501 lines
89 KiB
Plaintext
501 lines
89 KiB
Plaintext
18x8E (18x8E.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 0.0772 0.0283 0.004 0.271 0.258 3.209 0.031 1.149 36.499 0.07 29930. 0.6046
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0.34 0.0202 0.0536 0.0758 0.0285 0.004 0.273 0.253 3.229 0.031 1.127 35.610 0.07 29946. 0.5844
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0.69 0.0403 0.1046 0.0743 0.0286 0.004 0.274 0.248 3.246 0.031 1.105 34.720 0.07 29963. 0.5641
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1.03 0.0605 0.1529 0.0727 0.0287 0.004 0.275 0.243 3.259 0.031 1.081 33.831 0.07 29981. 0.5437
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1.37 0.0806 0.1985 0.0710 0.0288 0.004 0.276 0.237 3.269 0.031 1.056 32.943 0.07 30000. 0.5233
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1.72 0.1008 0.2414 0.0692 0.0289 0.004 0.277 0.231 3.274 0.031 1.029 32.056 0.07 30021. 0.5027
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2.06 0.1210 0.2817 0.0673 0.0289 0.004 0.277 0.225 3.275 0.031 1.001 31.172 0.07 30043. 0.4821
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2.41 0.1411 0.3194 0.0653 0.0288 0.004 0.276 0.218 3.270 0.031 0.971 30.288 0.07 30066. 0.4614
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2.75 0.1613 0.3544 0.0632 0.0287 0.004 0.276 0.211 3.259 0.031 0.940 29.406 0.07 30090. 0.4406
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3.09 0.1814 0.3867 0.0609 0.0286 0.004 0.274 0.204 3.243 0.031 0.907 28.522 0.07 30116. 0.4198
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3.44 0.2016 0.4163 0.0586 0.0284 0.004 0.272 0.196 3.219 0.031 0.872 27.636 0.07 30144. 0.3990
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3.78 0.2217 0.4432 0.0562 0.0281 0.004 0.269 0.188 3.188 0.030 0.836 26.746 0.07 30173. 0.3780
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4.12 0.2419 0.4672 0.0536 0.0278 0.004 0.266 0.179 3.149 0.030 0.798 25.848 0.07 30204. 0.3569
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4.47 0.2621 0.4884 0.0510 0.0274 0.004 0.262 0.171 3.102 0.030 0.759 24.938 0.07 30236. 0.3357
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4.81 0.2822 0.5064 0.0482 0.0269 0.004 0.257 0.161 3.046 0.029 0.717 24.013 0.07 30269. 0.3144
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5.15 0.3024 0.5213 0.0453 0.0263 0.004 0.252 0.152 2.983 0.028 0.675 23.069 0.07 30305. 0.2929
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5.50 0.3225 0.5326 0.0424 0.0257 0.004 0.246 0.142 2.911 0.028 0.631 22.098 0.07 30341. 0.2713
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5.84 0.3427 0.5402 0.0394 0.0250 0.004 0.239 0.132 2.831 0.027 0.586 21.095 0.07 30380. 0.2495
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6.19 0.3629 0.5437 0.0363 0.0242 0.004 0.232 0.121 2.744 0.026 0.540 20.051 0.07 30420. 0.2276
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6.53 0.3830 0.5426 0.0331 0.0234 0.004 0.224 0.111 2.648 0.025 0.492 18.957 0.07 30462. 0.2056
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6.87 0.4032 0.5363 0.0299 0.0224 0.003 0.215 0.100 2.545 0.024 0.444 17.800 0.07 30505. 0.1834
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7.22 0.4233 0.5241 0.0266 0.0215 0.003 0.206 0.089 2.434 0.023 0.395 16.566 0.07 30551. 0.1610
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7.56 0.4435 0.5050 0.0232 0.0204 0.003 0.196 0.078 2.315 0.022 0.346 15.237 0.07 30597. 0.1385
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7.90 0.4637 0.4777 0.0199 0.0193 0.003 0.185 0.067 2.189 0.021 0.296 13.788 0.07 30646. 0.1159
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8.25 0.4838 0.4407 0.0165 0.0181 0.003 0.174 0.055 2.056 0.020 0.246 12.188 0.07 30696. 0.0934
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8.59 0.5040 0.3916 0.0131 0.0169 0.003 0.162 0.044 1.916 0.018 0.195 10.397 0.07 30748. 0.0710
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8.93 0.5241 0.3274 0.0098 0.0156 0.002 0.150 0.033 1.770 0.017 0.145 8.360 0.07 30802. 0.0492
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9.28 0.5443 0.2439 0.0064 0.0143 0.002 0.137 0.021 1.619 0.015 0.095 5.998 0.07 30858. 0.0286
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9.62 0.5644 0.1350 0.0031 0.0129 0.002 0.124 0.010 1.463 0.014 0.046 3.201 0.07 30915. 0.0106
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9.96 0.5846 -0.0092 -0.0002 0.0115 0.002 0.110 -0.001 1.302 0.012 -0.003 -0.210 0.07 30973. 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 0.0775 0.0259 0.031 0.991 1.037 23.458 0.112 4.612 20.048 0.14 59860. 0.6655
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0.69 0.0202 0.0590 0.0761 0.0261 0.032 0.999 1.018 23.640 0.113 4.528 19.529 0.14 59891. 0.6423
