501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
17x8N (17x8N.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 0.0803 0.0330 0.004 0.238 0.214 2.813 0.027 0.951 34.457 0.07 29265. 0.5498
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0.35 0.0220 0.0522 0.0789 0.0333 0.004 0.240 0.210 2.836 0.027 0.934 33.594 0.07 29281. 0.5315
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0.71 0.0440 0.1017 0.0775 0.0335 0.004 0.242 0.206 2.858 0.027 0.917 32.728 0.07 29300. 0.5129
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1.06 0.0660 0.1485 0.0759 0.0338 0.004 0.243 0.202 2.876 0.027 0.899 31.860 0.07 29319. 0.4943
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1.42 0.0880 0.1926 0.0742 0.0339 0.004 0.244 0.198 2.891 0.028 0.879 30.992 0.07 29340. 0.4755
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1.77 0.1101 0.2340 0.0724 0.0341 0.004 0.245 0.193 2.903 0.028 0.858 30.125 0.07 29362. 0.4566
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2.13 0.1321 0.2727 0.0705 0.0342 0.004 0.246 0.188 2.910 0.028 0.835 29.260 0.07 29386. 0.4376
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2.48 0.1541 0.3088 0.0685 0.0342 0.004 0.246 0.182 2.913 0.028 0.811 28.397 0.07 29412. 0.4186
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2.83 0.1761 0.3422 0.0664 0.0342 0.004 0.246 0.177 2.910 0.028 0.786 27.535 0.07 29439. 0.3995
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3.19 0.1981 0.3729 0.0641 0.0341 0.004 0.245 0.171 2.902 0.028 0.759 26.675 0.07 29468. 0.3803
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3.54 0.2201 0.4010 0.0617 0.0339 0.004 0.244 0.164 2.887 0.028 0.731 25.815 0.07 29499. 0.3612
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3.90 0.2421 0.4264 0.0592 0.0336 0.004 0.242 0.158 2.865 0.027 0.701 24.954 0.07 29532. 0.3419
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4.25 0.2641 0.4490 0.0566 0.0333 0.004 0.240 0.151 2.836 0.027 0.670 24.089 0.07 29566. 0.3227
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4.61 0.2861 0.4689 0.0538 0.0329 0.004 0.237 0.143 2.799 0.027 0.637 23.220 0.07 29602. 0.3034
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4.96 0.3081 0.4859 0.0510 0.0323 0.004 0.233 0.136 2.755 0.026 0.604 22.342 0.07 29641. 0.2841
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5.31 0.3302 0.4999 0.0480 0.0317 0.004 0.228 0.128 2.703 0.026 0.569 21.453 0.07 29681. 0.2647
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5.67 0.3522 0.5107 0.0450 0.0310 0.004 0.223 0.120 2.643 0.025 0.532 20.547 0.07 29723. 0.2454
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6.02 0.3742 0.5181 0.0418 0.0302 0.003 0.218 0.111 2.575 0.025 0.495 19.620 0.07 29767. 0.2260
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6.38 0.3962 0.5219 0.0386 0.0293 0.003 0.211 0.103 2.499 0.024 0.457 18.664 0.07 29812. 0.2066
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6.73 0.4182 0.5215 0.0353 0.0283 0.003 0.204 0.094 2.415 0.023 0.418 17.671 0.07 29860. 0.1871
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7.09 0.4402 0.5167 0.0320 0.0273 0.003 0.196 0.085 2.322 0.022 0.379 16.630 0.07 29910. 0.1675
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7.44 0.4622 0.5065 0.0286 0.0261 0.003 0.188 0.076 2.222 0.021 0.338 15.528 0.07 29962. 0.1478
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7.80 0.4842 0.4903 0.0251 0.0248 0.003 0.179 0.067 2.113 0.020 0.297 14.347 0.07 30016. 0.1280
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8.15 0.5062 0.4667 0.0216 0.0234 0.003 0.169 0.057 1.996 0.019 0.256 13.063 0.07 30072. 0.1081
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8.50 0.5282 0.4341 0.0180 0.0220 0.003 0.158 0.048 1.871 0.018 0.214 11.644 0.07 30130. 0.0881
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8.86 0.5503 0.3902 0.0145 0.0204 0.002 0.147 0.039 1.738 0.017 0.171 10.047 0.07 30190. 0.0680
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9.21 0.5723 0.3315 0.0109 0.0187 0.002 0.135 0.029 1.597 0.015 0.129 8.208 0.07 30252. 0.0482
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9.57 0.5943 0.2531 0.0072 0.0170 0.002 0.122 0.019 1.448 0.014 0.086 6.035 0.07 30316. 0.0289
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9.92 0.6163 0.1471 0.0036 0.0152 0.002 0.109 0.010 1.292 0.012 0.043 3.383 0.07 30382. 0.0115
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10.28 0.6383 0.0006 0.0000 0.0133 0.002 0.095 0.000 1.129 0.011 0.000 0.014 0.07 30450. 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 0.0807 0.0290 0.027 0.836 0.859 19.780 0.094 3.821 19.698 0.13 58529. 0.6301
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0.71 0.0221 0.0599 0.0793 0.0293 0.027 0.845 0.845 19.993 0.095 3.756 19.159 0.13 58563. 0.6077
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1.43 0.0443 0.1164 0.0779 0.0296 0.027 0.853 0.829 20.189 0.096 3.687 18.622 0.13 58599. 0.5852
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2.14 0.0664 0.1696 0.0763 0.0299 0.027 0.861 0.812 20.365 0.097 3.613 18.090 0.13 58638. 0.5627
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2.85 0.0886 0.2195 0.0746 0.0301 0.028 0.867 0.794 20.515 0.098 3.533 17.562 0.13 58680. 0.5403
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3.56 0.1107 0.2663 0.0728 0.0303 0.028 0.872 0.775 20.634 0.099 3.448 17.041 0.13 58725. 0.5179
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4.28 0.1328 0.3099 0.0709 0.0304 0.028 0.876 0.755 20.720 0.099 3.358 16.526 0.13 58774. 0.4956
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4.99 0.1550 0.3504 0.0689 0.0305 0.028 0.878 0.733 20.765 0.099 3.262 16.017 0.14 58826. 0.4734
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5.70 0.1771 0.3879 0.0667 0.0305 0.028 0.878 0.710 20.767 0.099 3.160 15.515 0.14 58881. 0.4513
