501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x6W (18x6W.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 0.0684 0.0268 0.004 0.257 0.229 3.044 0.029 1.018 34.094 0.07 38504. 0.5316
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0.29 0.0170 0.0422 0.0669 0.0269 0.004 0.258 0.224 3.047 0.029 0.995 33.297 0.07 38521. 0.5133
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0.58 0.0339 0.0823 0.0653 0.0269 0.004 0.258 0.218 3.048 0.029 0.971 32.494 0.07 38539. 0.4949
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0.87 0.0509 0.1204 0.0636 0.0269 0.004 0.257 0.213 3.046 0.029 0.946 31.687 0.07 38558. 0.4765
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1.16 0.0678 0.1564 0.0619 0.0268 0.004 0.257 0.207 3.041 0.029 0.921 30.874 0.07 38578. 0.4579
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1.44 0.0848 0.1903 0.0601 0.0268 0.004 0.256 0.201 3.033 0.029 0.894 30.056 0.07 38598. 0.4393
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1.73 0.1017 0.2222 0.0582 0.0267 0.004 0.255 0.195 3.022 0.029 0.866 29.232 0.07 38620. 0.4206
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2.02 0.1187 0.2518 0.0563 0.0265 0.004 0.254 0.188 3.008 0.029 0.838 28.401 0.07 38643. 0.4018
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2.31 0.1356 0.2793 0.0543 0.0264 0.004 0.253 0.182 2.990 0.029 0.808 27.563 0.07 38667. 0.3830
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2.60 0.1526 0.3046 0.0523 0.0262 0.004 0.251 0.175 2.968 0.028 0.778 26.717 0.07 38692. 0.3641
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2.89 0.1695 0.3276 0.0501 0.0259 0.004 0.249 0.168 2.942 0.028 0.746 25.861 0.07 38718. 0.3453
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3.18 0.1865 0.3482 0.0480 0.0257 0.004 0.246 0.160 2.912 0.028 0.714 24.994 0.07 38746. 0.3264
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3.47 0.2034 0.3665 0.0457 0.0254 0.004 0.243 0.153 2.877 0.027 0.680 24.114 0.07 38774. 0.3074
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3.76 0.2204 0.3823 0.0434 0.0250 0.004 0.240 0.145 2.837 0.027 0.646 23.218 0.07 38804. 0.2884
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4.04 0.2373 0.3955 0.0411 0.0246 0.004 0.236 0.137 2.793 0.027 0.611 22.303 0.07 38836. 0.2694
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4.33 0.2543 0.4060 0.0386 0.0242 0.004 0.232 0.129 2.743 0.026 0.575 21.367 0.07 38868. 0.2504
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4.62 0.2712 0.4135 0.0362 0.0237 0.004 0.227 0.121 2.689 0.026 0.538 20.405 0.07 38902. 0.2313
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4.91 0.2882 0.4180 0.0336 0.0232 0.004 0.222 0.112 2.628 0.025 0.500 19.412 0.07 38937. 0.2122
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5.20 0.3051 0.4191 0.0310 0.0226 0.003 0.217 0.104 2.562 0.024 0.462 18.382 0.07 38974. 0.1931
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5.49 0.3221 0.4165 0.0284 0.0220 0.003 0.211 0.095 2.491 0.024 0.423 17.307 0.07 39012. 0.1739
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5.78 0.3390 0.4099 0.0257 0.0213 0.003 0.204 0.086 2.413 0.023 0.383 16.179 0.07 39051. 0.1547
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6.07 0.3560 0.3986 0.0230 0.0205 0.003 0.197 0.077 2.329 0.022 0.342 14.986 0.07 39092. 0.1355
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6.36 0.3729 0.3821 0.0202 0.0197 0.003 0.189 0.068 2.239 0.021 0.301 13.714 0.07 39135. 0.1163
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6.65 0.3899 0.3596 0.0174 0.0189 0.003 0.181 0.058 2.142 0.020 0.259 12.344 0.07 39179. 0.0972
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6.93 0.4068 0.3299 0.0146 0.0180 0.003 0.172 0.049 2.039 0.019 0.217 10.854 0.07 39224. 0.0782
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7.22 0.4238 0.2917 0.0117 0.0170 0.003 0.163 0.039 1.930 0.018 0.174 9.211 0.07 39271. 0.0594
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7.51 0.4407 0.2429 0.0088 0.0160 0.002 0.153 0.029 1.814 0.017 0.131 7.377 0.07 39319. 0.0413
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7.80 0.4577 0.1810 0.0059 0.0149 0.002 0.143 0.020 1.691 0.016 0.088 5.294 0.07 39369. 0.0242
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8.09 0.4746 0.1022 0.0030 0.0138 0.002 0.132 0.010 1.562 0.015 0.044 2.883 0.07 39420. 0.0094
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8.38 0.4916 0.0004 0.0000 0.0126 0.002 0.121 0.000 1.426 0.014 0.000 0.010 0.07 39470. 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 0.0687 0.0233 0.028 0.894 0.920 21.144 0.101 4.091 19.732 0.14 77008. 0.6169
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0.58 0.0170 0.0490 0.0672 0.0234 0.028 0.895 0.899 21.183 0.101 4.000 19.256 0.14 77042. 0.5952
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1.16 0.0341 0.0956 0.0656 0.0234 0.028 0.896 0.878 21.202 0.101 3.905 18.779 0.14 77078. 0.5736
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1.74 0.0511 0.1398 0.0639 0.0234 0.028 0.896 0.856 21.199 0.101 3.805 18.304 0.14 77115. 0.5519
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2.32 0.0681 0.1816 0.0622 0.0233 0.028 0.895 0.832 21.172 0.101 3.702 17.830 0.14 77155. 0.5302
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2.90 0.0852 0.2209 0.0604 0.0233 0.028 0.893 0.808 21.119 0.101 3.595 17.356 0.14 77197. 0.5086
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3.48 0.1022 0.2579 0.0585 0.0232 0.028 0.889 0.783 21.038 0.100 3.483 16.884 0.14 77241. 0.4870
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4.07 0.1192 0.2925 0.0566 0.0231 0.028 0.884 0.757 20.929 0.100 3.368 16.411 0.14 77287. 0.4655
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4.65 0.1363 0.3246 0.0546 0.0229 0.028 0.879 0.730 20.787 0.099 3.249 15.938 0.14 77335. 0.4440
