538 lines
95 KiB
Plaintext
538 lines
95 KiB
Plaintext
17x7E (17x7E.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 0.0735 0.0271 0.003 0.192 0.193 2.275 0.022 0.860 38.529 0.07 26812. 0.5863
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0.31 0.0190 0.0504 0.0720 0.0272 0.003 0.193 0.189 2.285 0.022 0.843 37.615 0.07 26825. 0.5668
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0.61 0.0381 0.0983 0.0705 0.0273 0.003 0.194 0.186 2.293 0.022 0.825 36.696 0.07 26839. 0.5471
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0.92 0.0571 0.1438 0.0689 0.0274 0.003 0.194 0.181 2.299 0.022 0.806 35.776 0.07 26854. 0.5273
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1.22 0.0762 0.1868 0.0672 0.0274 0.003 0.195 0.177 2.302 0.022 0.787 34.854 0.07 26870. 0.5074
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1.53 0.0952 0.2273 0.0655 0.0274 0.003 0.195 0.172 2.302 0.022 0.766 33.930 0.07 26887. 0.4874
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1.83 0.1142 0.2653 0.0636 0.0274 0.003 0.194 0.167 2.299 0.022 0.744 33.003 0.07 26905. 0.4673
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2.14 0.1333 0.3008 0.0616 0.0273 0.003 0.194 0.162 2.293 0.022 0.721 32.073 0.07 26924. 0.4471
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2.45 0.1523 0.3338 0.0596 0.0272 0.003 0.193 0.157 2.283 0.022 0.697 31.138 0.07 26944. 0.4268
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2.75 0.1714 0.3642 0.0574 0.0270 0.003 0.192 0.151 2.269 0.022 0.672 30.198 0.07 26965. 0.4063
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3.06 0.1904 0.3919 0.0552 0.0268 0.003 0.190 0.145 2.251 0.021 0.646 29.249 0.07 26987. 0.3858
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3.36 0.2094 0.4170 0.0528 0.0265 0.003 0.188 0.139 2.228 0.021 0.618 28.290 0.07 27011. 0.3651
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3.67 0.2285 0.4392 0.0504 0.0262 0.003 0.186 0.133 2.201 0.021 0.590 27.318 0.07 27035. 0.3443
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3.97 0.2475 0.4586 0.0478 0.0258 0.003 0.183 0.126 2.168 0.021 0.560 26.329 0.07 27061. 0.3233
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4.28 0.2666 0.4749 0.0452 0.0254 0.003 0.180 0.119 2.131 0.020 0.529 25.319 0.07 27088. 0.3023
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4.58 0.2856 0.4880 0.0425 0.0249 0.003 0.177 0.112 2.089 0.020 0.498 24.283 0.07 27116. 0.2811
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4.89 0.3047 0.4977 0.0397 0.0243 0.003 0.173 0.105 2.043 0.020 0.465 23.215 0.07 27146. 0.2599
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5.20 0.3237 0.5036 0.0369 0.0237 0.003 0.168 0.097 1.991 0.019 0.432 22.109 0.07 27177. 0.2384
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5.50 0.3427 0.5055 0.0340 0.0230 0.003 0.164 0.089 1.935 0.018 0.398 20.958 0.07 27209. 0.2169
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5.81 0.3618 0.5028 0.0310 0.0223 0.003 0.158 0.082 1.874 0.018 0.363 19.750 0.07 27242. 0.1953
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6.11 0.3808 0.4951 0.0280 0.0215 0.002 0.153 0.074 1.808 0.017 0.328 18.476 0.07 27277. 0.1736
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6.42 0.3999 0.4818 0.0249 0.0207 0.002 0.147 0.066 1.737 0.017 0.292 17.122 0.07 27313. 0.1518
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6.72 0.4189 0.4619 0.0218 0.0198 0.002 0.140 0.057 1.662 0.016 0.255 15.669 0.07 27351. 0.1300
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7.03 0.4379 0.4344 0.0187 0.0188 0.002 0.134 0.049 1.582 0.015 0.219 14.098 0.07 27389. 0.1082
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7.34 0.4570 0.3981 0.0155 0.0178 0.002 0.127 0.041 1.498 0.014 0.182 12.380 0.07 27430. 0.0866
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7.64 0.4760 0.3511 0.0124 0.0168 0.002 0.119 0.033 1.409 0.013 0.145 10.481 0.07 27471. 0.0655
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7.95 0.4951 0.2911 0.0092 0.0157 0.002 0.111 0.024 1.317 0.013 0.108 8.356 0.07 27514. 0.0451
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8.25 0.5141 0.2150 0.0061 0.0145 0.002 0.103 0.016 1.221 0.012 0.071 5.944 0.07 27558. 0.0260
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8.56 0.5331 0.1187 0.0030 0.0134 0.002 0.095 0.008 1.122 0.011 0.035 3.163 0.07 27604. 0.0097
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8.86 0.5522 -0.0046 -0.0001 0.0121 0.001 0.086 0.000 1.019 0.010 -0.001 -0.118 0.07 27650. 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 0.0737 0.0246 0.022 0.697 0.776 16.495 0.079 3.451 21.335 0.13 53623. 0.6505
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0.61 0.0191 0.0559 0.0723 0.0247 0.022 0.701 0.761 16.590 0.079 3.384 20.801 0.13 53649. 0.6281
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1.23 0.0382 0.1089 0.0708 0.0248 0.022 0.704 0.745 16.670 0.080 3.313 20.268 0.13 53677. 0.6055
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1.84 0.0573 0.1591 0.0692 0.0249 0.022 0.707 0.728 16.730 0.080 3.238 19.738 0.13 53707. 0.5830
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2.45 0.0764 0.2065 0.0675 0.0250 0.022 0.709 0.710 16.769 0.080 3.159 19.211 0.13 53739. 0.5605
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3.06 0.0955 0.2511 0.0657 0.0250 0.023 0.709 0.692 16.785 0.080 3.076 18.687 0.13 53773. 0.5379
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3.68 0.1146 0.2929 0.0638 0.0250 0.022 0.709 0.672 16.774 0.080 2.988 18.166 0.13 53809. 0.5154
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4.29 0.1337 0.3320 0.0619 0.0249 0.022 0.707 0.651 16.735 0.080 2.896 17.648 0.13 53848. 0.4930
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4.90 0.1527 0.3683 0.0598 0.0248 0.022 0.704 0.629 16.665 0.080 2.800 17.132 0.13 53888. 0.4705
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5.52 0.1718 0.4019 0.0577 0.0247 0.022 0.700 0.607 16.561 0.079 2.699 16.617 0.13 53930. 0.4481
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6.13 0.1909 0.4327 0.0554 0.0244 0.022 0.694 0.583 16.419 0.078 2.593 16.103 0.13 53975. 0.4256
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6.74 0.2100 0.4608 0.0530 0.0242 0.022 0.686 0.558 16.239 0.078 2.482 15.588 0.13 54022. 0.4031
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7.36 0.2291 0.4860 0.0506 0.0238 0.021 0.677 0.532 16.018 0.076 2.367 15.071 0.13 54072. 0.3806