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6.42 0.1993 0.4224 0.0644 0.0304 0.028 0.876 0.686 20.720 0.099 3.052 15.019 0.14 58939. 0.4294
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7.13 0.2214 0.4540 0.0620 0.0303 0.028 0.871 0.660 20.619 0.098 2.938 14.529 0.14 59002. 0.4076
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7.84 0.2435 0.4828 0.0595 0.0300 0.027 0.865 0.634 20.461 0.098 2.818 14.044 0.14 59067. 0.3858
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8.55 0.2657 0.5087 0.0569 0.0297 0.027 0.855 0.605 20.241 0.097 2.692 13.564 0.14 59137. 0.3642
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9.27 0.2878 0.5317 0.0541 0.0293 0.027 0.843 0.576 19.957 0.095 2.561 13.087 0.14 59210. 0.3428
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9.98 0.3100 0.5517 0.0512 0.0288 0.026 0.829 0.545 19.607 0.094 2.425 12.611 0.14 59287. 0.3214
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10.69 0.3321 0.5688 0.0482 0.0282 0.026 0.811 0.513 19.191 0.092 2.284 12.135 0.14 59368. 0.3001
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11.41 0.3542 0.5828 0.0452 0.0274 0.025 0.791 0.481 18.707 0.089 2.138 11.656 0.14 59453. 0.2789
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12.12 0.3764 0.5935 0.0420 0.0266 0.024 0.767 0.447 18.155 0.087 1.989 11.171 0.14 59542. 0.2578
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12.83 0.3985 0.6006 0.0388 0.0257 0.024 0.741 0.413 17.532 0.084 1.836 10.677 0.14 59635. 0.2367
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13.54 0.4207 0.6037 0.0355 0.0247 0.023 0.712 0.377 16.839 0.080 1.679 10.168 0.14 59732. 0.2156
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14.26 0.4428 0.6024 0.0321 0.0236 0.022 0.679 0.342 16.075 0.077 1.519 9.638 0.14 59832. 0.1944
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14.97 0.4649 0.5959 0.0287 0.0224 0.020 0.644 0.305 15.239 0.073 1.357 9.080 0.14 59937. 0.1731
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15.68 0.4871 0.5832 0.0252 0.0210 0.019 0.606 0.268 14.330 0.068 1.192 8.482 0.14 60046. 0.1516
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16.40 0.5092 0.5627 0.0216 0.0196 0.018 0.564 0.230 13.349 0.064 1.025 7.829 0.14 60160. 0.1297
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17.11 0.5314 0.5325 0.0181 0.0180 0.016 0.520 0.192 12.296 0.059 0.856 7.099 0.14 60277. 0.1075
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17.82 0.5535 0.4891 0.0145 0.0164 0.015 0.472 0.154 11.172 0.053 0.686 6.260 0.14 60398. 0.0848
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18.53 0.5756 0.4274 0.0109 0.0146 0.013 0.422 0.116 9.978 0.048 0.515 5.260 0.14 60524. 0.0618
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19.25 0.5978 0.3387 0.0072 0.0128 0.012 0.368 0.077 8.719 0.042 0.343 4.014 0.14 60653. 0.0385
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19.96 0.6199 0.2074 0.0036 0.0108 0.010 0.313 0.039 7.395 0.035 0.172 2.370 0.14 60787. 0.0161
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20.67 0.6421 0.0018 0.0000 0.0088 0.008 0.254 0.000 6.010 0.029 0.001 0.019 0.14 60922. 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 0.0810 0.0274 0.085 1.778 1.941 63.109 0.201 8.636 13.954 0.20 87792. 0.6711
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1.07 0.0222 0.0637 0.0797 0.0278 0.086 1.799 1.909 63.869 0.203 8.490 13.555 0.20 87842. 0.6464
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2.14 0.0444 0.1237 0.0782 0.0281 0.087 1.819 1.874 64.573 0.206 8.334 13.161 0.20 87897. 0.6218
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3.22 0.0666 0.1801 0.0766 0.0283 0.087 1.837 1.836 65.205 0.208 8.166 12.771 0.20 87956. 0.5973
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4.29 0.0888 0.2329 0.0750 0.0286 0.088 1.852 1.796 65.750 0.209 7.987 12.387 0.20 88020. 0.5729
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5.36 0.1110 0.2823 0.0732 0.0288 0.089 1.865 1.753 66.192 0.211 7.795 12.009 0.20 88088. 0.5487
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6.43 0.1332 0.3282 0.0712 0.0289 0.089 1.874 1.707 66.516 0.212 7.591 11.637 0.20 88161. 0.5247
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7.51 0.1554 0.3709 0.0692 0.0290 0.089 1.879 1.658 66.704 0.212 7.374 11.272 0.20 88239. 0.5009
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8.58 0.1776 0.4104 0.0670 0.0290 0.090 1.880 1.606 66.740 0.212 7.143 10.914 0.20 88322. 0.4774
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9.65 0.1998 0.4469 0.0647 0.0290 0.089 1.877 1.551 66.608 0.212 6.899 10.562 0.20 88410. 0.4540
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10.72 0.2220 0.4802 0.0623 0.0288 0.089 1.868 1.493 66.292 0.211 6.641 10.216 0.20 88504. 0.4308
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11.80 0.2442 0.5107 0.0598 0.0286 0.088 1.853 1.432 65.776 0.209 6.370 9.875 0.20 88603. 0.4079
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12.87 0.2664 0.5382 0.0571 0.0283 0.087 1.833 1.368 65.046 0.207 6.086 9.540 0.20 88708. 0.3852
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13.94 0.2886 0.5628 0.0543 0.0279 0.086 1.806 1.301 64.094 0.204 5.789 9.209 0.20 88819. 0.3626
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15.01 0.3109 0.5846 0.0514 0.0273 0.084 1.773 1.232 62.913 0.200 5.480 8.882 0.20 88935. 0.3403
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16.09 0.3331 0.6034 0.0484 0.0267 0.082 1.733 1.160 61.500 0.196 5.160 8.556 0.20 89057. 0.3181
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17.16 0.3553 0.6191 0.0453 0.0260 0.080 1.686 1.086 59.851 0.191 4.831 8.231 0.20 89185. 0.2961
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18.23 0.3775 0.6317 0.0422 0.0252 0.078 1.633 1.010 57.961 0.184 4.493 7.904 0.20 89319. 0.2742