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1.38 0.0405 0.1150 0.0746 0.0262 0.032 1.006 0.998 23.800 0.114 4.438 19.014 0.14 59925. 0.6191
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2.07 0.0607 0.1678 0.0730 0.0264 0.032 1.011 0.976 23.932 0.114 4.342 18.502 0.14 59962. 0.5959
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2.76 0.0809 0.2176 0.0713 0.0265 0.032 1.016 0.953 24.032 0.115 4.241 17.995 0.14 60000. 0.5728
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3.45 0.1011 0.2644 0.0694 0.0266 0.032 1.018 0.929 24.097 0.115 4.134 17.493 0.14 60042. 0.5497
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4.14 0.1214 0.3083 0.0675 0.0266 0.032 1.019 0.904 24.121 0.115 4.020 16.995 0.14 60086. 0.5267
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4.83 0.1416 0.3492 0.0655 0.0266 0.032 1.019 0.877 24.101 0.115 3.901 16.503 0.14 60132. 0.5038
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5.52 0.1618 0.3873 0.0634 0.0265 0.032 1.016 0.849 24.032 0.115 3.774 16.015 0.14 60182. 0.4809
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6.21 0.1820 0.4226 0.0612 0.0264 0.032 1.010 0.819 23.910 0.114 3.642 15.532 0.14 60234. 0.4581
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6.90 0.2023 0.4550 0.0588 0.0262 0.032 1.003 0.787 23.730 0.113 3.503 15.051 0.14 60290. 0.4354
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7.58 0.2225 0.4846 0.0564 0.0259 0.031 0.993 0.755 23.489 0.112 3.357 14.573 0.14 60348. 0.4127
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8.27 0.2427 0.5113 0.0538 0.0256 0.031 0.980 0.720 23.181 0.111 3.204 14.095 0.14 60409. 0.3900
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8.96 0.2629 0.5351 0.0512 0.0251 0.031 0.964 0.685 22.803 0.109 3.045 13.617 0.14 60474. 0.3673
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9.65 0.2832 0.5559 0.0484 0.0246 0.030 0.945 0.647 22.355 0.107 2.879 13.135 0.14 60542. 0.3445
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10.34 0.3034 0.5735 0.0455 0.0241 0.029 0.923 0.609 21.835 0.104 2.708 12.648 0.14 60613. 0.3217
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11.03 0.3236 0.5877 0.0425 0.0234 0.028 0.898 0.569 21.245 0.101 2.532 12.152 0.14 60687. 0.2988
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11.72 0.3438 0.5984 0.0395 0.0227 0.028 0.870 0.528 20.584 0.098 2.350 11.644 0.14 60764. 0.2759
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12.41 0.3641 0.6050 0.0364 0.0219 0.027 0.839 0.487 19.853 0.095 2.165 11.119 0.14 60845. 0.2528
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13.10 0.3843 0.6072 0.0332 0.0210 0.026 0.805 0.444 19.052 0.091 1.975 10.572 0.14 60929. 0.2296
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13.79 0.4045 0.6043 0.0299 0.0200 0.024 0.768 0.401 18.181 0.087 1.782 9.996 0.14 61017. 0.2063
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14.48 0.4248 0.5956 0.0267 0.0190 0.023 0.729 0.357 17.242 0.082 1.586 9.382 0.14 61107. 0.1826
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15.17 0.4450 0.5798 0.0233 0.0179 0.022 0.686 0.312 16.236 0.078 1.388 8.719 0.14 61202. 0.1588
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15.86 0.4652 0.5555 0.0200 0.0167 0.020 0.641 0.267 15.164 0.072 1.188 7.990 0.14 61300. 0.1346
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16.55 0.4854 0.5206 0.0166 0.0155 0.019 0.593 0.222 14.030 0.067 0.987 7.176 0.14 61401. 0.1102
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17.24 0.5057 0.4719 0.0132 0.0142 0.017 0.543 0.177 12.837 0.061 0.786 6.245 0.14 61506. 0.0856
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17.93 0.5259 0.4049 0.0098 0.0128 0.016 0.490 0.132 11.590 0.055 0.586 5.152 0.14 61614. 0.0609
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18.62 0.5461 0.3125 0.0065 0.0113 0.014 0.435 0.087 10.293 0.049 0.387 3.829 0.14 61726. 0.0368
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19.31 0.5663 0.1833 0.0032 0.0099 0.012 0.378 0.043 8.954 0.043 0.190 2.165 0.15 61841. 0.0146
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20.00 0.5866 -0.0042 -0.0001 0.0083 0.010 0.320 -0.001 7.573 0.036 -0.004 -0.048 0.15 61957. 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 0.0778 0.0249 0.102 2.144 2.343 76.093 0.242 10.420 13.964 0.21 89788. 0.6967
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1.04 0.0202 0.0617 0.0764 0.0251 0.103 2.162 2.300 76.744 0.244 10.230 13.593 0.21 89835. 0.6720
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2.07 0.0405 0.1201 0.0749 0.0253 0.104 2.178 2.254 77.317 0.246 10.027 13.225 0.21 89886. 0.6473
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3.11 0.0607 0.1751 0.0733 0.0254 0.104 2.192 2.206 77.797 0.248 9.812 12.861 0.21 89941. 0.6227