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7.97 0.2482 0.5083 0.0480 0.0235 0.021 0.666 0.505 15.756 0.075 2.248 14.550 0.13 54124. 0.3581
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8.58 0.2673 0.5275 0.0454 0.0230 0.021 0.653 0.478 15.453 0.074 2.125 14.023 0.13 54178. 0.3355
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9.19 0.2864 0.5436 0.0427 0.0225 0.020 0.638 0.449 15.107 0.072 1.998 13.487 0.14 54235. 0.3129
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9.81 0.3055 0.5563 0.0399 0.0219 0.020 0.622 0.420 14.720 0.070 1.868 12.939 0.14 54295. 0.2902
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10.42 0.3246 0.5653 0.0370 0.0213 0.019 0.604 0.390 14.289 0.068 1.734 12.375 0.14 54356. 0.2675
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11.03 0.3437 0.5703 0.0341 0.0206 0.019 0.584 0.359 13.816 0.066 1.597 11.791 0.14 54421. 0.2446
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11.65 0.3628 0.5708 0.0312 0.0198 0.018 0.562 0.328 13.300 0.064 1.458 11.181 0.14 54488. 0.2216
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12.26 0.3819 0.5663 0.0281 0.0190 0.017 0.538 0.296 12.740 0.061 1.317 10.538 0.14 54558. 0.1985
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12.87 0.4010 0.5560 0.0251 0.0181 0.016 0.513 0.264 12.138 0.058 1.173 9.854 0.14 54631. 0.1752
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13.48 0.4200 0.5389 0.0220 0.0171 0.015 0.486 0.231 11.495 0.055 1.028 9.116 0.14 54706. 0.1517
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14.10 0.4391 0.5137 0.0188 0.0161 0.014 0.457 0.198 10.810 0.052 0.881 8.311 0.14 54784. 0.1280
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14.71 0.4582 0.4784 0.0157 0.0150 0.014 0.426 0.165 10.085 0.048 0.734 7.418 0.14 54865. 0.1043
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15.32 0.4773 0.4306 0.0125 0.0139 0.013 0.394 0.132 9.323 0.045 0.586 6.409 0.14 54948. 0.0805
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15.94 0.4964 0.3665 0.0094 0.0127 0.011 0.360 0.099 8.525 0.041 0.439 5.246 0.14 55034. 0.0570
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16.55 0.5155 0.2809 0.0062 0.0115 0.010 0.325 0.066 7.695 0.037 0.292 3.872 0.14 55123. 0.0343
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17.16 0.5346 0.1654 0.0031 0.0102 0.009 0.289 0.033 6.836 0.033 0.147 2.198 0.14 55215. 0.0138
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17.78 0.5537 0.0055 0.0001 0.0089 0.008 0.251 0.001 5.947 0.028 0.004 0.071 0.14 55307. 0.0001
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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 0.0740 0.0235 0.071 1.501 1.753 53.262 0.170 7.795 14.924 0.20 80433. 0.6839
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0.93 0.0193 0.0593 0.0726 0.0236 0.072 1.510 1.718 53.610 0.171 7.643 14.537 0.20 80473. 0.6596
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1.86 0.0386 0.1154 0.0710 0.0238 0.072 1.519 1.682 53.901 0.172 7.481 14.153 0.20 80516. 0.6354
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2.79 0.0579 0.1684 0.0694 0.0239 0.073 1.525 1.643 54.127 0.172 7.310 13.771 0.20 80562. 0.6111
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3.72 0.0772 0.2184 0.0677 0.0239 0.073 1.529 1.603 54.277 0.173 7.129 13.394 0.20 80610. 0.5870
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4.65 0.0965 0.2654 0.0659 0.0240 0.073 1.531 1.560 54.345 0.173 6.939 13.020 0.20 80662. 0.5629
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5.58 0.1158 0.3094 0.0640 0.0240 0.073 1.530 1.515 54.320 0.173 6.739 12.650 0.20 80717. 0.5390
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6.51 0.1352 0.3505 0.0620 0.0239 0.073 1.527 1.468 54.193 0.173 6.528 12.283 0.20 80775. 0.5151
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7.44 0.1545 0.3887 0.0599 0.0238 0.072 1.520 1.418 53.955 0.172 6.307 11.920 0.20 80837. 0.4914
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8.37 0.1738 0.4240 0.0577 0.0236 0.072 1.510 1.366 53.596 0.171 6.076 11.559 0.20 80902. 0.4677
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9.30 0.1931 0.4565 0.0554 0.0234 0.071 1.496 1.311 53.105 0.169 5.833 11.201 0.20 80970. 0.4440
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10.23 0.2124 0.4862 0.0530 0.0231 0.070 1.478 1.254 52.474 0.167 5.580 10.843 0.20 81042. 0.4204
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11.16 0.2317 0.5129 0.0505 0.0228 0.069 1.457 1.195 51.699 0.165 5.316 10.486 0.20 81118. 0.3968
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12.09 0.2510 0.5367 0.0479 0.0224 0.068 1.431 1.134 50.777 0.162 5.043 10.128 0.20 81197. 0.3733
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13.02 0.2703 0.5573 0.0452 0.0219 0.067 1.400 1.070 49.706 0.158 4.761 9.767 0.20 81280. 0.3498
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13.95 0.2896 0.5748 0.0424 0.0214 0.065 1.366 1.005 48.484 0.154 4.470 9.401 0.20 81367. 0.3263
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14.88 0.3089 0.5889 0.0396 0.0208 0.063 1.327 0.938 47.110 0.150 4.171 9.029 0.20 81458. 0.3027
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15.81 0.3282 0.5992 0.0367 0.0201 0.061 1.284 0.869 45.581 0.145 3.865 8.648 0.20 81553. 0.2791
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16.74 0.3475 0.6055 0.0337 0.0194 0.059 1.237 0.799 43.897 0.140 3.553 8.253 0.20 81651. 0.2553
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17.67 0.3668 0.6073 0.0307 0.0186 0.056 1.185 0.727 42.058 0.134 3.234 7.842 0.20 81754. 0.2315
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18.60 0.3862 0.6039 0.0276 0.0177 0.054 1.129 0.654 40.063 0.128 2.910 7.408 0.20 81861. 0.2074
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19.52 0.4055 0.5944 0.0245 0.0167 0.051 1.068 0.581 37.915 0.121 2.582 6.945 0.20 81972. 0.1832
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20.45 0.4248 0.5777 0.0214 0.0157 0.048 1.003 0.506 35.614 0.113 2.250 6.443 0.20 82087. 0.1586
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21.38 0.4441 0.5522 0.0182 0.0146 0.044 0.934 0.431 33.167 0.106 1.916 5.890 0.20 82207. 0.1338
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22.31 0.4634 0.5154 0.0150 0.0135 0.041 0.861 0.355 30.576 0.097 1.580 5.269 0.20 82330. 0.1087
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23.24 0.4827 0.4640 0.0118 0.0123 0.037 0.785 0.280 27.851 0.089 1.244 4.553 0.20 82458. 0.0833