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19.30 0.3997 0.6408 0.0389 0.0243 0.075 1.573 0.932 55.826 0.178 4.146 7.573 0.20 89459. 0.2523
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20.37 0.4219 0.6462 0.0356 0.0232 0.072 1.506 0.852 53.444 0.170 3.791 7.234 0.20 89605. 0.2305
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21.45 0.4441 0.6472 0.0322 0.0221 0.068 1.432 0.771 50.811 0.162 3.430 6.884 0.20 89757. 0.2086
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22.52 0.4663 0.6433 0.0287 0.0208 0.064 1.350 0.689 47.926 0.153 3.062 6.516 0.20 89916. 0.1866
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23.59 0.4885 0.6333 0.0252 0.0195 0.060 1.262 0.605 44.786 0.143 2.689 6.123 0.20 90080. 0.1643
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24.66 0.5107 0.6157 0.0217 0.0180 0.056 1.166 0.520 41.392 0.132 2.311 5.694 0.20 90251. 0.1417
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25.74 0.5329 0.5882 0.0181 0.0164 0.051 1.063 0.434 37.745 0.120 1.930 5.213 0.21 90427. 0.1185
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26.81 0.5551 0.5470 0.0145 0.0147 0.045 0.954 0.347 33.849 0.108 1.545 4.654 0.21 90611. 0.0947
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27.88 0.5773 0.4859 0.0109 0.0129 0.040 0.837 0.260 29.710 0.095 1.158 3.976 0.21 90800. 0.0700
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28.95 0.5995 0.3938 0.0072 0.0110 0.034 0.714 0.173 25.337 0.081 0.771 3.103 0.21 90995. 0.0446
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30.03 0.6217 0.2487 0.0036 0.0090 0.028 0.584 0.086 20.743 0.066 0.384 1.889 0.21 91197. 0.0192
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31.10 0.6439 -0.0012 0.0000 0.0069 0.021 0.449 0.000 15.928 0.051 -0.001 -0.009 0.21 91399. 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 0.0815 0.0266 0.195 3.067 3.470 145.155 0.347 15.434 10.843 0.27 117052. 0.6971
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1.43 0.0222 0.0661 0.0801 0.0270 0.197 3.107 3.412 147.018 0.351 15.176 10.526 0.27 117120. 0.6711
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2.86 0.0445 0.1282 0.0786 0.0273 0.199 3.143 3.349 148.747 0.355 14.897 10.213 0.27 117193. 0.6451
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4.30 0.0667 0.1865 0.0771 0.0276 0.202 3.176 3.282 150.303 0.359 14.599 9.904 0.27 117272. 0.6193
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5.73 0.0890 0.2411 0.0754 0.0278 0.203 3.204 3.210 151.651 0.362 14.279 9.601 0.27 117357. 0.5938
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7.16 0.1112 0.2921 0.0736 0.0280 0.205 3.228 3.133 152.752 0.365 13.937 9.304 0.27 117448. 0.5684
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8.59 0.1334 0.3395 0.0716 0.0282 0.206 3.245 3.051 153.568 0.367 13.572 9.012 0.27 117546. 0.5434
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10.02 0.1557 0.3835 0.0696 0.0283 0.207 3.255 2.964 154.057 0.368 13.184 8.727 0.27 117651. 0.5186
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11.46 0.1779 0.4243 0.0674 0.0283 0.207 3.258 2.871 154.182 0.368 12.772 8.447 0.27 117762. 0.4940
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12.89 0.2002 0.4618 0.0651 0.0282 0.206 3.252 2.773 153.900 0.367 12.336 8.173 0.27 117880. 0.4698
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14.32 0.2224 0.4963 0.0627 0.0281 0.205 3.237 2.670 153.174 0.366 11.875 7.906 0.27 118006. 0.4459
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15.75 0.2446 0.5279 0.0601 0.0279 0.204 3.211 2.561 151.965 0.363 11.390 7.643 0.27 118139. 0.4222
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17.19 0.2669 0.5564 0.0574 0.0276 0.201 3.175 2.446 150.239 0.359 10.882 7.386 0.27 118279. 0.3987
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18.62 0.2891 0.5821 0.0546 0.0271 0.198 3.127 2.327 147.976 0.353 10.350 7.133 0.27 118427. 0.3755
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20.05 0.3114 0.6050 0.0517 0.0266 0.195 3.067 2.203 145.161 0.347 9.798 6.883 0.27 118583. 0.3526
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21.48 0.3336 0.6249 0.0487 0.0260 0.190 2.996 2.074 141.781 0.338 9.227 6.636 0.27 118746. 0.3299
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22.91 0.3558 0.6419 0.0456 0.0253 0.185 2.912 1.942 137.828 0.329 8.638 6.390 0.27 118917. 0.3074
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24.35 0.3781 0.6558 0.0424 0.0244 0.179 2.817 1.806 133.290 0.318 8.032 6.145 0.27 119097. 0.2850
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25.78 0.4003 0.6664 0.0391 0.0235 0.172 2.708 1.666 128.160 0.306 7.412 5.897 0.27 119284. 0.2627
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27.21 0.4226 0.6734 0.0358 0.0225 0.164 2.587 1.524 122.427 0.292 6.777 5.645 0.27 119479. 0.2405
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28.64 0.4448 0.6762 0.0324 0.0213 0.156 2.453 1.378 116.086 0.277 6.131 5.385 0.27 119683. 0.2182
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30.07 0.4670 0.6743 0.0289 0.0200 0.146 2.306 1.230 109.129 0.261 5.473 5.114 0.27 119894. 0.1958
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31.51 0.4893 0.6665 0.0254 0.0186 0.136 2.146 1.080 101.554 0.242 4.806 4.825 0.27 120114. 0.1731
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32.94 0.5115 0.6513 0.0218 0.0171 0.125 1.973 0.928 93.360 0.223 4.130 4.511 0.27 120343. 0.1500
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34.37 0.5338 0.6264 0.0182 0.0155 0.113 1.787 0.775 84.552 0.202 3.447 4.157 0.27 120579. 0.1263
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35.80 0.5560 0.5876 0.0146 0.0138 0.101 1.588 0.620 75.139 0.179 2.759 3.744 0.27 120824. 0.1018
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37.23 0.5782 0.5283 0.0109 0.0119 0.087 1.376 0.465 65.135 0.155 2.067 3.237 0.27 121077. 0.0762
