8.857 0.20 104797. 0.3550
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15.83 0.3287 0.5929 0.0533 0.0295 0.090 1.885 1.261 66.923 0.213 5.608 8.545 0.20 104941. 0.3321
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16.88 0.3506 0.6092 0.0498 0.0287 0.087 1.830 1.179 64.953 0.207 5.243 8.232 0.20 105091. 0.3094
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17.94 0.3725 0.6224 0.0462 0.0277 0.084 1.768 1.095 62.739 0.200 4.870 7.915 0.20 105247. 0.2867
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18.99 0.3944 0.6322 0.0426 0.0266 0.081 1.698 1.009 60.273 0.192 4.488 7.592 0.20 105410. 0.2640
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20.05 0.4163 0.6381 0.0389 0.0254 0.077 1.621 0.921 57.552 0.183 4.097 7.260 0.20 105580. 0.2412
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21.10 0.4382 0.6396 0.0351 0.0241 0.073 1.537 0.832 54.570 0.174 3.700 6.914 0.20 105756. 0.2183
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22.16 0.4601 0.6361 0.0313 0.0226 0.069 1.446 0.741 51.326 0.163 3.296 6.548 0.20 105940. 0.1951
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23.21 0.4821 0.6263 0.0274 0.0211 0.064 1.347 0.649 47.816 0.152 2.886 6.154 0.20 106130. 0.1716
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24.27 0.5040 0.6086 0.0235 0.0194 0.059 1.241 0.555 44.039 0.140 2.470 5.720 0.20 106327. 0.1476
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25.32 0.5259 0.5804 0.0195 0.0176 0.054 1.127 0.461 39.998 0.127 2.051 5.228 0.20 106531. 0.1229
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26.38 0.5478 0.5376 0.0155 0.0157 0.048 1.006 0.366 35.694 0.114 1.627 4.649 0.20 106742. 0.0973
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27.43 0.5697 0.4734 0.0114 0.0137 0.042 0.877 0.270 31.134 0.099 1.202 3.936 0.20 106960. 0.0708
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28.49 0.5916 0.3750 0.0074 0.0116 0.035 0.742 0.174 26.326 0.084 0.775 3.003 0.21 107184. 0.0434
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29.54 0.6135 0.2165 0.0033 0.0094 0.029 0.600 0.078 21.280 0.068 0.349 1.672 0.21 107414. 0.0162
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30.60 0.6354
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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 0.0919 0.0311 0.224 3.526 3.868 166.880 0.398 17.206 10.514 0.27 137876. 0.7158
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1.40 0.0218 0.0628 0.0902 0.0313 0.226 3.559 3.797 168.432 0.402 16.891 10.226 0.27 137962. 0.6898
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2.80 0.0436 0.1220 0.0884 0.0316 0.228 3.588 3.722 169.800 0.405 16.554 9.942 0.27 138054. 0.6639
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4.20 0.0654 0.1779 0.0865 0.0318 0.229 3.612 3.641 170.946 0.408 16.196 9.661 0.27 138152. 0.6382
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5.60 0.0872 0.2304 0.0845 0.0320 0.230 3.631 3.556 171.836 0.410 15.816 9.386 0.27 138257. 0.6126
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7.00 0.1090 0.2797 0.0823 0.0321 0.231 3.644 3.465 172.433 0.412 15.413 9.115 0.27 138369. 0.5873
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8.40 0.1308 0.3259 0.0800 0.0321 0.232 3.649 3.369 172.700 0.412 14.986 8.848 0.27 138488. 0.5622
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9.80 0.1526 0.3690 0.0776 0.0321 0.231 3.647 3.268 172.600 0.412 14.535 8.587 0.27 138615. 0.5374
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11.20 0.1745 0.4091 0.0751 0.0320 0.231 3.636 3.161 172.094 0.411 14.059 8.331 0.27 138748. 0.5127
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12.60 0.1963 0.4463 0.0724 0.0318 0.230 3.616 3.048 171.145 0.409 13.559 8.079 0.27 138890. 0.4883
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14.00 0.2181 0.4807 0.0696 0.0316 0.228 3.586 2.930 169.722 0.405 13.034 7.831 0.27 139039. 0.4641
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15.40 0.2399 0.5123 0.0667 0.0312 0.225 3.546 2.807 167.801 0.401 12.486 7.588 0.27 139196. 0.4401
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16.80 0.2617 0.5412 0.0636 0.0308 0.222 3.494 2.679 165.366 0.395 11.916 7.348 0.27 139361. 0.4163
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18.20 0.2835 0.5674 0.0605 0.0302 0.218 3.432 2.546 162.401 0.388 11.325 7.111 0.27 139534. 0.3928
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19.60 0.3053 0.5909 0.0572 0.0296 0.213 3.357 2.409 158.891 0.379 10.714 6.876 0.27 139716. 0.3694
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21.00 0.3271 0.6116 0.0539 0.0288 0.208 3.271 2.267 154.822 0.370 10.085 6.643 0.27 139906. 0.3462
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22.40 0.3489 0.6294 0.0504 0.0279 0.201 3.173 2.122 150.182 0.359 9.439 6.409 0.27 140104. 0.3232
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23.80 0.3707 0.6443 0.0469 0.0270 0.194 3.063 1.973 144.954 0.346 8.777 6.174 0.27 140311. 0.3002
