538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
16x5.5MR (16x55MR.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 0.0794 0.0288 0.002 0.153 0.166 1.812 0.017 0.737 41.480 0.06 29141. 0.6193
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0.25 0.0164 0.0443 0.0777 0.0288 0.002 0.153 0.162 1.812 0.017 0.721 40.602 0.06 29154. 0.5997
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0.50 0.0328 0.0866 0.0759 0.0288 0.002 0.153 0.158 1.810 0.017 0.705 39.714 0.06 29169. 0.5798
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0.75 0.0492 0.1269 0.0740 0.0287 0.002 0.153 0.155 1.807 0.017 0.688 38.815 0.06 29184. 0.5597
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0.99 0.0656 0.1653 0.0721 0.0286 0.002 0.152 0.151 1.802 0.017 0.670 37.901 0.06 29200. 0.5394
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1.24 0.0820 0.2015 0.0701 0.0285 0.002 0.152 0.146 1.796 0.017 0.651 36.975 0.06 29217. 0.5188
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1.49 0.0985 0.2357 0.0680 0.0284 0.002 0.151 0.142 1.788 0.017 0.632 36.035 0.06 29235. 0.4980
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1.74 0.1149 0.2676 0.0658 0.0283 0.002 0.150 0.137 1.778 0.017 0.612 35.077 0.06 29253. 0.4770
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1.99 0.1313 0.2974 0.0636 0.0281 0.002 0.149 0.133 1.766 0.017 0.591 34.100 0.06 29272. 0.4557
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2.24 0.1477 0.3247 0.0612 0.0278 0.002 0.148 0.128 1.752 0.017 0.569 33.101 0.06 29292. 0.4341
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2.49 0.1641 0.3497 0.0588 0.0276 0.002 0.147 0.123 1.736 0.017 0.546 32.080 0.06 29313. 0.4123
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2.73 0.1805 0.3720 0.0563 0.0273 0.002 0.145 0.118 1.718 0.016 0.523 31.027 0.06 29334. 0.3901
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2.98 0.1969 0.3916 0.0537 0.0270 0.002 0.143 0.112 1.698 0.016 0.498 29.942 0.06 29357. 0.3676
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3.23 0.2133 0.4084 0.0510 0.0266 0.002 0.142 0.106 1.675 0.016 0.473 28.822 0.06 29380. 0.3448
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3.48 0.2297 0.4221 0.0482 0.0262 0.002 0.139 0.101 1.650 0.016 0.448 27.662 0.06 29404. 0.3218
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3.73 0.2461 0.4326 0.0453 0.0258 0.002 0.137 0.095 1.623 0.016 0.421 26.458 0.06 29430. 0.2986
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3.98 0.2626 0.4396 0.0424 0.0253 0.002 0.135 0.089 1.594 0.015 0.394 25.206 0.06 29456. 0.2751
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4.23 0.2790 0.4428 0.0394 0.0248 0.002 0.132 0.082 1.563 0.015 0.366 23.898 0.06 29483. 0.2515
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4.48 0.2954 0.4420 0.0364 0.0243 0.002 0.129 0.076 1.530 0.015 0.338 22.528 0.06 29510. 0.2277
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4.72 0.3118 0.4367 0.0333 0.0237 0.002 0.126 0.069 1.494 0.014 0.309 21.088 0.06 29539. 0.2038
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4.97 0.3282 0.4266 0.0301 0.0231 0.002 0.123 0.063 1.456 0.014 0.279 19.568 0.06 29569. 0.1799
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5.22 0.3446 0.4111 0.0268 0.0225 0.002 0.120 0.056 1.416 0.014 0.249 17.959 0.06 29600. 0.1559
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5.47 0.3610 0.3896 0.0236 0.0218 0.002 0.116 0.049 1.373 0.013 0.219 16.247 0.06 29632. 0.1321
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5.72 0.3774 0.3615 0.0202 0.0211 0.002 0.112 0.042 1.328 0.013 0.188 14.419 0.06 29665. 0.1087
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5.97 0.3938 0.3259 0.0169 0.0204 0.002 0.108 0.035 1.281 0.012 0.157 12.457 0.06 29699. 0.0857
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6.22 0.4102 0.2819 0.0135 0.0196 0.002 0.104 0.028 1.232 0.012 0.125 10.343 0.06 29734. 0.0636
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6.46 0.4267 0.2283 0.0100 0.0188 0.002 0.100 0.021 1.181 0.011 0.093 8.054 0.06 29770. 0.0428
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6.71 0.4431 0.1638 0.0066 0.0179 0.002 0.095 0.014 1.127 0.011 0.062 5.565 0.06 29806. 0.0240
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6.96 0.4595 0.0870 0.0032 0.0170 0.001 0.091 0.007 1.072 0.010 0.030 2.849 0.06 29844. 0.0086
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7.21 0.4759 -0.0051 -0.0002 0.0161 0.001 0.086 0.000 1.015 0.010 -0.002 -0.160 0.06 29881. 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 0.0796 0.0265 0.018 0.564 0.665 13.337 0.064 2.958 22.618 0.13 58281. 0.6764
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0.50 0.0165 0.0484 0.0779 0.0265 0.018 0.564 0.651 13.337 0.064 2.895 22.132 0.13 58308. 0.6548
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1.00 0.0329 0.0946 0.0761 0.0265 0.018 0.563 0.636 13.324 0.064 2.828 21.644 0.13 58338. 0.6329
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1.50 0.0494 0.1387 0.0743 0.0264 0.018 0.562 0.620 13.300 0.064 2.759 21.154 0.13 58368. 0.6110
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1.99 0.0658 0.1807 0.0723 0.0264 0.018 0.561 0.604 13.267 0.063 2.688 20.659 0.13 58401. 0.5889
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2.49 0.0823 0.2204 0.0703 0.0262 0.018 0.558 0.587 13.214 0.063 2.612 20.160 0.13 58434. 0.5666
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2.99 0.0987 0.2579 0.0682 0.0261 0.018 0.556 0.570 13.148 0.063 2.535 19.658 0.13 58469. 0.5442
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3.49 0.1152 0.2931 0.0660 0.0260 0.018 0.552 0.552 13.066 0.062 2.454 19.150 0.13 58506. 0.5216
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3.99 0.1317 0.3259 0.0638 0.0258 0.017 0.548 0.533 12.964 0.062 2.369 18.636 0.13 58545. 0.4988
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4.49 0.1481 0.3564 0.0614 0.0255 0.017 0.543 0.513 12.847 0.061 2.282 18.113 0.13 58585. 0.4758
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4.99 0.1646 0.3844 0.0590 0.0252 0.017 0.537 0.493 12.709 0.061 2.191 17.583 0.13 58626. 0.4526
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5.49 0.1810 0.4098 0.0564 0.0249 0.017 0.530 0.472 12.551 0.060 2.097 17.040 0.13 58670. 0.4291