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4.14 0.0810 0.2270 0.0716 0.0255 0.105 2.202 2.155 78.169 0.249 9.583 12.502 0.21 89999. 0.5982
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5.18 0.1012 0.2757 0.0698 0.0256 0.105 2.209 2.100 78.418 0.250 9.341 12.147 0.21 90062. 0.5738
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6.21 0.1215 0.3213 0.0678 0.0257 0.105 2.212 2.043 78.528 0.250 9.085 11.798 0.21 90128. 0.5496
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7.25 0.1417 0.3639 0.0658 0.0256 0.105 2.211 1.982 78.485 0.250 8.815 11.453 0.21 90198. 0.5256
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8.28 0.1620 0.4036 0.0637 0.0256 0.105 2.205 1.918 78.272 0.249 8.530 11.113 0.21 90272. 0.5017
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9.32 0.1822 0.4403 0.0615 0.0254 0.104 2.194 1.850 77.876 0.248 8.231 10.777 0.21 90351. 0.4779
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10.35 0.2025 0.4742 0.0591 0.0252 0.104 2.177 1.780 77.281 0.246 7.916 10.445 0.21 90435. 0.4542
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11.39 0.2227 0.5052 0.0566 0.0250 0.103 2.155 1.706 76.472 0.243 7.587 10.116 0.21 90522. 0.4307
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12.43 0.2430 0.5333 0.0541 0.0246 0.101 2.125 1.628 75.432 0.240 7.242 9.790 0.21 90615. 0.4072
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13.46 0.2632 0.5585 0.0514 0.0242 0.099 2.089 1.547 74.148 0.236 6.882 9.464 0.21 90712. 0.3837
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14.50 0.2835 0.5808 0.0486 0.0237 0.097 2.046 1.463 72.616 0.231 6.508 9.138 0.22 90814. 0.3603
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15.53 0.3037 0.5999 0.0457 0.0231 0.095 1.996 1.376 70.837 0.225 6.121 8.811 0.22 90920. 0.3369
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16.57 0.3240 0.6158 0.0427 0.0225 0.092 1.939 1.286 68.810 0.219 5.722 8.479 0.22 91032. 0.3135
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17.60 0.3442 0.6283 0.0397 0.0217 0.089 1.875 1.194 66.535 0.212 5.312 8.141 0.22 91148. 0.2900
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18.64 0.3645 0.6368 0.0365 0.0209 0.086 1.803 1.100 64.012 0.204 4.893 7.794 0.22 91270. 0.2665
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19.67 0.3847 0.6411 0.0333 0.0200 0.082 1.725 1.004 61.242 0.195 4.464 7.434 0.22 91396. 0.2428
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20.71 0.4050 0.6406 0.0301 0.0190 0.078 1.640 0.906 58.226 0.185 4.029 7.055 0.22 91528. 0.2189
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21.74 0.4252 0.6342 0.0268 0.0180 0.074 1.549 0.806 54.968 0.175 3.586 6.653 0.22 91664. 0.1948
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22.78 0.4455 0.6211 0.0234 0.0168 0.069 1.450 0.706 51.472 0.164 3.139 6.219 0.22 91806. 0.1703
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23.82 0.4657 0.5994 0.0201 0.0156 0.064 1.345 0.604 47.745 0.152 2.688 5.741 0.22 91953. 0.1455
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24.85 0.4860 0.5668 0.0167 0.0143 0.059 1.234 0.502 43.797 0.139 2.235 5.203 0.22 92105. 0.1202
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25.89 0.5062 0.5199 0.0133 0.0129 0.053 1.117 0.400 39.640 0.126 1.781 4.581 0.22 92263. 0.0945
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26.92 0.5265 0.4531 0.0099 0.0115 0.047 0.994 0.299 35.290 0.112 1.329 3.839 0.22 92426. 0.0684
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27.96 0.5467 0.3576 0.0066 0.0100 0.041 0.867 0.198 30.767 0.098 0.880 2.918 0.22 92594. 0.0423
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28.99 0.5670 0.2175 0.0033 0.0085 0.035 0.735 0.098 26.094 0.083 0.438 1.712 0.22 92767. 0.0175
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30.03 0.5872 0.0010 0.0000 0.0069 0.029 0.599 0.000 21.269 0.068 0.002 0.008 0.22 92940. 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 0.0782 0.0243 0.237 3.733 4.187 176.660 0.422 18.622 10.749 0.29 119714. 0.7169
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1.38 0.0203 0.0634 0.0768 0.0246 0.239 3.767 4.110 178.257 0.426 18.282 10.458 0.29 119777. 0.6912
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2.76 0.0406 0.1233 0.0753 0.0248 0.241 3.796 4.029 179.665 0.429 17.921 10.171 0.29 119846. 0.6655
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4.15 0.0608 0.1798 0.0737 0.0249 0.243 3.821 3.943 180.850 0.432 17.536 9.888 0.29 119919. 0.6400
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5.53 0.0811 0.2329 0.0719 0.0250 0.244 3.841 3.851 181.774 0.434 17.128 9.609 0.29 119997. 0.6147
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6.91 0.1014 0.2828 0.0701 0.0251 0.245 3.854 3.754 182.401 0.435 16.696 9.334 0.29 120080. 0.5895