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25.20 0.3925 0.6558 0.0433 0.0259 0.187 2.940 1.821 139.128 0.332 8.099 5.936 0.27 140527. 0.2773
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26.60 0.4143 0.6639 0.0396 0.0247 0.178 2.804 1.665 132.691 0.317 7.407 5.692 0.27 140752. 0.2543
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28.00 0.4361 0.6678 0.0358 0.0234 0.168 2.655 1.507 125.632 0.300 6.702 5.440 0.27 140985. 0.2312
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29.40 0.4579 0.6670 0.0320 0.0219 0.158 2.492 1.346 117.944 0.282 5.985 5.175 0.27 141228. 0.2078
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30.80 0.4798 0.6605 0.0281 0.0204 0.147 2.316 1.182 109.620 0.262 5.258 4.891 0.27 141479. 0.1841
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32.20 0.5016 0.6466 0.0241 0.0187 0.135 2.127 1.016 100.658 0.240 4.521 4.580 0.27 141740. 0.1598
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33.60 0.5234 0.6229 0.0202 0.0169 0.122 1.924 0.849 91.061 0.217 3.776 4.229 0.27 142009. 0.1349
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35.00 0.5452 0.5856 0.0162 0.0150 0.108 1.708 0.680 80.834 0.193 3.025 3.816 0.27 142288. 0.1089
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36.40 0.5670 0.5277 0.0121 0.0130 0.094 1.479 0.510 69.991 0.167 2.270 3.307 0.27 142576. 0.0818
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37.80 0.5888 0.4365 0.0081 0.0109 0.079 1.237 0.340 58.553 0.140 1.512 2.634 0.27 142873. 0.0532
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39.20 0.6106 0.2843 0.0040 0.0087 0.062 0.983 0.170 46.542 0.111 0.755 1.654 0.27 143177. 0.0236
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40.60 0.6324 -0.0040 0.0000 0.0063 0.045 0.715 -0.002 33.850 0.081 -0.007 -0.022 0.27 143466. 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 0.0925 0.0306 0.431 5.435 6.084 321.493 0.614 27.061 8.583 0.34 172337. 0.7329
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1.75 0.0218 0.0641 0.0908 0.0309 0.435 5.487 5.973 324.599 0.620 26.566 8.346 0.34 172445. 0.7060
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3.50 0.0437 0.1246 0.0890 0.0312 0.439 5.533 5.854 327.339 0.625 26.038 8.111 0.34 172561. 0.6793
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5.26 0.0655 0.1816 0.0871 0.0314 0.442 5.572 5.728 329.640 0.630 25.476 7.881 0.34 172684. 0.6529
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7.01 0.0873 0.2352 0.0850 0.0316 0.444 5.603 5.593 331.433 0.633 24.879 7.654 0.34 172816. 0.6267
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8.76 0.1092 0.2855 0.0829 0.0317 0.446 5.623 5.451 332.646 0.635 24.246 7.432 0.34 172957. 0.6007
|
|
10.51 0.1310 0.3326 0.0806 0.0317 0.447 5.633 5.300 333.203 0.636 23.575 7.215 0.34 173106. 0.5750
|
|
12.27 0.1528 0.3765 0.0782 0.0317 0.447 5.630 5.141 333.031 0.636 22.866 7.001 0.34 173265. 0.5495
|
|
14.02 0.1747 0.4175 0.0756 0.0316 0.445 5.613 4.973 332.054 0.634 22.119 6.792 0.34 173433. 0.5243
|
|
15.77 0.1965 0.4555 0.0729 0.0315 0.443 5.582 4.796 330.197 0.631 21.332 6.588 0.34 173610. 0.4994
|
|
17.52 0.2183 0.4907 0.0701 0.0312 0.439 5.534 4.610 327.398 0.625 20.506 6.387 0.34 173797. 0.4747
|
|
19.28 0.2402 0.5231 0.0672 0.0308 0.434 5.470 4.416 323.610 0.618 19.644 6.190 0.34 173994. 0.4503
|
|
21.03 0.2620 0.5528 0.0641 0.0304 0.428 5.389 4.215 318.799 0.609 18.747 5.996 0.34 174201. 0.4261
|
|
22.78 0.2839 0.5798 0.0609 0.0298 0.420 5.290 4.006 312.934 0.598 17.817 5.806 0.34 174419. 0.4022
|
|
24.53 0.3057 0.6042 0.0576 0.0292 0.410 5.173 3.789 305.987 0.584 16.856 5.617 0.34 174646. 0.3785
|
|
26.29 0.3275 0.6258 0.0542 0.0284 0.400 5.036 3.567 297.928 0.569 15.866 5.430 0.34 174885. 0.3550
|
|
28.04 0.3494 0.6446 0.0508 0.0275 0.387 4.881 3.338 288.730 0.551 14.848 5.244 0.34 175133. 0.3317
|
|
29.79 0.3712 0.6605 0.0472 0.0265 0.373 4.706 3.104 278.366 0.532 13.805 5.057 0.34 175393. 0.3084
|
|
31.54 0.3930 0.6732 0.0435 0.0254 0.358 4.510 2.864 266.809 0.510 12.738 4.868 0.34 175664. 0.2852
|
|
33.30 0.4149 0.6826 0.0398 0.0242 0.341 4.294 2.619 254.037 0.485 11.649 4.676 0.34 175945. 0.2620
|
|
35.05 0.4367 0.6880 0.0360 0.0229 0.322 4.058 2.369 240.029 0.458 10.539 4.477 0.34 176238. 0.2386
|
|
36.80 0.4585 0.6888 0.0322 0.0214 0.301 3.800 2.116 224.767 0.429 9.411 4.270 0.34 176542. 0.2150
|
|
38.55 0.4804 0.6841 0.0283 0.0198 0.279 3.520 1.858 208.241 0.398 8.266 4.047 0.34 176857. 0.1910
|
|
40.31 0.5022 0.6722 0.0243 0.0181 0.255 3.219 1.597 190.446 0.364 7.105 3.804 0.34 177184. 0.1665
|
|
42.06 0.5240 0.6508 0.0203 0.0163 0.230 2.897 1.334 171.386 0.327 5.933 3.530 0.34 177522. 0.1411
|
|
43.81 0.5459 0.6158 0.0162 0.0144 0.203 2.554 1.068 151.075 0.289 4.750 3.206 0.34 177871. 0.1147
|
|
45.56 0.5677 0.5600 0.0122 0.0123 0.174 2.190 0.801 129.539 0.247 3.561 2.803 0.34 178232. 0.0868
|
|
47.32 0.5895 0.4691 0.0081 0.0102 0.143 1.806 0.533 106.818 0.204 2.369 2.262 0.34 178604. 0.0571
|
|
49.07 0.6114 0.3112 0.0040 0.0079 0.111 1.402 0.265 82.961 0.158 1.177 1.447 0.34 178985. 0.0258