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5.98 0.1975 0.4324 0.0538 0.0246 0.017 0.523 0.450 12.371 0.059 2.000 16.483 0.13 58715. 0.4053
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6.48 0.2139 0.4522 0.0511 0.0242 0.016 0.514 0.427 12.171 0.058 1.899 15.911 0.13 58762. 0.3813
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6.98 0.2304 0.4690 0.0483 0.0237 0.016 0.505 0.404 11.952 0.057 1.796 15.322 0.13 58811. 0.3570
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7.48 0.2468 0.4825 0.0455 0.0233 0.016 0.495 0.380 11.712 0.056 1.690 14.713 0.13 58861. 0.3326
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7.98 0.2633 0.4925 0.0425 0.0227 0.015 0.484 0.355 11.451 0.055 1.581 14.080 0.13 58913. 0.3079
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8.48 0.2798 0.4988 0.0396 0.0222 0.015 0.472 0.330 11.169 0.053 1.470 13.420 0.13 58968. 0.2829
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8.98 0.2962 0.5009 0.0365 0.0216 0.015 0.459 0.305 10.866 0.052 1.356 12.728 0.13 59024. 0.2577
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9.47 0.3127 0.4984 0.0334 0.0209 0.014 0.445 0.279 10.541 0.050 1.240 11.998 0.13 59082. 0.2324
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9.97 0.3291 0.4908 0.0302 0.0203 0.014 0.431 0.252 10.195 0.049 1.122 11.225 0.13 59142. 0.2068
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10.47 0.3456 0.4774 0.0270 0.0195 0.013 0.415 0.225 9.826 0.047 1.002 10.399 0.13 59204. 0.1810
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10.97 0.3620 0.4575 0.0237 0.0187 0.013 0.399 0.198 9.436 0.045 0.880 9.512 0.13 59268. 0.1552
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11.47 0.3785 0.4300 0.0204 0.0179 0.012 0.381 0.170 9.023 0.043 0.757 8.552 0.13 59334. 0.1294
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11.97 0.3950 0.3937 0.0170 0.0171 0.012 0.363 0.142 8.588 0.041 0.632 7.503 0.13 59402. 0.1037
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12.47 0.4114 0.3469 0.0136 0.0162 0.011 0.344 0.114 8.132 0.039 0.506 6.347 0.13 59472. 0.0785
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12.97 0.4279 0.2876 0.0102 0.0152 0.010 0.324 0.085 7.656 0.037 0.380 5.061 0.13 59544. 0.0542
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13.46 0.4443 0.2133 0.0068 0.0142 0.010 0.303 0.057 7.160 0.034 0.254 3.614 0.13 59619. 0.0317
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13.96 0.4608 0.1205 0.0035 0.0132 0.009 0.281 0.029 6.647 0.032 0.128 1.969 0.13 59694. 0.0123
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14.46 0.4772 0.0029 0.0001 0.0121 0.008 0.258 0.001 6.114 0.029 0.003 0.046 0.13 59768. 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 0.0799 0.0255 0.058 1.221 1.501 43.330 0.138 6.678 15.715 0.19 87420. 0.7061
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0.76 0.0168 0.0514 0.0781 0.0255 0.058 1.221 1.468 43.336 0.138 6.532 15.369 0.19 87462. 0.6830
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1.52 0.0335 0.1004 0.0763 0.0255 0.058 1.220 1.434 43.292 0.138 6.378 15.024 0.19 87507. 0.6598
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2.29 0.0503 0.1472 0.0744 0.0254 0.058 1.217 1.398 43.212 0.138 6.220 14.677 0.19 87554. 0.6365
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3.05 0.0671 0.1916 0.0724 0.0254 0.058 1.214 1.361 43.092 0.137 6.055 14.329 0.19 87604. 0.6131
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3.81 0.0839 0.2336 0.0703 0.0253 0.058 1.209 1.322 42.902 0.137 5.881 13.979 0.19 87655. 0.5895
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4.57 0.1006 0.2733 0.0682 0.0251 0.057 1.202 1.282 42.666 0.136 5.702 13.629 0.19 87709. 0.5659
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5.34 0.1174 0.3106 0.0660 0.0249 0.057 1.194 1.240 42.365 0.135 5.515 13.274 0.19 87766. 0.5421
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6.10 0.1342 0.3454 0.0636 0.0247 0.056 1.183 1.196 41.999 0.134 5.320 12.918 0.19 87825. 0.5181
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6.86 0.1510 0.3777 0.0612 0.0245 0.056 1.171 1.151 41.567 0.132 5.118 12.556 0.19 87887. 0.4940
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7.62 0.1677 0.4075 0.0587 0.0242 0.055 1.157 1.104 41.064 0.131 4.909 12.191 0.19 87951. 0.4697
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8.39 0.1845 0.4345 0.0561 0.0238 0.054 1.140 1.055 40.480 0.129 4.691 11.817 0.19 88018. 0.4450
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9.15 0.2013 0.4586 0.0534 0.0234 0.053 1.122 1.004 39.819 0.127 4.465 11.435 0.19 88088. 0.4202
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9.91 0.2180 0.4799 0.0506 0.0230 0.052 1.101 0.952 39.083 0.124 4.233 11.044 0.19 88160. 0.3951
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10.67 0.2348 0.4980 0.0478 0.0225 0.051 1.078 0.898 38.272 0.122 3.994 10.642 0.19 88236. 0.3698
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11.44 0.2516 0.5127 0.0448 0.0220 0.050 1.053 0.843 37.383 0.119 3.749 10.226 0.19 88314. 0.3443
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12.20 0.2684 0.5238 0.0418 0.0214 0.049 1.026 0.786 36.417 0.116 3.498 9.794 0.19 88395. 0.3185
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12.96 0.2851 0.5309 0.0388 0.0208 0.047 0.997 0.729 35.370 0.113 3.241 9.343 0.19 88478. 0.2925
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13.72 0.3019 0.5336 0.0356 0.0202 0.046 0.965 0.670 34.243 0.109 2.978 8.869 0.19 88565. 0.2661
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14.49 0.3187 0.5314 0.0324 0.0194 0.044 0.931 0.609 33.033 0.105 2.711 8.368 0.19 88655. 0.2395
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15.25 0.3355 0.5236 0.0292 0.0187 0.043 0.894 0.548 31.740 0.101 2.438 7.833 0.19 88748. 0.2127
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16.01 0.3522 0.5094 0.0258 0.0179 0.041 0.855 0.486 30.363 0.097 2.161 7.258 0.19 88844. 0.1855
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16.77 0.3690 0.4877 0.0225 0.0170 0.039 0.814 0.423 28.902 0.092 1.880 6.633 0.19 88943. 0.1581
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17.54 0.3858 0.4572 0.0191 0.0161 0.037 0.771 0.359 27.358 0.087 1.596 5.948 0.19 89046. 0.1306