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8.29 0.1217 0.3296 0.0682 0.0252 0.245 3.860 3.651 182.693 0.436 16.238 9.064 0.29 120169. 0.5645
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9.68 0.1419 0.3732 0.0662 0.0252 0.245 3.859 3.542 182.614 0.436 15.755 8.798 0.29 120263. 0.5397
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11.06 0.1622 0.4139 0.0640 0.0251 0.244 3.848 3.428 182.127 0.435 15.246 8.536 0.29 120362. 0.5152
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12.44 0.1825 0.4516 0.0618 0.0250 0.243 3.829 3.307 181.194 0.433 14.710 8.279 0.29 120468. 0.4908
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13.82 0.2028 0.4864 0.0594 0.0248 0.241 3.799 3.181 179.781 0.429 14.148 8.025 0.29 120579. 0.4665
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15.21 0.2230 0.5183 0.0569 0.0245 0.238 3.758 3.048 177.848 0.425 13.558 7.774 0.29 120697. 0.4424
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16.59 0.2433 0.5473 0.0544 0.0242 0.235 3.705 2.909 175.355 0.419 12.941 7.526 0.29 120820. 0.4184
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17.97 0.2636 0.5735 0.0516 0.0237 0.231 3.640 2.765 172.270 0.411 12.297 7.279 0.29 120950. 0.3945
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19.35 0.2839 0.5968 0.0488 0.0232 0.226 3.562 2.614 168.583 0.402 11.628 7.033 0.29 121086. 0.3707
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20.74 0.3041 0.6170 0.0459 0.0226 0.220 3.472 2.458 164.293 0.392 10.935 6.787 0.29 121229. 0.3469
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22.12 0.3244 0.6341 0.0429 0.0220 0.214 3.368 2.298 159.399 0.381 10.221 6.539 0.29 121378. 0.3231
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23.50 0.3447 0.6477 0.0398 0.0212 0.206 3.252 2.133 153.900 0.367 9.488 6.286 0.29 121534. 0.2993
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24.88 0.3650 0.6576 0.0367 0.0204 0.198 3.123 1.964 147.794 0.353 8.737 6.028 0.29 121696. 0.2754
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26.27 0.3852 0.6634 0.0335 0.0194 0.189 2.981 1.792 141.085 0.337 7.971 5.761 0.29 121865. 0.2514
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27.65 0.4055 0.6644 0.0302 0.0184 0.179 2.827 1.617 133.775 0.319 7.191 5.482 0.29 122041. 0.2272
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29.03 0.4258 0.6599 0.0269 0.0173 0.169 2.660 1.439 125.872 0.300 6.400 5.185 0.29 122224. 0.2027
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30.41 0.4461 0.6486 0.0235 0.0162 0.157 2.480 1.259 117.387 0.280 5.600 4.864 0.29 122414. 0.1779
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31.80 0.4664 0.6288 0.0201 0.0149 0.145 2.289 1.078 108.337 0.259 4.793 4.511 0.29 122610. 0.1527
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33.18 0.4866 0.5982 0.0167 0.0136 0.132 2.087 0.895 98.746 0.236 3.982 4.112 0.29 122814. 0.1268
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34.56 0.5069 0.5527 0.0133 0.0122 0.119 1.873 0.713 88.643 0.212 3.171 3.648 0.29 123024. 0.1004
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35.94 0.5272 0.4864 0.0099 0.0108 0.105 1.650 0.531 78.070 0.186 2.363 3.086 0.29 123242. 0.0733
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37.33 0.5475 0.3886 0.0066 0.0092 0.090 1.417 0.351 67.075 0.160 1.562 2.375 0.29 123467. 0.0459
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38.71 0.5677 0.2398 0.0032 0.0077 0.075 1.177 0.174 55.716 0.133 0.772 1.413 0.29 123698. 0.0192
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40.09 0.5880 -0.0034 0.0000 0.0061 0.059 0.929 -0.002 43.967 0.105 -0.008 -0.019 0.29 123928. 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 0.0787 0.0241 0.458 5.773 6.585 341.487 0.652 29.288 8.746 0.36 149637. 0.7316
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1.73 0.0203 0.0645 0.0773 0.0243 0.462 5.827 6.465 344.676 0.658 28.756 8.507 0.36 149717. 0.7051
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3.46 0.0406 0.1254 0.0758 0.0245 0.466 5.874 6.337 347.494 0.664 28.189 8.272 0.36 149802. 0.6788
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5.19 0.0609 0.1828 0.0742 0.0247 0.469 5.914 6.202 349.866 0.668 27.585 8.040 0.36 149894. 0.6527
|
|
6.92 0.0812 0.2369 0.0724 0.0248 0.472 5.946 6.058 351.721 0.672 26.945 7.812 0.36 149992. 0.6268
|
|
8.65 0.1014 0.2876 0.0706 0.0249 0.473 5.967 5.905 352.986 0.674 26.265 7.588 0.36 150096. 0.6010
|
|
10.37 0.1217 0.3351 0.0687 0.0249 0.474 5.977 5.743 353.586 0.675 25.547 7.367 0.36 150208. 0.5756
|
|
12.10 0.1420 0.3795 0.0666 0.0249 0.474 5.975 5.573 353.448 0.675 24.787 7.151 0.36 150325. 0.5503
|
|
13.83 0.1623 0.4208 0.0645 0.0249 0.473 5.959 5.393 352.497 0.673 23.987 6.939 0.36 150450. 0.5253