|
|
50.82 0.6332 -0.0106 -0.0001 0.0055 0.077 0.975 -0.006 57.665 0.110 -0.027 -0.047 0.34 179337. 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 0.0932 0.0305 0.741 7.783 8.830 552.517 0.879 39.277 7.249 0.40 206793. 0.7457
|
|
2.10 0.0219 0.0650 0.0915 0.0308 0.748 7.860 8.669 557.991 0.888 38.561 7.047 0.40 206923. 0.7183
|
|
4.21 0.0437 0.1264 0.0897 0.0310 0.755 7.928 8.498 562.818 0.896 37.798 6.848 0.40 207062. 0.6911
|
|
6.31 0.0656 0.1842 0.0878 0.0313 0.760 7.986 8.315 566.874 0.902 36.985 6.653 0.40 207212. 0.6641
|
|
8.42 0.0874 0.2385 0.0857 0.0314 0.764 8.030 8.121 570.037 0.907 36.121 6.461 0.40 207371. 0.6374
|
|
10.52 0.1093 0.2894 0.0836 0.0315 0.767 8.060 7.914 572.178 0.911 35.204 6.274 0.40 207540. 0.6110
|
|
12.63 0.1311 0.3371 0.0813 0.0316 0.769 8.074 7.696 573.169 0.912 34.232 6.090 0.40 207720. 0.5849
|
|
14.73 0.1530 0.3817 0.0788 0.0316 0.768 8.070 7.465 572.877 0.912 33.205 5.910 0.40 207911. 0.5590
|
|
16.84 0.1748 0.4233 0.0762 0.0315 0.766 8.046 7.221 571.170 0.909 32.121 5.735 0.40 208113. 0.5334
|
|
18.94 0.1967 0.4619 0.0735 0.0313 0.762 8.000 6.965 567.919 0.904 30.979 5.562 0.40 208327. 0.5082
|
|
21.05 0.2185 0.4977 0.0707 0.0310 0.755 7.931 6.696 563.011 0.896 29.782 5.394 0.40 208552. 0.4832
|
|
23.15 0.2404 0.5307 0.0677 0.0307 0.746 7.838 6.414 556.366 0.885 28.531 5.229 0.40 208790. 0.4584
|
|
25.26 0.2622 0.5610 0.0646 0.0302 0.735 7.719 6.121 547.922 0.872 27.228 5.067 0.40 209039. 0.4340
|
|
27.36 0.2841 0.5887 0.0614 0.0296 0.721 7.574 5.818 537.625 0.856 25.878 4.908 0.41 209301. 0.4098
|
|
29.46 0.3059 0.6138 0.0581 0.0290 0.705 7.402 5.504 525.425 0.836 24.482 4.751 0.41 209575. 0.3859
|
|
31.57 0.3278 0.6361 0.0547 0.0282 0.686 7.202 5.181 511.274 0.814 23.045 4.596 0.41 209862. 0.3621
|
|
33.67 0.3496 0.6557 0.0512 0.0273 0.664 6.975 4.849 495.120 0.788 21.567 4.442 0.41 210161. 0.3386
|
|
35.78 0.3715 0.6725 0.0476 0.0263 0.640 6.718 4.508 476.918 0.759 20.052 4.287 0.41 210474. 0.3151
|
|
37.88 0.3934 0.6862 0.0439 0.0252 0.612 6.432 4.160 456.622 0.727 18.503 4.132 0.41 210799. 0.2917
|
|
39.99 0.4152 0.6966 0.0402 0.0239 0.582 6.116 3.804 434.190 0.691 16.921 3.974 0.41 211138. 0.2683
|
|
42.09 0.4371 0.7033 0.0363 0.0226 0.549 5.770 3.442 409.587 0.652 15.308 3.811 0.41 211490. 0.2448
|
|
44.20 0.4589 0.7055 0.0324 0.0211 0.513 5.392 3.073 382.783 0.609 13.669 3.641 0.41 211856. 0.2210
|
|
46.30 0.4808 0.7024 0.0285 0.0195 0.474 4.983 2.699 353.758 0.563 12.005 3.460 0.41 212235. 0.1968
|
|
48.41 0.5026 0.6924 0.0245 0.0178 0.432 4.543 2.320 322.505 0.513 10.319 3.263 0.41 212627. 0.1720
|
|
50.51 0.5245 0.6731 0.0205 0.0159 0.388 4.072 1.937 289.030 0.460 8.615 3.039 0.41 213034. 0.1464
|
|
52.62 0.5463 0.6403 0.0164 0.0140 0.340 3.569 1.551 253.358 0.403 6.897 2.776 0.41 213454. 0.1197
|
|
54.72 0.5682 0.5867 0.0123 0.0119 0.289 3.036 1.162 215.537 0.343 5.169 2.446 0.41 213888. 0.0913
|
|
56.82 0.5900 0.4971 0.0082 0.0097 0.236 2.474 0.773 175.637 0.280 3.437 1.995 0.41 214334. 0.0607
|
|
58.93 0.6119 0.3358 0.0040 0.0074 0.179 1.884 0.383 133.741 0.213 1.705 1.300 0.41 214793. 0.0279
|
|
61.03 0.6337 -0.0154 -0.0001 0.0049 0.120 1.256 -0.011 89.174 0.142 -0.050 -0.058 0.41 215204. 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 0.0941 0.0305 1.178 10.603 12.133 878.132 1.198 53.969 6.267 0.47 241242. 0.7557
|
|
2.46 0.0219 0.0656 0.0924 0.0308 1.189 10.710 11.914 886.978 1.210 52.992 6.092 0.47 241394. 0.7279
|
|
4.91 0.0437 0.1275 0.0906 0.0311 1.200 10.804 11.679 894.775 1.221 51.947 5.920 0.47 241558. 0.7003
|
|
7.37 0.0656 0.1858 0.0887 0.0313 1.209 10.883 11.429 901.319 1.230 50.835 5.751 0.47 241733. 0.6730
|
|
9.83 0.0875 0.2407 0.0866 0.0315 1.216 10.945 11.163 906.413 1.237 49.651 5.586 0.47 241919. 0.6460
|
|
12.29 0.1093 0.2921 0.0844 0.0316 1.220 10.986 10.880 909.853 1.241 48.394 5.424 0.47 242118. 0.6193
|
|
14.74 0.1312 0.3403 0.0821 0.0316 1.222 11.005 10.581 911.427 1.243 47.062 5.265 0.47 242329. 0.5929
|
|
17.20 0.1531 0.3853 0.0796 0.0316 1.222 10.999 10.264 910.927 1.243 45.654 5.111 0.47 242553. 0.5668
|
|
19.66 0.1749 0.4274 0.0770 0.0315 1.218 10.965 9.929 908.139 1.239 44.166 4.959 0.47 242790. 0.5410
|
|
22.11 0.1968 0.4664 0.0743 0.0313 1.211 10.902 9.577 902.852 1.232 42.600 4.811 0.47 243040. 0.5154
|
|
24.57 0.2187 0.5027 0.0714 0.0311 1.200 10.805 9.208 894.887 1.221 40.956 4.667 0.47 243304. 0.4902
|
|
27.03 0.2405 0.5362 0.0684 0.0307 1.186 10.675 8.821 884.110 1.206 39.237 4.526 0.47 243582. 0.4653
|
|
29.48 0.2624 0.5671 0.0653 0.0302 1.167 10.510 8.419 870.425 1.187 37.448 4.387 0.47 243874. 0.4406
|
|
31.94 0.2843 0.5953 0.0621 0.0296 1.145 10.309 8.002 853.747 1.165 35.592 4.251 0.47 244181. 0.4163
|
|
34.40 0.3061 0.6209 0.0587 0.0290 1.118 10.070 7.571 833.992 1.138 33.674 4.117 0.47 244501. 0.3922
|
|
36.86 0.3280 0.6439 0.0553 0.0282 1.088 9.794 7.126 811.084 1.106 31.697 3.985 0.47 244837. 0.3683
|
|
39.31 0.3499 0.6642 0.0517 0.0273 1.053 9.478 6.670 784.945 1.071 29.666 3.854 0.47 245187. 0.3445