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18.30 0.4025 0.4161 0.0157 0.0151 0.035 0.725 0.294 25.732 0.082 1.309 5.187 0.19 89151. 0.1032
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19.06 0.4193 0.3618 0.0122 0.0141 0.032 0.677 0.229 24.027 0.076 1.020 4.330 0.19 89260. 0.0761
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19.82 0.4361 0.2913 0.0087 0.0131 0.030 0.627 0.164 22.247 0.071 0.731 3.352 0.19 89372. 0.0498
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20.58 0.4529 0.2000 0.0053 0.0120 0.027 0.575 0.100 20.398 0.065 0.443 2.216 0.19 89486. 0.0257
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21.35 0.4696 0.0812 0.0019 0.0109 0.025 0.521 0.035 18.485 0.059 0.157 0.868 0.19 89602. 0.0060
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22.11 0.4864
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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 0.0802 0.0250 0.135 2.125 2.680 100.558 0.240 11.919 12.087 0.25 116557. 0.7256
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1.00 0.0166 0.0520 0.0785 0.0250 0.135 2.125 2.622 100.580 0.240 11.663 11.824 0.25 116613. 0.7021
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2.01 0.0331 0.1018 0.0766 0.0250 0.135 2.123 2.561 100.480 0.240 11.393 11.562 0.25 116673. 0.6786
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3.01 0.0497 0.1492 0.0748 0.0249 0.134 2.119 2.499 100.289 0.239 11.113 11.300 0.25 116735. 0.6550
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4.02 0.0663 0.1943 0.0728 0.0248 0.134 2.113 2.434 100.010 0.239 10.824 11.037 0.25 116800. 0.6314
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5.02 0.0828 0.2371 0.0708 0.0247 0.134 2.104 2.365 99.564 0.238 10.519 10.773 0.25 116868. 0.6076
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6.02 0.0994 0.2775 0.0686 0.0246 0.133 2.092 2.294 99.001 0.236 10.204 10.510 0.25 116939. 0.5838
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7.03 0.1160 0.3156 0.0664 0.0244 0.132 2.077 2.220 98.296 0.235 9.875 10.245 0.25 117013. 0.5598
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8.03 0.1325 0.3513 0.0641 0.0242 0.131 2.059 2.143 97.424 0.233 9.533 9.978 0.25 117091. 0.5357
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9.04 0.1491 0.3846 0.0618 0.0239 0.129 2.037 2.064 96.407 0.230 9.179 9.709 0.25 117172. 0.5115
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10.04 0.1657 0.4154 0.0593 0.0236 0.128 2.012 1.981 95.211 0.227 8.812 9.438 0.25 117256. 0.4872
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11.04 0.1822 0.4436 0.0567 0.0233 0.126 1.983 1.895 93.829 0.224 8.430 9.162 0.25 117344. 0.4625
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12.05 0.1988 0.4690 0.0541 0.0229 0.124 1.949 1.806 92.259 0.220 8.034 8.880 0.25 117436. 0.4377
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13.05 0.2153 0.4917 0.0513 0.0225 0.121 1.913 1.715 90.509 0.216 7.627 8.593 0.25 117531. 0.4126
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14.06 0.2319 0.5113 0.0485 0.0220 0.119 1.872 1.621 88.576 0.211 7.208 8.298 0.25 117629. 0.3874
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15.06 0.2485 0.5278 0.0456 0.0215 0.116 1.827 1.524 86.458 0.206 6.778 7.995 0.25 117731. 0.3619
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16.06 0.2650 0.5409 0.0426 0.0209 0.113 1.778 1.425 84.151 0.201 6.338 7.680 0.25 117837. 0.3362
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17.07 0.2816 0.5502 0.0396 0.0203 0.109 1.725 1.324 81.652 0.195 5.888 7.353 0.25 117947. 0.3102
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18.07 0.2982 0.5554 0.0365 0.0196 0.106 1.668 1.220 78.957 0.188 5.428 7.010 0.26 118061. 0.2840
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19.08 0.3147 0.5559 0.0334 0.0189 0.102 1.607 1.115 76.064 0.182 4.959 6.648 0.26 118178. 0.2574
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20.08 0.3313 0.5512 0.0301 0.0181 0.098 1.542 1.007 72.969 0.174 4.481 6.262 0.26 118299. 0.2305
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21.08 0.3479 0.5405 0.0269 0.0173 0.093 1.472 0.898 69.673 0.166 3.996 5.848 0.26 118425. 0.2033
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22.09 0.3644 0.5227 0.0236 0.0164 0.089 1.398 0.788 66.172 0.158 3.503 5.398 0.26 118554. 0.1757
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23.09 0.3810 0.4965 0.0202 0.0155 0.084 1.320 0.676 62.470 0.149 3.005 4.905 0.26 118688. 0.1478
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24.10 0.3976 0.4600 0.0168 0.0145 0.079 1.238 0.562 58.569 0.140 2.501 4.355 0.26 118826. 0.1198
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25.10 0.4141 0.4109 0.0134 0.0135 0.073 1.151 0.448 54.473 0.130 1.995 3.734 0.26 118968. 0.0917
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26.10 0.4307 0.3456 0.0100 0.0125 0.067 1.061 0.334 50.192 0.120 1.487 3.020 0.26 119114. 0.0640
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27.11 0.4473 0.2595 0.0066 0.0114 0.061 0.967 0.220 45.739 0.109 0.980 2.184 0.26 119264. 0.0376
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28.11 0.4638 0.1455 0.0032 0.0102 0.055 0.869 0.107 41.135 0.098 0.476 1.181 0.26 119417. 0.0142
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29.11 0.4804 -0.0122 -0.0002 0.0090 0.049 0.767 -0.008 36.278 0.087 -0.034 -0.096 0.26 119555. 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 0.0806 0.0247 0.260 3.281 4.208 194.071 0.371 18.718 9.835 0.32 145692. 0.7399
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1.25 0.0166 0.0529 0.0789 0.0247 0.260 3.281 4.118 194.114 0.371 18.316 9.622 0.32 145763. 0.7160
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2.51 0.0331 0.1035 0.0770 0.0247 0.260 3.278 4.023 193.911 0.370 17.892 9.409 0.32 145837. 0.6920
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3.76 0.0497 0.1517 0.0752 0.0246 0.260 3.271 3.924 193.520 0.370 17.454 9.197 0.32 145915. 0.6681
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5.02 0.0662 0.1976 0.0732 0.0245 0.259 3.262 3.822 192.959 0.369 17.000 8.984 0.32 145996. 0.6441