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38.67 0.6005 0.4356 0.0073 0.0100 0.073 1.153 0.309 54.564 0.130 1.375 2.570 0.27 121339. 0.0493
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40.10 0.6227 0.2821 0.0036 0.0080 0.058 0.918 0.154 43.457 0.104 0.684 1.605 0.27 121608. 0.0217
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41.53 0.6450 -0.0035 0.0000 0.0058 0.043 0.672 -0.001 31.799 0.076 -0.006 -0.019 0.28 121876. 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 0.0820 0.0262 0.374 4.715 5.457 278.897 0.533 24.274 8.875 0.34 146310. 0.7156
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1.79 0.0223 0.0677 0.0806 0.0265 0.379 4.778 5.366 282.629 0.540 23.869 8.612 0.34 146395. 0.6886
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3.58 0.0445 0.1312 0.0792 0.0269 0.384 4.836 5.268 286.094 0.546 23.434 8.352 0.34 146486. 0.6617
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5.38 0.0668 0.1908 0.0776 0.0272 0.388 4.889 5.163 289.218 0.552 22.966 8.097 0.34 146586. 0.6351
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|
7.17 0.0891 0.2466 0.0759 0.0274 0.391 4.935 5.050 291.929 0.558 22.464 7.847 0.34 146692. 0.6087
|
|
8.96 0.1113 0.2986 0.0741 0.0276 0.394 4.972 4.930 294.151 0.562 21.928 7.602 0.34 146807. 0.5826
|
|
10.75 0.1336 0.3470 0.0722 0.0278 0.397 5.000 4.801 295.806 0.565 21.356 7.362 0.34 146930. 0.5568
|
|
12.54 0.1558 0.3920 0.0701 0.0279 0.398 5.018 4.664 296.815 0.567 20.746 7.127 0.34 147061. 0.5313
|
|
14.34 0.1781 0.4336 0.0679 0.0279 0.398 5.022 4.519 297.097 0.567 20.099 6.898 0.34 147200. 0.5061
|
|
16.13 0.2004 0.4720 0.0656 0.0278 0.398 5.013 4.365 296.575 0.566 19.414 6.675 0.34 147349. 0.4813
|
|
17.92 0.2226 0.5073 0.0631 0.0277 0.396 4.990 4.202 295.170 0.564 18.690 6.457 0.34 147506. 0.4568
|
|
19.71 0.2449 0.5396 0.0606 0.0275 0.393 4.950 4.030 292.805 0.559 17.927 6.243 0.34 147673. 0.4326
|
|
21.50 0.2672 0.5689 0.0579 0.0272 0.388 4.892 3.851 289.416 0.553 17.127 6.035 0.34 147849. 0.4087
|
|
23.30 0.2894 0.5954 0.0550 0.0268 0.382 4.817 3.663 284.957 0.544 16.291 5.830 0.34 148034. 0.3851
|
|
25.09 0.3117 0.6191 0.0521 0.0262 0.375 4.723 3.467 279.399 0.534 15.422 5.629 0.34 148230. 0.3618
|
|
26.88 0.3340 0.6399 0.0491 0.0256 0.366 4.610 3.265 272.719 0.521 14.523 5.430 0.34 148434. 0.3387
|
|
28.67 0.3562 0.6579 0.0459 0.0249 0.355 4.478 3.057 264.897 0.506 13.596 5.234 0.34 148649. 0.3158
|
|
30.47 0.3785 0.6728 0.0427 0.0240 0.343 4.326 2.842 255.912 0.489 12.642 5.038 0.34 148874. 0.2931
|
|
32.26 0.4008 0.6845 0.0394 0.0231 0.330 4.154 2.623 245.745 0.469 11.665 4.841 0.34 149108. 0.2706
|
|
34.05 0.4230 0.6928 0.0360 0.0220 0.314 3.962 2.398 234.379 0.448 10.667 4.641 0.34 149353. 0.2481
|
|
35.84 0.4453 0.6970 0.0326 0.0208 0.297 3.749 2.169 221.799 0.424 9.649 4.436 0.34 149608. 0.2255
|
|
37.63 0.4675 0.6967 0.0291 0.0195 0.279 3.516 1.937 207.994 0.397 8.614 4.223 0.34 149873. 0.2028
|
|
39.43 0.4898 0.6908 0.0256 0.0181 0.259 3.262 1.700 192.956 0.369 7.563 3.997 0.34 150149. 0.1799
|
|
41.22 0.5121 0.6777 0.0220 0.0166 0.237 2.987 1.461 176.686 0.337 6.498 3.750 0.34 150435. 0.1565
|
|
43.01 0.5343 0.6550 0.0183 0.0149 0.213 2.691 1.219 159.192 0.304 5.423 3.474 0.34 150731. 0.1324
|
|
44.80 0.5566 0.6187 0.0147 0.0132 0.188 2.375 0.976 140.491 0.268 4.340 3.150 0.34 151038. 0.1074
|
|
46.59 0.5789 0.5615 0.0110 0.0113 0.162 2.039 0.731 120.615 0.230 3.251 2.749 0.34 151356. 0.0811
|
|
48.39 0.6011 0.4693 0.0073 0.0094 0.134 1.684 0.486 99.610 0.190 2.161 2.213 0.34 151683. 0.0532
|
|
50.18 0.6234 0.3106 0.0036 0.0073 0.104 1.311 0.241 77.537 0.148 1.074 1.412 0.34 152020. 0.0239
|
|
51.97 0.6457 -0.0057 0.0000 0.0051 0.073 0.919 -0.003 54.345 0.104 -0.013 -0.025 0.34 152354. 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 0.0827 0.0260 0.641 6.739 7.921 478.348 0.761 35.231 7.510 0.40 175563. 0.7296
|
|
2.15 0.0223 0.0687 0.0813 0.0264 0.650 6.831 7.790 484.938 0.772 34.648 7.286 0.40 175665. 0.7019
|
|
4.30 0.0446 0.1333 0.0798 0.0267 0.659 6.918 7.648 491.061 0.782 34.020 7.064 0.40 175776. 0.6743
|
|
6.46 0.0668 0.1938 0.0782 0.0270 0.666 6.995 7.496 496.583 0.790 33.344 6.847 0.40 175896. 0.6471
|
|
8.61 0.0891 0.2504 0.0765 0.0272 0.672 7.063 7.334 501.379 0.798 32.620 6.634 0.40 176024. 0.6201
|
|
10.76 0.1114 0.3032 0.0747 0.0275 0.678 7.118 7.159 505.315 0.804 31.844 6.426 0.40 176162. 0.5935
|
|
12.91 0.1337 0.3523 0.0728 0.0276 0.682 7.160 6.973 508.252 0.809 31.016 6.223 0.40 176310. 0.5672
|
|
15.07 0.1560 0.3979 0.0707 0.0277 0.684 7.185 6.775 510.052 0.812 30.133 6.024 0.41 176468. 0.5412
|
|
17.22 0.1783 0.4401 0.0685 0.0277 0.685 7.193 6.564 510.575 0.813 29.196 5.831 0.41 176636. 0.5156
|
|
19.37 0.2005 0.4791 0.0662 0.0277 0.683 7.180 6.340 509.683 0.811 28.202 5.642 0.41 176815. 0.4904
|
|
21.52 0.2228 0.5150 0.0637 0.0276 0.680 7.146 6.104 507.240 0.807 27.153 5.459 0.41 177005. 0.4655
|
|
23.67 0.2451 0.5479 0.0611 0.0273 0.675 7.087 5.856 503.109 0.801 26.047 5.279 0.41 177205. 0.4409
|
|
25.83 0.2674 0.5779 0.0584 0.0270 0.667 7.004 5.595 497.178 0.791 24.885 5.104 0.41 177417. 0.4167
|
|
27.98 0.2897 0.6050 0.0555 0.0266 0.656 6.894 5.322 489.366 0.779 23.672 4.933 0.41 177640. 0.3928
|
|
30.13 0.3119 0.6294 0.0526 0.0261 0.643 6.756 5.038 479.621 0.763 22.411 4.765 0.41 177875. 0.3691
|
|
32.28 0.3342 0.6509 0.0495 0.0254 0.627 6.591 4.745 467.901 0.745 21.104 4.599 0.41 178122. 0.3458
|
|
34.44 0.3565 0.6697 0.0464 0.0247 0.609 6.398 4.442 454.172 0.723 19.757 4.436 0.41 178380. 0.3227
|
|
36.59 0.3788 0.6855 0.0431 0.0238 0.588 6.176 4.130 438.397 0.698 18.372 4.273 0.41 178650. 0.2998
|
|
38.74 0.4011 0.6981 0.0398 0.0229 0.564 5.924 3.811 420.544 0.669 16.953 4.111 0.41 178933. 0.2770
|
|
40.89 0.4234 0.7074 0.0364 0.0218 0.537 5.643 3.485 400.581 0.638 15.502 3.946 0.41 179227. 0.2543
|
|