|
|
15.56 0.1826 0.4592 0.0622 0.0247 0.470 5.928 5.203 350.660 0.670 23.144 6.730 0.36 150583. 0.5005
|
|
17.29 0.2029 0.4946 0.0598 0.0245 0.466 5.881 5.004 347.866 0.664 22.260 6.525 0.36 150722. 0.4758
|
|
19.02 0.2232 0.5272 0.0573 0.0243 0.461 5.816 4.796 344.040 0.657 21.333 6.323 0.36 150869. 0.4514
|
|
20.75 0.2435 0.5570 0.0547 0.0239 0.455 5.732 4.578 339.098 0.648 20.362 6.123 0.36 151024. 0.4271
|
|
22.48 0.2637 0.5839 0.0520 0.0235 0.447 5.629 4.350 332.977 0.636 19.348 5.925 0.36 151187. 0.4028
|
|
24.21 0.2840 0.6079 0.0492 0.0230 0.437 5.505 4.113 325.657 0.622 18.294 5.728 0.36 151358. 0.3787
|
|
25.94 0.3043 0.6290 0.0462 0.0224 0.425 5.361 3.868 317.132 0.606 17.204 5.532 0.36 151537. 0.3546
|
|
27.66 0.3246 0.6469 0.0432 0.0217 0.412 5.196 3.615 307.401 0.587 16.080 5.334 0.36 151723. 0.3306
|
|
29.39 0.3449 0.6616 0.0401 0.0209 0.398 5.011 3.356 296.459 0.566 14.926 5.134 0.36 151918. 0.3066
|
|
31.12 0.3652 0.6726 0.0369 0.0201 0.381 4.806 3.090 284.306 0.543 13.744 4.930 0.36 152122. 0.2825
|
|
32.85 0.3855 0.6796 0.0337 0.0191 0.363 4.580 2.819 270.944 0.517 12.538 4.719 0.36 152333. 0.2582
|
|
34.58 0.4058 0.6820 0.0304 0.0181 0.344 4.334 2.543 256.381 0.490 11.310 4.498 0.36 152554. 0.2338
|
|
36.31 0.4260 0.6789 0.0271 0.0170 0.323 4.068 2.263 240.631 0.460 10.065 4.265 0.36 152782. 0.2091
|
|
38.04 0.4463 0.6693 0.0237 0.0158 0.300 3.782 1.979 223.716 0.427 8.805 4.013 0.36 153020. 0.1841
|
|
39.77 0.4666 0.6513 0.0203 0.0145 0.276 3.477 1.694 205.671 0.393 7.534 3.736 0.36 153266. 0.1585
|
|
41.50 0.4869 0.6224 0.0168 0.0132 0.250 3.153 1.407 186.542 0.356 6.258 3.421 0.36 153520. 0.1323
|
|
43.23 0.5072 0.5786 0.0134 0.0117 0.223 2.813 1.120 166.390 0.318 4.982 3.053 0.36 153784. 0.1053
|
|
44.96 0.5275 0.5131 0.0100 0.0103 0.195 2.456 0.834 145.298 0.277 3.710 2.604 0.36 154056. 0.0775
|
|
46.68 0.5478 0.4144 0.0066 0.0087 0.165 2.085 0.551 123.365 0.236 2.449 2.025 0.36 154338. 0.0490
|
|
48.41 0.5681 0.2593 0.0032 0.0071 0.135 1.702 0.271 100.706 0.192 1.207 1.222 0.36 154627. 0.0207
|
|
50.14 0.5883 -0.0065 -0.0001 0.0054 0.104 1.306 -0.005 77.238 0.148 -0.022 -0.029 0.36 154912. 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 0.0794 0.0240 0.789 8.286 9.559 588.209 0.936 42.517 7.371 0.43 179556. 0.7429
|
|
2.08 0.0203 0.0652 0.0779 0.0242 0.796 8.365 9.386 593.820 0.945 41.748 7.169 0.43 179652. 0.7160
|
|
4.15 0.0406 0.1268 0.0764 0.0244 0.803 8.435 9.201 598.774 0.953 40.927 6.970 0.43 179755. 0.6892
|
|
6.23 0.0609 0.1849 0.0748 0.0246 0.809 8.494 9.005 602.944 0.960 40.054 6.774 0.43 179866. 0.6626
|
|
8.30 0.0812 0.2395 0.0730 0.0248 0.813 8.540 8.796 606.204 0.965 39.127 6.582 0.43 179984. 0.6363
|
|
10.38 0.1014 0.2908 0.0712 0.0248 0.816 8.571 8.575 608.424 0.968 38.143 6.393 0.43 180110. 0.6102
|
|
12.45 0.1217 0.3388 0.0693 0.0249 0.817 8.586 8.341 609.475 0.970 37.101 6.207 0.43 180243. 0.5844
|
|
14.53 0.1420 0.3837 0.0672 0.0249 0.817 8.582 8.094 609.224 0.970 36.001 6.026 0.43 180385. 0.5588
|
|
16.60 0.1623 0.4256 0.0650 0.0248 0.815 8.558 7.833 607.543 0.967 34.840 5.848 0.43 180536. 0.5335
|
|
18.68 0.1826 0.4645 0.0628 0.0247 0.810 8.513 7.558 604.304 0.962 33.618 5.673 0.43 180695. 0.5084
|
|
20.75 0.2029 0.5004 0.0604 0.0245 0.804 8.444 7.270 599.380 0.954 32.335 5.501 0.43 180863. 0.4835
|
|
22.83 0.2232 0.5336 0.0578 0.0242 0.795 8.349 6.967 592.640 0.943 30.989 5.332 0.43 181040. 0.4588
|
|
24.90 0.2435 0.5639 0.0552 0.0238 0.783 8.226 6.650 583.938 0.929 29.580 5.166 0.43 181226. 0.4342
|
|
26.98 0.2638 0.5914 0.0525 0.0234 0.769 8.074 6.319 573.161 0.912 28.109 5.001 0.43 181422. 0.4098
|
|
29.05 0.2841 0.6161 0.0496 0.0229 0.751 7.893 5.975 560.271 0.892 26.578 4.837 0.43 181627. 0.3855
|
|
31.13 0.3043 0.6379 0.0467 0.0223 0.731 7.681 5.619 545.258 0.868 24.995 4.674 0.43 181842. 0.3612
|
|
33.20 0.3246 0.6566 0.0436 0.0216 0.708 7.440 5.252 528.115 0.841 23.362 4.511 0.43 182066. 0.3370
|
|
35.28 0.3449 0.6721 0.0405 0.0208 0.682 7.168 4.875 508.838 0.810 21.685 4.346 0.43 182301. 0.3128
|
|
37.35 0.3652 0.6840 0.0373 0.0199 0.654 6.866 4.489 487.424 0.776 19.968 4.177 0.43 182545. 0.2885
|
|
39.43 0.3855 0.6921 0.0340 0.0189 0.622 6.535 4.095 463.878 0.738 18.215 4.004 0.43 182800. 0.2641
|
|
41.50 0.4058 0.6957 0.0307 0.0179 0.588 6.173 3.694 438.211 0.697 16.431 3.823 0.43 183064. 0.2396
|
|
43.58 0.4261 0.6939 0.0273 0.0168 0.550 5.782 3.287 410.449 0.653 14.621 3.632 0.43 183339. 0.2147
|
|
45.65 0.4464 0.6857 0.0239 0.0155 0.510 5.362 2.875 380.632 0.606 12.789 3.426 0.43 183624. 0.1894
|
|
47.73 0.4667 0.6693 0.0204 0.0142 0.468 4.914 2.460 348.819 0.555 10.943 3.199 0.43 183919. 0.1636
|
|
49.80 0.4870 0.6422 0.0170 0.0129 0.423 4.439 2.043 315.093 0.501 9.088 2.941 0.43 184225. 0.1371