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6.27 0.0828 0.2412 0.0711 0.0244 0.258 3.247 3.714 192.064 0.367 16.522 8.772 0.32 146081. 0.6200
|
|
7.53 0.0993 0.2824 0.0690 0.0243 0.256 3.228 3.603 190.929 0.365 16.027 8.560 0.32 146171. 0.5959
|
|
8.78 0.1159 0.3213 0.0668 0.0241 0.254 3.204 3.487 189.518 0.362 15.512 8.346 0.32 146264. 0.5716
|
|
10.03 0.1325 0.3578 0.0645 0.0239 0.252 3.174 3.367 187.767 0.359 14.975 8.133 0.32 146361. 0.5472
|
|
11.29 0.1490 0.3918 0.0621 0.0236 0.249 3.140 3.242 185.728 0.355 14.420 7.917 0.32 146462. 0.5228
|
|
12.54 0.1656 0.4234 0.0596 0.0233 0.246 3.099 3.112 183.329 0.350 13.844 7.700 0.32 146568. 0.4982
|
|
13.80 0.1821 0.4524 0.0570 0.0230 0.242 3.052 2.978 180.559 0.345 13.245 7.480 0.32 146678. 0.4733
|
|
15.05 0.1987 0.4788 0.0544 0.0226 0.238 2.999 2.838 177.413 0.339 12.624 7.256 0.32 146792. 0.4483
|
|
16.31 0.2152 0.5024 0.0516 0.0221 0.233 2.940 2.694 173.903 0.332 11.985 7.028 0.32 146911. 0.4230
|
|
17.56 0.2318 0.5230 0.0488 0.0216 0.228 2.874 2.547 170.026 0.325 11.328 6.794 0.32 147034. 0.3976
|
|
18.81 0.2484 0.5406 0.0459 0.0211 0.222 2.802 2.395 165.776 0.317 10.654 6.554 0.32 147162. 0.3720
|
|
20.07 0.2649 0.5547 0.0429 0.0205 0.216 2.724 2.240 161.146 0.308 9.964 6.305 0.32 147294. 0.3461
|
|
21.32 0.2815 0.5652 0.0399 0.0199 0.209 2.639 2.081 156.128 0.298 9.258 6.047 0.32 147432. 0.3199
|
|
22.58 0.2980 0.5717 0.0368 0.0192 0.202 2.548 1.919 150.715 0.288 8.537 5.776 0.32 147574. 0.2934
|
|
23.83 0.3146 0.5736 0.0336 0.0184 0.194 2.450 1.754 144.902 0.277 7.801 5.490 0.32 147720. 0.2666
|
|
25.09 0.3311 0.5703 0.0304 0.0176 0.186 2.344 1.586 138.685 0.265 7.053 5.186 0.32 147872. 0.2395
|
|
26.34 0.3477 0.5610 0.0271 0.0168 0.177 2.232 1.415 132.058 0.252 6.292 4.858 0.32 148029. 0.2119
|
|
27.59 0.3642 0.5447 0.0238 0.0159 0.168 2.113 1.241 125.023 0.239 5.520 4.502 0.32 148191. 0.1839
|
|
28.85 0.3808 0.5198 0.0204 0.0149 0.158 1.988 1.065 117.580 0.225 4.739 4.110 0.32 148358. 0.1556
|
|
30.10 0.3974 0.4844 0.0170 0.0140 0.147 1.855 0.888 109.735 0.210 3.950 3.671 0.32 148530. 0.1269
|
|
31.36 0.4139 0.4359 0.0136 0.0129 0.136 1.716 0.710 101.499 0.194 3.156 3.171 0.32 148707. 0.0980
|
|
32.61 0.4305 0.3705 0.0102 0.0118 0.125 1.570 0.531 92.890 0.177 2.360 2.591 0.32 148890. 0.0692
|
|
33.87 0.4470 0.2824 0.0067 0.0107 0.113 1.419 0.352 83.936 0.160 1.566 1.902 0.32 149077. 0.0414
|
|
35.12 0.4636 0.1634 0.0033 0.0095 0.100 1.262 0.175 74.677 0.143 0.777 1.061 0.32 149268. 0.0163
|
|
36.37 0.4801 -0.0053 -0.0001 0.0083 0.087 1.097 -0.005 64.919 0.124 -0.021 -0.033 0.32 149442. 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 0.0811 0.0245 0.447 4.697 6.097 333.415 0.531 27.121 8.295 0.38 174825. 0.7511
|
|
1.53 0.0168 0.0543 0.0793 0.0245 0.447 4.698 5.964 333.476 0.531 26.530 8.112 0.38 174911. 0.7266
|
|
3.05 0.0336 0.1062 0.0775 0.0245 0.447 4.692 5.824 333.083 0.530 25.907 7.931 0.38 175002. 0.7020
|
|
4.58 0.0504 0.1556 0.0755 0.0245 0.446 4.682 5.679 332.342 0.529 25.261 7.751 0.38 175097. 0.6774
|
|
6.11 0.0672 0.2027 0.0735 0.0244 0.444 4.667 5.529 331.287 0.527 24.594 7.570 0.38 175196. 0.6528
|
|
7.63 0.0840 0.2473 0.0714 0.0243 0.442 4.644 5.371 329.629 0.525 23.888 7.390 0.38 175301. 0.6281
|
|
9.16 0.1008 0.2896 0.0693 0.0241 0.439 4.614 5.207 327.539 0.521 23.159 7.210 0.38 175410. 0.6034
|
|
10.69 0.1176 0.3294 0.0670 0.0239 0.436 4.577 5.036 324.924 0.517 22.399 7.030 0.38 175524. 0.5785
|
|
12.22 0.1344 0.3668 0.0646 0.0237 0.431 4.532 4.858 321.712 0.512 21.608 6.849 0.38 175643. 0.5536
|
|
13.74 0.1512 0.4017 0.0622 0.0234 0.426 4.479 4.674 317.949 0.506 20.788 6.667 0.38 175768. 0.5286
|
|
15.27 0.1680 0.4340 0.0596 0.0231 0.420 4.417 4.482 313.548 0.499 19.938 6.484 0.38 175897. 0.5034
|
|
16.80 0.1848 0.4638 0.0570 0.0227 0.414 4.345 4.283 308.450 0.491 19.052 6.298 0.38 176032. 0.4780
|
|
18.32 0.2015 0.4908 0.0542 0.0223 0.406 4.264 4.077 302.677 0.482 18.135 6.110 0.38 176173. 0.4524
|
|
19.85 0.2183 0.5149 0.0514 0.0218 0.397 4.173 3.865 296.241 0.471 17.191 5.917 0.38 176318. 0.4266
|
|
21.38 0.2351 0.5361 0.0485 0.0213 0.388 4.073 3.647 289.135 0.460 16.221 5.721 0.38 176470. 0.4006
|
|
22.90 0.2519 0.5541 0.0455 0.0207 0.377 3.963 3.423 281.344 0.448 15.226 5.518 0.38 176627. 0.3744
|
|
24.43 0.2687 0.5686 0.0425 0.0201 0.366 3.844 3.194 272.857 0.434 14.206 5.309 0.38 176790. 0.3480
|
|
25.96 0.2855 0.5793 0.0394 0.0194 0.354 3.714 2.959 263.660 0.420 13.164 5.091 0.38 176958. 0.3212
|
|
27.48 0.3023 0.5859 0.0362 0.0187 0.340 3.574 2.720 253.740 0.404 12.099 4.862 0.38 177133. 0.2941
|
|
29.01 0.3191 0.5876 0.0329 0.0179 0.326 3.424 2.476 243.088 0.387 11.014 4.620 0.38 177313. 0.2666
|
|
30.54 0.3359 0.5838 0.0296 0.0170 0.311 3.264 2.228 231.694 0.369 9.909 4.361 0.38 177500. 0.2387
|
|
32.06 0.3527 0.5736 0.0263 0.0162 0.294 3.093 1.975 219.554 0.349 8.786 4.081 0.38 177693. 0.2103
|
|
33.59 0.3695 0.5557 0.0229 0.0152 0.277 2.911 1.719 206.668 0.329 7.648 3.774 0.38 177892. 0.1815
|
|
35.12 0.3863 0.5284 0.0194 0.0142 0.259 2.719 1.461 193.042 0.307 6.497 3.432 0.38 178097. 0.1521
|
|
36.65 0.4031 0.4892 0.0160 0.0131 0.240 2.517 1.200 178.689 0.284 5.336 3.045 0.38 178309. 0.1223
|
|
38.17 0.4199 0.4348 0.0125 0.0120 0.219 2.305 0.937 163.633 0.260 4.169 2.598 0.38 178527. 0.0922
|
|
39.70 0.4367 0.3600 0.0090 0.0109 0.198 2.084 0.675 147.913 0.235 3.000 2.068 0.38 178751. 0.0623
|
|
41.23 0.4535 0.2572 0.0055 0.0097 0.176 1.854 0.413 131.593 0.209 1.837 1.423 0.38 178981. 0.0335
|
|
42.75 0.4703 0.1135 0.0020 0.0084 0.154 1.616 0.153 114.709 0.183 0.681 0.606 0.39 179213. 0.0087
|
|
44.28 0.4871
|
|
|
|
|
|
|
|
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 0.0817 0.0245 0.709 6.386 8.361 528.879 0.721 37.188 7.170 0.44 203953. 0.7603
|
|
1.78 0.0168 0.0547 0.0799 0.0245 0.709 6.387 8.179 528.945 0.722 36.380 7.013 0.44 204054. 0.7356
|
|
3.56 0.0336 0.1071 0.0780 0.0245 0.708 6.379 7.987 528.256 0.721 35.526 6.858 0.44 204161. 0.7108
|
|
5.34 0.0504 0.1570 0.0761 0.0244 0.707 6.363 7.788 526.984 0.719 34.641 6.703 0.44 204272. 0.6860
|
|
7.12 0.0672 0.2045 0.0741 0.0243 0.704 6.342 7.582 525.217 0.716 33.726 6.548 0.44 204389. 0.6612
|
|
8.90 0.0839 0.2496 0.0720 0.0242 0.701 6.309 7.365 522.478 0.713 32.760 6.394 0.44 204511. 0.6363