43.04 0.4456 0.7129 0.0329 0.0206 0.508 5.332 3.153 378.483 0.602 14.023 3.778 0.41 179534. 0.2315
|
|
45.20 0.4679 0.7140 0.0294 0.0192 0.475 4.990 2.814 354.228 0.564 12.518 3.603 0.41 179853. 0.2086
|
|
47.35 0.4902 0.7097 0.0258 0.0178 0.440 4.618 2.471 327.805 0.522 10.990 3.419 0.41 180184. 0.1855
|
|
49.50 0.5125 0.6984 0.0222 0.0163 0.401 4.215 2.123 299.214 0.476 9.443 3.218 0.41 180528. 0.1618
|
|
51.65 0.5348 0.6778 0.0185 0.0146 0.360 3.782 1.772 268.468 0.427 7.880 2.993 0.41 180885. 0.1375
|
|
53.81 0.5571 0.6437 0.0148 0.0128 0.316 3.319 1.418 235.601 0.375 6.305 2.729 0.41 181253. 0.1121
|
|
55.96 0.5793 0.5887 0.0111 0.0109 0.269 2.827 1.062 200.666 0.319 4.723 2.400 0.41 181635. 0.0854
|
|
58.11 0.6016 0.4978 0.0074 0.0089 0.220 2.307 0.705 163.747 0.261 3.138 1.954 0.41 182028. 0.0566
|
|
60.26 0.6239 0.3356 0.0037 0.0068 0.168 1.760 0.350 124.951 0.199 1.556 1.270 0.41 182434. 0.0259
|
|
62.42 0.6462 -0.0084 -0.0001 0.0046 0.113 1.185 -0.006 84.145 0.134 -0.025 -0.031 0.41 182831. 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 0.0834 0.0260 1.018 9.165 10.883 759.030 1.035 48.410 6.504 0.47 204811. 0.7405
|
|
2.51 0.0223 0.0695 0.0821 0.0263 1.032 9.294 10.705 769.724 1.050 47.616 6.308 0.47 204931. 0.7124
|
|
5.03 0.0446 0.1347 0.0806 0.0267 1.046 9.414 10.512 779.655 1.064 46.759 6.116 0.47 205061. 0.6844
|
|
7.54 0.0669 0.1959 0.0790 0.0270 1.058 9.522 10.305 788.611 1.076 45.837 5.927 0.47 205201. 0.6567
|
|
10.05 0.0892 0.2530 0.0773 0.0273 1.068 9.616 10.082 796.389 1.086 44.846 5.742 0.47 205352. 0.6293
|
|
12.56 0.1115 0.3063 0.0755 0.0275 1.077 9.693 9.844 802.768 1.095 43.786 5.562 0.47 205513. 0.6023
|
|
15.08 0.1338 0.3560 0.0735 0.0276 1.083 9.751 9.589 807.529 1.102 42.652 5.386 0.47 205687. 0.5756
|
|
17.59 0.1561 0.4021 0.0714 0.0277 1.087 9.786 9.317 810.447 1.106 41.443 5.214 0.47 205872. 0.5494
|
|
20.10 0.1784 0.4448 0.0692 0.0278 1.088 9.796 9.028 811.296 1.107 40.158 5.047 0.47 206069. 0.5235
|
|
22.61 0.2007 0.4843 0.0669 0.0277 1.086 9.779 8.722 809.852 1.105 38.795 4.885 0.47 206278. 0.4979
|
|
25.13 0.2230 0.5206 0.0644 0.0276 1.081 9.731 8.398 805.897 1.099 37.355 4.727 0.47 206500. 0.4728
|
|
27.64 0.2453 0.5540 0.0618 0.0273 1.072 9.650 8.057 799.215 1.090 35.837 4.572 0.47 206735. 0.4480
|
|
30.15 0.2676 0.5845 0.0590 0.0270 1.059 9.534 7.698 789.619 1.077 34.242 4.422 0.47 206983. 0.4235
|
|
32.66 0.2899 0.6122 0.0562 0.0266 1.042 9.382 7.323 776.980 1.060 32.575 4.275 0.47 207245. 0.3993
|
|
35.18 0.3122 0.6371 0.0532 0.0260 1.021 9.191 6.934 761.214 1.038 30.841 4.131 0.47 207520. 0.3755
|
|
37.69 0.3345 0.6593 0.0501 0.0254 0.995 8.962 6.530 742.256 1.013 29.045 3.990 0.47 207808. 0.3519
|
|
40.20 0.3567 0.6787 0.0469 0.0246 0.966 8.694 6.113 720.046 0.982 27.192 3.851 0.48 208110. 0.3286
|
|
42.71 0.3790 0.6952 0.0436 0.0238 0.931 8.386 5.685 694.530 0.947 25.287 3.713 0.48 208426. 0.3055
|
|
45.23 0.4013 0.7088 0.0402 0.0228 0.893 8.038 5.246 665.654 0.908 23.335 3.575 0.48 208756. 0.2826
|
|
47.74 0.4236 0.7190 0.0368 0.0217 0.849 7.648 4.797 633.368 0.864 21.338 3.435 0.48 209101. 0.2597
|
|
50.25 0.4459 0.7256 0.0333 0.0204 0.801 7.216 4.340 597.630 0.815 19.302 3.294 0.48 209459. 0.2368
|
|
52.76 0.4682 0.7279 0.0297 0.0191 0.749 6.743 3.874 558.407 0.762 17.231 3.147 0.48 209832. 0.2138
|
|
55.28 0.4905 0.7249 0.0261 0.0176 0.692 6.227 3.401 515.681 0.703 15.128 2.991 0.48 210220. 0.1904
|
|
57.79 0.5128 0.7153 0.0224 0.0161 0.630 5.668 2.922 469.450 0.640 12.998 2.823 0.48 210622. 0.1666
|
|
60.30 0.5351 0.6966 0.0187 0.0144 0.563 5.068 2.438 419.736 0.573 10.846 2.635 0.48 211038. 0.1420
|
|
62.82 0.5574 0.6647 0.0150 0.0125 0.492 4.426 1.951 366.593 0.500 8.677 2.414 0.48 211469. 0.1164
|
|
65.33 0.5797 0.6120 0.0112 0.0106 0.416 3.744 1.461 310.111 0.423 6.498 2.137 0.48 211915. 0.0891
|
|
67.84 0.6020 0.5226 0.0074 0.0086 0.336 3.024 0.970 250.423 0.342 4.316 1.757 0.48 212375. 0.0597
|
|
70.35 0.6243 0.3581 0.0037 0.0064 0.252 2.266 0.481 187.706 0.256 2.137 1.161 0.48 212848. 0.0278
|
|
72.87 0.6466 -0.0117 -0.0001 0.0042 0.163 1.469 -0.010 121.664 0.166 -0.044 -0.037 0.48 213308. 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 0.0844 0.0261 1.527 12.030 14.375 1138.606 1.359 63.941 5.726 0.54 234053. 0.7494
|
|
2.87 0.0223 0.0700 0.0830 0.0265 1.549 12.202 14.142 1154.938 1.379 62.904 5.554 0.54 234191. 0.7209
|
|
5.75 0.0446 0.1356 0.0815 0.0268 1.569 12.362 13.890 1170.097 1.397 61.783 5.384 0.54 234340. 0.6926
|
|
8.62 0.0669 0.1972 0.0799 0.0271 1.587 12.507 13.619 1183.761 1.413 60.575 5.218 0.54 234501. 0.6647
|
|
11.49 0.0892 0.2547 0.0782 0.0274 1.603 12.632 13.327 1195.613 1.427 59.277 5.056 0.54 234674. 0.6370
|
|
14.37 0.1115 0.3084 0.0764 0.0276 1.616 12.735 13.014 1205.325 1.439 57.884 4.897 0.54 234860. 0.6097
|
|
17.24 0.1339 0.3584 0.0744 0.0278 1.626 12.811 12.678 1212.558 1.447 56.394 4.743 0.54 235058. 0.5829
|
|
20.11 0.1562 0.4049 0.0723 0.0279 1.632 12.858 12.321 1216.969 1.453 54.804 4.592 0.54 235271. 0.5563
|
|
22.99 0.1785 0.4480 0.0701 0.0279 1.634 12.871 11.941 1218.219 1.454 53.112 4.446 0.54 235497. 0.5302
|
|
25.86 0.2008 0.4879 0.0677 0.0279 1.631 12.847 11.537 1215.970 1.451 51.316 4.303 0.54 235738. 0.5045
|
|
28.73 0.2231 0.5246 0.0652 0.0277 1.622 12.783 11.110 1209.889 1.444 49.417 4.165 0.54 235993. 0.4792
|
|
31.61 0.2454 0.5584 0.0626 0.0275 1.609 12.675 10.660 1199.651 1.432 47.414 4.030 0.54 236262. 0.4542
|
|
34.48 0.2677 0.5893 0.0598 0.0272 1.589 12.520 10.186 1184.973 1.414 45.309 3.899 0.54 236547. 0.4295
|
|
37.35 0.2900 0.6175 0.0569 0.0267 1.563 12.316 9.691 1165.658 1.391 43.107 3.771 0.54 236847. 0.4052
|
|
40.22 0.3123 0.6429 0.0539 0.0262 1.531 12.061 9.176 1141.579 1.363 40.816 3.646 0.54 237162. 0.3812
|
|
43.10 0.3346 0.6657 0.0507 0.0255 1.492 11.755 8.643 1112.641 1.328 38.442 3.523 0.54 237493. 0.3575
|
|