|
|
51.88 0.5072 0.6000 0.0135 0.0114 0.375 3.938 1.626 279.564 0.445 7.233 2.638 0.43 184542. 0.1097
|
|
53.95 0.5275 0.5358 0.0101 0.0099 0.325 3.414 1.210 242.376 0.386 5.384 2.265 0.43 184869. 0.0812
|
|
56.03 0.5478 0.4367 0.0066 0.0083 0.273 2.870 0.799 203.708 0.324 3.552 1.778 0.43 185206. 0.0518
|
|
58.10 0.5681 0.2770 0.0033 0.0067 0.220 2.307 0.393 163.764 0.261 1.746 1.087 0.44 185553. 0.0222
|
|
60.18 0.5884 -0.0092 -0.0001 0.0050 0.164 1.723 -0.009 122.342 0.195 -0.042 -0.035 0.44 185894. 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 0.0802 0.0241 1.256 11.307 13.139 936.432 1.277 58.441 6.364 0.50 209470. 0.7519
|
|
2.42 0.0203 0.0657 0.0787 0.0243 1.268 11.416 12.902 945.476 1.290 57.389 6.190 0.50 209583. 0.7247
|
|
4.84 0.0406 0.1277 0.0772 0.0245 1.279 11.513 12.650 953.454 1.301 56.266 6.018 0.50 209704. 0.6977
|
|
7.26 0.0609 0.1862 0.0755 0.0247 1.288 11.594 12.381 960.159 1.310 55.071 5.849 0.50 209833. 0.6709
|
|
9.68 0.0811 0.2412 0.0738 0.0248 1.295 11.657 12.096 965.386 1.317 53.801 5.683 0.50 209971. 0.6443
|
|
12.10 0.1014 0.2929 0.0719 0.0249 1.299 11.699 11.792 968.927 1.322 52.453 5.520 0.50 210119. 0.6179
|
|
14.52 0.1217 0.3413 0.0700 0.0250 1.302 11.719 11.471 970.571 1.324 51.025 5.361 0.50 210275. 0.5919
|
|
16.94 0.1420 0.3866 0.0679 0.0249 1.301 11.714 11.132 970.107 1.323 49.515 5.205 0.50 210441. 0.5661
|
|
19.36 0.1623 0.4288 0.0657 0.0249 1.297 11.680 10.774 967.325 1.320 47.923 5.052 0.50 210617. 0.5405
|
|
21.78 0.1826 0.4681 0.0634 0.0247 1.290 11.616 10.397 962.019 1.312 46.246 4.902 0.50 210804. 0.5152
|
|
24.20 0.2028 0.5045 0.0610 0.0245 1.279 11.519 10.001 953.987 1.301 44.484 4.755 0.50 211000. 0.4902
|
|
26.62 0.2231 0.5381 0.0585 0.0242 1.265 11.387 9.586 943.017 1.286 42.636 4.610 0.50 211207. 0.4653
|
|
29.04 0.2434 0.5689 0.0558 0.0239 1.246 11.216 9.150 928.877 1.267 40.701 4.468 0.50 211425. 0.4406
|
|
31.46 0.2637 0.5970 0.0530 0.0234 1.222 11.005 8.696 911.378 1.243 38.678 4.328 0.50 211654. 0.4160
|
|
33.89 0.2840 0.6222 0.0502 0.0229 1.194 10.752 8.223 890.456 1.215 36.575 4.188 0.50 211894. 0.3915
|
|
36.31 0.3043 0.6446 0.0472 0.0223 1.161 10.458 7.733 866.094 1.182 34.397 4.050 0.50 212145. 0.3671
|
|
38.73 0.3246 0.6640 0.0441 0.0216 1.124 10.122 7.228 838.283 1.144 32.152 3.911 0.50 212407. 0.3428
|
|
41.15 0.3448 0.6803 0.0409 0.0208 1.082 9.744 6.710 807.014 1.101 29.845 3.771 0.50 212681. 0.3184
|
|
43.57 0.3651 0.6931 0.0377 0.0199 1.036 9.325 6.179 772.283 1.054 27.483 3.629 0.50 212966. 0.2940
|
|
45.99 0.3854 0.7021 0.0344 0.0189 0.984 8.864 5.636 734.098 1.001 25.071 3.483 0.50 213263. 0.2695
|
|
48.41 0.4057 0.7067 0.0310 0.0178 0.929 8.361 5.084 692.477 0.945 22.616 3.330 0.50 213572. 0.2448
|
|
50.83 0.4260 0.7062 0.0276 0.0166 0.868 7.818 4.524 647.462 0.883 20.124 3.169 0.50 213893. 0.2198
|
|
53.25 0.4463 0.6994 0.0241 0.0154 0.803 7.234 3.958 599.118 0.817 17.603 2.996 0.50 214225. 0.1943
|
|
55.67 0.4666 0.6845 0.0207 0.0141 0.734 6.611 3.386 547.541 0.747 15.061 2.805 0.51 214570. 0.1683
|
|
58.09 0.4868 0.6590 0.0172 0.0127 0.661 5.951 2.812 492.864 0.672 12.508 2.588 0.51 214927. 0.1415
|
|
60.51 0.5071 0.6185 0.0136 0.0112 0.584 5.256 2.237 435.269 0.594 9.952 2.332 0.51 215296. 0.1137
|
|
62.93 0.5274 0.5557 0.0102 0.0096 0.503 4.528 1.665 374.989 0.512 7.407 2.014 0.51 215677. 0.0847
|
|
65.35 0.5477 0.4568 0.0067 0.0080 0.419 3.771 1.098 312.315 0.426 4.884 1.595 0.51 216071. 0.0545
|
|
67.77 0.5680 0.2933 0.0033 0.0064 0.332 2.989 0.539 247.581 0.338 2.397 0.987 0.51 216476. 0.0236
|
|
70.19 0.5883 -0.0119 -0.0001 0.0046 0.242 2.178 -0.015 180.380 0.246 -0.068 -0.039 0.51 216870. 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 0.0811 0.0243 1.889 14.882 17.364 1408.613 1.681 77.233 5.591 0.57 239377. 0.7595
|
|
2.76 0.0203 0.0659 0.0796 0.0245 1.907 15.027 17.053 1422.309 1.698 75.853 5.438 0.57 239507. 0.7321
|
|
5.53 0.0405 0.1282 0.0781 0.0247 1.924 15.155 16.722 1434.369 1.712 74.378 5.288 0.57 239646. 0.7048
|
|
8.29 0.0608 0.1869 0.0765 0.0249 1.937 15.261 16.369 1444.476 1.724 72.808 5.140 0.57 239795. 0.6779
|
|
11.06 0.0811 0.2421 0.0747 0.0250 1.948 15.344 15.993 1452.320 1.734 71.137 4.995 0.57 239953. 0.6511
|
|
13.82 0.1014 0.2941 0.0728 0.0251 1.955 15.400 15.594 1457.587 1.740 69.363 4.853 0.57 240122. 0.6247
|
|
16.59 0.1216 0.3428 0.0709 0.0251 1.958 15.425 15.171 1459.950 1.743 67.483 4.713 0.57 240302. 0.5985
|
|
19.35 0.1419 0.3883 0.0688 0.0251 1.957 15.416 14.724 1459.094 1.742 65.494 4.577 0.57 240493. 0.5725
|
|
22.12 0.1622 0.4309 0.0666 0.0251 1.951 15.369 14.252 1454.697 1.736 63.395 4.444 0.57 240694. 0.5469
|
|
24.88 0.1825 0.4705 0.0642 0.0249 1.940 15.282 13.755 1446.449 1.727 61.183 4.313 0.57 240908. 0.5215