|
|
10.68 0.1007 0.2923 0.0698 0.0240 0.696 6.267 7.140 519.015 0.708 31.760 6.240 0.44 204639. 0.6115
|
|
12.46 0.1175 0.3325 0.0675 0.0238 0.690 6.215 6.906 514.732 0.702 30.719 6.086 0.44 204772. 0.5865
|
|
14.25 0.1343 0.3704 0.0651 0.0236 0.683 6.152 6.662 509.458 0.695 29.634 5.931 0.44 204912. 0.5615
|
|
16.03 0.1511 0.4058 0.0626 0.0233 0.675 6.077 6.410 503.308 0.687 28.511 5.776 0.44 205057. 0.5363
|
|
17.81 0.1679 0.4388 0.0601 0.0230 0.665 5.990 6.148 496.114 0.677 27.345 5.621 0.44 205209. 0.5111
|
|
19.59 0.1847 0.4691 0.0574 0.0226 0.654 5.890 5.875 487.799 0.665 26.131 5.463 0.45 205367. 0.4856
|
|
21.37 0.2015 0.4967 0.0546 0.0222 0.642 5.776 5.592 478.387 0.653 24.875 5.302 0.45 205531. 0.4598
|
|
23.15 0.2183 0.5215 0.0518 0.0217 0.627 5.650 5.302 467.898 0.638 23.582 5.139 0.45 205701. 0.4340
|
|
24.93 0.2350 0.5435 0.0489 0.0211 0.612 5.510 5.003 456.322 0.623 22.252 4.973 0.45 205878. 0.4079
|
|
26.71 0.2518 0.5622 0.0459 0.0206 0.595 5.357 4.696 443.636 0.605 20.888 4.801 0.45 206061. 0.3816
|
|
28.49 0.2686 0.5776 0.0428 0.0199 0.576 5.190 4.382 429.820 0.586 19.492 4.624 0.45 206251. 0.3550
|
|
30.27 0.2854 0.5892 0.0397 0.0192 0.556 5.009 4.061 414.853 0.566 18.063 4.440 0.45 206448. 0.3281
|
|
32.05 0.3022 0.5967 0.0365 0.0185 0.535 4.814 3.733 398.714 0.544 16.604 4.247 0.45 206652. 0.3009
|
|
33.83 0.3190 0.5995 0.0332 0.0177 0.511 4.605 3.399 381.386 0.520 15.117 4.042 0.45 206863. 0.2733
|
|
35.61 0.3358 0.5969 0.0299 0.0168 0.487 4.381 3.058 362.857 0.495 13.603 3.823 0.45 207080. 0.2452
|
|
37.39 0.3526 0.5878 0.0265 0.0159 0.460 4.143 2.713 343.119 0.468 12.066 3.586 0.45 207305. 0.2166
|
|
39.17 0.3694 0.5711 0.0231 0.0149 0.432 3.890 2.362 322.171 0.440 10.507 3.326 0.45 207538. 0.1874
|
|
40.96 0.3862 0.5449 0.0196 0.0139 0.402 3.623 2.008 300.023 0.409 8.930 3.035 0.45 207777. 0.1577
|
|
42.74 0.4029 0.5067 0.0161 0.0128 0.371 3.341 1.650 276.697 0.377 7.339 2.705 0.45 208024. 0.1274
|
|
44.52 0.4197 0.4529 0.0126 0.0117 0.338 3.046 1.291 252.233 0.344 5.740 2.321 0.45 208279. 0.0967
|
|
46.30 0.4365 0.3779 0.0091 0.0105 0.304 2.737 0.931 226.695 0.309 4.139 1.862 0.45 208540. 0.0659
|
|
48.08 0.4533 0.2733 0.0056 0.0093 0.268 2.417 0.572 200.185 0.273 2.545 1.296 0.45 208809. 0.0360
|
|
49.86 0.4701 0.1242 0.0021 0.0080 0.232 2.086 0.216 172.765 0.236 0.963 0.568 0.45 209079. 0.0097
|
|
51.64 0.4869
|
|
|
|
|
|
|
|
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 0.0824 0.0246 1.062 8.366 11.016 791.810 0.945 49.001 6.310 0.51 233078. 0.7681
|
|
2.02 0.0166 0.0546 0.0806 0.0246 1.062 8.366 10.780 791.845 0.945 47.947 6.175 0.51 233192. 0.7434
|
|
4.03 0.0333 0.1068 0.0788 0.0245 1.060 8.354 10.529 790.716 0.944 46.834 6.040 0.51 233313. 0.7187
|
|
6.05 0.0499 0.1567 0.0768 0.0245 1.058 8.333 10.269 788.672 0.941 45.677 5.906 0.51 233440. 0.6940
|
|
8.07 0.0666 0.2041 0.0748 0.0244 1.054 8.303 10.001 785.917 0.938 44.485 5.772 0.51 233573. 0.6694
|
|
10.08 0.0832 0.2493 0.0727 0.0243 1.048 8.259 9.718 781.728 0.933 43.226 5.639 0.51 233712. 0.6446
|
|
12.10 0.0998 0.2921 0.0705 0.0241 1.041 8.203 9.425 776.391 0.927 41.920 5.506 0.51 233857. 0.6199
|
|
14.12 0.1165 0.3326 0.0682 0.0239 1.032 8.134 9.120 769.916 0.919 40.567 5.373 0.51 234008. 0.5950
|
|
16.14 0.1331 0.3707 0.0659 0.0236 1.022 8.050 8.802 761.896 0.909 39.151 5.240 0.51 234166. 0.5701
|
|
18.15 0.1498 0.4064 0.0634 0.0234 1.009 7.952 8.473 752.618 0.898 37.690 5.107 0.51 234331. 0.5451
|
|
20.17 0.1664 0.4397 0.0608 0.0230 0.995 7.837 8.132 741.735 0.885 36.171 4.973 0.51 234503. 0.5200
|
|
22.19 0.1830 0.4705 0.0582 0.0226 0.978 7.705 7.777 729.234 0.870 34.592 4.837 0.51 234681. 0.4947
|
|
24.20 0.1997 0.4987 0.0554 0.0222 0.959 7.555 7.409 715.063 0.854 32.957 4.700 0.51 234867. 0.4692
|
|
26.22 0.2163 0.5242 0.0526 0.0217 0.938 7.388 7.031 699.281 0.835 31.273 4.560 0.51 235060. 0.4434
|
|
28.24 0.2330 0.5469 0.0497 0.0212 0.914 7.204 6.642 681.873 0.814 29.542 4.418 0.51 235260. 0.4175
|
|
30.25 0.2496 0.5666 0.0467 0.0206 0.889 7.003 6.243 662.809 0.791 27.767 4.272 0.51 235467. 0.3914
|
|
32.27 0.2662 0.5830 0.0436 0.0199 0.861 6.784 5.834 642.059 0.766 25.948 4.121 0.51 235681. 0.3650
|
|
34.29 0.2829 0.5959 0.0405 0.0192 0.831 6.546 5.416 619.591 0.740 24.089 3.964 0.51 235904. 0.3383
|
|
36.30 0.2995 0.6049 0.0373 0.0185 0.798 6.290 4.989 595.374 0.711 22.190 3.800 0.51 236134. 0.3113
|
|
38.32 0.3162 0.6094 0.0341 0.0177 0.764 6.016 4.553 569.384 0.680 20.253 3.627 0.51 236371. 0.2838
|
|
40.34 0.3328 0.6087 0.0308 0.0168 0.726 5.722 4.110 541.600 0.646 18.283 3.442 0.51 236617. 0.2559
|
|
42.36 0.3494 0.6021 0.0274 0.0159 0.687 5.410 3.660 512.010 0.611 16.280 3.242 0.51 236871. 0.2275
|
|
44.37 0.3661 0.5881 0.0240 0.0149 0.645 5.078 3.204 480.612 0.574 14.249 3.023 0.51 237132. 0.1984
|
|
46.39 0.3827 0.5652 0.0205 0.0139 0.600 4.727 2.742 447.417 0.534 12.195 2.779 0.51 237402. 0.1688
|
|
48.41 0.3994 0.5310 0.0170 0.0128 0.553 4.358 2.275 412.456 0.492 10.121 2.502 0.51 237681. 0.1384
|
|
50.42 0.4160 0.4820 0.0135 0.0117 0.504 3.970 1.806 375.780 0.449 8.035 2.180 0.51 237967. 0.1075
|
|
52.44 0.4326 0.4129 0.0100 0.0105 0.453 3.566 1.336 337.475 0.403 5.944 1.796 0.51 238262. 0.0761
|
|
54.46 0.4493 0.3156 0.0065 0.0092 0.399 3.145 0.868 297.680 0.355 3.859 1.322 0.51 238564. 0.0452
|
|
56.47 0.4659 0.1763 0.0030 0.0080 0.344 2.711 0.403 256.560 0.306 1.791 0.712 0.51 238871. 0.0166
|
|
58.49 0.4826
|
|
|
|
|
|
|
|
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 0.0833 0.0247 1.522 10.660 14.087 1135.039 1.204 62.661 5.629 0.57 262196. 0.7749
|
|
2.26 0.0166 0.0546 0.0815 0.0247 1.522 10.659 13.787 1134.960 1.204 61.323 5.510 0.57 262325. 0.7502
|
|
4.52 0.0331 0.1068 0.0796 0.0247 1.520 10.642 13.468 1133.152 1.202 59.905 5.391 0.57 262462. 0.7255
|
|
6.78 0.0497 0.1567 0.0777 0.0246 1.515 10.612 13.137 1129.967 1.199 58.431 5.273 0.57 262605. 0.7009
|
|
9.04 0.0663 0.2043 0.0756 0.0245 1.510 10.572 12.795 1125.758 1.194 56.914 5.155 0.57 262754. 0.6763
|
|
11.30 0.0829 0.2496 0.0735 0.0244 1.501 10.514 12.435 1119.535 1.188 55.312 5.038 0.57 262910. 0.6515
|
|
13.56 0.0994 0.2926 0.0713 0.0242 1.491 10.439 12.061 1111.577 1.179 53.649 4.922 0.57 263074. 0.6268