|
|
41.77 0.3717 0.6817 0.0481 0.0262 1.013 9.122 6.201 755.498 1.031 27.583 3.723 0.47 245553. 0.3209
|
|
44.23 0.3936 0.6963 0.0444 0.0251 0.969 8.726 5.722 722.672 0.986 25.452 3.591 0.47 245934. 0.2974
|
|
46.68 0.4155 0.7077 0.0406 0.0238 0.920 8.288 5.233 686.401 0.936 23.276 3.458 0.47 246330. 0.2738
|
|
49.14 0.4374 0.7154 0.0367 0.0225 0.867 7.808 4.734 646.625 0.882 21.058 3.321 0.48 246742. 0.2501
|
|
51.60 0.4592 0.7189 0.0328 0.0209 0.809 7.285 4.227 603.299 0.823 18.803 3.178 0.48 247169. 0.2262
|
|
54.06 0.4811 0.7172 0.0288 0.0193 0.746 6.718 3.713 556.391 0.759 16.513 3.026 0.48 247612. 0.2019
|
|
56.51 0.5030 0.7088 0.0248 0.0176 0.678 6.108 3.191 505.887 0.690 14.194 2.861 0.48 248071. 0.1769
|
|
58.97 0.5248 0.6914 0.0207 0.0157 0.606 5.455 2.664 451.799 0.616 11.849 2.674 0.48 248546. 0.1511
|
|
61.43 0.5467 0.6608 0.0165 0.0137 0.529 4.759 2.132 394.168 0.538 9.485 2.454 0.48 249037. 0.1240
|
|
63.88 0.5686 0.6093 0.0124 0.0116 0.447 4.022 1.598 333.069 0.454 7.107 2.176 0.48 249544. 0.0952
|
|
66.34 0.5904 0.5213 0.0082 0.0093 0.360 3.243 1.062 268.620 0.366 4.722 1.793 0.48 250066. 0.0639
|
|
68.80 0.6123 0.3578 0.0041 0.0070 0.269 2.426 0.526 200.955 0.274 2.338 1.186 0.48 250602. 0.0298
|
|
71.25 0.6342 -0.0217 -0.0002 0.0045 0.173 1.554 -0.020 128.687 0.176 -0.087 -0.069 0.48 251064. 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 0.0952 0.0307 1.769 13.936 16.027 1319.043 1.574 71.288 5.511 0.54 275682. 0.7637
|
|
2.81 0.0219 0.0660 0.0935 0.0310 1.787 14.078 15.739 1332.483 1.591 70.005 5.357 0.54 275857. 0.7357
|
|
5.62 0.0438 0.1283 0.0916 0.0313 1.803 14.203 15.430 1344.309 1.605 68.634 5.206 0.54 276045. 0.7079
|
|
8.43 0.0656 0.1869 0.0897 0.0315 1.816 14.308 15.102 1354.216 1.616 67.172 5.058 0.54 276246. 0.6804
|
|
11.24 0.0875 0.2421 0.0876 0.0317 1.826 14.389 14.752 1361.901 1.626 65.615 4.913 0.54 276460. 0.6532
|
|
14.05 0.1094 0.2938 0.0854 0.0318 1.833 14.443 14.380 1367.057 1.632 63.961 4.771 0.54 276689. 0.6263
|
|
16.86 0.1313 0.3424 0.0831 0.0319 1.836 14.468 13.985 1369.366 1.635 62.207 4.632 0.54 276931. 0.5997
|
|
19.67 0.1532 0.3877 0.0806 0.0318 1.835 14.459 13.568 1368.509 1.634 60.351 4.497 0.54 277188. 0.5734
|
|
22.48 0.1750 0.4301 0.0780 0.0317 1.829 14.413 13.127 1364.159 1.628 58.390 4.365 0.54 277461. 0.5474
|
|
25.29 0.1969 0.4696 0.0752 0.0315 1.818 14.327 12.663 1356.004 1.619 56.325 4.236 0.54 277748. 0.5218
|
|
28.10 0.2188 0.5062 0.0723 0.0313 1.802 14.197 12.175 1343.768 1.604 54.155 4.110 0.54 278051. 0.4964
|
|
30.91 0.2407 0.5401 0.0693 0.0309 1.780 14.023 11.665 1327.250 1.584 51.886 3.986 0.54 278370. 0.4713
|
|
33.72 0.2626 0.5714 0.0661 0.0304 1.752 13.801 11.134 1306.301 1.559 49.523 3.866 0.54 278706. 0.4465
|
|
36.53 0.2844 0.6001 0.0629 0.0298 1.718 13.532 10.583 1280.794 1.529 47.072 3.748 0.54 279057. 0.4220
|
|
39.34 0.3063 0.6262 0.0595 0.0291 1.677 13.213 10.013 1250.609 1.493 44.538 3.631 0.54 279425. 0.3978
|
|
42.15 0.3282 0.6498 0.0560 0.0283 1.630 12.844 9.426 1215.631 1.451 41.926 3.517 0.54 279810. 0.3738
|
|
44.95 0.3501 0.6707 0.0524 0.0273 1.577 12.422 8.822 1175.745 1.403 39.241 3.403 0.54 280212. 0.3499
|
|
47.76 0.3720 0.6890 0.0487 0.0263 1.516 11.948 8.203 1130.836 1.350 36.487 3.290 0.54 280631. 0.3262
|
|
50.57 0.3938 0.7043 0.0450 0.0251 1.449 11.419 7.569 1080.797 1.290 33.669 3.177 0.54 281067. 0.3025
|
|
53.38 0.4157 0.7165 0.0411 0.0239 1.375 10.835 6.923 1025.528 1.224 30.792 3.062 0.54 281521. 0.2789
|
|
56.19 0.4376 0.7253 0.0372 0.0224 1.294 10.195 6.263 964.943 1.152 27.859 2.944 0.54 281993. 0.2550
|
|
59.00 0.4595 0.7299 0.0332 0.0209 1.206 9.498 5.593 898.971 1.073 24.875 2.822 0.54 282482. 0.2310
|
|
61.81 0.4814 0.7295 0.0292 0.0192 1.110 8.743 4.912 827.563 0.988 21.847 2.692 0.54 282990. 0.2065
|
|
64.62 0.5032 0.7226 0.0251 0.0175 1.007 7.931 4.222 750.700 0.896 18.778 2.551 0.54 283516. 0.1814
|
|
67.43 0.5251 0.7069 0.0209 0.0155 0.896 7.062 3.524 668.400 0.798 15.675 2.391 0.55 284059. 0.1554
|
|
70.24 0.5470 0.6784 0.0168 0.0135 0.779 6.136 2.821 580.725 0.693 12.546 2.203 0.55 284621. 0.1281
|
|
73.05 0.5689 0.6292 0.0125 0.0113 0.654 5.154 2.113 487.791 0.582 9.398 1.965 0.55 285201. 0.0989
|
|
75.86 0.5908 0.5430 0.0083 0.0091 0.523 4.118 1.403 389.777 0.465 6.241 1.633 0.55 285799. 0.0669
|
|
78.67 0.6126 0.3781 0.0041 0.0067 0.385 3.031 0.693 286.888 0.342 3.085 1.096 0.55 286412. 0.0316
|
|
81.48 0.6345 -0.0297 -0.0002 0.0041 0.237 1.864 -0.032 176.419 0.211 -0.144 -0.083 0.55 286912. 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 0.0965 0.0310 2.547 17.839 20.555 1899.543 2.015 91.428 4.908 0.61 310110. 0.7703
|
|
3.16 0.0219 0.0662 0.0947 0.0314 2.573 18.023 20.188 1919.048 2.036 89.798 4.772 0.61 310308. 0.7422
|
|
6.33 0.0438 0.1286 0.0929 0.0316 2.596 18.183 19.796 1936.180 2.054 88.052 4.637 0.61 310521. 0.7142
|
|
9.49 0.0657 0.1874 0.0909 0.0319 2.616 18.318 19.377 1950.485 2.070 86.189 4.506 0.61 310749. 0.6866