45.97 0.3570 0.6857 0.0475 0.0247 1.447 11.397 8.092 1078.752 1.288 35.993 3.402 0.54 237839. 0.3341
|
|
48.84 0.3793 0.7029 0.0442 0.0238 1.394 10.986 7.526 1039.834 1.241 33.474 3.283 0.54 238201. 0.3108
|
|
51.72 0.4016 0.7172 0.0408 0.0228 1.335 10.521 6.945 995.805 1.189 30.891 3.163 0.54 238580. 0.2877
|
|
54.59 0.4239 0.7283 0.0373 0.0217 1.269 10.001 6.351 946.591 1.130 28.250 3.043 0.54 238974. 0.2647
|
|
57.46 0.4462 0.7359 0.0337 0.0205 1.196 9.426 5.745 892.129 1.065 25.556 2.921 0.54 239385. 0.2417
|
|
60.34 0.4685 0.7393 0.0301 0.0191 1.116 8.794 5.129 832.369 0.994 22.814 2.795 0.55 239812. 0.2185
|
|
63.21 0.4908 0.7377 0.0264 0.0176 1.029 8.107 4.503 767.282 0.916 20.030 2.662 0.55 240255. 0.1950
|
|
66.08 0.5131 0.7296 0.0227 0.0160 0.935 7.363 3.869 696.867 0.832 17.210 2.518 0.55 240715. 0.1710
|
|
68.96 0.5354 0.7127 0.0190 0.0142 0.833 6.563 3.228 621.159 0.741 14.360 2.357 0.55 241192. 0.1462
|
|
71.83 0.5577 0.6828 0.0152 0.0124 0.724 5.708 2.583 540.237 0.645 11.488 2.168 0.55 241686. 0.1203
|
|
74.70 0.5801 0.6323 0.0114 0.0104 0.609 4.799 1.934 454.240 0.542 8.601 1.931 0.55 242196. 0.0927
|
|
77.58 0.6024 0.5448 0.0075 0.0083 0.487 3.839 1.283 363.373 0.434 5.709 1.602 0.55 242722. 0.0626
|
|
80.45 0.6247 0.3789 0.0037 0.0061 0.359 2.831 0.635 267.907 0.320 2.822 1.074 0.55 243264. 0.0295
|
|
83.32 0.6470 -0.0160 -0.0001 0.0038 0.224 1.767 -0.016 167.248 0.200 -0.072 -0.044 0.55 243783. 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 0.0855 0.0264 2.196 15.381 18.435 1637.779 1.738 81.998 5.105 0.61 263286. 0.7566
|
|
3.23 0.0223 0.0702 0.0841 0.0268 2.228 15.605 18.140 1661.635 1.763 80.687 4.952 0.61 263442. 0.7279
|
|
6.47 0.0446 0.1361 0.0827 0.0271 2.258 15.813 17.821 1683.767 1.787 79.268 4.801 0.61 263611. 0.6995
|
|
9.70 0.0670 0.1979 0.0811 0.0274 2.285 16.000 17.476 1703.696 1.808 77.735 4.653 0.61 263793. 0.6713
|
|
12.94 0.0893 0.2557 0.0793 0.0277 2.308 16.162 17.106 1720.958 1.826 76.086 4.508 0.61 263989. 0.6436
|
|
16.17 0.1116 0.3096 0.0775 0.0279 2.327 16.295 16.707 1735.071 1.841 74.313 4.367 0.61 264199. 0.6162
|
|
19.40 0.1339 0.3599 0.0755 0.0281 2.341 16.393 16.280 1745.545 1.852 72.414 4.230 0.61 264424. 0.5891
|
|
22.64 0.1562 0.4066 0.0734 0.0282 2.349 16.453 15.824 1751.882 1.859 70.385 4.097 0.61 264664. 0.5625
|
|
25.87 0.1786 0.4500 0.0711 0.0282 2.352 16.469 15.338 1753.591 1.861 68.224 3.967 0.61 264920. 0.5363
|
|
29.11 0.2009 0.4901 0.0687 0.0282 2.347 16.437 14.822 1750.181 1.857 65.929 3.841 0.61 265192. 0.5104
|
|
32.34 0.2232 0.5272 0.0662 0.0280 2.335 16.352 14.276 1741.178 1.847 63.499 3.719 0.61 265480. 0.4850
|
|
35.57 0.2455 0.5614 0.0635 0.0278 2.315 16.211 13.699 1726.111 1.831 60.934 3.600 0.61 265785. 0.4599
|
|
38.81 0.2679 0.5927 0.0607 0.0274 2.286 16.008 13.093 1704.569 1.809 58.237 3.484 0.61 266107. 0.4351
|
|
42.04 0.2902 0.6213 0.0578 0.0270 2.248 15.742 12.458 1676.268 1.779 55.414 3.371 0.61 266445. 0.4107
|
|
45.28 0.3125 0.6472 0.0547 0.0264 2.201 15.411 11.797 1641.025 1.741 52.475 3.261 0.61 266801. 0.3866
|
|
48.51 0.3348 0.6705 0.0515 0.0257 2.144 15.014 11.113 1598.707 1.696 49.429 3.153 0.61 267175. 0.3628
|
|
51.74 0.3571 0.6911 0.0483 0.0249 2.077 14.549 10.406 1549.190 1.644 46.284 3.047 0.61 267566. 0.3392
|
|
54.98 0.3795 0.7090 0.0449 0.0240 2.001 14.015 9.678 1492.358 1.583 43.049 2.941 0.61 267975. 0.3158
|
|
58.21 0.4018 0.7240 0.0414 0.0230 1.915 13.412 8.932 1428.100 1.515 39.731 2.837 0.61 268401. 0.2926
|
|
61.45 0.4241 0.7359 0.0379 0.0218 1.819 12.738 8.169 1356.310 1.439 36.337 2.732 0.61 268846. 0.2695
|
|
64.68 0.4464 0.7444 0.0343 0.0206 1.712 11.992 7.391 1276.897 1.355 32.874 2.625 0.61 269309. 0.2463
|
|
67.92 0.4687 0.7489 0.0306 0.0192 1.596 11.174 6.598 1189.790 1.262 29.349 2.515 0.61 269791. 0.2230
|
|
71.15 0.4911 0.7485 0.0269 0.0176 1.468 10.283 5.793 1094.948 1.162 25.768 2.400 0.61 270291. 0.1994
|
|
74.38 0.5134 0.7419 0.0231 0.0160 1.331 9.320 4.978 992.369 1.053 22.141 2.275 0.61 270810. 0.1752
|
|
77.62 0.5357 0.7267 0.0193 0.0142 1.183 8.284 4.153 882.104 0.936 18.474 2.136 0.62 271347. 0.1502
|
|
80.85 0.5580 0.6988 0.0154 0.0123 1.025 7.178 3.322 764.268 0.811 14.777 1.972 0.62 271903. 0.1240
|
|
84.09 0.5804 0.6506 0.0115 0.0103 0.857 6.002 2.487 639.065 0.678 11.061 1.765 0.62 272477. 0.0961
|
|
87.32 0.6027 0.5651 0.0077 0.0082 0.680 4.759 1.650 506.794 0.538 7.337 1.476 0.62 273070. 0.0654
|
|
90.55 0.6250 0.3984 0.0038 0.0059 0.493 3.455 0.814 367.851 0.390 3.621 1.004 0.62 273680. 0.0313
|
|
93.79 0.6473 -0.0215 -0.0001 0.0036 0.297 2.077 -0.025 221.120 0.235 -0.113 -0.052 0.62 274256. 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 0.0868 0.0268 3.061 19.291 23.112 2282.312 2.179 102.803 4.593 0.67 292509. 0.7622
|
|
3.60 0.0223 0.0702 0.0855 0.0272 3.106 19.574 22.750 2315.828 2.211 101.191 4.456 0.67 292683. 0.7335
|
|
7.19 0.0447 0.1362 0.0840 0.0275 3.147 19.837 22.356 2346.941 2.241 99.440 4.321 0.67 292872. 0.7051
|
|
10.79 0.0670 0.1980 0.0824 0.0279 3.185 20.074 21.930 2374.968 2.268 97.547 4.188 0.67 293075. 0.6770
|
|
14.38 0.0893 0.2559 0.0807 0.0282 3.217 20.279 21.471 2399.226 2.291 95.503 4.059 0.67 293294. 0.6492
|
|
17.98 0.1117 0.3100 0.0788 0.0284 3.244 20.446 20.976 2419.022 2.310 93.303 3.933 0.67 293530. 0.6218
|
|
21.57 0.1340 0.3604 0.0768 0.0286 3.264 20.570 20.446 2433.645 2.324 90.942 3.811 0.67 293781. 0.5947
|
|
25.17 0.1563 0.4073 0.0747 0.0287 3.275 20.644 19.878 2442.392 2.332 88.415 3.691 0.68 294050. 0.5681
|
|
28.76 0.1787 0.4509 0.0724 0.0287 3.278 20.662 19.271 2444.568 2.334 85.720 3.576 0.68 294336. 0.5418
|
|
32.36 0.2010 0.4913 0.0700 0.0286 3.271 20.619 18.627 2439.500 2.330 82.853 3.463 0.68 294640. 0.5159
|
|
35.95 0.2233 0.5287 0.0674 0.0285 3.254 20.510 17.944 2426.523 2.317 79.815 3.354 0.68 294962. 0.4904
|
|