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5.23 0.1533 0.3543 0.0525 0.0227 0.028 0.871 0.703 20.613 0.098 3.126 15.464 0.14 77386. 0.4226
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5.81 0.1703 0.3816 0.0504 0.0225 0.027 0.862 0.674 20.404 0.097 2.999 14.989 0.14 77439. 0.4012
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6.39 0.1874 0.4064 0.0482 0.0222 0.027 0.852 0.645 20.158 0.096 2.869 14.512 0.14 77494. 0.3799
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6.97 0.2044 0.4286 0.0459 0.0219 0.027 0.840 0.615 19.874 0.095 2.734 14.031 0.14 77552. 0.3586
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7.55 0.2215 0.4483 0.0436 0.0216 0.026 0.826 0.584 19.549 0.093 2.597 13.545 0.14 77612. 0.3373
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8.13 0.2385 0.4652 0.0412 0.0211 0.026 0.811 0.552 19.181 0.092 2.455 13.052 0.14 77675. 0.3161
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8.71 0.2555 0.4793 0.0388 0.0207 0.025 0.793 0.519 18.769 0.090 2.310 12.551 0.14 77741. 0.2949
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9.29 0.2726 0.4904 0.0363 0.0202 0.025 0.774 0.486 18.312 0.087 2.162 12.040 0.14 77809. 0.2736
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9.87 0.2896 0.4983 0.0338 0.0196 0.024 0.753 0.452 17.806 0.085 2.011 11.514 0.14 77881. 0.2523
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10.45 0.3066 0.5027 0.0312 0.0190 0.023 0.729 0.417 17.252 0.082 1.856 10.970 0.14 77954. 0.2310
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11.03 0.3237 0.5032 0.0285 0.0184 0.022 0.704 0.382 16.647 0.079 1.698 10.404 0.14 78031. 0.2096
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11.61 0.3407 0.4994 0.0258 0.0176 0.021 0.676 0.346 15.989 0.076 1.538 9.809 0.14 78111. 0.1880
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12.20 0.3577 0.4906 0.0231 0.0168 0.020 0.646 0.309 15.278 0.073 1.375 9.177 0.14 78193. 0.1663
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12.78 0.3748 0.4759 0.0203 0.0160 0.019 0.613 0.272 14.513 0.069 1.209 8.498 0.14 78279. 0.1444
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13.36 0.3918 0.4542 0.0175 0.0151 0.018 0.579 0.234 13.693 0.065 1.042 7.757 0.14 78367. 0.1224
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13.94 0.4088 0.4239 0.0146 0.0141 0.017 0.542 0.196 12.817 0.061 0.872 6.937 0.14 78459. 0.1001
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14.52 0.4259 0.3825 0.0118 0.0131 0.016 0.502 0.157 11.885 0.057 0.700 6.010 0.14 78553. 0.0777
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15.10 0.4429 0.3268 0.0089 0.0120 0.015 0.461 0.119 10.897 0.052 0.528 4.937 0.14 78651. 0.0554
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15.68 0.4599 0.2515 0.0059 0.0109 0.013 0.416 0.079 9.853 0.047 0.354 3.659 0.14 78751. 0.0336
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16.26 0.4770 0.1483 0.0030 0.0096 0.012 0.370 0.040 8.753 0.042 0.179 2.081 0.14 78854. 0.0136
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16.84 0.4940 0.0014 0.0000 0.0084 0.010 0.321 0.000 7.585 0.036 0.001 0.019 0.14 78952. 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 0.0691 0.0219 0.090 1.890 2.080 67.071 0.213 9.253 14.068 0.21 115509. 0.6614
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0.87 0.0171 0.0526 0.0676 0.0220 0.090 1.894 2.034 67.221 0.214 9.047 13.723 0.21 115561. 0.6380
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1.75 0.0342 0.1025 0.0659 0.0220 0.090 1.896 1.985 67.300 0.214 8.831 13.380 0.21 115615. 0.6146
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2.62 0.0512 0.1498 0.0643 0.0220 0.090 1.896 1.935 67.303 0.214 8.606 13.039 0.21 115672. 0.5912
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3.49 0.0683 0.1945 0.0625 0.0220 0.090 1.894 1.882 67.222 0.214 8.372 12.700 0.21 115732. 0.5679
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4.37 0.0854 0.2367 0.0607 0.0219 0.090 1.889 1.828 67.051 0.213 8.129 12.362 0.21 115795. 0.5448
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5.24 0.1025 0.2764 0.0588 0.0218 0.090 1.882 1.771 66.785 0.213 7.877 12.027 0.21 115861. 0.5217
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6.11 0.1196 0.3135 0.0569 0.0217 0.089 1.871 1.712 66.416 0.211 7.616 11.693 0.21 115930. 0.4988
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6.99 0.1367 0.3481 0.0549 0.0215 0.088 1.858 1.652 65.939 0.210 7.346 11.361 0.21 116003. 0.4760
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7.86 0.1537 0.3802 0.0528 0.0213 0.088 1.841 1.589 65.345 0.208 7.068 11.030 0.21 116080. 0.4532
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8.74 0.1708 0.4097 0.0506 0.0211 0.087 1.821 1.524 64.631 0.206 6.781 10.699 0.21 116159. 0.4306
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9.61 0.1879 0.4367 0.0484 0.0208 0.086 1.797 1.458 63.787 0.203 6.485 10.367 0.21 116243. 0.4081
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10.48 0.2050 0.4612 0.0462 0.0205 0.084 1.770 1.390 62.808 0.200 6.181 10.035 0.21 116330. 0.3856
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11.36 0.2221 0.4830 0.0438 0.0201 0.083 1.738 1.319 61.688 0.196 5.869 9.702 0.21 116421. 0.3633
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12.23 0.2392 0.5021 0.0414 0.0197 0.081 1.702 1.247 60.419 0.192 5.549 9.365 0.21 116516. 0.3410
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13.10 0.2562 0.5184 0.0390 0.0193 0.079 1.662 1.174 58.995 0.188 5.221 9.024 0.21 116615. 0.3187
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13.98 0.2733 0.5317 0.0365 0.0188 0.077 1.618 1.098 57.411 0.183 4.885 8.676 0.22 116718. 0.2964
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14.85 0.2904 0.5417 0.0339 0.0182 0.075 1.568 1.021 55.660 0.177 4.542 8.321 0.22 116826. 0.2741