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24.17 0.5020 0.3928 0.0086 0.0110 0.034 0.704 0.204 25.001 0.080 0.909 3.706 0.20 82590. 0.0580
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25.10 0.5213 0.2936 0.0055 0.0097 0.030 0.621 0.130 22.037 0.070 0.576 2.668 0.20 82726. 0.0332
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26.03 0.5406 0.1524 0.0024 0.0084 0.025 0.535 0.056 18.972 0.060 0.248 1.335 0.20 82867. 0.0109
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26.96 0.5599
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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 0.0744 0.0229 0.165 2.604 3.131 123.236 0.294 13.925 11.522 0.27 107241. 0.7057
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1.23 0.0192 0.0606 0.0729 0.0231 0.166 2.622 3.070 124.087 0.296 13.655 11.221 0.27 107294. 0.6806
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2.46 0.0383 0.1179 0.0714 0.0232 0.167 2.637 3.006 124.803 0.298 13.369 10.923 0.27 107351. 0.6555
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3.69 0.0575 0.1721 0.0698 0.0233 0.168 2.649 2.938 125.363 0.299 13.066 10.628 0.27 107412. 0.6306
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4.92 0.0767 0.2231 0.0681 0.0234 0.169 2.657 2.866 125.747 0.300 12.747 10.337 0.27 107477. 0.6057
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6.16 0.0959 0.2712 0.0663 0.0234 0.169 2.661 2.790 125.933 0.301 12.410 10.049 0.27 107545. 0.5811
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7.39 0.1150 0.3162 0.0644 0.0234 0.169 2.660 2.710 125.900 0.301 12.056 9.765 0.27 107618. 0.5565
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8.62 0.1342 0.3583 0.0624 0.0234 0.168 2.655 2.627 125.626 0.300 11.684 9.484 0.27 107695. 0.5321
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9.85 0.1534 0.3975 0.0603 0.0233 0.168 2.643 2.539 125.089 0.299 11.293 9.206 0.27 107776. 0.5078
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11.08 0.1726 0.4338 0.0581 0.0231 0.167 2.626 2.447 124.265 0.297 10.884 8.932 0.27 107862. 0.4836
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12.31 0.1917 0.4673 0.0558 0.0229 0.165 2.602 2.351 123.128 0.294 10.456 8.659 0.27 107952. 0.4596
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13.54 0.2109 0.4980 0.0535 0.0226 0.163 2.571 2.250 121.658 0.290 10.008 8.389 0.27 108047. 0.4356
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14.77 0.2301 0.5258 0.0510 0.0223 0.161 2.532 2.145 119.844 0.286 9.543 8.119 0.27 108147. 0.4117
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16.00 0.2493 0.5508 0.0484 0.0219 0.158 2.487 2.037 117.679 0.281 9.060 7.850 0.27 108252. 0.3878
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17.23 0.2684 0.5728 0.0457 0.0214 0.154 2.433 1.925 115.157 0.275 8.561 7.581 0.27 108362. 0.3641
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18.47 0.2876 0.5917 0.0430 0.0209 0.151 2.372 1.809 112.273 0.268 8.047 7.309 0.27 108477. 0.3403
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19.70 0.3068 0.6073 0.0402 0.0203 0.146 2.304 1.690 109.023 0.260 7.519 7.033 0.27 108596. 0.3165
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20.93 0.3259 0.6194 0.0373 0.0196 0.141 2.227 1.569 105.403 0.252 6.978 6.751 0.27 108721. 0.2927
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22.16 0.3451 0.6276 0.0343 0.0189 0.136 2.143 1.445 101.410 0.242 6.425 6.461 0.27 108851. 0.2688
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23.39 0.3643 0.6316 0.0313 0.0181 0.130 2.051 1.318 97.042 0.232 5.862 6.160 0.27 108987. 0.2448
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24.62 0.3835 0.6307 0.0282 0.0172 0.124 1.950 1.189 92.299 0.220 5.289 5.843 0.27 109128. 0.2206
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25.85 0.4026 0.6241 0.0251 0.0162 0.117 1.842 1.058 87.185 0.208 4.708 5.507 0.27 109274. 0.1961
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27.08 0.4218 0.6106 0.0220 0.0152 0.110 1.726 0.926 81.704 0.195 4.121 5.143 0.27 109426. 0.1714
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28.31 0.4410 0.5888 0.0188 0.0141 0.102 1.603 0.793 75.866 0.181 3.529 4.743 0.27 109583. 0.1462
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29.55 0.4602 0.5561 0.0157 0.0130 0.093 1.472 0.660 69.682 0.166 2.934 4.294 0.27 109746. 0.1207
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30.78 0.4793 0.5093 0.0125 0.0118 0.085 1.335 0.526 63.169 0.151 2.338 3.775 0.27 109914. 0.0947
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32.01 0.4985 0.4430 0.0093 0.0105 0.076 1.191 0.392 56.349 0.135 1.745 3.157 0.27 110088. 0.0684
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33.24 0.5177 0.3485 0.0062 0.0092 0.066 1.041 0.260 49.251 0.118 1.155 2.391 0.27 110267. 0.0422
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34.47 0.5369 0.2106 0.0031 0.0078 0.056 0.885 0.129 41.904 0.100 0.573 1.393 0.27 110452. 0.0173
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35.70 0.5560 -0.0023 0.0000 0.0064 0.046 0.724 -0.001 34.275 0.082 -0.005 -0.015 0.27 110634. 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 0.0748 0.0226 0.319 4.015 4.921 237.521 0.454 21.889 9.397 0.34 134047. 0.7216
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1.56 0.0194 0.0626 0.0734 0.0228 0.321 4.044 4.824 239.244 0.457 21.459 9.146 0.34 134115. 0.6954
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3.12 0.0389 0.1218 0.0718 0.0229 0.323 4.069 4.722 240.691 0.460 21.003 8.898 0.34 134188. 0.6693
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4.68 0.0583 0.1776 0.0701 0.0230 0.324 4.088 4.613 241.820 0.462 20.520 8.653 0.34 134265. 0.6434
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6.24 0.0778 0.2302 0.0684 0.0231 0.325 4.101 4.499 242.586 0.463 20.010 8.411 0.34 134347. 0.6176
|
|
7.80 0.0972 0.2797 0.0666 0.0231 0.326 4.107 4.378 242.945 0.464 19.472 8.173 0.34 134435. 0.5920
|
|
9.37 0.1167 0.3259 0.0646 0.0231 0.326 4.105 4.250 242.854 0.464 18.906 7.938 0.34 134528. 0.5665
|
|
10.93 0.1361 0.3692 0.0626 0.0231 0.325 4.095 4.117 242.267 0.463 18.310 7.707 0.34 134626. 0.5413
|
|
12.49 0.1556 0.4094 0.0605 0.0230 0.323 4.076 3.976 241.137 0.461 17.685 7.479 0.34 134730. 0.5162
|
|
14.05 0.1750 0.4467 0.0582 0.0228 0.321 4.047 3.829 239.416 0.457 17.029 7.253 0.34 134840. 0.4913
|
|