|
|
12.65 0.0876 0.2428 0.0888 0.0320 2.630 18.421 18.931 1961.531 2.081 84.203 4.377 0.61 310992. 0.6593
|
|
15.81 0.1095 0.2947 0.0866 0.0322 2.640 18.490 18.456 1968.866 2.089 82.092 4.252 0.61 311250. 0.6323
|
|
18.98 0.1314 0.3435 0.0842 0.0322 2.645 18.520 17.952 1972.034 2.092 79.851 4.129 0.61 311525. 0.6056
|
|
22.14 0.1532 0.3891 0.0817 0.0322 2.643 18.506 17.419 1970.573 2.091 77.478 4.009 0.61 311816. 0.5792
|
|
25.30 0.1751 0.4317 0.0791 0.0321 2.634 18.445 16.855 1964.018 2.084 74.970 3.892 0.61 312124. 0.5532
|
|
28.46 0.1970 0.4715 0.0763 0.0319 2.618 18.331 16.260 1951.914 2.071 72.326 3.778 0.61 312450. 0.5274
|
|
31.63 0.2189 0.5084 0.0734 0.0316 2.593 18.162 15.636 1933.862 2.052 69.547 3.667 0.61 312793. 0.5020
|
|
34.79 0.2408 0.5427 0.0703 0.0312 2.561 17.933 14.982 1909.566 2.026 66.640 3.559 0.61 313153. 0.4768
|
|
37.95 0.2627 0.5744 0.0671 0.0307 2.520 17.645 14.301 1878.816 1.993 63.611 3.452 0.61 313532. 0.4520
|
|
41.11 0.2846 0.6035 0.0638 0.0301 2.469 17.294 13.594 1841.429 1.954 60.467 3.348 0.61 313929. 0.4274
|
|
44.28 0.3065 0.6301 0.0604 0.0294 2.410 16.879 12.863 1797.245 1.907 57.216 3.246 0.61 314345. 0.4030
|
|
47.44 0.3284 0.6542 0.0568 0.0285 2.342 16.398 12.110 1746.096 1.853 53.864 3.146 0.61 314780. 0.3789
|
|
50.60 0.3503 0.6757 0.0532 0.0276 2.263 15.851 11.335 1687.822 1.791 50.418 3.046 0.61 315234. 0.3550
|
|
53.76 0.3722 0.6946 0.0495 0.0265 2.175 15.235 10.540 1622.261 1.721 46.883 2.947 0.61 315707. 0.3312
|
|
56.93 0.3941 0.7107 0.0456 0.0253 2.078 14.550 9.727 1549.263 1.644 43.265 2.848 0.61 316199. 0.3074
|
|
60.09 0.4159 0.7237 0.0417 0.0240 1.970 13.793 8.896 1468.684 1.558 39.569 2.747 0.61 316711. 0.2837
|
|
63.25 0.4378 0.7334 0.0378 0.0226 1.851 12.964 8.049 1380.400 1.465 35.802 2.645 0.61 317243. 0.2597
|
|
66.41 0.4597 0.7390 0.0337 0.0210 1.722 12.061 7.187 1284.310 1.363 31.970 2.538 0.61 317795. 0.2356
|
|
69.58 0.4816 0.7399 0.0296 0.0193 1.583 11.085 6.312 1180.344 1.252 28.078 2.426 0.61 318368. 0.2110
|
|
72.74 0.5035 0.7345 0.0255 0.0175 1.433 10.034 5.426 1068.477 1.134 24.134 2.303 0.61 318960. 0.1857
|
|
75.90 0.5254 0.7205 0.0213 0.0155 1.272 8.910 4.529 948.732 1.007 20.145 2.165 0.61 319573. 0.1595
|
|
79.06 0.5473 0.6939 0.0170 0.0134 1.101 7.712 3.624 821.199 0.871 16.122 2.002 0.61 320206. 0.1319
|
|
82.23 0.5692 0.6469 0.0127 0.0112 0.920 6.443 2.714 686.051 0.728 12.074 1.795 0.61 320860. 0.1024
|
|
85.39 0.5911 0.5628 0.0085 0.0089 0.729 5.105 1.802 543.545 0.577 8.014 1.503 0.62 321533. 0.0699
|
|
88.55 0.6130 0.3972 0.0042 0.0064 0.528 3.700 0.889 393.984 0.418 3.953 1.023 0.62 322223. 0.0334
|
|
91.71 0.6349 -0.0418 -0.0002 0.0038 0.311 2.178 -0.053 231.957 0.246 -0.237 -0.104 0.62 322729. 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 0.0980 0.0316 3.553 22.392 25.775 2649.286 2.530 114.648 4.413 0.67 344523. 0.7755
|
|
3.52 0.0219 0.0661 0.0962 0.0319 3.589 22.623 25.321 2676.625 2.556 112.626 4.291 0.67 344746. 0.7474
|
|
7.03 0.0438 0.1286 0.0944 0.0322 3.622 22.826 24.833 2700.572 2.579 110.459 4.171 0.67 344984. 0.7195
|
|
10.55 0.0657 0.1874 0.0924 0.0324 3.648 22.994 24.312 2720.493 2.598 108.142 4.053 0.67 345239. 0.6919
|
|
14.06 0.0876 0.2428 0.0903 0.0326 3.669 23.123 23.757 2735.775 2.612 105.670 3.939 0.67 345511. 0.6645
|
|
17.58 0.1095 0.2949 0.0881 0.0327 3.682 23.208 23.165 2745.784 2.622 103.038 3.827 0.67 345801. 0.6375
|
|
21.09 0.1314 0.3437 0.0857 0.0327 3.688 23.243 22.536 2749.888 2.626 100.242 3.717 0.67 346108. 0.6109
|
|
24.61 0.1533 0.3895 0.0831 0.0327 3.684 23.222 21.870 2747.442 2.624 97.278 3.610 0.67 346434. 0.5845
|
|
28.13 0.1752 0.4323 0.0805 0.0326 3.671 23.141 21.165 2737.804 2.614 94.143 3.506 0.67 346779. 0.5584
|
|
31.64 0.1971 0.4723 0.0776 0.0324 3.648 22.993 20.422 2720.337 2.598 90.836 3.405 0.67 347143. 0.5327
|
|
35.16 0.2190 0.5096 0.0747 0.0321 3.613 22.774 19.640 2694.486 2.573 87.359 3.306 0.67 347526. 0.5072
|
|
38.67 0.2409 0.5441 0.0715 0.0317 3.567 22.482 18.821 2659.832 2.540 83.717 3.210 0.67 347929. 0.4820
|
|
42.19 0.2628 0.5762 0.0683 0.0312 3.508 22.112 17.968 2616.084 2.498 79.921 3.115 0.67 348353. 0.4571
|
|
45.70 0.2847 0.6057 0.0649 0.0305 3.437 21.663 17.082 2563.002 2.447 75.979 3.023 0.68 348796. 0.4325
|
|
49.22 0.3066 0.6327 0.0614 0.0298 3.353 21.134 16.165 2500.367 2.388 71.902 2.932 0.68 349260. 0.4081
|
|
52.74 0.3285 0.6573 0.0579 0.0289 3.256 20.522 15.219 2427.959 2.319 67.696 2.843 0.68 349746. 0.3840
|
|
56.25 0.3504 0.6794 0.0542 0.0279 3.145 19.825 14.247 2345.562 2.240 63.370 2.755 0.68 350252. 0.3600
|
|
59.77 0.3723 0.6989 0.0504 0.0268 3.021 19.043 13.249 2252.960 2.151 58.932 2.667 0.68 350779. 0.3361
|
|
63.28 0.3942 0.7157 0.0465 0.0256 2.883 18.172 12.228 2149.947 2.053 54.389 2.580 0.68 351328. 0.3123
|
|
66.80 0.4162 0.7295 0.0425 0.0243 2.731 17.212 11.184 2036.325 1.945 49.747 2.491 0.68 351899. 0.2884
|
|
70.31 0.4381 0.7401 0.0385 0.0228 2.564 16.160 10.120 1911.927 1.826 45.015 2.401 0.68 352492. 0.2644
|
|