|
|
15.82 0.1160 0.3333 0.0690 0.0240 1.478 10.350 11.674 1102.047 1.169 51.928 4.805 0.57 263244. 0.6021
|
|
18.08 0.1326 0.3716 0.0666 0.0238 1.462 10.239 11.269 1090.250 1.157 50.126 4.688 0.57 263422. 0.5772
|
|
20.34 0.1492 0.4077 0.0641 0.0235 1.444 10.111 10.851 1076.662 1.142 48.267 4.571 0.57 263607. 0.5523
|
|
22.60 0.1657 0.4413 0.0616 0.0231 1.422 9.962 10.416 1060.720 1.125 46.333 4.454 0.57 263800. 0.5272
|
|
24.86 0.1823 0.4726 0.0589 0.0227 1.398 9.791 9.965 1042.516 1.106 44.326 4.336 0.57 264001. 0.5019
|
|
27.12 0.1989 0.5012 0.0561 0.0223 1.370 9.597 9.498 1021.871 1.084 42.246 4.216 0.57 264209. 0.4765
|
|
29.38 0.2155 0.5273 0.0533 0.0218 1.340 9.381 9.016 998.901 1.060 40.103 4.094 0.57 264425. 0.4508
|
|
31.64 0.2320 0.5507 0.0504 0.0212 1.306 9.143 8.521 973.588 1.033 37.901 3.970 0.57 264649. 0.4250
|
|
33.90 0.2486 0.5711 0.0474 0.0206 1.268 8.883 8.013 945.892 1.004 35.642 3.842 0.57 264882. 0.3989
|
|
36.16 0.2652 0.5883 0.0443 0.0200 1.228 8.600 7.493 915.770 0.972 33.328 3.711 0.57 265122. 0.3725
|
|
38.42 0.2818 0.6022 0.0411 0.0193 1.184 8.294 6.961 883.176 0.937 30.962 3.575 0.57 265371. 0.3459
|
|
40.68 0.2983 0.6122 0.0379 0.0185 1.137 7.965 6.418 848.068 0.900 28.546 3.432 0.57 265629. 0.3189
|
|
42.94 0.3149 0.6178 0.0347 0.0177 1.087 7.611 5.864 810.411 0.860 26.083 3.282 0.57 265895. 0.2914
|
|
45.20 0.3315 0.6185 0.0313 0.0168 1.033 7.233 5.300 770.175 0.817 23.575 3.121 0.57 266170. 0.2635
|
|
47.46 0.3481 0.6134 0.0279 0.0159 0.975 6.831 4.727 727.343 0.772 21.027 2.948 0.57 266454. 0.2350
|
|
49.72 0.3646 0.6012 0.0245 0.0149 0.914 6.404 4.146 681.911 0.724 18.442 2.758 0.58 266747. 0.2059
|
|
51.98 0.3812 0.5802 0.0210 0.0138 0.850 5.953 3.558 633.894 0.673 15.827 2.546 0.58 267049. 0.1761
|
|
54.24 0.3978 0.5482 0.0175 0.0127 0.782 5.478 2.965 583.333 0.619 13.187 2.305 0.58 267360. 0.1456
|
|
56.50 0.4144 0.5016 0.0140 0.0116 0.711 4.980 2.367 530.301 0.563 10.530 2.025 0.58 267681. 0.1143
|
|
58.76 0.4309 0.4351 0.0105 0.0104 0.637 4.460 1.769 474.917 0.504 7.867 1.689 0.58 268010. 0.0824
|
|
61.02 0.4475 0.3405 0.0069 0.0091 0.560 3.920 1.171 417.372 0.443 5.209 1.273 0.58 268348. 0.0505
|
|
63.28 0.4641 0.2033 0.0034 0.0078 0.480 3.361 0.578 357.920 0.380 2.572 0.733 0.58 268692. 0.0204
|
|
65.54 0.4807 -0.0127 -0.0002 0.0064 0.395 2.767 -0.029 294.655 0.313 -0.128 -0.044 0.58 268983. 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 0.0843 0.0250 2.110 13.300 17.604 1573.519 1.503 78.304 5.074 0.63 291307. 0.7808
|
|
2.55 0.0169 0.0556 0.0825 0.0250 2.110 13.297 17.223 1573.138 1.502 76.607 4.966 0.63 291455. 0.7557
|
|
5.11 0.0337 0.1088 0.0805 0.0250 2.106 13.272 16.818 1570.192 1.499 74.805 4.858 0.63 291610. 0.7306
|
|
7.66 0.0506 0.1596 0.0785 0.0249 2.099 13.229 16.395 1565.176 1.495 72.926 4.751 0.63 291773. 0.7055
|
|
10.22 0.0674 0.2081 0.0764 0.0248 2.090 13.174 15.960 1558.629 1.488 70.992 4.645 0.63 291943. 0.6805
|
|
12.77 0.0843 0.2541 0.0742 0.0246 2.078 13.094 15.501 1549.192 1.479 68.950 4.538 0.63 292122. 0.6553
|
|
15.33 0.1012 0.2979 0.0719 0.0244 2.061 12.993 15.024 1537.212 1.468 66.828 4.433 0.63 292308. 0.6301
|
|
17.88 0.1180 0.3392 0.0696 0.0242 2.042 12.872 14.530 1522.880 1.454 64.628 4.327 0.64 292503. 0.6049
|
|
20.44 0.1349 0.3783 0.0671 0.0239 2.019 12.723 14.012 1505.293 1.437 62.327 4.222 0.64 292706. 0.5796
|
|
22.99 0.1517 0.4149 0.0645 0.0236 1.991 12.552 13.478 1485.025 1.418 59.949 4.117 0.64 292918. 0.5542
|
|
25.55 0.1686 0.4492 0.0619 0.0232 1.960 12.352 12.922 1461.422 1.396 57.479 4.011 0.64 293138. 0.5287
|
|
28.10 0.1855 0.4809 0.0591 0.0228 1.924 12.124 12.344 1434.371 1.370 54.907 3.903 0.64 293368. 0.5029
|
|
30.65 0.2023 0.5100 0.0562 0.0223 1.883 11.866 11.746 1403.859 1.341 52.245 3.795 0.64 293606. 0.4770
|
|
33.21 0.2192 0.5364 0.0533 0.0218 1.837 11.579 11.129 1369.975 1.308 49.503 3.685 0.64 293853. 0.4508
|
|
35.76 0.2360 0.5601 0.0503 0.0212 1.787 11.264 10.496 1332.684 1.273 46.686 3.572 0.64 294110. 0.4244
|
|
38.32 0.2529 0.5807 0.0471 0.0205 1.733 10.920 9.846 1291.928 1.234 43.795 3.457 0.64 294375. 0.3978
|
|
40.87 0.2698 0.5980 0.0440 0.0198 1.673 10.545 9.180 1247.642 1.191 40.834 3.337 0.64 294651. 0.3708
|
|
43.43 0.2866 0.6118 0.0407 0.0191 1.609 10.141 8.500 1199.766 1.146 37.807 3.213 0.64 294936. 0.3436
|
|
45.98 0.3035 0.6215 0.0374 0.0182 1.540 9.705 7.805 1148.239 1.096 34.715 3.083 0.64 295230. 0.3159
|
|
48.54 0.3203 0.6266 0.0340 0.0174 1.466 9.238 7.096 1093.013 1.044 31.564 2.945 0.64 295535. 0.2877
|
|
51.09 0.3372 0.6263 0.0305 0.0164 1.387 8.740 6.375 1034.051 0.987 28.357 2.796 0.64 295850. 0.2589
|
|
53.65 0.3541 0.6197 0.0270 0.0154 1.303 8.210 5.643 971.335 0.928 25.099 2.635 0.64 296175. 0.2295
|
|
56.20 0.3709 0.6052 0.0235 0.0144 1.213 7.648 4.900 904.871 0.864 21.797 2.456 0.64 296510. 0.1994
|
|
58.75 0.3878 0.5808 0.0199 0.0133 1.119 7.055 4.150 834.694 0.797 18.457 2.255 0.64 296856. 0.1684
|
|
61.31 0.4046 0.5435 0.0162 0.0121 1.020 6.431 3.392 760.884 0.727 15.090 2.022 0.64 297212. 0.1366
|
|
63.86 0.4215 0.4889 0.0126 0.0109 0.917 5.778 2.632 683.573 0.653 11.705 1.746 0.64 297579. 0.1039
|
|
66.42 0.4384 0.4096 0.0090 0.0096 0.809 5.097 1.870 602.980 0.576 8.318 1.407 0.64 297956. 0.0705
|
|
68.97 0.4552 0.2937 0.0053 0.0083 0.697 4.390 1.112 519.446 0.496 4.948 0.971 0.64 298342. 0.0376
|
|
71.53 0.4721 0.1180 0.0017 0.0069 0.581 3.660 0.359 433.016 0.413 1.598 0.376 0.64 298728. 0.0083
|
|
74.08 0.4889
|
|
|
|
|
|
|
|
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 0.0855 0.0254 2.850 16.331 21.607 2125.399 1.845 96.109 4.611 0.70 320409. 0.7860
|
|
2.76 0.0166 0.0546 0.0837 0.0254 2.849 16.324 21.149 2124.467 1.844 94.071 4.515 0.70 320570. 0.7615
|
|
5.52 0.0331 0.1069 0.0818 0.0253 2.843 16.291 20.662 2120.132 1.841 91.905 4.420 0.70 320739. 0.7369
|
|
8.28 0.0497 0.1570 0.0797 0.0252 2.833 16.235 20.154 2112.896 1.834 89.643 4.326 0.70 320916. 0.7123
|
|
11.04 0.0662 0.2048 0.0777 0.0251 2.821 16.163 19.630 2103.566 1.826 87.315 4.233 0.70 321101. 0.6877
|
|
13.80 0.0828 0.2504 0.0755 0.0250 2.804 16.065 19.080 2090.756 1.815 84.868 4.139 0.70 321294. 0.6631
|
|