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15.72 0.3075 0.5484 0.0313 0.0176 0.072 1.514 0.942 53.736 0.171 4.192 7.955 0.22 116937. 0.2517
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16.60 0.3246 0.5511 0.0286 0.0169 0.069 1.455 0.862 51.635 0.164 3.835 7.574 0.22 117053. 0.2293
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17.47 0.3417 0.5495 0.0259 0.0161 0.066 1.390 0.781 49.351 0.157 3.472 7.174 0.22 117173. 0.2066
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18.34 0.3587 0.5428 0.0232 0.0153 0.063 1.321 0.698 46.880 0.149 3.103 6.750 0.22 117297. 0.1838
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19.22 0.3758 0.5301 0.0204 0.0144 0.059 1.246 0.613 44.219 0.141 2.728 6.292 0.22 117426. 0.1606
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20.09 0.3929 0.5100 0.0175 0.0135 0.055 1.165 0.528 41.365 0.132 2.349 5.790 0.22 117560. 0.1372
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20.97 0.4100 0.4806 0.0147 0.0125 0.051 1.080 0.442 38.316 0.122 1.965 5.229 0.22 117698. 0.1133
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21.84 0.4271 0.4390 0.0118 0.0115 0.047 0.988 0.355 35.070 0.112 1.577 4.585 0.22 117840. 0.0890
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22.71 0.4442 0.3807 0.0089 0.0103 0.042 0.891 0.267 31.629 0.101 1.186 3.823 0.22 117987. 0.0643
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23.59 0.4612 0.2984 0.0059 0.0091 0.038 0.789 0.178 27.993 0.089 0.792 2.886 0.22 118139. 0.0397
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24.46 0.4783 0.1796 0.0030 0.0079 0.032 0.681 0.089 24.162 0.077 0.397 1.675 0.22 118293. 0.0163
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25.33 0.4954 -0.0034 0.0000 0.0066 0.027 0.565 -0.001 20.070 0.064 -0.006 -0.030 0.22 118433. 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 0.0695 0.0212 0.206 3.249 3.722 153.779 0.367 16.555 10.978 0.29 154008. 0.6904
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1.17 0.0172 0.0550 0.0680 0.0212 0.207 3.257 3.638 154.152 0.368 16.184 10.705 0.29 154077. 0.6657
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2.34 0.0344 0.1073 0.0663 0.0213 0.207 3.262 3.551 154.353 0.368 15.795 10.435 0.29 154150. 0.6410
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3.52 0.0516 0.1568 0.0646 0.0213 0.207 3.262 3.460 154.366 0.369 15.390 10.167 0.29 154227. 0.6165
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4.69 0.0688 0.2036 0.0629 0.0212 0.207 3.258 3.365 154.174 0.368 14.969 9.901 0.29 154308. 0.5921
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5.86 0.0860 0.2477 0.0610 0.0212 0.206 3.249 3.267 153.763 0.367 14.532 9.637 0.29 154392. 0.5678
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7.03 0.1032 0.2891 0.0591 0.0211 0.205 3.235 3.165 153.116 0.366 14.078 9.376 0.29 154482. 0.5437
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8.21 0.1204 0.3280 0.0572 0.0210 0.204 3.216 3.059 152.219 0.363 13.609 9.116 0.29 154575. 0.5198
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9.38 0.1376 0.3643 0.0551 0.0208 0.203 3.192 2.950 151.054 0.361 13.123 8.859 0.29 154674. 0.4960
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10.55 0.1548 0.3979 0.0530 0.0206 0.201 3.161 2.837 149.606 0.357 12.621 8.603 0.29 154777. 0.4724
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11.72 0.1720 0.4290 0.0508 0.0204 0.198 3.124 2.721 147.859 0.353 12.104 8.347 0.29 154884. 0.4489
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12.90 0.1892 0.4576 0.0486 0.0201 0.196 3.081 2.601 145.796 0.348 11.571 8.093 0.29 154997. 0.4255
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14.07 0.2063 0.4835 0.0463 0.0198 0.192 3.030 2.478 143.401 0.342 11.023 7.839 0.29 155115. 0.4023
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15.24 0.2235 0.5067 0.0439 0.0194 0.189 2.972 2.352 140.657 0.336 10.461 7.584 0.29 155237. 0.3791
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16.41 0.2407 0.5272 0.0415 0.0190 0.184 2.907 2.222 137.550 0.328 9.883 7.327 0.29 155366. 0.3560
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17.59 0.2579 0.5449 0.0390 0.0185 0.180 2.833 2.089 134.061 0.320 9.292 7.068 0.29 155499. 0.3330
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18.76 0.2751 0.5596 0.0365 0.0179 0.175 2.751 1.953 130.178 0.311 8.687 6.805 0.29 155638. 0.3100
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19.93 0.2923 0.5711 0.0339 0.0173 0.169 2.660 1.814 125.885 0.301 8.069 6.536 0.29 155783. 0.2870
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21.10 0.3095 0.5792 0.0312 0.0167 0.162 2.560 1.672 121.167 0.289 7.438 6.260 0.29 155933. 0.2639
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22.28 0.3267 0.5833 0.0285 0.0160 0.156 2.451 1.528 116.014 0.277 6.796 5.973 0.29 156089. 0.2407
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23.45 0.3439 0.5831 0.0258 0.0152 0.148 2.333 1.381 110.412 0.264 6.141 5.672 0.29 156251. 0.2173
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24.62 0.3611 0.5776 0.0230 0.0144 0.140 2.205 1.231 104.352 0.249 5.477 5.352 0.29 156419. 0.1936
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25.79 0.3783 0.5660 0.0202 0.0135 0.131 2.067 1.080 97.824 0.234 4.802 5.005 0.29 156593. 0.1695
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26.97 0.3955 0.5466 0.0173 0.0125 0.122 1.919 0.926 90.823 0.217 4.118 4.624 0.29 156773. 0.1450
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28.14 0.4127 0.5172 0.0144 0.0115 0.112 1.761 0.770 83.343 0.199 3.427 4.192 0.29 156960. 0.1200
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29.31 0.4299 0.4742 0.0115 0.0104 0.101 1.593 0.613 75.384 0.180 2.728 3.690 0.29 157152. 0.0942