73.83 0.4600 0.7468 0.0344 0.0212 2.382 15.016 9.037 1776.612 1.697 40.198 2.307 0.68 353107. 0.2401
|
|
77.35 0.4819 0.7488 0.0302 0.0194 2.186 13.780 7.938 1630.287 1.557 35.307 2.208 0.68 353745. 0.2154
|
|
80.86 0.5038 0.7448 0.0259 0.0175 1.975 12.449 6.823 1472.913 1.407 30.348 2.101 0.68 354405. 0.1900
|
|
84.38 0.5257 0.7325 0.0216 0.0155 1.749 11.026 5.695 1304.523 1.246 25.332 1.980 0.68 355087. 0.1636
|
|
87.89 0.5476 0.7078 0.0173 0.0134 1.509 9.511 4.557 1125.251 1.075 20.272 1.837 0.68 355792. 0.1358
|
|
91.41 0.5695 0.6631 0.0130 0.0111 1.254 7.906 3.412 935.355 0.893 15.179 1.655 0.68 356519. 0.1058
|
|
94.92 0.5914 0.5811 0.0086 0.0088 0.986 6.214 2.264 735.232 0.702 10.069 1.396 0.68 357268. 0.0727
|
|
98.44 0.6133 0.4153 0.0042 0.0063 0.705 4.440 1.115 525.357 0.502 4.958 0.962 0.69 358036. 0.0352
|
|
101.96 0.6352
|
|
|
|
|
|
|
|
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 0.0998 0.0324 4.862 27.858 31.763 3625.516 3.147 141.283 3.974 0.74 378918. 0.7753
|
|
3.87 0.0219 0.0656 0.0981 0.0327 4.907 28.114 31.212 3658.846 3.176 138.832 3.869 0.74 379164. 0.7483
|
|
7.74 0.0438 0.1277 0.0962 0.0330 4.946 28.337 30.620 3687.913 3.202 136.198 3.766 0.74 379429. 0.7214
|
|
11.61 0.0657 0.1864 0.0942 0.0332 4.978 28.522 29.986 3711.890 3.222 133.376 3.664 0.74 379712. 0.6945
|
|
15.47 0.0876 0.2418 0.0921 0.0334 5.002 28.660 29.307 3729.931 3.238 130.359 3.564 0.74 380014. 0.6679
|
|
19.34 0.1096 0.2939 0.0898 0.0335 5.017 28.746 28.584 3741.148 3.248 127.142 3.465 0.74 380335. 0.6414
|
|
23.21 0.1315 0.3428 0.0874 0.0335 5.022 28.773 27.815 3744.646 3.251 123.720 3.369 0.74 380676. 0.6151
|
|
27.08 0.1534 0.3888 0.0848 0.0335 5.015 28.734 26.998 3739.514 3.246 120.088 3.275 0.74 381038. 0.5890
|
|
30.95 0.1753 0.4318 0.0821 0.0333 4.995 28.621 26.133 3724.818 3.234 116.242 3.182 0.74 381420. 0.5631
|
|
34.82 0.1972 0.4720 0.0792 0.0331 4.961 28.428 25.220 3699.644 3.212 112.180 3.092 0.74 381823. 0.5375
|
|
38.69 0.2191 0.5095 0.0762 0.0328 4.912 28.147 24.259 3663.153 3.180 107.906 3.004 0.74 382248. 0.5121
|
|
42.56 0.2410 0.5443 0.0730 0.0323 4.847 27.775 23.252 3614.714 3.138 103.426 2.918 0.74 382695. 0.4870
|
|
46.42 0.2629 0.5767 0.0697 0.0318 4.766 27.307 22.201 3553.866 3.085 98.752 2.833 0.74 383163. 0.4622
|
|
50.29 0.2848 0.6066 0.0663 0.0311 4.667 26.742 21.110 3480.249 3.021 93.896 2.751 0.74 383654. 0.4376
|
|
54.16 0.3068 0.6341 0.0628 0.0304 4.551 26.076 19.980 3393.560 2.946 88.869 2.670 0.74 384168. 0.4132
|
|
58.03 0.3287 0.6591 0.0591 0.0295 4.417 25.307 18.814 3293.525 2.859 83.683 2.591 0.74 384704. 0.3890
|
|
61.90 0.3506 0.6818 0.0553 0.0285 4.264 24.434 17.614 3179.868 2.760 78.347 2.512 0.74 385264. 0.3650
|
|
65.77 0.3725 0.7019 0.0515 0.0273 4.093 23.453 16.383 3052.300 2.650 72.870 2.434 0.74 385847. 0.3411
|
|
69.64 0.3944 0.7194 0.0475 0.0260 3.903 22.364 15.122 2910.561 2.527 67.262 2.357 0.75 386453. 0.3172
|
|
73.51 0.4163 0.7341 0.0435 0.0246 3.694 21.165 13.833 2754.415 2.391 61.530 2.278 0.75 387084. 0.2933
|
|
77.37 0.4382 0.7455 0.0393 0.0231 3.465 19.853 12.519 2583.666 2.243 55.685 2.198 0.75 387738. 0.2692
|
|
81.24 0.4601 0.7532 0.0351 0.0215 3.216 18.427 11.181 2398.179 2.082 49.734 2.115 0.75 388417. 0.2448
|
|
85.11 0.4820 0.7563 0.0309 0.0197 2.947 16.888 9.822 2197.909 1.908 43.688 2.027 0.75 389120. 0.2199
|
|
88.98 0.5040 0.7534 0.0265 0.0177 2.659 15.236 8.444 1982.916 1.721 37.557 1.931 0.75 389847. 0.1943
|
|
92.85 0.5259 0.7422 0.0221 0.0157 2.351 13.473 7.049 1753.404 1.522 31.354 1.823 0.75 390599. 0.1676
|
|
96.72 0.5478 0.7186 0.0177 0.0135 2.025 11.601 5.641 1509.755 1.311 25.092 1.695 0.75 391376. 0.1393
|
|
100.59 0.5697 0.6744 0.0133 0.0112 1.680 9.625 4.224 1252.566 1.087 18.787 1.529 0.75 392178. 0.1088
|
|
104.46 0.5916 0.5920 0.0088 0.0088 1.318 7.551 2.801 982.678 0.853 12.458 1.293 0.75 393003. 0.0749
|
|
108.32 0.6135 0.4230 0.0043 0.0063 0.940 5.387 1.377 701.065 0.609 6.124 0.891 0.75 393847. 0.0362
|
|
112.19 0.6354
|
|
|
|
|
|
|
|
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 0.1019 0.0347 6.761 35.511 38.610 5041.680 4.012 171.737 3.473 0.81 413286. 0.7471
|
|
4.22 0.0219 0.0628 0.1002 0.0349 6.794 35.683 37.957 5066.102 4.031 168.831 3.398 0.81 413557. 0.7247
|
|
8.43 0.0438 0.1229 0.0983 0.0350 6.819 35.816 37.252 5085.012 4.047 165.698 3.323 0.81 413848. 0.7020
|
|
12.65 0.0657 0.1801 0.0963 0.0351 6.836 35.905 36.496 5097.521 4.056 162.333 3.247 0.81 414160. 0.6791
|
|
16.87 0.0876 0.2346 0.0942 0.0352 6.843 35.941 35.685 5102.729 4.061 158.725 3.172 0.81 414492. 0.6559
|
|
21.09 0.1095 0.2863 0.0919 0.0351 6.839 35.920 34.818 5099.667 4.058 154.869 3.097 0.81 414846. 0.6325
|
|
25.30 0.1314 0.3352 0.0895 0.0351 6.822 35.833 33.893 5087.327 4.048 150.758 3.022 0.81 415221. 0.6090
|
|
29.52 0.1533 0.3814 0.0869 0.0349 6.792 35.673 32.910 5064.643 4.030 146.386 2.947 0.81 415619. 0.5853
|
|
33.74 0.1752 0.4250 0.0841 0.0347 6.746 35.433 31.868 5030.517 4.003 141.749 2.873 0.81 416040. 0.5615