15.61 0.1945 0.4811 0.0559 0.0226 0.318 4.007 3.674 237.049 0.453 16.343 7.030 0.34 134955. 0.4665
|
|
17.17 0.2139 0.5126 0.0534 0.0223 0.314 3.956 3.513 233.995 0.447 15.625 6.809 0.34 135077. 0.4418
|
|
18.73 0.2334 0.5411 0.0509 0.0219 0.309 3.892 3.345 230.233 0.440 14.878 6.590 0.34 135205. 0.4172
|
|
20.29 0.2528 0.5668 0.0482 0.0215 0.303 3.816 3.171 225.749 0.431 14.104 6.371 0.34 135339. 0.3927
|
|
21.85 0.2723 0.5893 0.0455 0.0210 0.296 3.728 2.991 220.532 0.421 13.304 6.151 0.34 135479. 0.3683
|
|
23.41 0.2917 0.6088 0.0427 0.0204 0.288 3.627 2.806 214.570 0.410 12.479 5.931 0.34 135626. 0.3439
|
|
24.98 0.3112 0.6249 0.0398 0.0198 0.279 3.514 2.615 207.853 0.397 11.633 5.707 0.34 135780. 0.3195
|
|
26.54 0.3306 0.6374 0.0368 0.0191 0.269 3.387 2.420 200.374 0.383 10.766 5.479 0.34 135940. 0.2951
|
|
28.10 0.3501 0.6459 0.0338 0.0183 0.258 3.248 2.221 192.126 0.367 9.880 5.244 0.34 136107. 0.2705
|
|
29.66 0.3695 0.6501 0.0307 0.0174 0.246 3.095 2.018 183.107 0.350 8.978 5.000 0.34 136281. 0.2459
|
|
31.22 0.3890 0.6491 0.0276 0.0165 0.232 2.930 1.812 173.319 0.331 8.060 4.742 0.34 136461. 0.2210
|
|
32.78 0.4084 0.6420 0.0244 0.0155 0.218 2.752 1.603 162.769 0.311 7.131 4.467 0.34 136649. 0.1958
|
|
34.34 0.4279 0.6276 0.0212 0.0144 0.203 2.560 1.392 151.468 0.289 6.192 4.169 0.34 136843. 0.1703
|
|
35.90 0.4473 0.6039 0.0179 0.0133 0.187 2.357 1.180 139.439 0.266 5.246 3.837 0.34 137045. 0.1442
|
|
37.46 0.4668 0.5680 0.0147 0.0121 0.170 2.142 0.966 126.708 0.242 4.297 3.458 0.34 137254. 0.1177
|
|
39.02 0.4862 0.5155 0.0114 0.0108 0.152 1.916 0.753 113.315 0.216 3.348 3.013 0.34 137470. 0.0905
|
|
40.59 0.5057 0.4392 0.0082 0.0095 0.133 1.679 0.540 99.312 0.190 2.404 2.468 0.34 137693. 0.0628
|
|
42.15 0.5251 0.3264 0.0050 0.0081 0.114 1.433 0.330 84.759 0.162 1.468 1.766 0.34 137923. 0.0351
|
|
43.71 0.5446 0.1528 0.0019 0.0066 0.093 1.178 0.123 69.714 0.133 0.545 0.798 0.34 138159. 0.0097
|
|
45.27 0.5640
|
|
|
|
|
|
|
|
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 0.0754 0.0225 0.547 5.747 7.138 407.990 0.649 31.751 7.936 0.40 160851. 0.7340
|
|
1.85 0.0192 0.0626 0.0739 0.0227 0.551 5.789 7.000 410.977 0.654 31.137 7.726 0.40 160931. 0.7076
|
|
3.70 0.0384 0.1219 0.0724 0.0228 0.555 5.825 6.854 413.494 0.658 30.486 7.518 0.40 161017. 0.6814
|
|
5.55 0.0576 0.1779 0.0707 0.0229 0.557 5.853 6.699 415.465 0.661 29.798 7.314 0.40 161109. 0.6553
|
|
7.40 0.0768 0.2306 0.0690 0.0230 0.559 5.872 6.536 416.818 0.663 29.071 7.112 0.40 161207. 0.6294
|
|
9.25 0.0960 0.2802 0.0672 0.0230 0.560 5.881 6.363 417.479 0.664 28.304 6.913 0.40 161310. 0.6037
|
|
11.09 0.1152 0.3267 0.0653 0.0230 0.560 5.880 6.182 417.371 0.664 27.497 6.718 0.40 161420. 0.5782
|
|
12.94 0.1344 0.3703 0.0633 0.0230 0.558 5.866 5.991 416.421 0.663 26.649 6.526 0.40 161536. 0.5529
|
|
14.79 0.1536 0.4109 0.0611 0.0229 0.556 5.840 5.791 414.549 0.660 25.758 6.336 0.40 161659. 0.5278
|
|
16.64 0.1728 0.4486 0.0589 0.0227 0.552 5.799 5.581 411.672 0.655 24.825 6.149 0.40 161789. 0.5029
|
|
18.49 0.1920 0.4835 0.0566 0.0225 0.547 5.743 5.361 407.700 0.649 23.847 5.965 0.40 161925. 0.4781
|
|
20.34 0.2112 0.5156 0.0542 0.0222 0.540 5.671 5.132 402.559 0.641 22.826 5.782 0.40 162068. 0.4534
|
|
22.19 0.2304 0.5448 0.0517 0.0218 0.531 5.581 4.893 396.207 0.631 21.763 5.601 0.40 162219. 0.4289
|
|
24.04 0.2496 0.5713 0.0490 0.0214 0.521 5.475 4.645 388.620 0.619 20.660 5.421 0.40 162377. 0.4044
|
|
25.89 0.2688 0.5948 0.0463 0.0209 0.509 5.350 4.389 379.777 0.604 19.520 5.241 0.40 162543. 0.3801
|
|
27.74 0.2880 0.6154 0.0436 0.0204 0.496 5.207 4.125 369.659 0.588 18.346 5.061 0.41 162715. 0.3558
|
|
29.58 0.3072 0.6328 0.0407 0.0198 0.480 5.047 3.853 358.248 0.570 17.140 4.879 0.41 162896. 0.3315
|
|
31.43 0.3264 0.6468 0.0378 0.0191 0.463 4.867 3.576 345.529 0.550 15.904 4.694 0.41 163084. 0.3072
|
|
33.28 0.3456 0.6571 0.0348 0.0183 0.445 4.670 3.292 331.492 0.528 14.641 4.504 0.41 163280. 0.2829
|
|
35.13 0.3648 0.6634 0.0317 0.0174 0.424 4.453 3.002 316.131 0.503 13.353 4.307 0.41 163484. 0.2583
|
|
36.98 0.3840 0.6650 0.0286 0.0165 0.402 4.218 2.708 299.447 0.477 12.045 4.102 0.41 163696. 0.2336
|
|
38.83 0.4032 0.6610 0.0254 0.0155 0.377 3.965 2.409 281.448 0.448 10.717 3.883 0.41 163916. 0.2086
|
|
40.68 0.4224 0.6504 0.0223 0.0145 0.352 3.693 2.108 262.154 0.417 9.376 3.647 0.41 164145. 0.1833
|
|
42.53 0.4416 0.6313 0.0190 0.0133 0.324 3.403 1.804 241.595 0.385 8.023 3.386 0.41 164381. 0.1574
|
|
44.38 0.4608 0.6014 0.0158 0.0121 0.295 3.097 1.498 219.815 0.350 6.664 3.091 0.41 164626. 0.1310
|
|
46.23 0.4800 0.5567 0.0126 0.0109 0.264 2.773 1.192 196.875 0.313 5.304 2.747 0.41 164879. 0.1038
|
|
48.08 0.4992 0.4909 0.0094 0.0095 0.232 2.435 0.888 172.856 0.275 3.948 2.329 0.41 165141. 0.0760
|
|
49.92 0.5184 0.3928 0.0062 0.0082 0.198 2.083 0.585 147.858 0.235 2.602 1.795 0.41 165411. 0.0475
|
|
51.77 0.5376 0.2416 0.0030 0.0067 0.164 1.718 0.286 121.991 0.194 1.274 1.065 0.41 165688. 0.0197
|
|
53.62 0.5568 -0.0125 -0.0001 0.0052 0.127 1.338 -0.011 95.015 0.151 -0.050 -0.053 0.41 165957. 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 0.0760 0.0225 0.869 7.820 9.802 647.666 0.884 43.600 6.865 0.47 187650. 0.7440
|
|
2.15 0.0192 0.0631 0.0746 0.0227 0.875 7.878 9.614 652.454 0.890 42.761 6.683 0.47 187744. 0.7173
|
|
4.31 0.0383 0.1228 0.0730 0.0228 0.880 7.927 9.413 656.483 0.896 41.871 6.504 0.47 187845. 0.6908
|
|
6.46 0.0575 0.1792 0.0714 0.0229 0.885 7.965 9.202 659.629 0.900 40.929 6.327 0.47 187953. 0.6644
|
|
8.61 0.0767 0.2324 0.0696 0.0230 0.887 7.991 8.978 661.777 0.903 39.935 6.153 0.47 188067. 0.6383
|
|
10.77 0.0958 0.2824 0.0678 0.0230 0.889 8.003 8.742 662.808 0.904 38.886 5.983 0.47 188188. 0.6123
|
|
12.92 0.1150 0.3294 0.0659 0.0230 0.889 8.001 8.494 662.601 0.904 37.781 5.814 0.47 188316. 0.5866
|
|
15.08 0.1342 0.3733 0.0639 0.0230 0.886 7.982 8.233 661.033 0.902 36.620 5.649 0.47 188452. 0.5611
|
|
17.23 0.1533 0.4144 0.0617 0.0228 0.882 7.945 7.959 657.982 0.898 35.401 5.486 0.47 188595. 0.5358
|
|
19.38 0.1725 0.4526 0.0595 0.0227 0.876 7.889 7.672 653.314 0.891 34.123 5.326 0.47 188746. 0.5107
|
|
21.54 0.1917 0.4879 0.0572 0.0225 0.867 7.811 7.371 646.886 0.882 32.784 5.168 0.47 188905. 0.4857
|
|
23.69 0.2108 0.5205 0.0547 0.0222 0.856 7.711 7.056 638.574 0.871 31.386 5.012 0.47 189073. 0.4609
|
|
25.84 0.2300 0.5503 0.0522 0.0218 0.843 7.587 6.729 628.310 0.857 29.929 4.857 0.47 189249. 0.4362