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30.48 0.4471 0.4121 0.0085 0.0092 0.090 1.415 0.455 66.945 0.160 2.024 3.083 0.29 157350. 0.0678
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31.66 0.4643 0.3210 0.0055 0.0080 0.078 1.226 0.296 58.030 0.139 1.316 2.313 0.29 157555. 0.0410
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32.83 0.4815 0.1825 0.0025 0.0067 0.065 1.028 0.136 48.635 0.116 0.605 1.268 0.29 157763. 0.0152
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34.00 0.4987
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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 0.0701 0.0208 0.396 4.987 5.862 294.992 0.563 26.074 9.013 0.36 192503. 0.7113
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1.46 0.0171 0.0562 0.0685 0.0209 0.397 4.999 5.731 295.726 0.565 25.492 8.790 0.36 192589. 0.6860
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2.92 0.0342 0.1096 0.0669 0.0209 0.397 5.006 5.594 296.120 0.566 24.884 8.569 0.36 192680. 0.6607
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4.38 0.0514 0.1602 0.0652 0.0209 0.397 5.006 5.452 296.142 0.566 24.250 8.350 0.36 192776. 0.6356
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5.84 0.0685 0.2081 0.0634 0.0209 0.397 5.000 5.304 295.763 0.565 23.591 8.134 0.36 192877. 0.6106
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7.29 0.0856 0.2533 0.0616 0.0208 0.396 4.986 5.150 294.951 0.563 22.906 7.919 0.36 192983. 0.5858
|
|
8.75 0.1027 0.2958 0.0597 0.0207 0.394 4.964 4.990 293.677 0.561 22.197 7.707 0.36 193094. 0.5612
|
|
10.21 0.1198 0.3357 0.0577 0.0206 0.391 4.935 4.825 291.909 0.558 21.462 7.497 0.36 193211. 0.5368
|
|
11.67 0.1369 0.3729 0.0556 0.0204 0.388 4.896 4.654 289.617 0.553 20.701 7.289 0.36 193333. 0.5126
|
|
13.13 0.1541 0.4077 0.0535 0.0202 0.385 4.848 4.478 286.769 0.548 19.917 7.082 0.36 193461. 0.4885
|
|
14.59 0.1712 0.4398 0.0514 0.0200 0.380 4.790 4.296 283.332 0.541 19.108 6.877 0.36 193596. 0.4646
|
|
16.05 0.1883 0.4694 0.0491 0.0197 0.375 4.721 4.108 279.275 0.533 18.274 6.673 0.36 193736. 0.4409
|
|
17.51 0.2054 0.4965 0.0468 0.0194 0.368 4.641 3.916 274.567 0.524 17.418 6.469 0.36 193882. 0.4173
|
|
18.97 0.2225 0.5209 0.0445 0.0190 0.361 4.550 3.718 269.175 0.514 16.538 6.265 0.36 194035. 0.3938
|
|
20.43 0.2397 0.5427 0.0420 0.0186 0.353 4.447 3.515 263.068 0.502 15.635 6.061 0.36 194194. 0.3704
|
|
21.88 0.2568 0.5617 0.0395 0.0181 0.344 4.331 3.307 256.216 0.489 14.711 5.855 0.36 194360. 0.3471
|
|
23.34 0.2739 0.5778 0.0370 0.0175 0.333 4.202 3.095 248.589 0.475 13.765 5.646 0.36 194533. 0.3238
|
|
24.80 0.2910 0.5909 0.0344 0.0169 0.322 4.060 2.877 240.158 0.459 12.798 5.434 0.36 194713. 0.3005
|
|
26.26 0.3081 0.6006 0.0318 0.0163 0.310 3.903 2.656 230.896 0.441 11.812 5.217 0.36 194900. 0.2771
|
|
27.72 0.3252 0.6066 0.0290 0.0156 0.296 3.732 2.430 220.777 0.422 10.807 4.991 0.36 195094. 0.2536
|
|
29.18 0.3424 0.6084 0.0263 0.0148 0.281 3.546 2.200 209.780 0.401 9.784 4.756 0.36 195295. 0.2299
|
|
30.64 0.3595 0.6052 0.0235 0.0140 0.265 3.345 1.966 197.883 0.378 8.744 4.506 0.36 195503. 0.2059
|
|
32.10 0.3766 0.5961 0.0207 0.0131 0.248 3.128 1.729 185.069 0.353 7.689 4.236 0.36 195719. 0.1816
|
|
33.56 0.3937 0.5796 0.0178 0.0121 0.230 2.896 1.488 171.325 0.327 6.619 3.940 0.36 195943. 0.1567
|
|
35.01 0.4108 0.5533 0.0149 0.0111 0.210 2.648 1.245 156.642 0.299 5.537 3.605 0.36 196174. 0.1311
|
|
36.47 0.4280 0.5139 0.0119 0.0099 0.189 2.384 0.999 141.015 0.269 4.445 3.214 0.36 196412. 0.1047
|
|
37.93 0.4451 0.4555 0.0090 0.0088 0.167 2.104 0.752 124.447 0.238 3.343 2.739 0.36 196658. 0.0774
|
|
39.39 0.4622 0.3680 0.0060 0.0075 0.143 1.808 0.502 106.942 0.204 2.235 2.131 0.36 196912. 0.0492
|
|
40.85 0.4793 0.2313 0.0030 0.0062 0.119 1.496 0.252 88.498 0.169 1.121 1.292 0.36 197170. 0.0211
|
|
42.31 0.4964 -0.0064 -0.0001 0.0048 0.092 1.160 -0.005 68.616 0.131 -0.023 -0.035 0.36 197384. 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 0.0708 0.0206 0.678 7.124 8.524 505.739 0.805 37.915 7.645 0.43 230992. 0.7276
|
|
1.75 0.0171 0.0573 0.0692 0.0207 0.680 7.142 8.334 506.992 0.807 37.069 7.456 0.43 231096. 0.7016
|
|
3.51 0.0343 0.1117 0.0675 0.0207 0.681 7.151 8.135 507.642 0.808 36.184 7.268 0.43 231206. 0.6758
|
|
5.26 0.0514 0.1633 0.0658 0.0207 0.681 7.151 7.928 507.636 0.808 35.262 7.083 0.43 231322. 0.6501
|
|
7.01 0.0686 0.2122 0.0640 0.0207 0.680 7.141 7.712 506.919 0.807 34.303 6.900 0.43 231444. 0.6247
|
|
8.77 0.0857 0.2582 0.0622 0.0206 0.678 7.120 7.488 505.438 0.804 33.306 6.719 0.43 231572. 0.5994
|
|
10.52 0.1029 0.3017 0.0602 0.0205 0.675 7.088 7.256 503.140 0.801 32.273 6.541 0.43 231706. 0.5743
|
|
12.27 0.1200 0.3424 0.0582 0.0204 0.670 7.043 7.015 499.970 0.796 31.203 6.364 0.43 231847. 0.5495
|
|
14.03 0.1371 0.3806 0.0562 0.0202 0.665 6.985 6.766 495.875 0.789 30.097 6.189 0.43 231995. 0.5248
|
|
15.78 0.1543 0.4162 0.0540 0.0200 0.658 6.914 6.509 490.798 0.781 28.954 6.016 0.43 232150. 0.5003
|
|
17.53 0.1714 0.4492 0.0519 0.0198 0.650 6.828 6.245 484.685 0.771 27.776 5.844 0.43 232312. 0.4760
|
|
19.29 0.1886 0.4797 0.0496 0.0195 0.640 6.726 5.972 477.479 0.760 26.563 5.673 0.43 232481. 0.4519
|
|
21.04 0.2057 0.5076 0.0473 0.0192 0.629 6.609 5.692 469.125 0.747 25.316 5.503 0.43 232657. 0.4280
|
|
22.79 0.2229 0.5329 0.0449 0.0188 0.616 6.474 5.404 459.568 0.731 24.035 5.333 0.43 232842. 0.4041
|
|
24.55 0.2400 0.5556 0.0424 0.0183 0.602 6.322 5.108 448.752 0.714 22.721 5.163 0.43 233034. 0.3804
|
|
26.30 0.2572 0.5756 0.0399 0.0178 0.586 6.151 4.806 436.624 0.695 21.375 4.992 0.43 233234. 0.3567
|
|
28.05 0.2743 0.5927 0.0373 0.0173 0.567 5.961 4.496 423.131 0.673 19.999 4.820 0.43 233442. 0.3331
|
|
29.81 0.2914 0.6068 0.0347 0.0167 0.547 5.751 4.180 408.224 0.650 18.592 4.644 0.43 233659. 0.3095
|
|