|
|
27.65 0.2027 0.5073 0.0618 0.0247 1.923 15.151 13.233 1434.044 1.712 58.859 4.185 0.57 241133. 0.4963
|
|
30.41 0.2230 0.5412 0.0592 0.0244 1.900 14.973 12.684 1417.165 1.692 56.420 4.060 0.57 241370. 0.4713
|
|
33.18 0.2433 0.5725 0.0566 0.0240 1.871 14.743 12.110 1395.463 1.666 53.864 3.936 0.57 241620. 0.4465
|
|
35.94 0.2636 0.6010 0.0538 0.0236 1.835 14.460 11.509 1368.646 1.634 51.193 3.814 0.57 241882. 0.4218
|
|
38.70 0.2838 0.6267 0.0508 0.0230 1.792 14.122 10.884 1336.608 1.595 48.414 3.694 0.57 242157. 0.3972
|
|
41.47 0.3041 0.6497 0.0478 0.0224 1.742 13.728 10.237 1299.327 1.551 45.535 3.574 0.57 242444. 0.3727
|
|
44.23 0.3244 0.6698 0.0447 0.0216 1.685 13.278 9.570 1256.787 1.500 42.567 3.454 0.57 242744. 0.3483
|
|
47.00 0.3447 0.6867 0.0415 0.0208 1.621 12.773 8.884 1208.979 1.443 39.516 3.333 0.57 243058. 0.3238
|
|
49.76 0.3649 0.7004 0.0382 0.0199 1.550 12.212 8.181 1155.897 1.380 36.391 3.210 0.58 243384. 0.2993
|
|
52.53 0.3852 0.7103 0.0349 0.0189 1.472 11.596 7.464 1097.552 1.310 33.199 3.084 0.58 243723. 0.2747
|
|
55.29 0.4055 0.7160 0.0314 0.0178 1.387 10.924 6.733 1033.976 1.234 29.949 2.954 0.58 244076. 0.2498
|
|
58.06 0.4258 0.7166 0.0280 0.0166 1.294 10.198 5.992 965.229 1.152 26.651 2.816 0.58 244443. 0.2247
|
|
60.82 0.4460 0.7111 0.0245 0.0154 1.195 9.418 5.241 891.413 1.064 23.313 2.667 0.58 244823. 0.1990
|
|
63.59 0.4663 0.6977 0.0209 0.0140 1.090 8.586 4.485 812.673 0.970 19.947 2.503 0.58 245217. 0.1728
|
|
66.35 0.4866 0.6738 0.0174 0.0126 0.978 7.704 3.724 729.215 0.870 16.565 2.316 0.58 245625. 0.1457
|
|
69.12 0.5068 0.6350 0.0138 0.0110 0.860 6.776 2.963 641.313 0.766 13.180 2.096 0.58 246046. 0.1176
|
|
71.88 0.5271 0.5737 0.0103 0.0095 0.737 5.804 2.205 549.324 0.656 9.807 1.821 0.58 246482. 0.0881
|
|
74.65 0.5474 0.4755 0.0068 0.0078 0.608 4.793 1.453 453.698 0.542 6.465 1.453 0.58 246932. 0.0571
|
|
77.41 0.5677 0.3090 0.0033 0.0061 0.476 3.750 0.713 354.945 0.424 3.169 0.911 0.58 247394. 0.0251
|
|
80.17 0.5879 -0.0143 -0.0001 0.0043 0.338 2.666 -0.023 252.335 0.301 -0.101 -0.041 0.58 247842. 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 0.0822 0.0246 2.724 19.078 22.286 2031.450 2.155 99.128 4.976 0.64 269276. 0.7657
|
|
3.11 0.0203 0.0659 0.0808 0.0248 2.751 19.264 21.891 2051.243 2.176 97.372 4.841 0.64 269423. 0.7383
|
|
6.22 0.0405 0.1283 0.0792 0.0250 2.774 19.427 21.469 2068.629 2.195 95.495 4.707 0.64 269580. 0.7110
|
|
9.32 0.0608 0.1871 0.0776 0.0252 2.794 19.564 21.019 2083.146 2.210 93.494 4.577 0.64 269749. 0.6840
|
|
12.43 0.0810 0.2424 0.0758 0.0253 2.809 19.669 20.540 2094.345 2.222 91.363 4.448 0.64 269928. 0.6572
|
|
15.54 0.1013 0.2945 0.0739 0.0254 2.819 19.738 20.031 2101.763 2.230 89.099 4.323 0.64 270119. 0.6307
|
|
18.65 0.1215 0.3433 0.0719 0.0255 2.823 19.768 19.491 2104.932 2.233 86.698 4.200 0.64 270322. 0.6045
|
|
21.75 0.1418 0.3891 0.0698 0.0254 2.821 19.754 18.920 2103.384 2.232 84.155 4.080 0.64 270537. 0.5785
|
|
24.86 0.1621 0.4318 0.0676 0.0254 2.812 19.691 18.316 2096.664 2.225 81.470 3.962 0.64 270765. 0.5528
|
|
27.97 0.1823 0.4717 0.0652 0.0252 2.795 19.575 17.680 2084.319 2.212 78.639 3.847 0.64 271006. 0.5273
|
|
31.08 0.2026 0.5088 0.0628 0.0250 2.770 19.402 17.010 2065.909 2.192 75.662 3.735 0.64 271261. 0.5021
|
|
34.18 0.2228 0.5431 0.0602 0.0247 2.737 19.168 16.308 2040.983 2.166 72.538 3.624 0.64 271529. 0.4771
|
|
37.29 0.2431 0.5747 0.0575 0.0243 2.694 18.868 15.572 2009.041 2.132 69.263 3.516 0.64 271810. 0.4522
|
|
40.40 0.2633 0.6037 0.0546 0.0238 2.641 18.498 14.802 1969.651 2.090 65.837 3.408 0.64 272106. 0.4275
|
|
43.51 0.2836 0.6299 0.0517 0.0233 2.578 18.056 14.000 1922.651 2.040 62.271 3.303 0.65 272415. 0.4028
|
|
46.61 0.3039 0.6534 0.0486 0.0226 2.505 17.543 13.169 1868.008 1.982 58.577 3.198 0.65 272739. 0.3783
|
|
49.72 0.3241 0.6741 0.0454 0.0218 2.421 16.958 12.312 1805.707 1.916 54.765 3.093 0.65 273077. 0.3537
|
|
52.83 0.3444 0.6918 0.0422 0.0210 2.328 16.301 11.431 1735.736 1.842 50.846 2.987 0.65 273430. 0.3292
|
|
55.94 0.3646 0.7063 0.0389 0.0201 2.224 15.572 10.528 1658.090 1.759 46.830 2.880 0.65 273797. 0.3046
|
|
59.04 0.3849 0.7171 0.0354 0.0190 2.109 14.771 9.606 1572.788 1.669 42.727 2.770 0.65 274179. 0.2799
|
|
62.15 0.4051 0.7238 0.0320 0.0179 1.985 13.898 8.667 1479.876 1.570 38.549 2.656 0.65 274577. 0.2549
|
|
65.26 0.4254 0.7256 0.0285 0.0167 1.850 12.955 7.713 1379.446 1.464 34.307 2.536 0.65 274989. 0.2296
|
|
68.37 0.4457 0.7213 0.0249 0.0154 1.705 11.942 6.748 1271.644 1.349 30.013 2.407 0.65 275417. 0.2038
|
|
71.48 0.4659 0.7094 0.0213 0.0140 1.551 10.863 5.774 1156.682 1.227 25.682 2.264 0.65 275859. 0.1773
|
|
74.58 0.4862 0.6872 0.0177 0.0125 1.388 9.719 4.795 1034.862 1.098 21.328 2.102 0.65 276318. 0.1500