16.56 0.0993 0.2937 0.0732 0.0248 2.782 15.939 18.506 2074.299 1.801 82.315 4.047 0.70 321497. 0.6384
|
|
19.32 0.1159 0.3348 0.0709 0.0245 2.756 15.790 17.914 2054.980 1.784 79.681 3.954 0.70 321707. 0.6137
|
|
22.07 0.1324 0.3737 0.0684 0.0243 2.724 15.608 17.293 2031.268 1.763 76.918 3.861 0.70 321927. 0.5889
|
|
24.83 0.1490 0.4103 0.0659 0.0239 2.688 15.400 16.653 2004.148 1.740 74.071 3.769 0.70 322155. 0.5640
|
|
27.59 0.1656 0.4447 0.0633 0.0236 2.645 15.156 15.985 1972.471 1.712 71.102 3.676 0.70 322393. 0.5390
|
|
30.35 0.1821 0.4767 0.0605 0.0231 2.597 14.881 15.295 1936.628 1.681 68.031 3.582 0.70 322641. 0.5138
|
|
33.11 0.1987 0.5062 0.0577 0.0226 2.543 14.569 14.578 1896.066 1.646 64.842 3.487 0.70 322897. 0.4883
|
|
35.87 0.2152 0.5333 0.0548 0.0221 2.482 14.223 13.839 1851.076 1.607 61.557 3.391 0.70 323163. 0.4626
|
|
38.63 0.2318 0.5577 0.0518 0.0215 2.416 13.843 13.080 1801.626 1.564 58.180 3.293 0.70 323439. 0.4368
|
|
41.39 0.2483 0.5793 0.0487 0.0209 2.344 13.429 12.301 1747.658 1.517 54.717 3.193 0.70 323725. 0.4106
|
|
44.15 0.2649 0.5979 0.0455 0.0202 2.265 12.979 11.504 1689.094 1.466 51.169 3.089 0.70 324020. 0.3842
|
|
46.91 0.2815 0.6132 0.0423 0.0194 2.180 12.493 10.688 1625.853 1.411 47.541 2.982 0.70 324326. 0.3575
|
|
49.67 0.2980 0.6248 0.0390 0.0186 2.089 11.970 9.855 1557.860 1.352 43.837 2.869 0.70 324642. 0.3303
|
|
52.43 0.3146 0.6322 0.0356 0.0177 1.991 11.411 9.006 1485.052 1.289 40.059 2.751 0.70 324968. 0.3027
|
|
55.19 0.3311 0.6348 0.0322 0.0168 1.887 10.814 8.142 1407.382 1.222 36.214 2.624 0.70 325305. 0.2746
|
|
57.95 0.3477 0.6317 0.0287 0.0158 1.777 10.180 7.263 1324.827 1.150 32.307 2.487 0.70 325653. 0.2458
|
|
60.71 0.3642 0.6216 0.0252 0.0148 1.659 9.508 6.372 1237.391 1.074 28.343 2.336 0.70 326011. 0.2162
|
|
63.46 0.3808 0.6028 0.0216 0.0137 1.536 8.799 5.470 1145.122 0.994 24.332 2.167 0.70 326381. 0.1858
|
|
66.22 0.3973 0.5729 0.0180 0.0125 1.406 8.054 4.560 1048.117 0.910 20.282 1.973 0.70 326761. 0.1545
|
|
68.98 0.4139 0.5280 0.0144 0.0113 1.269 7.273 3.643 946.543 0.822 16.206 1.746 0.70 327153. 0.1222
|
|
71.74 0.4305 0.4623 0.0108 0.0100 1.127 6.460 2.725 840.669 0.730 12.119 1.470 0.70 327555. 0.0890
|
|
74.50 0.4470 0.3663 0.0072 0.0087 0.980 5.616 1.807 730.908 0.635 8.039 1.122 0.71 327968. 0.0553
|
|
77.26 0.4636 0.2231 0.0035 0.0074 0.829 4.747 0.897 617.818 0.536 3.990 0.659 0.71 328388. 0.0229
|
|
80.02 0.4801 -0.0114 -0.0001 0.0059 0.667 3.824 -0.036 497.686 0.432 -0.159 -0.033 0.71 328738. 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 0.0870 0.0259 3.775 19.827 26.152 2814.900 2.240 116.324 4.214 0.76 349499. 0.7903
|
|
3.04 0.0167 0.0549 0.0851 0.0259 3.772 19.810 25.594 2812.443 2.238 113.841 4.128 0.76 349678. 0.7658
|
|
6.07 0.0334 0.1076 0.0831 0.0258 3.762 19.761 25.000 2805.570 2.233 111.201 4.042 0.76 349866. 0.7411
|
|
9.11 0.0501 0.1580 0.0811 0.0257 3.748 19.684 24.379 2794.608 2.224 108.437 3.957 0.76 350063. 0.7165
|
|
12.15 0.0668 0.2062 0.0789 0.0256 3.729 19.586 23.738 2780.647 2.213 105.587 3.872 0.76 350269. 0.6918
|
|
15.18 0.0835 0.2521 0.0767 0.0254 3.704 19.456 23.066 2762.284 2.198 102.599 3.788 0.76 350484. 0.6671
|
|
18.22 0.1002 0.2958 0.0744 0.0252 3.673 19.291 22.364 2738.796 2.179 99.474 3.704 0.76 350709. 0.6423
|
|
21.26 0.1169 0.3373 0.0720 0.0249 3.636 19.098 21.639 2711.406 2.158 96.250 3.620 0.76 350943. 0.6175
|
|
24.29 0.1336 0.3766 0.0694 0.0246 3.591 18.863 20.879 2678.066 2.131 92.868 3.536 0.76 351187. 0.5925
|
|
27.33 0.1503 0.4136 0.0668 0.0243 3.540 18.595 20.094 2640.048 2.101 89.380 3.452 0.76 351442. 0.5675
|
|
30.37 0.1670 0.4484 0.0641 0.0239 3.481 18.284 19.277 2595.885 2.066 85.744 3.368 0.76 351706. 0.5423
|
|
33.40 0.1837 0.4808 0.0613 0.0234 3.414 17.933 18.431 2546.027 2.026 81.979 3.283 0.76 351981. 0.5169
|
|
36.44 0.2004 0.5108 0.0584 0.0229 3.339 17.537 17.552 2489.826 1.981 78.071 3.197 0.76 352266. 0.4913
|
|
39.48 0.2171 0.5382 0.0554 0.0223 3.256 17.099 16.647 2427.665 1.932 74.044 3.110 0.76 352562. 0.4654
|
|
42.51 0.2338 0.5630 0.0523 0.0217 3.164 16.619 15.716 2359.526 1.878 69.905 3.021 0.76 352868. 0.4392
|
|
45.55 0.2505 0.5850 0.0491 0.0210 3.065 16.097 14.761 2285.348 1.819 65.659 2.930 0.76 353185. 0.4128
|
|
48.58 0.2672 0.6039 0.0458 0.0203 2.957 15.531 13.784 2205.066 1.755 61.310 2.835 0.76 353513. 0.3860
|
|
51.62 0.2839 0.6194 0.0425 0.0195 2.841 14.923 12.784 2118.618 1.686 56.862 2.737 0.76 353853. 0.3589
|
|
54.66 0.3006 0.6310 0.0391 0.0186 2.717 14.270 11.763 2025.958 1.612 52.321 2.633 0.77 354203. 0.3312
|
|
57.69 0.3173 0.6383 0.0357 0.0177 2.584 13.573 10.722 1927.071 1.534 47.690 2.524 0.77 354566. 0.3030
|
|
60.73 0.3340 0.6404 0.0321 0.0168 2.443 12.833 9.662 1821.974 1.450 42.976 2.405 0.77 354939. 0.2742
|
|
63.77 0.3507 0.6363 0.0285 0.0157 2.294 12.050 8.585 1710.738 1.361 38.186 2.276 0.77 355325. 0.2446
|
|
66.80 0.3674 0.6246 0.0249 0.0147 2.137 11.224 7.493 1593.501 1.268 33.328 2.133 0.77 355723. 0.2141
|
|
69.84 0.3841 0.6033 0.0212 0.0135 1.972 10.357 6.388 1470.477 1.170 28.413 1.970 0.77 356132. 0.1826
|
|
72.88 0.4008 0.5693 0.0175 0.0123 1.800 9.452 5.272 1341.980 1.068 23.452 1.782 0.77 356554. 0.1501
|
|
75.91 0.4175 0.5184 0.0138 0.0111 1.621 8.512 4.150 1208.445 0.962 18.461 1.558 0.77 356988. 0.1164
|
|
78.95 0.4342 0.4437 0.0101 0.0098 1.436 7.540 3.026 1070.466 0.852 13.458 1.282 0.77 357434. 0.0818
|
|
81.99 0.4509 0.3343 0.0063 0.0085 1.246 6.542 1.904 928.861 0.739 8.471 0.930 0.77 357891. 0.0471
|
|
85.02 0.4676 0.1706 0.0026 0.0072 1.052 5.525 0.791 784.375 0.624 3.520 0.458 0.77 358353. 0.0149
|
|
88.06 0.4843
|
|
|
|
|
|
|
|
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 0.0887 0.0269 4.983 24.161 31.315 3716.164 2.730 139.288 3.822 0.83 378573. 0.7844
|
|
3.30 0.0168 0.0543 0.0868 0.0268 4.968 24.088 30.645 3704.811 2.721 136.309 3.752 0.83 378769. 0.7617
|
|
6.61 0.0336 0.1066 0.0848 0.0267 4.946 23.982 29.935 3688.576 2.709 133.149 3.681 0.83 378977. 0.7386
|
|
9.91 0.0503 0.1569 0.0827 0.0265 4.918 23.843 29.188 3667.120 2.694 129.827 3.610 0.83 379194. 0.7153
|
|
13.22 0.0671 0.2051 0.0805 0.0263 4.884 23.679 28.416 3641.915 2.675 126.393 3.539 0.83 379421. 0.6918
|
|