|
|
28.00 0.2492 0.5774 0.0496 0.0214 0.826 7.439 6.389 616.053 0.840 28.418 4.704 0.47 189433. 0.4116
|
|
30.15 0.2683 0.6015 0.0468 0.0209 0.807 7.266 6.038 601.771 0.821 26.856 4.551 0.47 189626. 0.3871
|
|
32.30 0.2875 0.6228 0.0440 0.0203 0.785 7.069 5.676 585.432 0.799 25.247 4.398 0.47 189827. 0.3627
|
|
34.46 0.3067 0.6410 0.0411 0.0197 0.760 6.846 5.304 567.007 0.774 23.593 4.243 0.47 190038. 0.3383
|
|
36.61 0.3258 0.6559 0.0382 0.0190 0.733 6.598 4.923 546.474 0.745 21.899 4.086 0.47 190257. 0.3139
|
|
38.77 0.3450 0.6672 0.0352 0.0182 0.702 6.325 4.534 523.814 0.715 20.167 3.926 0.47 190485. 0.2894
|
|
40.92 0.3642 0.6745 0.0321 0.0173 0.669 6.025 4.137 499.019 0.681 18.401 3.760 0.47 190723. 0.2647
|
|
43.07 0.3833 0.6773 0.0290 0.0164 0.633 5.700 3.733 472.088 0.644 16.606 3.587 0.47 190970. 0.2399
|
|
45.23 0.4025 0.6747 0.0258 0.0154 0.594 5.349 3.324 443.036 0.604 14.785 3.403 0.47 191226. 0.2148
|
|
47.38 0.4217 0.6656 0.0226 0.0143 0.552 4.973 2.910 411.892 0.562 12.944 3.205 0.47 191492. 0.1892
|
|
49.53 0.4408 0.6483 0.0193 0.0131 0.508 4.573 2.493 378.706 0.517 11.088 2.986 0.48 191767. 0.1632
|
|
51.69 0.4600 0.6203 0.0161 0.0119 0.461 4.148 2.074 343.548 0.469 9.223 2.738 0.48 192052. 0.1365
|
|
53.84 0.4792 0.5776 0.0128 0.0106 0.411 3.701 1.654 306.517 0.418 7.356 2.447 0.48 192347. 0.1089
|
|
56.00 0.4984 0.5137 0.0096 0.0093 0.359 3.233 1.235 267.741 0.365 5.494 2.093 0.48 192651. 0.0805
|
|
58.15 0.5175 0.4169 0.0064 0.0079 0.305 2.746 0.820 227.381 0.310 3.647 1.635 0.48 192965. 0.0513
|
|
60.30 0.5367 0.2646 0.0032 0.0064 0.249 2.241 0.410 185.617 0.253 1.822 1.001 0.48 193288. 0.0222
|
|
62.46 0.5559 0.0016 0.0000 0.0049 0.191 1.717 0.002 142.160 0.194 0.008 0.006 0.48 193603. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 8000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0768 0.0226 1.302 10.261 12.938 971.224 1.159 57.549 6.042 0.54 214445. 0.7524
|
|
2.46 0.0192 0.0635 0.0754 0.0228 1.312 10.337 12.690 978.431 1.168 56.446 5.883 0.54 214553. 0.7254
|
|
4.92 0.0383 0.1235 0.0738 0.0229 1.320 10.401 12.427 984.471 1.175 55.275 5.725 0.54 214669. 0.6987
|
|
7.38 0.0575 0.1803 0.0722 0.0230 1.326 10.451 12.148 989.164 1.181 54.035 5.570 0.54 214792. 0.6721
|
|
9.84 0.0767 0.2338 0.0704 0.0231 1.331 10.484 11.854 992.330 1.185 52.726 5.418 0.54 214923. 0.6457
|
|
12.31 0.0958 0.2842 0.0686 0.0231 1.333 10.500 11.543 993.789 1.186 51.344 5.268 0.54 215062. 0.6196
|
|
14.77 0.1150 0.3315 0.0666 0.0231 1.332 10.495 11.216 993.359 1.186 49.888 5.121 0.54 215209. 0.5937
|
|
17.23 0.1342 0.3759 0.0646 0.0230 1.329 10.469 10.872 990.855 1.183 48.357 4.977 0.54 215365. 0.5680
|
|
19.69 0.1533 0.4173 0.0624 0.0229 1.322 10.418 10.510 986.088 1.177 46.749 4.834 0.54 215530. 0.5425
|
|
22.15 0.1725 0.4559 0.0602 0.0228 1.313 10.342 10.131 978.862 1.168 45.064 4.694 0.54 215703. 0.5173
|
|
24.61 0.1917 0.4916 0.0578 0.0225 1.299 10.237 9.734 968.957 1.157 43.298 4.557 0.54 215886. 0.4921
|
|
27.07 0.2108 0.5247 0.0554 0.0222 1.282 10.102 9.319 956.185 1.141 41.452 4.421 0.54 216077. 0.4672
|
|
29.53 0.2300 0.5550 0.0528 0.0219 1.261 9.936 8.887 940.439 1.123 39.530 4.286 0.54 216279. 0.4423
|
|
31.99 0.2492 0.5825 0.0501 0.0214 1.236 9.738 8.439 921.658 1.100 37.535 4.153 0.54 216490. 0.4176
|
|
34.46 0.2683 0.6072 0.0474 0.0209 1.207 9.507 7.975 899.791 1.074 35.472 4.020 0.54 216711. 0.3930
|
|
36.92 0.2875 0.6291 0.0445 0.0203 1.173 9.242 7.497 874.793 1.044 33.347 3.887 0.54 216942. 0.3684
|
|
39.38 0.3067 0.6479 0.0416 0.0197 1.135 8.945 7.006 846.620 1.011 31.162 3.753 0.54 217183. 0.3439
|
|
41.84 0.3258 0.6636 0.0386 0.0190 1.093 8.613 6.502 815.238 0.973 28.923 3.618 0.54 217434. 0.3193
|
|
44.30 0.3450 0.6757 0.0356 0.0182 1.047 8.247 5.988 780.620 0.932 26.634 3.479 0.54 217695. 0.2947
|
|
46.76 0.3642 0.6839 0.0324 0.0173 0.996 7.847 5.463 742.752 0.887 24.301 3.336 0.54 217967. 0.2699
|
|
49.22 0.3833 0.6877 0.0293 0.0163 0.941 7.413 4.930 701.636 0.838 21.927 3.187 0.54 218249. 0.2449
|
|
51.68 0.4025 0.6862 0.0261 0.0153 0.881 6.945 4.389 657.293 0.785 19.521 3.028 0.54 218542. 0.2196
|
|
54.15 0.4217 0.6783 0.0228 0.0142 0.818 6.442 3.841 609.770 0.728 17.087 2.857 0.54 218846. 0.1939
|
|
56.61 0.4408 0.6622 0.0195 0.0130 0.750 5.907 3.290 559.140 0.667 14.633 2.669 0.54 219161. 0.1675
|
|
59.07 0.4600 0.6355 0.0162 0.0118 0.678 5.341 2.735 505.512 0.603 12.166 2.454 0.54 219487. 0.1405
|
|
61.53 0.4791 0.5940 0.0129 0.0104 0.602 4.744 2.180 449.037 0.536 9.697 2.202 0.54 219824. 0.1126
|
|
63.99 0.4983 0.5308 0.0097 0.0091 0.523 4.120 1.627 389.912 0.465 7.235 1.892 0.54 220172. 0.0835
|
|
66.45 0.5175 0.4335 0.0064 0.0076 0.440 3.469 1.077 328.384 0.392 4.792 1.488 0.55 220531. 0.0535
|
|
68.91 0.5366 0.2768 0.0032 0.0062 0.355 2.797 0.535 264.731 0.316 2.378 0.916 0.55 220900. 0.0232
|
|
71.37 0.5558 -0.0039 0.0000 0.0046 0.266 2.096 -0.005 198.390 0.237 -0.024 -0.013 0.55 221257. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 9000
|
|
|
|
V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
|
|
(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
|
|
0.00 0.0000 0.0000 0.0778 0.0228 1.872 13.108 16.580 1395.719 1.481 73.750 5.388 0.61 241233. 0.7595
|
|
2.77 0.0192 0.0636 0.0763 0.0230 1.886 13.205 16.264 1406.039 1.492 72.343 5.247 0.61 241356. 0.7324
|
|
5.53 0.0383 0.1239 0.0747 0.0231 1.897 13.286 15.928 1414.652 1.501 70.849 5.107 0.61 241487. 0.7056
|
|
8.30 0.0575 0.1809 0.0731 0.0232 1.906 13.348 15.573 1421.290 1.508 69.267 4.970 0.61 241626. 0.6789
|
|
11.07 0.0766 0.2346 0.0713 0.0233 1.912 13.389 15.196 1425.695 1.513 67.594 4.835 0.61 241774. 0.6524
|
|
13.84 0.0958 0.2852 0.0695 0.0233 1.914 13.407 14.800 1427.609 1.515 65.828 4.702 0.61 241932. 0.6262
|
|
16.60 0.1149 0.3328 0.0675 0.0233 1.913 13.399 14.381 1426.765 1.514 63.968 4.572 0.61 242098. 0.6002
|
|
19.37 0.1341 0.3774 0.0654 0.0232 1.908 13.363 13.941 1422.895 1.510 62.010 4.444 0.61 242274. 0.5744
|
|
22.14 0.1532 0.4191 0.0633 0.0231 1.899 13.296 13.479 1415.734 1.502 59.954 4.318 0.61 242460. 0.5488
|
|
24.90 0.1724 0.4580 0.0610 0.0230 1.884 13.195 12.994 1404.994 1.491 57.797 4.195 0.61 242655. 0.5234
|
|
27.67 0.1915 0.4941 0.0586 0.0227 1.865 13.057 12.486 1390.365 1.475 55.537 4.073 0.61 242862. 0.4982
|
|
30.44 0.2107 0.5275 0.0561 0.0224 1.839 12.881 11.955 1371.569 1.455 53.174 3.953 0.61 243078. 0.4732
|
|