31.56 0.3086 0.6177 0.0320 0.0160 0.525 5.520 3.857 391.856 0.624 17.156 4.464 0.43 233884. 0.2858
|
|
33.31 0.3257 0.6249 0.0293 0.0153 0.502 5.268 3.528 373.981 0.595 15.693 4.279 0.43 234117. 0.2620
|
|
35.07 0.3429 0.6280 0.0265 0.0145 0.475 4.995 3.193 354.561 0.564 14.203 4.085 0.43 234360. 0.2379
|
|
36.82 0.3600 0.6262 0.0237 0.0136 0.447 4.699 2.853 333.558 0.531 12.690 3.879 0.43 234611. 0.2136
|
|
38.57 0.3772 0.6185 0.0208 0.0127 0.417 4.380 2.507 310.942 0.495 11.153 3.658 0.43 234871. 0.1888
|
|
40.33 0.3943 0.6034 0.0179 0.0117 0.384 4.039 2.157 286.692 0.456 9.596 3.413 0.43 235140. 0.1634
|
|
42.08 0.4114 0.5786 0.0150 0.0106 0.350 3.674 1.803 260.790 0.415 8.021 3.136 0.43 235418. 0.1373
|
|
43.83 0.4286 0.5402 0.0120 0.0095 0.313 3.286 1.446 233.231 0.371 6.430 2.811 0.43 235705. 0.1102
|
|
45.59 0.4457 0.4821 0.0090 0.0083 0.274 2.874 1.085 204.017 0.325 4.827 2.412 0.43 236001. 0.0819
|
|
47.34 0.4629 0.3927 0.0060 0.0071 0.232 2.439 0.722 173.158 0.276 3.213 1.892 0.43 236306. 0.0524
|
|
49.09 0.4800 0.2484 0.0030 0.0057 0.189 1.981 0.358 140.648 0.224 1.592 1.154 0.43 236617. 0.0225
|
|
50.85 0.4972 -0.0222 -0.0002 0.0043 0.141 1.479 -0.023 104.984 0.167 -0.103 -0.100 0.43 236823. 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 0.0716 0.0206 1.077 9.696 11.741 803.019 1.095 52.223 6.632 0.50 269474. 0.7407
|
|
2.07 0.0173 0.0585 0.0700 0.0207 1.079 9.720 11.476 804.954 1.098 51.047 6.467 0.50 269598. 0.7141
|
|
4.13 0.0346 0.1141 0.0683 0.0207 1.081 9.731 11.200 805.894 1.099 49.817 6.303 0.50 269729. 0.6877
|
|
6.20 0.0519 0.1668 0.0666 0.0207 1.081 9.729 10.912 805.741 1.099 48.534 6.142 0.50 269866. 0.6614
|
|
8.26 0.0692 0.2167 0.0647 0.0207 1.079 9.713 10.611 804.406 1.097 47.200 5.983 0.50 270011. 0.6354
|
|
10.33 0.0865 0.2638 0.0628 0.0206 1.075 9.682 10.300 801.808 1.094 45.813 5.826 0.50 270163. 0.6095
|
|
12.39 0.1039 0.3081 0.0609 0.0205 1.070 9.634 9.976 797.853 1.088 44.374 5.671 0.50 270322. 0.5839
|
|
14.46 0.1212 0.3497 0.0588 0.0204 1.063 9.569 9.641 792.455 1.081 42.884 5.518 0.50 270490. 0.5585
|
|
16.52 0.1385 0.3887 0.0567 0.0202 1.053 9.485 9.295 785.524 1.072 41.343 5.367 0.50 270665. 0.5334
|
|
18.59 0.1558 0.4251 0.0545 0.0200 1.042 9.382 8.937 776.968 1.060 39.752 5.217 0.50 270849. 0.5084
|
|
20.65 0.1731 0.4589 0.0523 0.0197 1.028 9.258 8.568 766.698 1.046 38.110 5.069 0.50 271041. 0.4836
|
|
22.72 0.1904 0.4901 0.0499 0.0194 1.012 9.112 8.188 754.621 1.029 36.420 4.921 0.50 271242. 0.4591
|
|
24.78 0.2077 0.5188 0.0476 0.0190 0.993 8.943 7.797 740.645 1.010 34.682 4.775 0.50 271452. 0.4346
|
|
26.85 0.2250 0.5448 0.0451 0.0186 0.972 8.750 7.396 724.680 0.989 32.896 4.629 0.50 271670. 0.4104
|
|
28.91 0.2423 0.5682 0.0426 0.0182 0.948 8.532 6.984 706.635 0.964 31.065 4.483 0.50 271899. 0.3862
|
|
30.98 0.2596 0.5889 0.0400 0.0176 0.921 8.288 6.562 686.424 0.936 29.188 4.336 0.50 272136. 0.3621
|
|
33.04 0.2769 0.6067 0.0374 0.0171 0.890 8.017 6.131 663.959 0.906 27.269 4.188 0.50 272384. 0.3380
|
|
35.11 0.2942 0.6214 0.0347 0.0164 0.857 7.718 5.690 639.160 0.872 25.307 4.038 0.50 272641. 0.3139
|
|
37.17 0.3116 0.6329 0.0320 0.0157 0.821 7.389 5.240 611.949 0.835 23.306 3.884 0.50 272908. 0.2898
|
|
39.24 0.3289 0.6407 0.0292 0.0150 0.781 7.030 4.781 582.254 0.794 21.266 3.724 0.50 273186. 0.2655
|
|
41.30 0.3462 0.6442 0.0263 0.0141 0.738 6.641 4.314 550.009 0.750 19.189 3.558 0.50 273473. 0.2409
|
|
43.37 0.3635 0.6428 0.0234 0.0132 0.691 6.220 3.840 515.158 0.703 17.079 3.381 0.50 273772. 0.2160
|
|
45.44 0.3808 0.6352 0.0205 0.0123 0.641 5.767 3.358 477.652 0.652 14.938 3.189 0.50 274080. 0.1905
|
|
47.50 0.3981 0.6198 0.0175 0.0112 0.587 5.282 2.871 437.457 0.597 12.768 2.976 0.50 274400. 0.1644
|
|
49.57 0.4154 0.5938 0.0145 0.0101 0.529 4.764 2.377 394.548 0.538 10.573 2.733 0.50 274730. 0.1373
|
|
51.63 0.4327 0.5528 0.0115 0.0090 0.468 4.213 1.879 348.918 0.476 8.357 2.442 0.50 275071. 0.1091
|
|
53.70 0.4500 0.4890 0.0084 0.0077 0.403 3.629 1.377 300.577 0.410 6.124 2.077 0.50 275423. 0.0795
|
|
55.76 0.4673 0.3873 0.0053 0.0064 0.335 3.013 0.872 249.541 0.340 3.877 1.584 0.51 275784. 0.0482
|
|
57.83 0.4846 0.2138 0.0022 0.0050 0.263 2.364 0.364 195.760 0.267 1.619 0.843 0.51 276151. 0.0166
|
|
59.89 0.5019
|
|
|
|
|
|
|
|
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 0.0727 0.0208 1.618 12.749 15.555 1206.733 1.440 69.190 5.847 0.57 307948. 0.7517
|
|
2.34 0.0172 0.0586 0.0710 0.0208 1.622 12.778 15.208 1209.450 1.444 67.646 5.703 0.57 308089. 0.7250
|
|
4.68 0.0343 0.1142 0.0693 0.0209 1.624 12.791 14.845 1210.658 1.445 66.032 5.562 0.57 308238. 0.6986
|
|
7.03 0.0515 0.1670 0.0676 0.0208 1.623 12.786 14.467 1210.221 1.445 64.349 5.422 0.57 308395. 0.6723
|
|
9.37 0.0687 0.2170 0.0657 0.0208 1.620 12.763 14.073 1208.008 1.442 62.598 5.284 0.57 308560. 0.6462
|
|
11.71 0.0859 0.2643 0.0638 0.0207 1.614 12.719 13.664 1203.891 1.437 60.779 5.148 0.57 308733. 0.6203
|
|
14.05 0.1030 0.3088 0.0618 0.0206 1.606 12.654 13.240 1197.738 1.430 58.892 5.014 0.57 308915. 0.5947
|
|
16.39 0.1202 0.3508 0.0598 0.0205 1.595 12.567 12.801 1189.423 1.420 56.938 4.881 0.57 309105. 0.5693
|
|
18.73 0.1374 0.3902 0.0577 0.0203 1.581 12.455 12.347 1178.816 1.407 54.918 4.751 0.57 309305. 0.5441
|
|
21.08 0.1546 0.4270 0.0555 0.0201 1.563 12.317 11.878 1165.780 1.392 52.831 4.621 0.57 309514. 0.5192
|
|
23.42 0.1717 0.4613 0.0532 0.0198 1.542 12.152 11.394 1150.188 1.373 50.680 4.493 0.57 309732. 0.4944
|
|
25.76 0.1889 0.4931 0.0509 0.0195 1.518 11.959 10.896 1131.901 1.351 48.465 4.366 0.57 309960. 0.4698
|
|
28.10 0.2061 0.5223 0.0485 0.0191 1.490 11.736 10.384 1110.786 1.326 46.187 4.240 0.57 310198. 0.4454
|
|
30.44 0.2232 0.5491 0.0460 0.0187 1.457 11.481 9.858 1086.712 1.297 43.848 4.114 0.57 310446. 0.4211
|
|