|
|
37.96 0.1971 0.4659 0.0812 0.0343 6.683 35.104 30.766 4983.838 3.966 136.846 2.800 0.81 416483. 0.5376
|
|
42.17 0.2189 0.5042 0.0781 0.0339 6.603 34.679 29.604 4923.542 3.918 131.678 2.727 0.81 416950. 0.5137
|
|
46.39 0.2408 0.5400 0.0749 0.0334 6.502 34.153 28.385 4848.794 3.859 126.255 2.655 0.81 417440. 0.4897
|
|
50.61 0.2627 0.5733 0.0716 0.0328 6.382 33.520 27.111 4758.954 3.787 120.592 2.584 0.81 417954. 0.4657
|
|
54.83 0.2846 0.6041 0.0681 0.0321 6.240 32.777 25.787 4653.476 3.703 114.702 2.513 0.81 418493. 0.4418
|
|
59.04 0.3065 0.6325 0.0645 0.0312 6.077 31.920 24.415 4531.808 3.606 108.600 2.444 0.81 419056. 0.4180
|
|
63.26 0.3284 0.6585 0.0607 0.0303 5.892 30.945 22.999 4393.432 3.496 102.300 2.374 0.81 419644. 0.3942
|
|
67.48 0.3503 0.6820 0.0569 0.0292 5.683 29.850 21.541 4237.995 3.372 95.813 2.305 0.81 420257. 0.3704
|
|
71.69 0.3722 0.7028 0.0529 0.0280 5.452 28.635 20.043 4065.480 3.235 89.152 2.236 0.81 420895. 0.3466
|
|
75.91 0.3941 0.7209 0.0489 0.0267 5.197 27.297 18.509 3875.471 3.084 82.328 2.166 0.81 421559. 0.3226
|
|
80.13 0.4160 0.7359 0.0447 0.0253 4.918 25.833 16.940 3667.548 2.919 75.350 2.095 0.81 422248. 0.2985
|
|
84.35 0.4379 0.7476 0.0405 0.0237 4.615 24.239 15.340 3441.291 2.738 68.231 2.022 0.81 422964. 0.2741
|
|
88.56 0.4598 0.7552 0.0362 0.0220 4.287 22.517 13.709 3196.888 2.544 60.979 1.945 0.82 423705. 0.2493
|
|
92.78 0.4817 0.7577 0.0318 0.0202 3.935 20.671 12.052 2934.692 2.335 53.608 1.863 0.82 424473. 0.2239
|
|
97.00 0.5036 0.7533 0.0274 0.0183 3.561 18.702 10.371 2655.217 2.113 46.129 1.772 0.82 425268. 0.1975
|
|
101.22 0.5255 0.7395 0.0229 0.0163 3.164 16.618 8.668 2359.260 1.877 38.557 1.667 0.82 426089. 0.1698
|
|
105.43 0.5474 0.7113 0.0183 0.0141 2.746 14.425 6.949 2047.927 1.630 30.908 1.539 0.82 426936. 0.1404
|
|
109.65 0.5693 0.6602 0.0138 0.0119 2.310 12.133 5.216 1722.597 1.371 23.200 1.373 0.82 427810. 0.1086
|
|
113.87 0.5912 0.5681 0.0092 0.0095 1.857 9.755 3.475 1385.006 1.102 15.457 1.138 0.82 428710. 0.0734
|
|
118.08 0.6131 0.3920 0.0046 0.0071 1.391 7.305 1.731 1037.083 0.825 7.701 0.757 0.82 429632. 0.0345
|
|
122.30 0.6349 -0.0199 -0.0001 0.0046 0.897 4.709 -0.055 668.539 0.532 -0.243 -0.037 0.82 430378. 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 0.1042 0.0402 9.934 48.163 46.331 7407.771 5.441 206.079 2.837 0.87 447626. 0.6684
|
|
4.58 0.0219 0.0561 0.1025 0.0401 9.916 48.076 45.580 7394.350 5.432 202.738 2.796 0.87 447923. 0.6534
|
|
9.16 0.0439 0.1106 0.1007 0.0400 9.885 47.928 44.764 7371.613 5.415 199.112 2.754 0.87 448242. 0.6379
|
|
13.74 0.0658 0.1633 0.0987 0.0398 9.842 47.715 43.884 7338.868 5.391 195.195 2.712 0.87 448583. 0.6220
|
|
18.32 0.0878 0.2143 0.0966 0.0395 9.783 47.433 42.935 7295.487 5.359 190.976 2.669 0.87 448947. 0.6055
|
|
22.90 0.1097 0.2635 0.0943 0.0393 9.710 47.078 41.917 7240.809 5.319 186.445 2.626 0.87 449335. 0.5885
|
|
27.47 0.1317 0.3109 0.0918 0.0389 9.620 46.643 40.826 7173.995 5.270 181.595 2.581 0.87 449748. 0.5709
|
|
32.05 0.1536 0.3563 0.0892 0.0385 9.513 46.124 39.662 7094.077 5.211 176.418 2.536 0.88 450184. 0.5528
|
|
36.63 0.1756 0.3998 0.0864 0.0379 9.387 45.513 38.424 7000.068 5.142 170.910 2.490 0.88 450646. 0.5342
|
|
41.21 0.1975 0.4413 0.0835 0.0374 9.241 44.803 37.111 6890.990 5.062 165.068 2.443 0.88 451132. 0.5151
|
|
45.79 0.2194 0.4807 0.0803 0.0367 9.073 43.990 35.723 6765.929 4.970 158.895 2.395 0.88 451645. 0.4955
|
|
50.37 0.2414 0.5180 0.0771 0.0359 8.883 43.069 34.263 6624.200 4.866 152.402 2.346 0.88 452183. 0.4754
|
|
54.95 0.2633 0.5532 0.0736 0.0350 8.670 42.036 32.736 6465.356 4.749 145.609 2.297 0.88 452747. 0.4549
|
|
59.53 0.2853 0.5862 0.0701 0.0341 8.434 40.889 31.145 6288.997 4.620 138.533 2.246 0.88 453337. 0.4339
|
|
64.11 0.3072 0.6169 0.0663 0.0330 8.173 39.626 29.495 6094.641 4.477 131.195 2.195 0.88 453954. 0.4127
|
|
68.69 0.3292 0.6453 0.0625 0.0319 7.888 38.242 27.790 5881.762 4.321 123.611 2.143 0.88 454598. 0.3911
|
|
73.26 0.3511 0.6713 0.0586 0.0306 7.576 36.733 26.034 5649.706 4.150 115.798 2.090 0.88 455269. 0.3692
|
|
77.84 0.3730 0.6946 0.0545 0.0293 7.240 35.104 24.229 5399.165 3.966 107.769 2.035 0.88 455967. 0.3468
|
|
82.42 0.3950 0.7144 0.0503 0.0278 6.884 33.377 22.377 5133.547 3.771 99.534 1.977 0.88 456692. 0.3238
|
|
87.00 0.4169 0.7299 0.0461 0.0263 6.510 31.564 20.482 4854.678 3.566 91.105 1.914 0.88 457446. 0.2998
|
|
91.58 0.4389 0.7389 0.0417 0.0248 6.129 29.716 18.545 4570.447 3.357 82.490 1.840 0.88 458227. 0.2744
|
|
96.16 0.4608 0.7424 0.0373 0.0231 5.724 27.751 16.572 4268.231 3.135 73.710 1.761 0.88 459037. 0.2482
|
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100.74 0.4828 0.7388 0.0328 0.0214 5.295 25.673 14.564 3948.662 2.901 64.782 1.673 0.88 459875. 0.2210
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105.32 0.5047 0.7260 0.0282 0.0196 4.846 23.493 12.527 3613.331 2.654 55.720 1.572 0.89 460741. 0.1927
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|