33.21 0.2299 0.5583 0.0535 0.0220 1.808 12.664 11.401 1348.446 1.431 50.712 3.835 0.61 243305. 0.4482
|
|
35.97 0.2490 0.5863 0.0508 0.0216 1.771 12.405 10.826 1320.907 1.402 48.156 3.718 0.61 243543. 0.4234
|
|
38.74 0.2682 0.6115 0.0480 0.0211 1.728 12.104 10.232 1288.883 1.368 45.513 3.601 0.61 243792. 0.3987
|
|
41.51 0.2873 0.6340 0.0451 0.0205 1.679 11.761 9.620 1252.308 1.329 42.788 3.484 0.61 244052. 0.3741
|
|
44.27 0.3065 0.6535 0.0422 0.0198 1.624 11.374 8.990 1211.125 1.285 39.987 3.367 0.61 244324. 0.3494
|
|
47.04 0.3256 0.6698 0.0392 0.0190 1.563 10.944 8.344 1165.281 1.236 37.116 3.248 0.61 244607. 0.3248
|
|
49.81 0.3448 0.6827 0.0361 0.0182 1.495 10.469 7.684 1114.741 1.183 34.180 3.127 0.61 244901. 0.3000
|
|
52.58 0.3639 0.6918 0.0329 0.0173 1.421 9.950 7.011 1059.484 1.124 31.187 3.002 0.61 245207. 0.2751
|
|
55.34 0.3831 0.6966 0.0297 0.0163 1.340 9.387 6.327 999.515 1.061 28.142 2.871 0.61 245525. 0.2500
|
|
58.11 0.4022 0.6962 0.0264 0.0153 1.254 8.780 5.632 934.865 0.992 25.053 2.733 0.61 245855. 0.2245
|
|
60.88 0.4214 0.6894 0.0231 0.0141 1.161 8.129 4.930 865.601 0.918 21.929 2.583 0.61 246196. 0.1986
|
|
63.64 0.4406 0.6747 0.0198 0.0129 1.062 7.436 4.222 791.832 0.840 18.779 2.418 0.61 246551. 0.1720
|
|
66.41 0.4597 0.6494 0.0165 0.0117 0.957 6.703 3.510 713.716 0.757 15.612 2.231 0.61 246917. 0.1447
|
|
69.18 0.4789 0.6093 0.0131 0.0103 0.847 5.930 2.797 631.472 0.670 12.441 2.009 0.61 247296. 0.1163
|
|
71.95 0.4980 0.5472 0.0098 0.0089 0.731 5.122 2.086 545.389 0.579 9.279 1.735 0.61 247687. 0.0867
|
|
74.71 0.5172 0.4500 0.0065 0.0074 0.611 4.281 1.381 455.827 0.484 6.141 1.374 0.61 248090. 0.0559
|
|
77.48 0.5363 0.2900 0.0032 0.0059 0.487 3.411 0.684 363.193 0.385 3.041 0.854 0.61 248505. 0.0244
|
|
80.25 0.5555 -0.0067 -0.0001 0.0044 0.357 2.503 -0.011 266.554 0.283 -0.050 -0.019 0.61 248904. 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 0.0790 0.0231 2.604 16.412 20.774 1941.783 1.854 92.401 4.852 0.67 268014. 0.7656
|
|
3.07 0.0191 0.0636 0.0775 0.0233 2.623 16.533 20.380 1955.993 1.868 90.650 4.726 0.67 268151. 0.7385
|
|
6.14 0.0383 0.1239 0.0759 0.0234 2.639 16.632 19.962 1967.787 1.879 88.790 4.601 0.67 268298. 0.7116
|
|
9.22 0.0574 0.1809 0.0742 0.0235 2.651 16.708 19.518 1976.780 1.888 86.818 4.478 0.67 268453. 0.6849
|
|
12.29 0.0765 0.2348 0.0724 0.0236 2.659 16.758 19.049 1982.616 1.893 84.732 4.358 0.67 268619. 0.6584
|
|
15.36 0.0957 0.2855 0.0705 0.0236 2.662 16.777 18.554 1984.930 1.895 82.529 4.240 0.67 268795. 0.6322
|
|
18.43 0.1148 0.3332 0.0685 0.0236 2.660 16.764 18.032 1983.350 1.894 80.205 4.124 0.67 268980. 0.6062
|
|
21.50 0.1340 0.3780 0.0665 0.0236 2.652 16.714 17.482 1977.510 1.888 77.760 4.010 0.67 269177. 0.5804
|
|
24.57 0.1531 0.4199 0.0643 0.0234 2.638 16.626 16.904 1967.038 1.878 75.190 3.898 0.67 269384. 0.5548
|
|
27.65 0.1722 0.4591 0.0620 0.0232 2.617 16.495 16.298 1951.536 1.864 72.494 3.788 0.67 269603. 0.5294
|
|
30.72 0.1914 0.4955 0.0595 0.0230 2.589 16.318 15.663 1930.584 1.844 69.668 3.680 0.67 269832. 0.5041
|
|
33.79 0.2105 0.5293 0.0570 0.0227 2.553 16.091 14.998 1903.783 1.818 66.711 3.573 0.67 270074. 0.4790
|
|
36.86 0.2296 0.5604 0.0544 0.0223 2.509 15.813 14.305 1870.902 1.787 63.629 3.468 0.67 270327. 0.4541
|
|
39.93 0.2488 0.5889 0.0516 0.0218 2.457 15.483 13.586 1831.820 1.749 60.429 3.364 0.67 270592. 0.4292
|
|
43.01 0.2679 0.6147 0.0488 0.0213 2.396 15.099 12.841 1786.442 1.706 57.118 3.260 0.67 270869. 0.4044
|
|
46.08 0.2871 0.6377 0.0459 0.0207 2.326 14.662 12.074 1734.684 1.657 53.704 3.157 0.68 271159. 0.3797
|
|
49.15 0.3062 0.6578 0.0429 0.0200 2.248 14.170 11.284 1676.467 1.601 50.193 3.053 0.68 271461. 0.3550
|
|
52.22 0.3253 0.6749 0.0398 0.0192 2.161 13.623 10.475 1611.722 1.539 46.593 2.948 0.68 271776. 0.3303
|
|
55.29 0.3445 0.6886 0.0367 0.0183 2.066 13.020 9.647 1540.403 1.471 42.912 2.841 0.68 272103. 0.3054
|
|
58.36 0.3636 0.6986 0.0335 0.0174 1.961 12.361 8.803 1462.483 1.397 39.157 2.730 0.68 272443. 0.2804
|
|
61.44 0.3827 0.7043 0.0302 0.0164 1.848 11.647 7.944 1377.970 1.316 35.336 2.615 0.68 272796. 0.2551
|
|
64.51 0.4019 0.7050 0.0269 0.0153 1.726 10.877 7.073 1286.909 1.229 31.460 2.493 0.68 273163. 0.2295
|
|
67.58 0.4210 0.6995 0.0235 0.0142 1.595 10.053 6.191 1189.395 1.136 27.538 2.361 0.68 273542. 0.2034
|
|
70.65 0.4402 0.6861 0.0202 0.0129 1.456 9.176 5.302 1085.580 1.037 23.583 2.215 0.68 273936. 0.1766
|
|
73.72 0.4593 0.6623 0.0168 0.0116 1.308 8.247 4.408 975.689 0.932 19.606 2.049 0.68 274342. 0.1489
|
|
76.80 0.4784 0.6236 0.0134 0.0102 1.153 7.269 3.512 860.037 0.821 15.623 1.852 0.68 274763. 0.1202
|
|
79.87 0.4976 0.5629 0.0100 0.0088 0.991 6.247 2.619 739.045 0.706 11.651 1.608 0.68 275197. 0.0901
|
|
82.94 0.5167 0.4660 0.0066 0.0073 0.822 5.183 1.733 613.244 0.586 7.707 1.281 0.68 275645. 0.0584
|
|
86.01 0.5358 0.3032 0.0033 0.0058 0.648 4.084 0.857 483.239 0.461 3.810 0.804 0.68 276105. 0.0258
|
|
89.08 0.5550 -0.0089 -0.0001 0.0041 0.466 2.938 -0.018 347.616 0.332 -0.078 -0.023 0.68 276545. 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 0.0804 0.0236 3.537 20.267 25.579 2637.670 2.290 113.777 4.399 0.74 294784. 0.7701
|
|
3.37 0.0191 0.0634 0.0788 0.0238 3.562 20.409 25.099 2656.029 2.306 111.641 4.286 0.74 294936. 0.7433
|
|
6.75 0.0382 0.1235 0.0772 0.0239 3.582 20.525 24.588 2671.194 2.319 109.368 4.175 0.74 295099. 0.7167
|
|
10.12 0.0573 0.1804 0.0755 0.0240 3.597 20.613 24.046 2682.629 2.329 106.958 4.066 0.74 295271. 0.6901
|
|
13.50 0.0764 0.2342 0.0737 0.0241 3.607 20.668 23.472 2689.817 2.335 104.406 3.958 0.74 295455. 0.6638
|
|
16.87 0.0956 0.2849 0.0718 0.0241 3.610 20.687 22.866 2692.225 2.337 101.708 3.852 0.74 295649. 0.6377
|
|
20.25 0.1147 0.3327 0.0698 0.0241 3.606 20.664 22.226 2689.326 2.335 98.861 3.749 0.74 295855. 0.6117
|
|
23.62 0.1338 0.3776 0.0677 0.0240 3.595 20.597 21.552 2680.595 2.327 95.862 3.647 0.74 296072. 0.5860
|
|
27.00 0.1529 0.4197 0.0655 0.0239 3.575 20.481 20.843 2665.517 2.314 92.709 3.547 0.74 296301. 0.5605
|
|
30.37 0.1720 0.4591 0.0631 0.0237 3.545 20.313 20.099 2643.572 2.295 89.399 3.448 0.74 296542. 0.5352
|
|
33.74 0.1911 0.4958 0.0607 0.0234 3.506 20.087 19.319 2614.195 2.269 85.929 3.352 0.74 296796. 0.5100
|
|
37.12 0.2102 0.5299 0.0581 0.0231 3.456 19.800 18.502 2576.832 2.237 82.296 3.257 0.74 297063. 0.4849
|
|
40.49 0.2293 0.5615 0.0554 0.0226 3.394 19.449 17.650 2531.165 2.197 78.507 3.163 0.74 297342. 0.4600