16.52 0.0839 0.2511 0.0782 0.0261 4.844 23.484 27.610 3611.998 2.653 122.809 3.467 0.83 379657. 0.6681
|
|
19.83 0.1007 0.2951 0.0758 0.0259 4.795 23.247 26.764 3575.580 2.626 119.047 3.395 0.83 379905. 0.6441
|
|
23.13 0.1174 0.3369 0.0734 0.0256 4.740 22.980 25.892 3534.519 2.596 115.168 3.323 0.83 380163. 0.6200
|
|
26.43 0.1342 0.3766 0.0708 0.0252 4.675 22.667 24.977 3486.254 2.561 111.096 3.250 0.83 380432. 0.5956
|
|
29.74 0.1510 0.4140 0.0681 0.0248 4.603 22.318 24.032 3432.663 2.522 106.896 3.175 0.83 380711. 0.5709
|
|
33.04 0.1678 0.4491 0.0653 0.0244 4.522 21.923 23.047 3371.901 2.477 102.515 3.100 0.83 381002. 0.5458
|
|
36.35 0.1845 0.4818 0.0624 0.0239 4.431 21.485 22.028 3304.499 2.427 97.980 3.023 0.83 381304. 0.5204
|
|
39.65 0.2013 0.5119 0.0594 0.0234 4.331 20.999 20.969 3229.775 2.372 93.270 2.945 0.83 381617. 0.4945
|
|
42.95 0.2181 0.5393 0.0563 0.0228 4.221 20.467 19.878 3147.919 2.312 88.416 2.864 0.83 381941. 0.4683
|
|
46.26 0.2349 0.5640 0.0531 0.0221 4.102 19.888 18.756 3058.846 2.247 83.427 2.781 0.83 382277. 0.4417
|
|
49.56 0.2516 0.5856 0.0499 0.0214 3.973 19.262 17.605 2962.627 2.176 78.308 2.695 0.83 382625. 0.4147
|
|
52.87 0.2684 0.6039 0.0465 0.0207 3.834 18.590 16.426 2859.237 2.100 73.064 2.606 0.83 382985. 0.3873
|
|
56.17 0.2852 0.6185 0.0431 0.0199 3.686 17.872 15.220 2748.774 2.019 67.701 2.512 0.83 383357. 0.3593
|
|
59.48 0.3020 0.6287 0.0396 0.0190 3.529 17.109 13.989 2631.397 1.933 62.223 2.411 0.83 383741. 0.3307
|
|
62.78 0.3187 0.6340 0.0361 0.0181 3.362 16.302 12.733 2507.312 1.842 56.638 2.303 0.83 384138. 0.3014
|
|
66.08 0.3355 0.6333 0.0325 0.0172 3.187 15.454 11.455 2376.855 1.746 50.953 2.186 0.83 384547. 0.2713
|
|
69.39 0.3523 0.6255 0.0288 0.0162 3.004 14.566 10.156 2240.383 1.646 45.175 2.056 0.83 384969. 0.2403
|
|
72.69 0.3691 0.6089 0.0250 0.0152 2.814 13.643 8.839 2098.339 1.541 39.315 1.911 0.83 385404. 0.2083
|
|
76.00 0.3858 0.5813 0.0213 0.0141 2.617 12.687 7.506 1951.315 1.433 33.385 1.745 0.83 385852. 0.1753
|
|
79.30 0.4026 0.5396 0.0175 0.0130 2.414 11.703 6.160 1800.032 1.322 27.399 1.552 0.83 386314. 0.1413
|
|
82.61 0.4194 0.4798 0.0136 0.0119 2.206 10.698 4.806 1645.365 1.209 21.377 1.325 0.83 386788. 0.1065
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|
85.91 0.4362 0.3959 0.0098 0.0108 1.996 9.677 3.449 1488.407 1.093 15.343 1.051 0.83 387275. 0.0716
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|
89.21 0.4529 0.2796 0.0059 0.0096 1.784 8.650 2.097 1330.470 0.977 9.329 0.715 0.83 387775. 0.0380
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|
92.52 0.4697 0.1183 0.0021 0.0085 1.572 7.621 0.753 1172.156 0.861 3.351 0.292 0.83 388276. 0.0093
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|
95.82 0.4865
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|
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|
|
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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 0.0907 0.0293 6.787 30.553 37.143 5060.708 3.452 165.214 3.329 0.89 407627. 0.7440
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|
3.56 0.0168 0.0513 0.0888 0.0291 6.734 30.318 36.355 5021.794 3.425 161.707 3.284 0.89 407842. 0.7261
|
|
7.13 0.0336 0.1011 0.0868 0.0288 6.676 30.054 35.523 4977.960 3.395 158.008 3.237 0.89 408068. 0.7075
|
|
10.69 0.0504 0.1494 0.0846 0.0285 6.608 29.749 34.644 4927.453 3.361 154.097 3.189 0.89 408305. 0.6884
|
|
14.25 0.0672 0.1962 0.0824 0.0282 6.534 29.415 33.731 4872.225 3.323 150.037 3.140 0.89 408553. 0.6688
|
|
17.81 0.0840 0.2413 0.0801 0.0279 6.454 29.054 32.783 4812.481 3.283 145.820 3.090 0.89 408811. 0.6488
|
|
21.38 0.1008 0.2847 0.0776 0.0275 6.363 28.647 31.785 4744.946 3.236 141.378 3.038 0.89 409081. 0.6282
|
|
24.94 0.1176 0.3264 0.0751 0.0271 6.266 28.208 30.754 4672.328 3.187 136.794 2.985 0.89 409363. 0.6072
|
|
28.50 0.1344 0.3662 0.0725 0.0266 6.158 27.721 29.673 4591.650 3.132 131.984 2.931 0.89 409656. 0.5855
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|
32.06 0.1512 0.4042 0.0698 0.0261 6.041 27.196 28.556 4504.572 3.073 127.016 2.875 0.89 409960. 0.5635
|
|
35.63 0.1680 0.4399 0.0669 0.0255 5.915 26.629 27.390 4410.757 3.009 121.832 2.817 0.89 410277. 0.5406
|
|
39.19 0.1847 0.4731 0.0640 0.0250 5.783 26.036 26.184 4312.553 2.942 116.468 2.754 0.89 410605. 0.5168
|
|
42.75 0.2015 0.5037 0.0609 0.0244 5.643 25.403 24.931 4207.630 2.870 110.893 2.687 0.89 410946. 0.4921
|
|
46.31 0.2183 0.5310 0.0577 0.0237 5.498 24.753 23.639 4100.043 2.797 105.146 2.615 0.89 411299. 0.4663
|
|
49.88 0.2351 0.5540 0.0545 0.0231 5.356 24.111 22.310 3993.722 2.724 99.233 2.534 0.89 411664. 0.4389
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|
53.44 0.2519 0.5734 0.0512 0.0225 5.206 23.437 20.946 3881.957 2.648 93.167 2.447 0.89 412042. 0.4108
|
|
57.00 0.2687 0.5887 0.0478 0.0218 5.048 22.725 19.549 3764.019 2.567 86.953 2.356 0.89 412432. 0.3820
|
|
60.57 0.2855 0.5995 0.0443 0.0211 4.881 21.975 18.120 3639.838 2.483 80.599 2.258 0.89 412836. 0.3525
|
|
64.13 0.3023 0.6053 0.0407 0.0203 4.707 21.191 16.661 3509.924 2.394 74.110 2.153 0.89 413252. 0.3223
|
|
67.69 0.3191 0.6052 0.0371 0.0195 4.526 20.375 15.174 3374.898 2.302 67.494 2.039 0.89 413682. 0.2913
|
|
71.25 0.3359 0.5982 0.0334 0.0187 4.339 19.534 13.660 3235.490 2.207 60.761 1.915 0.89 414125. 0.2596
|
|
74.82 0.3527 0.5831 0.0296 0.0179 4.147 18.671 12.122 3092.632 2.109 53.919 1.778 0.89 414582. 0.2270
|
|
78.38 0.3695 0.5585 0.0258 0.0171 3.952 17.794 10.563 2947.343 2.010 46.983 1.626 0.89 415053. 0.1937
|
|
81.94 0.3863 0.5228 0.0220 0.0162 3.755 16.907 8.986 2800.469 1.910 39.968 1.455 0.90 415537. 0.1600
|
|
85.50 0.4031 0.4739 0.0181 0.0154 3.558 16.018 7.395 2653.157 1.810 32.891 1.264 0.90 416036. 0.1261
|
|
89.07 0.4199 0.4094 0.0142 0.0145 3.362 15.134 5.795 2506.686 1.710 25.776 1.049 0.90 416549. 0.0926
|
|
92.63 0.4367 0.3270 0.0102 0.0137 3.168 14.263 4.194 2362.474 1.611 18.653 0.805 0.90 417075. 0.0605
|
|
96.19 0.4535 0.2237 0.0063 0.0129 2.980 13.415 2.599 2222.062 1.516 11.561 0.531 0.90 417615. 0.0314
|
|
99.75 0.4703 0.0966 0.0025 0.0121 2.797 12.590 1.016 2085.415 1.422 4.518 0.221 0.90 418160. 0.0082
|
|
103.32 0.4871
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