32.78 0.2404 0.5733 0.0435 0.0183 1.421 11.194 9.319 1059.544 1.265 41.449 3.989 0.57 310705. 0.3970
|
|
35.13 0.2576 0.5949 0.0409 0.0177 1.380 10.873 8.766 1029.156 1.228 38.991 3.863 0.57 310974. 0.3729
|
|
37.47 0.2748 0.6138 0.0383 0.0171 1.335 10.517 8.201 995.422 1.188 36.476 3.737 0.57 311254. 0.3488
|
|
39.81 0.2919 0.6297 0.0356 0.0165 1.285 10.124 7.623 958.219 1.144 33.907 3.608 0.57 311545. 0.3248
|
|
42.15 0.3091 0.6426 0.0328 0.0158 1.230 9.693 7.033 917.434 1.095 31.284 3.477 0.57 311847. 0.3006
|
|
44.49 0.3263 0.6519 0.0300 0.0150 1.171 9.223 6.432 872.960 1.042 28.611 3.342 0.57 312160. 0.2763
|
|
46.83 0.3435 0.6573 0.0272 0.0142 1.106 8.713 5.821 824.699 0.984 25.891 3.201 0.57 312486. 0.2518
|
|
49.18 0.3606 0.6580 0.0243 0.0133 1.036 8.162 5.199 772.566 0.922 23.125 3.052 0.57 312822. 0.2269
|
|
51.52 0.3778 0.6531 0.0213 0.0123 0.961 7.570 4.568 716.486 0.855 20.318 2.892 0.58 313171. 0.2015
|
|
53.86 0.3950 0.6409 0.0183 0.0113 0.880 6.935 3.928 656.404 0.784 17.473 2.714 0.58 313531. 0.1754
|
|
56.20 0.4121 0.6191 0.0153 0.0102 0.794 6.258 3.281 592.284 0.707 14.595 2.513 0.58 313904. 0.1484
|
|
58.54 0.4293 0.5836 0.0123 0.0090 0.703 5.537 2.627 524.108 0.626 11.687 2.274 0.58 314289. 0.1201
|
|
60.89 0.4465 0.5273 0.0092 0.0078 0.606 4.774 1.968 451.888 0.539 8.755 1.976 0.58 314685. 0.0904
|
|
63.23 0.4637 0.4368 0.0061 0.0065 0.504 3.969 1.305 375.647 0.448 5.805 1.576 0.58 315093. 0.0587
|
|
65.57 0.4808 0.2819 0.0030 0.0051 0.396 3.121 0.639 295.368 0.353 2.840 0.981 0.58 315509. 0.0255
|
|
67.91 0.4980
|
|
|
|
|
|
|
|
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 0.0739 0.0211 2.335 16.352 20.027 1741.166 1.847 89.079 5.217 0.64 346409. 0.7610
|
|
2.63 0.0172 0.0588 0.0723 0.0211 2.340 16.385 19.581 1744.716 1.851 87.095 5.090 0.64 346569. 0.7343
|
|
5.27 0.0343 0.1146 0.0705 0.0211 2.341 16.398 19.114 1746.049 1.853 85.020 4.965 0.64 346739. 0.7076
|
|
7.90 0.0515 0.1677 0.0687 0.0211 2.340 16.388 18.628 1744.963 1.851 82.857 4.842 0.64 346917. 0.6812
|
|
10.53 0.0687 0.2180 0.0669 0.0211 2.335 16.353 18.122 1741.269 1.848 80.606 4.720 0.64 347104. 0.6550
|
|
13.17 0.0858 0.2656 0.0649 0.0210 2.326 16.292 17.596 1734.787 1.841 78.267 4.601 0.64 347300. 0.6291
|
|
15.80 0.1030 0.3105 0.0629 0.0209 2.314 16.203 17.050 1725.331 1.831 75.841 4.482 0.64 347506. 0.6033
|
|
18.43 0.1202 0.3528 0.0608 0.0207 2.297 16.085 16.486 1712.719 1.817 73.328 4.366 0.64 347722. 0.5778
|
|
21.07 0.1373 0.3926 0.0587 0.0205 2.275 15.935 15.902 1696.764 1.800 70.730 4.251 0.64 347948. 0.5526
|
|
23.70 0.1545 0.4298 0.0565 0.0203 2.249 15.752 15.298 1677.277 1.780 68.047 4.137 0.64 348185. 0.5275
|
|
26.33 0.1717 0.4646 0.0542 0.0200 2.218 15.534 14.677 1654.070 1.755 65.281 4.025 0.64 348431. 0.5026
|
|
28.97 0.1888 0.4969 0.0518 0.0197 2.182 15.279 14.036 1626.953 1.726 62.433 3.913 0.64 348689. 0.4779
|
|
31.60 0.2060 0.5268 0.0494 0.0193 2.140 14.986 13.378 1595.729 1.693 59.504 3.802 0.64 348958. 0.4534
|
|
34.23 0.2232 0.5542 0.0469 0.0189 2.092 14.653 12.702 1560.219 1.655 56.496 3.692 0.64 349239. 0.4290
|
|
36.87 0.2403 0.5790 0.0443 0.0184 2.039 14.277 12.008 1520.228 1.613 53.411 3.583 0.64 349531. 0.4047
|
|
39.50 0.2575 0.6014 0.0417 0.0179 1.979 13.858 11.297 1475.576 1.566 50.251 3.473 0.64 349834. 0.3805
|
|
42.13 0.2747 0.6210 0.0390 0.0173 1.912 13.393 10.570 1426.081 1.513 47.017 3.362 0.65 350150. 0.3563
|
|
44.77 0.2918 0.6378 0.0363 0.0166 1.839 12.881 9.828 1371.572 1.455 43.713 3.250 0.65 350478. 0.3321
|
|
47.40 0.3090 0.6516 0.0335 0.0159 1.759 12.320 9.069 1311.885 1.392 40.341 3.136 0.65 350819. 0.3078
|
|
50.03 0.3261 0.6620 0.0306 0.0151 1.672 11.710 8.297 1246.865 1.323 36.904 3.018 0.65 351173. 0.2834
|
|
52.67 0.3433 0.6686 0.0277 0.0142 1.578 11.048 7.510 1176.376 1.248 33.405 2.896 0.65 351539. 0.2587
|
|
55.30 0.3605 0.6706 0.0248 0.0133 1.476 10.333 6.710 1100.291 1.167 29.848 2.766 0.65 351918. 0.2336
|
|
57.93 0.3776 0.6672 0.0218 0.0123 1.366 9.565 5.899 1018.505 1.081 26.237 2.627 0.65 352311. 0.2080
|
|
60.57 0.3948 0.6566 0.0187 0.0113 1.248 8.743 5.076 930.938 0.988 22.577 2.473 0.65 352717. 0.1816
|
|
63.20 0.4120 0.6366 0.0157 0.0101 1.123 7.866 4.243 837.537 0.889 18.873 2.298 0.65 353136. 0.1543
|
|
65.83 0.4291 0.6032 0.0126 0.0089 0.990 6.933 3.402 738.279 0.783 15.131 2.090 0.65 353569. 0.1256
|
|
68.47 0.4463 0.5490 0.0094 0.0077 0.849 5.946 2.553 633.177 0.672 11.357 1.829 0.65 354015. 0.0953
|
|
71.10 0.4635 0.4601 0.0063 0.0063 0.700 4.905 1.700 522.270 0.554 7.560 1.476 0.65 354474. 0.0627
|
|
73.73 0.4806 0.3042 0.0031 0.0049 0.544 3.809 0.841 405.536 0.430 3.743 0.941 0.65 354942. 0.0281
|
|
76.37 0.4978
|
|
|
|
|
|
|
|
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 0.0754 0.0215 3.269 20.607 25.236 2438.006 2.328 112.252 4.695 0.71 384854. 0.7689
|
|
2.92 0.0171 0.0587 0.0738 0.0215 3.275 20.642 24.676 2442.188 2.332 109.760 4.583 0.71 385034. 0.7421
|
|
5.85 0.0343 0.1146 0.0720 0.0215 3.276 20.651 24.090 2443.218 2.333 107.152 4.472 0.71 385224. 0.7155
|
|
8.77 0.0514 0.1677 0.0702 0.0215 3.273 20.630 23.479 2440.824 2.331 104.434 4.363 0.71 385424. 0.6891
|
|
11.69 0.0686 0.2181 0.0683 0.0215 3.265 20.579 22.842 2434.730 2.325 101.603 4.255 0.71 385634. 0.6630
|
|
14.62 0.0857 0.2659 0.0663 0.0214 3.252 20.494 22.181 2424.695 2.315 98.662 4.149 0.71 385855. 0.6370
|
|
17.54 0.1029 0.3110 0.0643 0.0213 3.232 20.374 21.495 2410.464 2.302 95.611 4.045 0.71 386086. 0.6113
|
|
20.46 0.1200 0.3536 0.0621 0.0211 3.207 20.216 20.785 2391.786 2.284 92.452 3.942 0.71 386327. 0.5858
|
|
23.38 0.1372 0.3936 0.0599 0.0209 3.176 20.018 20.050 2368.409 2.262 89.184 3.840 0.71 386580. 0.5605
|
|
26.31 0.1543 0.4313 0.0577 0.0206 3.138 19.779 19.292 2340.073 2.235 85.811 3.739 0.71 386845. 0.5354
|
|
29.23 0.1715 0.4664 0.0553 0.0203 3.093 19.495 18.510 2306.522 2.203 82.332 3.640 0.72 387121. 0.5105