|
|
43.87 0.2484 0.5904 0.0527 0.0222 3.322 19.033 16.765 2477.027 2.150 74.570 3.070 0.74 297635. 0.4351
|
|
47.24 0.2676 0.6167 0.0498 0.0216 3.238 18.551 15.849 2414.297 2.096 70.496 2.977 0.74 297940. 0.4103
|
|
50.62 0.2867 0.6403 0.0468 0.0210 3.142 18.002 14.904 2342.877 2.034 66.292 2.885 0.74 298259. 0.3856
|
|
53.99 0.3058 0.6610 0.0438 0.0202 3.034 17.386 13.932 2262.671 1.964 61.968 2.793 0.74 298592. 0.3608
|
|
57.37 0.3249 0.6788 0.0406 0.0194 2.915 16.702 12.935 2173.613 1.887 57.533 2.699 0.74 298938. 0.3360
|
|
60.74 0.3440 0.6933 0.0374 0.0186 2.784 15.949 11.915 2075.667 1.802 52.996 2.604 0.74 299299. 0.3111
|
|
64.11 0.3631 0.7041 0.0342 0.0176 2.640 15.128 10.874 1968.830 1.709 48.367 2.505 0.74 299673. 0.2860
|
|
67.49 0.3822 0.7107 0.0308 0.0166 2.485 14.239 9.815 1853.159 1.609 43.655 2.402 0.75 300062. 0.2605
|
|
70.86 0.4013 0.7123 0.0275 0.0155 2.318 13.284 8.739 1728.771 1.501 38.873 2.293 0.75 300464. 0.2346
|
|
74.24 0.4204 0.7077 0.0240 0.0143 2.140 12.262 7.651 1595.868 1.385 34.033 2.175 0.75 300882. 0.2082
|
|
77.61 0.4396 0.6952 0.0206 0.0130 1.951 11.178 6.553 1454.750 1.263 29.150 2.043 0.75 301314. 0.1811
|
|
80.99 0.4587 0.6720 0.0171 0.0117 1.751 10.034 5.449 1305.843 1.134 24.238 1.893 0.75 301761. 0.1529
|
|
84.36 0.4778 0.6336 0.0136 0.0103 1.542 8.834 4.343 1149.709 0.998 19.317 1.713 0.75 302223. 0.1236
|
|
87.73 0.4969 0.5724 0.0102 0.0088 1.324 7.585 3.239 987.072 0.857 14.407 1.488 0.75 302699. 0.0927
|
|
91.11 0.5160 0.4740 0.0067 0.0073 1.098 6.292 2.142 818.825 0.711 9.529 1.187 0.75 303191. 0.0601
|
|
94.48 0.5351 0.3079 0.0033 0.0058 0.866 4.964 1.059 645.972 0.561 4.708 0.743 0.75 303696. 0.0265
|
|
97.86 0.5542 -0.0098 -0.0001 0.0042 0.626 3.584 -0.024 466.480 0.405 -0.105 -0.023 0.75 304178. 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 0.0820 0.0247 4.808 25.251 31.079 3585.048 2.853 138.241 3.932 0.81 321540. 0.7588
|
|
3.67 0.0191 0.0619 0.0805 0.0248 4.827 25.351 30.504 3599.213 2.864 135.680 3.844 0.81 321708. 0.7349
|
|
7.35 0.0381 0.1210 0.0789 0.0249 4.841 25.424 29.890 3609.597 2.872 132.953 3.756 0.81 321886. 0.7108
|
|
11.02 0.0572 0.1772 0.0772 0.0249 4.849 25.467 29.239 3615.589 2.877 130.056 3.668 0.81 322076. 0.6866
|
|
14.70 0.0763 0.2307 0.0754 0.0249 4.850 25.474 28.549 3616.583 2.878 126.984 3.580 0.81 322278. 0.6622
|
|
18.37 0.0954 0.2813 0.0734 0.0249 4.844 25.441 27.818 3611.948 2.874 123.734 3.493 0.81 322491. 0.6378
|
|
22.04 0.1144 0.3292 0.0714 0.0248 4.829 25.364 27.046 3601.010 2.866 120.300 3.407 0.81 322717. 0.6133
|
|
25.72 0.1335 0.3744 0.0692 0.0247 4.805 25.238 26.232 3583.097 2.851 116.679 3.321 0.81 322956. 0.5887
|
|
29.39 0.1526 0.4169 0.0670 0.0245 4.771 25.057 25.375 3557.515 2.831 112.869 3.235 0.81 323207. 0.5642
|
|
33.07 0.1717 0.4567 0.0646 0.0243 4.725 24.818 24.475 3523.531 2.804 108.866 3.151 0.81 323472. 0.5396
|
|
36.74 0.1907 0.4940 0.0621 0.0240 4.667 24.514 23.531 3480.339 2.770 104.667 3.067 0.81 323750. 0.5150
|
|
40.42 0.2098 0.5286 0.0595 0.0236 4.596 24.140 22.542 3427.244 2.727 100.268 2.983 0.81 324042. 0.4903
|
|
44.09 0.2289 0.5606 0.0568 0.0232 4.511 23.694 21.510 3363.941 2.677 95.675 2.900 0.81 324348. 0.4656
|
|
47.76 0.2480 0.5899 0.0539 0.0227 4.412 23.173 20.436 3290.030 2.618 90.900 2.817 0.81 324668. 0.4409
|
|
51.44 0.2670 0.6166 0.0510 0.0221 4.298 22.577 19.324 3205.293 2.551 85.954 2.734 0.81 325002. 0.4161
|
|
55.11 0.2861 0.6406 0.0480 0.0214 4.170 21.903 18.176 3109.611 2.475 80.849 2.651 0.81 325351. 0.3913
|
|
58.79 0.3052 0.6616 0.0449 0.0207 4.027 21.150 16.995 3002.783 2.390 75.595 2.567 0.81 325715. 0.3663
|
|
62.46 0.3243 0.6795 0.0417 0.0199 3.869 20.319 15.783 2884.784 2.296 70.203 2.482 0.81 326093. 0.3413
|
|
66.13 0.3433 0.6939 0.0384 0.0190 3.696 19.411 14.542 2755.792 2.193 64.684 2.393 0.81 326486. 0.3160
|
|
69.81 0.3624 0.7045 0.0350 0.0180 3.508 18.425 13.276 2615.896 2.082 59.050 2.302 0.81 326894. 0.2903
|
|
73.48 0.3815 0.7104 0.0316 0.0170 3.306 17.365 11.986 2465.387 1.962 53.313 2.205 0.81 327318. 0.2643
|
|
77.16 0.4006 0.7107 0.0282 0.0159 3.091 16.233 10.676 2304.689 1.834 47.488 2.101 0.81 327757. 0.2377
|
|
80.83 0.4196 0.7041 0.0247 0.0147 2.862 15.034 9.350 2134.370 1.698 41.589 1.987 0.81 328212. 0.2103
|
|
84.51 0.4387 0.6885 0.0211 0.0135 2.622 13.771 8.011 1955.088 1.556 35.634 1.859 0.81 328683. 0.1821
|
|
88.18 0.4578 0.6610 0.0176 0.0122 2.371 12.451 6.664 1767.717 1.407 29.640 1.710 0.82 329169. 0.1528
|
|
91.85 0.4769 0.6167 0.0140 0.0108 2.110 11.082 5.313 1573.332 1.252 23.630 1.532 0.82 329672. 0.1222
|
|
95.53 0.4959 0.5482 0.0105 0.0095 1.841 9.672 3.963 1373.193 1.093 17.629 1.309 0.82 330191. 0.0902
|
|
99.20 0.5150 0.4425 0.0069 0.0081 1.567 8.232 2.622 1168.775 0.930 11.663 1.018 0.82 330725. 0.0570
|
|
102.88 0.5341 0.2756 0.0034 0.0066 1.290 6.773 1.295 961.634 0.765 5.762 0.611 0.82 331275. 0.0241
|
|
106.55 0.5532 -0.0078 -0.0001 0.0052 1.004 5.274 -0.028 748.803 0.596 -0.123 -0.017 0.82 331804. 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 0.0840 0.0277 6.855 33.236 37.327 5111.838 3.755 166.028 3.312 0.87 348280. 0.7005
|
|
3.99 0.0191 0.0570 0.0824 0.0276 6.838 33.153 36.649 5099.120 3.746 163.016 3.260 0.87 348464. 0.6832
|
|
7.98 0.0382 0.1122 0.0808 0.0275 6.814 33.037 35.926 5081.334 3.733 159.799 3.207 0.87 348660. 0.6654
|
|
11.97 0.0574 0.1654 0.0791 0.0274 6.783 32.885 35.156 5057.931 3.715 156.373 3.153 0.87 348868. 0.6471
|
|
15.96 0.0765 0.2167 0.0772 0.0273 6.743 32.693 34.337 5028.305 3.694 152.733 3.097 0.87 349090. 0.6283
|
|
19.95 0.0956 0.2660 0.0753 0.0271 6.694 32.455 33.469 4991.826 3.667 148.871 3.041 0.87 349324. 0.6090
|
|
23.94 0.1147 0.3131 0.0732 0.0268 6.635 32.170 32.550 4947.853 3.635 144.782 2.984 0.87 349572. 0.5893
|
|
27.93 0.1338 0.3582 0.0710 0.0265 6.565 31.831 31.579 4895.748 3.596 140.463 2.926 0.87 349834. 0.5691
|
|
31.92 0.1530 0.4011 0.0687 0.0262 6.484 31.435 30.555 4834.834 3.551 135.910 2.866 0.88 350110. 0.5485
|
|
35.91 0.1721 0.4418 0.0663 0.0258 6.389 30.977 29.479 4764.381 3.500 131.121 2.806 0.88 350400. 0.5274
|
|
39.90 0.1912 0.4802 0.0638 0.0254 6.281 30.451 28.347 4683.536 3.440 126.090 2.745 0.88 350705. 0.5060
|
|
43.89 0.2103 0.5162 0.0611 0.0249 6.157 29.852 27.161 4591.385 3.373 120.813 2.683 0.88 351025. 0.4841
|
|
47.88 0.2294 0.5499 0.0583 0.0243 6.018 29.177 25.921 4487.540 3.296 115.298 2.620 0.88 351360. 0.4618