39.55 0.2457 0.5631 0.0647 0.0282 3.225 20.328 17.223 2404.988 2.297 76.606 3.248 0.68 295303. 0.4653
|
|
43.14 0.2680 0.5948 0.0619 0.0279 3.184 20.068 16.463 2374.321 2.267 73.228 3.145 0.68 295662. 0.4404
|
|
46.74 0.2903 0.6238 0.0589 0.0274 3.130 19.729 15.668 2334.128 2.229 69.690 3.045 0.68 296040. 0.4159
|
|
50.33 0.3127 0.6502 0.0558 0.0268 3.063 19.306 14.839 2284.160 2.181 66.003 2.947 0.68 296437. 0.3918
|
|
53.93 0.3350 0.6740 0.0525 0.0261 2.983 18.800 13.979 2224.232 2.124 62.180 2.851 0.68 296854. 0.3679
|
|
57.52 0.3573 0.6951 0.0492 0.0253 2.889 18.208 13.092 2154.188 2.057 58.232 2.756 0.68 297290. 0.3442
|
|
61.12 0.3797 0.7137 0.0458 0.0243 2.781 17.529 12.178 2073.871 1.980 54.168 2.663 0.68 297746. 0.3208
|
|
64.71 0.4020 0.7294 0.0422 0.0233 2.659 16.762 11.241 1983.129 1.894 49.999 2.571 0.68 298222. 0.2975
|
|
68.31 0.4243 0.7421 0.0386 0.0221 2.524 15.906 10.282 1881.818 1.797 45.733 2.478 0.68 298718. 0.2743
|
|
71.90 0.4467 0.7515 0.0350 0.0208 2.373 14.959 9.303 1769.814 1.690 41.378 2.384 0.68 299234. 0.2510
|
|
75.50 0.4690 0.7571 0.0312 0.0193 2.209 13.921 8.306 1647.025 1.573 36.944 2.287 0.68 299770. 0.2275
|
|
79.10 0.4913 0.7579 0.0274 0.0178 2.029 12.792 7.293 1513.390 1.445 32.439 2.186 0.68 300327. 0.2037
|
|
82.69 0.5137 0.7527 0.0235 0.0161 1.836 11.570 6.266 1368.909 1.307 27.873 2.076 0.68 300904. 0.1794
|
|
86.29 0.5360 0.7392 0.0196 0.0142 1.628 10.258 5.229 1213.653 1.159 23.256 1.954 0.68 301502. 0.1542
|
|
89.88 0.5583 0.7133 0.0157 0.0123 1.405 8.856 4.182 1047.790 1.001 18.600 1.810 0.68 302121. 0.1278
|
|
93.48 0.5807 0.6673 0.0118 0.0102 1.169 7.367 3.129 871.622 0.832 13.918 1.628 0.69 302760. 0.0994
|
|
97.07 0.6030 0.5840 0.0078 0.0080 0.919 5.795 2.074 685.610 0.655 9.226 1.372 0.69 303420. 0.0682
|
|
100.67 0.6253 0.4168 0.0038 0.0058 0.658 4.145 1.021 490.367 0.468 4.542 0.944 0.69 304099. 0.0329
|
|
104.26 0.6477 -0.0291 -0.0001 0.0033 0.381 2.400 -0.040 283.902 0.271 -0.177 -0.064 0.69 304725. 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 0.0884 0.0277 4.206 24.101 28.470 3136.622 2.723 126.636 4.117 0.74 321717. 0.7582
|
|
3.95 0.0223 0.0693 0.0871 0.0280 4.261 24.415 28.036 3177.487 2.758 124.705 4.002 0.74 321910. 0.7314
|
|
7.90 0.0446 0.1347 0.0856 0.0284 4.312 24.706 27.563 3215.340 2.791 122.602 3.888 0.74 322119. 0.7046
|
|
11.86 0.0670 0.1963 0.0840 0.0287 4.357 24.967 27.050 3249.323 2.821 120.318 3.776 0.74 322344. 0.6778
|
|
15.81 0.0893 0.2540 0.0823 0.0289 4.397 25.192 26.494 3278.571 2.846 117.846 3.665 0.74 322587. 0.6512
|
|
19.76 0.1116 0.3081 0.0804 0.0291 4.428 25.373 25.894 3302.175 2.867 115.178 3.557 0.74 322847. 0.6247
|
|
23.71 0.1339 0.3587 0.0784 0.0293 4.451 25.504 25.249 3319.165 2.881 112.307 3.450 0.74 323126. 0.5984
|
|
27.67 0.1562 0.4059 0.0762 0.0294 4.464 25.576 24.557 3328.577 2.890 109.228 3.346 0.74 323423. 0.5723
|
|
31.62 0.1786 0.4498 0.0740 0.0294 4.465 25.583 23.817 3329.439 2.890 105.936 3.245 0.74 323740. 0.5465
|
|
35.57 0.2009 0.4905 0.0715 0.0293 4.453 25.516 23.028 3320.787 2.883 102.430 3.145 0.74 324076. 0.5210
|
|
39.52 0.2232 0.5282 0.0689 0.0291 4.428 25.370 22.191 3301.665 2.866 98.707 3.049 0.74 324432. 0.4957
|
|
43.48 0.2455 0.5631 0.0662 0.0288 4.387 25.135 21.306 3271.123 2.840 94.770 2.954 0.74 324808. 0.4707
|
|
47.43 0.2678 0.5952 0.0633 0.0285 4.329 24.806 20.373 3228.314 2.803 90.621 2.862 0.74 325205. 0.4459
|
|
51.38 0.2902 0.6246 0.0602 0.0280 4.255 24.378 19.395 3172.606 2.754 86.271 2.773 0.74 325623. 0.4215
|
|
55.33 0.3125 0.6515 0.0571 0.0274 4.162 23.848 18.375 3103.594 2.694 81.734 2.685 0.75 326061. 0.3973
|
|
59.29 0.3348 0.6758 0.0538 0.0266 4.051 23.213 17.317 3021.002 2.623 77.026 2.600 0.75 326521. 0.3734
|
|
63.24 0.3571 0.6975 0.0504 0.0258 3.922 22.472 16.223 2924.607 2.539 72.160 2.516 0.75 327002. 0.3498
|
|
67.19 0.3794 0.7167 0.0469 0.0248 3.774 21.624 15.096 2814.195 2.443 67.149 2.433 0.75 327505. 0.3263
|
|
71.14 0.4018 0.7332 0.0433 0.0237 3.607 20.666 13.940 2689.592 2.335 62.006 2.351 0.75 328029. 0.3030
|
|
75.10 0.4241 0.7468 0.0396 0.0225 3.420 19.599 12.756 2550.619 2.214 56.740 2.268 0.75 328576. 0.2796
|
|
79.05 0.4464 0.7572 0.0359 0.0211 3.215 18.419 11.547 2397.114 2.081 51.363 2.185 0.75 329144. 0.2563
|
|
83.00 0.4687 0.7638 0.0320 0.0197 2.989 17.127 10.316 2229.020 1.935 45.885 2.099 0.75 329735. 0.2327
|
|
86.95 0.4910 0.7659 0.0281 0.0180 2.744 15.724 9.064 2046.318 1.776 40.318 2.009 0.75 330348. 0.2088
|
|
90.91 0.5134 0.7620 0.0242 0.0163 2.480 14.208 7.795 1849.099 1.605 34.672 1.912 0.75 330983. 0.1843
|
|
94.86 0.5357 0.7499 0.0202 0.0144 2.196 12.583 6.511 1637.604 1.422 28.960 1.803 0.75 331641. 0.1588
|
|
98.81 0.5580 0.7255 0.0162 0.0125 1.894 10.852 5.215 1412.263 1.226 23.196 1.675 0.75 332322. 0.1320
|
|
102.76 0.5803 0.6809 0.0121 0.0104 1.574 9.019 3.911 1173.734 1.019 17.397 1.511 0.75 333025. 0.1032
|
|
106.72 0.6026 0.5986 0.0081 0.0081 1.238 7.092 2.604 922.958 0.801 11.581 1.280 0.76 333750. 0.0713
|
|
110.67 0.6250 0.4318 0.0040 0.0058 0.887 5.080 1.297 661.136 0.574 5.771 0.890 0.76 334496. 0.0350
|
|
114.62 0.6473 -0.0092 0.0000 0.0034 0.519 2.971 -0.016 386.719 0.336 -0.069 -0.018 0.76 335202. 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 0.0902 0.0301 5.937 31.183 34.580 4427.209 3.523 153.812 3.543 0.81 350907. 0.7191
|
|
4.31 0.0223 0.0655 0.0889 0.0303 5.984 31.432 34.074 4462.500 3.551 151.560 3.463 0.81 351119. 0.6978
|
|
8.63 0.0447 0.1279 0.0875 0.0305 6.026 31.649 33.519 4493.290 3.576 149.093 3.384 0.81 351348. 0.6761
|
|
12.94 0.0670 0.1874 0.0859 0.0307 6.060 31.828 32.914 4518.695 3.596 146.402 3.304 0.81 351596. 0.6542
|
|
17.25 0.0893 0.2438 0.0842 0.0308 6.085 31.962 32.256 4537.786 3.611 143.474 3.224 0.81 351863. 0.6320
|
|
21.56 0.1116 0.2973 0.0823 0.0309 6.101 32.045 31.543 4549.624 3.620 140.301 3.145 0.81 352149. 0.6096