|
|
32.15 0.1886 0.4992 0.0529 0.0200 3.041 19.165 17.705 2267.492 2.165 78.750 3.541 0.72 387409. 0.4858
|
|
35.08 0.2058 0.5296 0.0504 0.0196 2.981 18.787 16.877 2222.727 2.123 75.067 3.444 0.72 387709. 0.4612
|
|
38.00 0.2229 0.5575 0.0479 0.0192 2.913 18.358 16.026 2171.963 2.074 71.285 3.347 0.72 388022. 0.4368
|
|
40.92 0.2401 0.5830 0.0453 0.0187 2.836 17.876 15.154 2114.947 2.020 67.405 3.250 0.72 388348. 0.4124
|
|
43.85 0.2572 0.6061 0.0426 0.0181 2.751 17.339 14.261 2051.421 1.959 63.431 3.153 0.72 388687. 0.3881
|
|
46.77 0.2744 0.6265 0.0399 0.0175 2.657 16.745 13.346 1981.146 1.892 59.365 3.056 0.72 389039. 0.3639
|
|
49.69 0.2915 0.6442 0.0371 0.0168 2.553 16.092 12.412 1903.882 1.818 55.209 2.957 0.72 389404. 0.3396
|
|
52.61 0.3087 0.6589 0.0343 0.0160 2.440 15.378 11.459 1819.406 1.737 50.968 2.857 0.72 389784. 0.3152
|
|
55.54 0.3258 0.6704 0.0313 0.0152 2.317 14.601 10.487 1727.503 1.650 46.645 2.753 0.72 390177. 0.2907
|
|
58.46 0.3430 0.6781 0.0284 0.0144 2.183 13.760 9.497 1627.988 1.555 42.244 2.646 0.72 390585. 0.2658
|
|
61.38 0.3601 0.6815 0.0254 0.0134 2.039 12.853 8.491 1520.704 1.452 37.769 2.533 0.72 391006. 0.2406
|
|
64.31 0.3773 0.6796 0.0223 0.0124 1.885 11.880 7.470 1405.531 1.342 33.225 2.411 0.72 391443. 0.2148
|
|
67.23 0.3944 0.6707 0.0192 0.0113 1.720 10.839 6.434 1282.380 1.225 28.619 2.276 0.72 391894. 0.1882
|
|
70.15 0.4116 0.6526 0.0161 0.0102 1.544 9.730 5.386 1151.225 1.099 23.957 2.122 0.72 392360. 0.1605
|
|
73.08 0.4287 0.6212 0.0129 0.0089 1.357 8.554 4.327 1012.085 0.966 19.245 1.939 0.72 392840. 0.1315
|
|
76.00 0.4459 0.5692 0.0097 0.0076 1.160 7.312 3.258 865.049 0.826 14.493 1.708 0.72 393336. 0.1005
|
|
78.92 0.4630 0.4823 0.0065 0.0063 0.952 6.003 2.183 710.261 0.678 9.710 1.394 0.72 393845. 0.0671
|
|
81.85 0.4802 0.3273 0.0033 0.0048 0.735 4.630 1.102 547.805 0.523 4.900 0.912 0.72 394364. 0.0312
|
|
84.77 0.4973 -0.0175 -0.0001 0.0033 0.494 3.116 -0.038 368.603 0.352 -0.170 -0.047 0.72 394648. 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 0.0773 0.0223 4.512 25.852 31.301 3364.406 2.921 139.225 4.220 0.79 423277. 0.7696
|
|
3.22 0.0172 0.0582 0.0756 0.0223 4.512 25.853 30.608 3364.535 2.921 136.143 4.126 0.79 423478. 0.7441
|
|
6.43 0.0343 0.1138 0.0738 0.0223 4.507 25.824 29.882 3360.755 2.918 132.917 4.033 0.79 423691. 0.7187
|
|
9.65 0.0515 0.1667 0.0720 0.0222 4.496 25.761 29.126 3352.672 2.911 129.551 3.940 0.79 423914. 0.6932
|
|
12.87 0.0686 0.2171 0.0700 0.0221 4.479 25.663 28.338 3339.907 2.899 126.046 3.848 0.79 424148. 0.6678
|
|
16.09 0.0858 0.2649 0.0680 0.0220 4.455 25.527 27.518 3322.110 2.884 122.402 3.757 0.79 424394. 0.6425
|
|
19.30 0.1029 0.3103 0.0659 0.0219 4.424 25.348 26.668 3298.914 2.864 118.620 3.667 0.79 424651. 0.6172
|
|
22.52 0.1201 0.3531 0.0637 0.0217 4.385 25.126 25.788 3269.954 2.839 114.703 3.577 0.79 424921. 0.5921
|
|
25.74 0.1373 0.3935 0.0615 0.0214 4.338 24.856 24.877 3234.856 2.808 110.652 3.488 0.79 425202. 0.5671
|
|
28.95 0.1544 0.4315 0.0591 0.0212 4.282 24.536 23.936 3193.244 2.772 106.469 3.400 0.79 425496. 0.5422
|
|
32.17 0.1716 0.4672 0.0567 0.0208 4.217 24.164 22.967 3144.724 2.730 102.155 3.313 0.79 425803. 0.5175
|
|
35.39 0.1887 0.5004 0.0543 0.0205 4.142 23.735 21.968 3088.911 2.682 97.714 3.226 0.79 426123. 0.4929
|
|
38.60 0.2059 0.5313 0.0517 0.0200 4.057 23.247 20.941 3025.425 2.626 93.146 3.139 0.79 426456. 0.4683
|
|
41.82 0.2230 0.5598 0.0491 0.0196 3.961 22.698 19.887 2953.946 2.564 88.456 3.054 0.79 426803. 0.4439
|
|
45.04 0.2402 0.5860 0.0465 0.0190 3.854 22.084 18.805 2874.077 2.495 83.644 2.968 0.79 427165. 0.4195
|
|
48.26 0.2574 0.6096 0.0437 0.0185 3.735 21.403 17.697 2785.501 2.418 78.715 2.882 0.79 427540. 0.3952
|
|
51.47 0.2745 0.6307 0.0409 0.0178 3.605 20.654 16.563 2687.954 2.333 73.671 2.795 0.79 427930. 0.3708
|
|
54.69 0.2917 0.6490 0.0381 0.0171 3.461 19.833 15.404 2581.171 2.241 68.517 2.707 0.79 428334. 0.3463
|
|
57.91 0.3088 0.6643 0.0351 0.0163 3.306 18.940 14.221 2464.929 2.140 63.255 2.617 0.79 428754. 0.3217
|
|
61.12 0.3260 0.6763 0.0322 0.0155 3.137 17.973 13.015 2339.090 2.031 57.891 2.524 0.79 429189. 0.2968
|
|
64.34 0.3431 0.6844 0.0291 0.0146 2.955 16.932 11.787 2203.519 1.913 52.429 2.426 0.79 429639. 0.2715
|
|
67.56 0.3603 0.6878 0.0260 0.0136 2.760 15.815 10.538 2058.166 1.787 46.875 2.322 0.79 430105. 0.2458
|
|
70.77 0.3775 0.6855 0.0229 0.0126 2.552 14.623 9.270 1903.052 1.652 41.234 2.209 0.79 430587. 0.2193
|
|
73.99 0.3946 0.6758 0.0197 0.0115 2.331 13.357 7.984 1738.262 1.509 35.514 2.083 0.79 431085. 0.1919
|
|
77.21 0.4118 0.6559 0.0165 0.0104 2.097 12.017 6.682 1563.978 1.358 29.721 1.938 0.79 431599. 0.1633
|
|
80.43 0.4289 0.6216 0.0133 0.0091 1.851 10.607 5.366 1380.484 1.198 23.866 1.763 0.79 432129. 0.1331
|
|
83.64 0.4461 0.5651 0.0100 0.0079 1.593 9.130 4.037 1188.159 1.031 17.958 1.541 0.79 432675. 0.1009
|
|
86.86 0.4632 0.4722 0.0067 0.0065 1.324 7.588 2.700 987.472 0.857 12.008 1.240 0.79 433236. 0.0664
|
|
90.08 0.4804 0.3114 0.0033 0.0052 1.044 5.984 1.354 778.784 0.676 6.023 0.789 0.79 433808. 0.0299
|
|
93.29 0.4976
|
|
|
|
|
|
|
|
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 0.0796 0.0245 6.432 33.783 38.360 4796.269 3.817 170.627 3.628 0.86 461668. 0.7324
|
|
3.51 0.0172 0.0550 0.0779 0.0243 6.397 33.599 37.516 4770.193 3.796 166.872 3.567 0.86 461893. 0.7122
|
|
7.03 0.0344 0.1080 0.0760 0.0242 6.356 33.383 36.632 4739.584 3.772 162.938 3.506 0.86 462129. 0.6916
|
|
10.54 0.0516 0.1592 0.0741 0.0240 6.308 33.133 35.708 4704.070 3.743 158.831 3.443 0.86 462377. 0.6707
|
|
14.06 0.0687 0.2083 0.0721 0.0238 6.254 32.846 34.746 4663.264 3.711 154.551 3.380 0.86 462638. 0.6494
|
|
17.57 0.0859 0.2554 0.0700 0.0236 6.191 32.518 33.745 4616.764 3.674 150.098 3.315 0.86 462910. 0.6278