|
|
51.87 0.2486 0.5806 0.0554 0.0237 5.867 28.446 24.631 4375.107 3.214 109.557 2.553 0.88 351711. 0.4387
|
|
55.86 0.2677 0.6083 0.0524 0.0231 5.703 27.649 23.292 4252.500 3.124 103.604 2.484 0.88 352077. 0.4150
|
|
59.85 0.2868 0.6330 0.0493 0.0223 5.524 26.781 21.909 4119.002 3.026 97.453 2.413 0.88 352459. 0.3909
|
|
63.84 0.3059 0.6539 0.0461 0.0216 5.333 25.854 20.485 3976.535 2.921 91.118 2.337 0.88 352856. 0.3661
|
|
67.83 0.3250 0.6704 0.0428 0.0207 5.132 24.882 19.022 3827.014 2.811 84.610 2.254 0.88 353269. 0.3404
|
|
71.82 0.3442 0.6821 0.0394 0.0199 4.920 23.853 17.524 3668.705 2.695 77.946 2.166 0.88 353699. 0.3139
|
|
75.80 0.3633 0.6888 0.0360 0.0190 4.693 22.754 15.994 3499.730 2.571 71.140 2.073 0.88 354145. 0.2870
|
|
79.79 0.3824 0.6898 0.0325 0.0180 4.453 21.587 14.436 3320.253 2.439 64.209 1.972 0.88 354607. 0.2594
|
|
83.78 0.4015 0.6838 0.0289 0.0170 4.199 20.359 12.853 3131.283 2.300 57.170 1.862 0.88 355086. 0.2311
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87.77 0.4206 0.6692 0.0253 0.0159 3.935 19.077 11.250 2934.095 2.155 50.042 1.739 0.88 355582. 0.2019
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91.76 0.4398 0.6438 0.0217 0.0148 3.661 17.751 9.633 2730.202 2.006 42.846 1.600 0.88 356095. 0.1719
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|
95.75 0.4589 0.6046 0.0180 0.0137 3.381 16.390 8.005 2520.929 1.852 35.606 1.440 0.88 356625. 0.1411
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|
99.74 0.4780 0.5477 0.0143 0.0125 3.095 15.006 6.373 2308.020 1.695 28.349 1.252 0.88 357173. 0.1095
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|
103.73 0.4971 0.4676 0.0107 0.0113 2.807 13.611 4.745 2093.445 1.538 21.107 1.028 0.88 357738. 0.0775
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|
107.72 0.5162 0.3567 0.0070 0.0102 2.520 12.218 3.129 1879.205 1.380 13.918 0.755 0.89 358320. 0.0462
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|
111.71 0.5354 0.2041 0.0034 0.0090 2.235 10.838 1.532 1667.005 1.225 6.814 0.417 0.89 358918. 0.0179
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|
115.70 0.5545 -0.0101 -0.0001 0.0079 1.942 9.417 -0.063 1448.427 1.064 -0.282 -0.020 0.89 359502. 0.0000
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PROP RPM = 14000
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V J Pe Ct Cp PWR Torque Thrust PWR Torque Thrust THR/PWR Mach Reyn FOM
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(mph) (Adv_Ratio) - - - (Hp) (In-Lbf) (Lbf) (W) (N-m) (N) (g/W) - - -
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0.00 0.0000 0.0000 0.0853 0.0332 10.273 46.247 43.973 7660.218 5.225 195.591 2.604 0.94 375026. 0.5977
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|
4.43 0.0197 0.0501 0.0838 0.0330 10.199 45.918 43.204 7605.618 5.188 192.172 2.577 0.94 375229. 0.5862
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|
8.87 0.0395 0.0991 0.0822 0.0327 10.111 45.521 42.374 7539.971 5.143 188.482 2.549 0.94 375447. 0.5744
|
|
13.30 0.0592 0.1470 0.0805 0.0324 10.008 45.056 41.483 7462.847 5.090 184.515 2.521 0.94 375680. 0.5621
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|
17.73 0.0789 0.1938 0.0786 0.0320 9.888 44.518 40.526 7373.773 5.030 180.260 2.493 0.94 375928. 0.5493
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|
22.16 0.0986 0.2394 0.0766 0.0316 9.752 43.906 39.503 7272.401 4.960 175.711 2.464 0.94 376191. 0.5360
|
|
26.60 0.1184 0.2838 0.0745 0.0311 9.600 43.218 38.413 7158.438 4.883 170.859 2.434 0.94 376471. 0.5222
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|
31.03 0.1381 0.3269 0.0722 0.0305 9.430 42.452 37.253 7031.613 4.796 165.700 2.403 0.94 376766. 0.5077
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|
35.46 0.1578 0.3686 0.0699 0.0299 9.242 41.607 36.023 6891.695 4.701 160.230 2.371 0.94 377078. 0.4926
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|
39.89 0.1775 0.4088 0.0673 0.0292 9.036 40.681 34.722 6738.183 4.596 154.444 2.337 0.94 377407. 0.4768
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|
44.33 0.1973 0.4474 0.0647 0.0285 8.812 39.670 33.350 6570.759 4.482 148.339 2.302 0.94 377753. 0.4602
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|
48.76 0.2170 0.4842 0.0619 0.0277 8.568 38.571 31.905 6388.800 4.358 141.912 2.265 0.94 378117. 0.4429
|
|
53.19 0.2367 0.5191 0.0589 0.0269 8.304 37.384 30.390 6192.084 4.224 135.176 2.226 0.94 378498. 0.4248
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|
57.63 0.2564 0.5518 0.0559 0.0260 8.023 36.122 28.810 5983.096 4.081 128.149 2.184 0.94 378896. 0.4058
|
|
62.06 0.2762 0.5810 0.0527 0.0250 7.739 34.839 27.169 5770.688 3.936 120.847 2.135 0.94 379313. 0.3853
|
|
66.49 0.2959 0.6064 0.0494 0.0241 7.447 33.528 25.470 5553.474 3.788 113.291 2.080 0.95 379747. 0.3634
|
|
70.92 0.3156 0.6276 0.0460 0.0231 7.148 32.179 23.719 5330.021 3.636 105.502 2.018 0.95 380200. 0.3403
|
|
75.36 0.3353 0.6427 0.0425 0.0222 6.853 30.852 21.919 5110.281 3.486 97.495 1.945 0.95 380670. 0.3153
|
|
79.79 0.3551 0.6462 0.0389 0.0214 6.608 29.751 20.071 4927.823 3.361 89.274 1.847 0.95 381160. 0.2865
|
|
84.22 0.3748 0.6421 0.0353 0.0206 6.360 28.633 18.184 4742.688 3.235 80.884 1.739 0.95 381668. 0.2567
|
|
88.65 0.3945 0.6299 0.0315 0.0198 6.105 27.485 16.266 4552.476 3.105 72.350 1.621 0.95 382194. 0.2263
|
|
93.09 0.4142 0.6083 0.0278 0.0189 5.843 26.307 14.321 4357.472 2.972 63.701 1.491 0.95 382740. 0.1953
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|
97.52 0.4340 0.5761 0.0240 0.0181 5.578 25.114 12.358 4159.752 2.837 54.969 1.348 0.95 383305. 0.1640
|
|
101.95 0.4537 0.5314 0.0201 0.0172 5.312 23.917 10.385 3961.488 2.702 46.191 1.189 0.95 383890. 0.1326
|
|
106.39 0.4734 0.4725 0.0163 0.0163 5.049 22.732 8.410 3765.307 2.568 37.407 1.013 0.95 384494. 0.1017
|
|
110.82 0.4931 0.3975 0.0125 0.0155 4.791 21.568 6.444 3572.368 2.437 28.665 0.818 0.95 385118. 0.0719
|
|
115.25 0.5129 0.3047 0.0087 0.0147 4.538 20.432 4.500 3384.275 2.308 20.017 0.603 0.95 385762. 0.0443
|
|
119.68 0.5326 0.1924 0.0050 0.0139 4.294 19.330 2.589 3201.785 2.184 11.514 0.367 0.95 386428. 0.0204
|
|
124.12 0.5523 0.0579 0.0014 0.0131 4.050 18.232 0.709 3019.961 2.060 3.153 0.106 0.96 387116. 0.0031
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|
128.55 0.5720
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