109.90 0.5267 0.7005 0.0235 0.0177 4.377 21.222 10.464 3264.011 2.398 46.543 1.454 0.89 461636. 0.1628
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|
114.48 0.5486 0.6571 0.0188 0.0157 3.893 18.875 8.380 2903.027 2.132 37.273 1.309 0.89 462560. 0.1312
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|
119.05 0.5705 0.5869 0.0141 0.0137 3.397 16.470 6.280 2533.099 1.861 27.935 1.125 0.89 463512. 0.0976
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|
123.63 0.5925 0.4756 0.0094 0.0117 2.893 14.025 4.173 2157.053 1.584 18.560 0.877 0.89 464492. 0.0620
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|
128.21 0.6144 0.2960 0.0046 0.0096 2.384 11.558 2.064 1777.751 1.306 9.180 0.527 0.89 465496. 0.0262
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|
132.79 0.6364 -0.0155 -0.0002 0.0075 1.852 8.979 -0.081 1380.981 1.014 -0.360 -0.027 0.89 466380. 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 0.1049 0.0476 14.716 66.252 54.095 10973.720 7.485 240.613 2.236 0.94 482024. 0.5693
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4.96 0.0221 0.0480 0.1034 0.0476 14.700 66.179 53.334 10961.739 7.477 237.231 2.207 0.94 482336. 0.5579
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|
9.92 0.0442 0.0948 0.1018 0.0474 14.658 65.992 52.496 10930.691 7.456 233.502 2.178 0.94 482674. 0.5463
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|
14.88 0.0662 0.1403 0.1000 0.0472 14.588 65.674 51.575 10878.015 7.420 229.407 2.150 0.94 483037. 0.5346
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|
19.85 0.0883 0.1847 0.0981 0.0469 14.485 65.212 50.567 10801.409 7.368 224.921 2.123 0.94 483426. 0.5227
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|
24.81 0.1104 0.2281 0.0959 0.0464 14.348 64.593 49.466 10699.009 7.298 220.024 2.097 0.94 483843. 0.5106
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|
29.77 0.1325 0.2703 0.0936 0.0459 14.174 63.812 48.269 10569.549 7.209 214.699 2.071 0.94 484287. 0.4982
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|
34.73 0.1545 0.3115 0.0911 0.0452 13.963 62.863 46.973 10412.359 7.102 208.935 2.046 0.94 484760. 0.4855
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|
39.69 0.1766 0.3517 0.0884 0.0444 13.715 61.746 45.576 10227.334 6.976 202.724 2.021 0.94 485261. 0.4724
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|
44.65 0.1987 0.3908 0.0855 0.0435 13.430 60.462 44.079 10014.772 6.831 196.064 1.996 0.94 485790. 0.4588
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|
49.61 0.2208 0.4287 0.0824 0.0424 13.109 59.017 42.482 9775.301 6.668 188.961 1.971 0.94 486349. 0.4447
|
|
54.58 0.2429 0.4655 0.0791 0.0413 12.753 57.414 40.789 9509.925 6.487 181.430 1.945 0.94 486937. 0.4301
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|
59.54 0.2649 0.5008 0.0756 0.0400 12.364 55.663 39.006 9219.882 6.289 173.499 1.919 0.94 487554. 0.4149
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|
64.50 0.2870 0.5348 0.0720 0.0387 11.944 53.771 37.139 8906.407 6.075 165.194 1.891 0.95 488200. 0.3990
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|
69.46 0.3091 0.5672 0.0683 0.0372 11.493 51.742 35.194 8570.377 5.846 156.543 1.863 0.95 488875. 0.3825
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|
74.42 0.3312 0.5978 0.0643 0.0356 11.013 49.580 33.176 8212.177 5.601 147.569 1.832 0.95 489580. 0.3654
|
|
79.38 0.3533 0.6266 0.0603 0.0340 10.503 47.283 31.091 7831.861 5.342 138.292 1.801 0.95 490314. 0.3475
|
|
84.34 0.3753 0.6533 0.0561 0.0322 9.963 44.855 28.942 7429.553 5.068 128.735 1.767 0.95 491078. 0.3291
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|
89.31 0.3974 0.6774 0.0519 0.0304 9.398 42.311 26.735 7008.219 4.780 118.918 1.730 0.95 491873. 0.3097
|
|
94.27 0.4195 0.6968 0.0475 0.0286 8.828 39.746 24.473 6583.335 4.490 108.855 1.686 0.95 492697. 0.2887
|
|
99.23 0.4416 0.7070 0.0430 0.0268 8.292 37.329 22.155 6183.029 4.217 98.547 1.625 0.95 493551. 0.2648
|
|
104.19 0.4636 0.7005 0.0384 0.0254 7.845 35.318 19.781 5849.929 3.990 87.985 1.534 0.95 494436. 0.2361
|
|
109.15 0.4857 0.6846 0.0337 0.0239 7.383 33.239 17.366 5505.616 3.755 77.245 1.431 0.95 495352. 0.2064
|
|
114.11 0.5078 0.6568 0.0289 0.0224 6.911 31.115 14.917 5153.703 3.515 66.352 1.313 0.95 496298. 0.1755
|
|
119.07 0.5299 0.6140 0.0241 0.0208 6.434 28.965 12.441 4797.693 3.272 55.339 1.176 0.95 497274. 0.1436
|
|
124.04 0.5520 0.5526 0.0193 0.0193 5.954 26.806 9.947 4440.068 3.029 44.246 1.016 0.96 498282. 0.1109
|
|
129.00 0.5740 0.4678 0.0144 0.0177 5.476 24.654 7.448 4083.645 2.785 33.126 0.827 0.96 499320. 0.0781
|
|
133.96 0.5961 0.3538 0.0096 0.0162 5.003 22.523 4.955 3730.699 2.545 22.041 0.602 0.96 500388. 0.0464
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|
138.92 0.6182 0.2029 0.0048 0.0147 4.535 20.418 2.484 3381.945 2.307 11.050 0.333 0.96 501483. 0.0182
|
|
143.88 0.6403 0.0004 0.0000 0.0131 4.045 18.211 0.005 3016.396 2.057 0.020 0.001 0.96 502549. 0.0000
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