|
|
21.09 0.1031 0.3005 0.0679 0.0233 6.121 32.148 32.706 4564.143 3.632 145.475 3.250 0.86 463196. 0.6059
|
|
24.60 0.1203 0.3435 0.0657 0.0230 6.041 31.731 31.629 4504.958 3.585 140.684 3.184 0.86 463494. 0.5838
|
|
28.12 0.1375 0.3844 0.0633 0.0227 5.952 31.264 30.514 4438.743 3.532 135.726 3.118 0.86 463806. 0.5615
|
|
31.63 0.1547 0.4231 0.0610 0.0223 5.854 30.745 29.362 4365.061 3.474 130.603 3.051 0.86 464132. 0.5389
|
|
35.15 0.1718 0.4597 0.0585 0.0219 5.744 30.171 28.174 4283.454 3.409 125.319 2.983 0.86 464471. 0.5162
|
|
38.66 0.1890 0.4941 0.0559 0.0214 5.624 29.537 26.951 4193.453 3.337 119.877 2.915 0.86 464825. 0.4933
|
|
42.18 0.2062 0.5262 0.0533 0.0209 5.491 28.840 25.692 4094.560 3.258 114.280 2.846 0.86 465194. 0.4703
|
|
45.69 0.2234 0.5561 0.0506 0.0203 5.346 28.079 24.400 3986.503 3.172 108.531 2.776 0.86 465577. 0.4470
|
|
49.21 0.2406 0.5832 0.0479 0.0198 5.191 27.267 23.074 3871.142 3.081 102.632 2.703 0.86 465975. 0.4233
|
|
52.72 0.2578 0.6074 0.0451 0.0191 5.026 26.398 21.715 3747.794 2.982 96.588 2.628 0.86 466389. 0.3992
|
|
56.24 0.2749 0.6283 0.0422 0.0185 4.851 25.479 20.324 3617.301 2.879 90.402 2.548 0.86 466819. 0.3745
|
|
59.75 0.2921 0.6455 0.0392 0.0178 4.666 24.508 18.902 3479.444 2.769 84.078 2.464 0.86 467264. 0.3492
|
|
63.27 0.3093 0.6590 0.0362 0.0170 4.467 23.462 17.451 3331.051 2.651 77.621 2.376 0.86 467726. 0.3236
|
|
66.78 0.3265 0.6685 0.0332 0.0162 4.254 22.345 15.971 3172.385 2.525 71.037 2.283 0.86 468204. 0.2975
|
|
70.30 0.3437 0.6730 0.0300 0.0153 4.028 21.158 14.463 3003.871 2.390 64.332 2.184 0.86 468699. 0.2707
|
|
73.81 0.3609 0.6716 0.0268 0.0144 3.789 19.902 12.930 2825.517 2.248 57.513 2.076 0.86 469211. 0.2433
|
|
77.33 0.3780 0.6629 0.0236 0.0135 3.537 18.579 11.373 2637.804 2.099 50.586 1.956 0.86 469740. 0.2150
|
|
80.84 0.3952 0.6448 0.0203 0.0125 3.274 17.196 9.793 2441.350 1.943 43.561 1.819 0.86 470286. 0.1856
|
|
84.35 0.4124 0.6145 0.0170 0.0114 2.999 15.754 8.194 2236.677 1.780 36.446 1.662 0.86 470849. 0.1550
|
|
87.87 0.4296 0.5676 0.0137 0.0103 2.715 14.260 6.577 2024.578 1.611 29.255 1.473 0.86 471430. 0.1232
|
|
91.38 0.4468 0.4976 0.0103 0.0092 2.422 12.720 4.946 1805.944 1.437 21.998 1.242 0.87 472029. 0.0900
|
|
94.90 0.4640 0.3940 0.0069 0.0081 2.121 11.141 3.303 1581.704 1.259 14.690 0.947 0.87 472644. 0.0561
|
|
98.41 0.4811 0.2388 0.0034 0.0069 1.814 9.526 1.650 1352.480 1.076 7.341 0.553 0.87 473271. 0.0232
|
|
101.93 0.4983 -0.0150 -0.0002 0.0056 1.471 7.726 -0.081 1096.931 0.873 -0.361 -0.034 0.87 473675. 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 0.0819 0.0296 9.877 47.888 46.330 7365.388 5.410 206.077 2.853 0.93 500037. 0.6330
|
|
3.84 0.0173 0.0476 0.0802 0.0292 9.761 47.324 45.338 7278.659 5.347 201.661 2.825 0.93 500285. 0.6201
|
|
7.69 0.0347 0.0942 0.0783 0.0288 9.634 46.708 44.292 7184.005 5.277 197.012 2.796 0.93 500547. 0.6067
|
|
11.53 0.0520 0.1398 0.0764 0.0284 9.496 46.042 43.196 7081.486 5.202 192.136 2.767 0.93 500822. 0.5928
|
|
15.37 0.0694 0.1844 0.0744 0.0280 9.348 45.324 42.049 6971.010 5.121 187.033 2.736 0.93 501111. 0.5783
|
|
19.21 0.0867 0.2278 0.0723 0.0275 9.189 44.553 40.851 6852.447 5.034 181.706 2.704 0.93 501413. 0.5634
|
|
23.06 0.1040 0.2700 0.0700 0.0270 9.019 43.728 39.604 6725.624 4.940 176.157 2.671 0.93 501730. 0.5479
|
|
26.90 0.1214 0.3109 0.0678 0.0265 8.838 42.848 38.307 6590.270 4.841 170.389 2.636 0.93 502062. 0.5319
|
|
30.74 0.1387 0.3505 0.0654 0.0259 8.644 41.911 36.962 6446.128 4.735 164.405 2.601 0.93 502409. 0.5154
|
|
34.58 0.1561 0.3887 0.0629 0.0253 8.439 40.915 35.569 6292.998 4.623 158.210 2.564 0.93 502771. 0.4984
|
|
38.43 0.1734 0.4254 0.0604 0.0246 8.221 39.860 34.129 6130.678 4.503 151.808 2.525 0.93 503148. 0.4809
|
|
42.27 0.1908 0.4605 0.0577 0.0239 7.991 38.744 32.645 5958.959 4.377 145.204 2.485 0.93 503541. 0.4628
|
|
46.11 0.2081 0.4938 0.0550 0.0232 7.748 37.564 31.116 5777.525 4.244 138.404 2.443 0.93 503950. 0.4442
|
|
49.96 0.2254 0.5254 0.0523 0.0224 7.491 36.319 29.544 5585.998 4.103 131.412 2.399 0.93 504376. 0.4251
|
|
53.80 0.2428 0.5550 0.0494 0.0216 7.220 35.004 27.930 5383.824 3.955 124.235 2.353 0.93 504818. 0.4054
|
|
57.64 0.2601 0.5817 0.0465 0.0208 6.943 33.662 26.275 5177.376 3.803 116.873 2.302 0.93 505277. 0.3846
|
|
61.48 0.2775 0.6043 0.0435 0.0200 6.668 32.330 24.579 4972.572 3.653 109.329 2.242 0.93 505753. 0.3623
|
|
65.33 0.2948 0.6193 0.0404 0.0192 6.424 31.147 22.841 4790.651 3.519 101.598 2.163 0.93 506247. 0.3369
|
|
69.17 0.3121 0.6262 0.0373 0.0186 6.205 30.082 21.064 4626.756 3.399 93.692 2.065 0.93 506758. 0.3089
|
|
73.01 0.3295 0.6272 0.0341 0.0179 5.976 28.973 19.251 4456.156 3.273 85.629 1.959 0.93 507288. 0.2803
|
|
76.85 0.3468 0.6217 0.0308 0.0172 5.738 27.819 17.405 4278.644 3.143 77.420 1.845 0.93 507835. 0.2509
|
|
80.70 0.3642 0.6082 0.0275 0.0164 5.494 26.637 15.529 4096.875 3.009 69.073 1.719 0.93 508401. 0.2209
|
|
84.54 0.3815 0.5857 0.0241 0.0157 5.244 25.423 13.625 3910.237 2.872 60.602 1.580 0.94 508985. 0.1902
|
|
88.38 0.3989 0.5525 0.0207 0.0149 4.988 24.185 11.695 3719.842 2.732 52.020 1.426 0.94 509589. 0.1590
|
|
92.23 0.4162 0.5066 0.0172 0.0142 4.730 22.934 9.744 3527.391 2.591 43.343 1.253 0.94 510211. 0.1275
|
|
96.07 0.4335 0.4457 0.0138 0.0134 4.470 21.673 7.777 3333.482 2.449 34.591 1.058 0.94 510852. 0.0962
|
|
99.91 0.4509 0.3669 0.0103 0.0126 4.209 20.409 5.798 3138.983 2.306 25.788 0.838 0.94 511512. 0.0658
|
|
103.75 0.4682 0.2671 0.0067 0.0118 3.949 19.145 3.812 2944.545 2.163 16.957 0.587 0.94 512190. 0.0374
|
|
107.60 0.4856 0.1420 0.0032 0.0110 3.687 17.874 1.824 2749.169 2.019 8.114 0.301 0.94 512881. 0.0133
|
|
111.44 0.5029
|
|
|
|
|
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