|
|
25.88 0.1340 0.3477 0.0803 0.0309 6.106 32.071 30.772 4553.225 3.623 136.874 3.065 0.81 352456. 0.5869
|
|
30.19 0.1563 0.3953 0.0781 0.0309 6.098 32.031 29.943 4547.515 3.619 133.187 2.987 0.81 352783. 0.5641
|
|
34.50 0.1786 0.4399 0.0758 0.0308 6.077 31.917 29.054 4531.401 3.606 129.233 2.908 0.81 353132. 0.5411
|
|
38.82 0.2009 0.4816 0.0733 0.0306 6.040 31.722 28.105 4503.768 3.584 125.011 2.830 0.81 353501. 0.5179
|
|
43.13 0.2233 0.5206 0.0707 0.0303 5.986 31.439 27.095 4463.514 3.552 120.519 2.753 0.81 353893. 0.4947
|
|
47.44 0.2456 0.5567 0.0679 0.0300 5.913 31.059 26.024 4409.519 3.509 115.757 2.677 0.81 354306. 0.4713
|
|
51.75 0.2679 0.5902 0.0650 0.0295 5.821 30.574 24.894 4340.706 3.454 110.730 2.601 0.81 354742. 0.4480
|
|
56.07 0.2902 0.6210 0.0619 0.0289 5.708 29.979 23.708 4256.250 3.387 105.452 2.526 0.81 355201. 0.4246
|
|
60.38 0.3126 0.6491 0.0586 0.0282 5.573 29.270 22.468 4155.579 3.307 99.940 2.452 0.81 355682. 0.4012
|
|
64.69 0.3349 0.6747 0.0553 0.0274 5.415 28.443 21.181 4038.226 3.214 94.213 2.379 0.81 356186. 0.3779
|
|
69.01 0.3572 0.6977 0.0518 0.0265 5.235 27.496 19.849 3903.751 3.107 88.288 2.306 0.81 356714. 0.3546
|
|
73.32 0.3795 0.7179 0.0482 0.0255 5.032 26.429 18.476 3752.218 2.986 82.182 2.233 0.82 357265. 0.3314
|
|
77.63 0.4019 0.7352 0.0445 0.0243 4.805 25.238 17.066 3583.175 2.851 75.910 2.160 0.82 357839. 0.3080
|
|
81.94 0.4242 0.7495 0.0408 0.0231 4.554 23.921 15.622 3396.208 2.703 69.485 2.086 0.82 358438. 0.2846
|
|
86.26 0.4465 0.7602 0.0369 0.0217 4.280 22.478 14.146 3191.362 2.540 62.920 2.010 0.82 359060. 0.2610
|
|
90.57 0.4688 0.7670 0.0330 0.0202 3.981 20.907 12.641 2968.317 2.362 56.228 1.932 0.82 359706. 0.2370
|
|
94.88 0.4912 0.7686 0.0290 0.0185 3.657 19.210 11.111 2727.342 2.170 49.421 1.848 0.82 360377. 0.2126
|
|
99.20 0.5135 0.7635 0.0249 0.0168 3.311 17.391 9.558 2469.134 1.965 42.514 1.756 0.82 361072. 0.1874
|
|
103.51 0.5358 0.7489 0.0208 0.0149 2.943 15.458 7.986 2194.577 1.746 35.521 1.650 0.82 361791. 0.1610
|
|
107.82 0.5581 0.7201 0.0167 0.0129 2.554 13.417 6.398 1904.867 1.516 28.459 1.523 0.82 362535. 0.1330
|
|
112.13 0.5805 0.6682 0.0125 0.0109 2.148 11.281 4.800 1601.569 1.274 21.349 1.359 0.82 363303. 0.1028
|
|
116.45 0.6028 0.5750 0.0083 0.0087 1.725 9.062 3.195 1286.625 1.024 14.212 1.126 0.82 364095. 0.0695
|
|
120.76 0.6251 0.3969 0.0041 0.0065 1.290 6.778 1.590 962.313 0.766 7.074 0.750 0.83 364910. 0.0326
|
|
125.07 0.6474 -0.0088 -0.0001 0.0043 0.841 4.416 -0.022 626.930 0.499 -0.099 -0.016 0.83 365686. 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 0.0920 0.0354 8.883 43.067 41.389 6623.882 4.866 184.099 2.834 0.88 380083. 0.6293
|
|
4.68 0.0224 0.0573 0.0908 0.0355 8.901 43.153 40.827 6637.123 4.875 181.599 2.790 0.88 380312. 0.6153
|
|
9.37 0.0448 0.1128 0.0894 0.0355 8.905 43.174 40.204 6640.421 4.878 178.830 2.746 0.88 380562. 0.6010
|
|
14.05 0.0671 0.1664 0.0879 0.0354 8.895 43.125 39.518 6632.883 4.872 175.776 2.702 0.88 380832. 0.5863
|
|
18.73 0.0895 0.2183 0.0862 0.0353 8.869 43.001 38.765 6613.799 4.858 172.425 2.658 0.88 381123. 0.5713
|
|
23.42 0.1119 0.2684 0.0843 0.0352 8.827 42.798 37.941 6582.528 4.835 168.762 2.614 0.88 381436. 0.5558
|
|
28.10 0.1343 0.3166 0.0824 0.0349 8.768 42.511 37.045 6538.467 4.803 164.777 2.570 0.88 381772. 0.5399
|
|
32.78 0.1566 0.3628 0.0802 0.0346 8.691 42.138 36.075 6481.035 4.761 160.463 2.525 0.88 382131. 0.5234
|
|
37.46 0.1790 0.4071 0.0779 0.0342 8.595 41.674 35.030 6409.624 4.708 155.812 2.479 0.88 382512. 0.5064
|
|
42.15 0.2014 0.4494 0.0754 0.0338 8.480 41.114 33.908 6323.565 4.645 150.822 2.432 0.88 382918. 0.4888
|
|
46.83 0.2238 0.4895 0.0727 0.0332 8.344 40.454 32.710 6222.109 4.571 145.494 2.384 0.88 383347. 0.4707
|
|
51.51 0.2461 0.5275 0.0699 0.0326 8.186 39.689 31.436 6104.396 4.484 139.827 2.336 0.88 383800. 0.4520
|
|
56.20 0.2685 0.5632 0.0669 0.0319 8.005 38.812 30.087 5969.501 4.385 133.827 2.286 0.88 384278. 0.4328
|
|
60.88 0.2909 0.5966 0.0637 0.0311 7.800 37.818 28.667 5816.671 4.273 127.510 2.235 0.88 384780. 0.4131
|
|
65.56 0.3133 0.6277 0.0604 0.0302 7.571 36.705 27.180 5645.375 4.147 120.896 2.184 0.88 385307. 0.3930
|
|
70.25 0.3357 0.6563 0.0570 0.0291 7.316 35.468 25.632 5455.241 4.007 114.010 2.131 0.88 385859. 0.3724
|
|
74.93 0.3580 0.6824 0.0534 0.0280 7.035 34.108 24.027 5245.938 3.853 106.874 2.077 0.88 386436. 0.3515
|
|
79.61 0.3804 0.7059 0.0497 0.0268 6.728 32.620 22.372 5017.115 3.685 99.510 2.023 0.88 387038. 0.3302
|
|
84.29 0.4028 0.7259 0.0459 0.0255 6.400 31.028 20.669 4772.273 3.506 91.934 1.964 0.88 387666. 0.3082
|
|
88.98 0.4252 0.7422 0.0421 0.0241 6.049 29.326 18.922 4510.465 3.313 84.166 1.903 0.88 388320. 0.2857
|
|
93.66 0.4475 0.7541 0.0381 0.0226 5.675 27.515 17.136 4232.006 3.109 76.221 1.837 0.89 388999. 0.2624
|
|
98.34 0.4699 0.7576 0.0340 0.0211 5.300 25.698 15.312 3952.469 2.903 68.107 1.757 0.89 389704. 0.2373
|
|
103.03 0.4923 0.7540 0.0299 0.0195 4.903 23.770 13.455 3655.997 2.686 59.849 1.669 0.89 390436. 0.2113
|
|
107.71 0.5147 0.7412 0.0257 0.0179 4.483 21.737 11.570 3343.285 2.456 51.465 1.570 0.89 391194. 0.1843
|
|
112.39 0.5370 0.7157 0.0215 0.0161 4.046 19.615 9.661 3016.858 2.216 42.974 1.453 0.89 391978. 0.1558
|
|
117.08 0.5594 0.6720 0.0172 0.0143 3.593 17.418 7.733 2678.978 1.968 34.398 1.309 0.89 392788. 0.1257
|
|
121.76 0.5818 0.6012 0.0129 0.0125 3.128 15.166 5.793 2332.563 1.713 25.765 1.126 0.89 393625. 0.0936
|
|
126.44 0.6042 0.4881 0.0085 0.0106 2.656 12.879 3.846 1980.901 1.455 17.107 0.881 0.89 394488. 0.0596
|
|
131.12 0.6266 0.3047 0.0042 0.0087 2.182 10.581 1.902 1627.352 1.195 8.460 0.530 0.89 395375. 0.0252
|
|
135.81 0.6489 -0.0097 -0.0001 0.0068 1.701 8.246 -0.046 1268.307 0.932 -0.204 -0.016 0.90 396238. 0.0000
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