|
|
77.69 0.5064 0.6501 0.0141 0.0110 1.216 8.514 3.815 906.582 0.962 16.970 1.909 0.65 276792. 0.1215
|
|
80.80 0.5267 0.5905 0.0105 0.0093 1.036 7.254 2.839 772.365 0.820 12.627 1.667 0.65 277281. 0.0916
|
|
83.91 0.5469 0.4932 0.0069 0.0077 0.849 5.943 1.871 632.866 0.671 8.322 1.341 0.65 277786. 0.0598
|
|
87.01 0.5672 0.3244 0.0034 0.0059 0.656 4.591 0.917 488.841 0.519 4.077 0.851 0.65 278306. 0.0265
|
|
90.12 0.5875 -0.0166 -0.0001 0.0041 0.455 3.185 -0.031 339.095 0.360 -0.140 -0.042 0.65 278806. 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 0.0836 0.0250 3.807 23.994 27.977 2838.771 2.711 124.442 4.470 0.71 299164. 0.7707
|
|
3.45 0.0202 0.0658 0.0822 0.0253 3.844 24.226 27.488 2866.168 2.737 122.266 4.350 0.71 299328. 0.7434
|
|
6.90 0.0405 0.1280 0.0806 0.0255 3.876 24.429 26.964 2890.223 2.760 119.935 4.232 0.71 299504. 0.7163
|
|
10.35 0.0607 0.1867 0.0789 0.0257 3.903 24.598 26.405 2910.249 2.779 117.448 4.115 0.71 299692. 0.6893
|
|
13.80 0.0809 0.2420 0.0771 0.0258 3.923 24.728 25.808 2925.582 2.794 114.796 4.001 0.71 299893. 0.6626
|
|
17.24 0.1012 0.2940 0.0753 0.0259 3.937 24.812 25.174 2935.561 2.803 111.975 3.890 0.71 300106. 0.6362
|
|
20.69 0.1214 0.3429 0.0732 0.0259 3.942 24.845 24.501 2939.513 2.807 108.979 3.780 0.71 300333. 0.6100
|
|
24.14 0.1416 0.3888 0.0711 0.0259 3.938 24.822 23.787 2936.791 2.804 105.805 3.674 0.71 300574. 0.5841
|
|
27.59 0.1619 0.4317 0.0688 0.0258 3.925 24.738 23.033 2926.747 2.795 102.449 3.569 0.71 300828. 0.5584
|
|
31.04 0.1821 0.4718 0.0665 0.0257 3.901 24.586 22.237 2908.757 2.778 98.909 3.467 0.72 301097. 0.5330
|
|
34.49 0.2023 0.5091 0.0640 0.0254 3.865 24.361 21.399 2882.210 2.752 95.183 3.368 0.72 301381. 0.5078
|
|
37.94 0.2226 0.5438 0.0613 0.0251 3.817 24.059 20.519 2846.484 2.718 91.271 3.270 0.72 301679. 0.4828
|
|
41.39 0.2428 0.5758 0.0586 0.0247 3.756 23.674 19.597 2800.903 2.675 87.167 3.173 0.72 301993. 0.4580
|
|
44.83 0.2630 0.6051 0.0557 0.0242 3.681 23.200 18.631 2744.840 2.621 82.873 3.079 0.72 302322. 0.4332
|
|
48.28 0.2833 0.6319 0.0527 0.0236 3.591 22.636 17.626 2678.059 2.557 78.399 2.985 0.72 302667. 0.4085
|
|
51.73 0.3035 0.6560 0.0496 0.0229 3.487 21.980 16.583 2600.512 2.483 73.762 2.892 0.72 303027. 0.3840
|
|
55.18 0.3237 0.6773 0.0464 0.0222 3.369 21.234 15.507 2512.195 2.399 68.974 2.800 0.72 303404. 0.3594
|
|
58.63 0.3440 0.6957 0.0430 0.0213 3.236 20.396 14.400 2413.089 2.304 64.050 2.707 0.72 303796. 0.3348
|
|
62.08 0.3642 0.7109 0.0397 0.0203 3.089 19.467 13.265 2303.203 2.199 59.002 2.612 0.72 304204. 0.3101
|
|
65.53 0.3844 0.7226 0.0362 0.0192 2.927 18.448 12.105 2182.565 2.084 53.843 2.516 0.72 304629. 0.2853
|
|
68.98 0.4047 0.7304 0.0327 0.0181 2.751 17.338 10.923 2051.259 1.959 48.587 2.415 0.72 305071. 0.2602
|
|
72.42 0.4249 0.7333 0.0291 0.0168 2.561 16.139 9.723 1909.436 1.823 43.248 2.310 0.72 305529. 0.2348
|
|
75.87 0.4451 0.7304 0.0254 0.0155 2.357 14.853 8.508 1757.340 1.678 37.843 2.196 0.72 306003. 0.2088
|
|
79.32 0.4654 0.7199 0.0218 0.0141 2.139 13.484 7.281 1595.314 1.523 32.387 2.070 0.72 306495. 0.1821
|
|
82.77 0.4856 0.6991 0.0181 0.0126 1.909 12.035 6.048 1423.849 1.360 26.902 1.927 0.72 307004. 0.1545
|
|
86.22 0.5058 0.6636 0.0144 0.0110 1.668 10.511 4.813 1243.594 1.188 21.409 1.756 0.72 307530. 0.1256
|
|
89.67 0.5260 0.6052 0.0107 0.0093 1.415 8.920 3.582 1055.399 1.008 15.933 1.539 0.72 308073. 0.0950
|
|
93.12 0.5463 0.5082 0.0071 0.0076 1.154 7.272 2.361 860.335 0.822 10.503 1.245 0.72 308633. 0.0624
|
|
96.57 0.5665 0.3368 0.0035 0.0058 0.885 5.575 1.157 659.640 0.630 5.146 0.796 0.73 309209. 0.0279
|
|
100.01 0.5867 -0.0177 -0.0001 0.0040 0.606 3.817 -0.040 451.605 0.431 -0.179 -0.040 0.73 309762. 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 0.0853 0.0260 5.269 30.189 34.533 3928.824 3.411 153.602 3.987 0.79 329037. 0.7637
|
|
3.79 0.0202 0.0646 0.0838 0.0262 5.307 30.407 33.940 3957.322 3.435 150.965 3.890 0.79 329219. 0.7388
|
|
7.57 0.0404 0.1259 0.0823 0.0264 5.340 30.595 33.304 3981.784 3.457 148.135 3.794 0.79 329414. 0.7137
|
|
11.36 0.0606 0.1841 0.0806 0.0265 5.366 30.746 32.623 4001.388 3.474 145.109 3.698 0.79 329622. 0.6885
|
|
15.14 0.0808 0.2392 0.0788 0.0266 5.385 30.853 31.897 4015.300 3.486 141.877 3.603 0.79 329844. 0.6633
|
|
18.93 0.1010 0.2912 0.0769 0.0267 5.394 30.909 31.123 4022.645 3.492 138.434 3.509 0.79 330080. 0.6382
|
|
22.72 0.1212 0.3403 0.0749 0.0267 5.394 30.908 30.299 4022.524 3.492 134.771 3.416 0.79 330331. 0.6130
|
|
26.50 0.1414 0.3863 0.0727 0.0266 5.383 30.843 29.426 4014.023 3.485 130.886 3.325 0.79 330597. 0.5880
|
|
30.29 0.1615 0.4296 0.0704 0.0265 5.359 30.706 28.501 3996.215 3.469 126.772 3.235 0.79 330879. 0.5630
|
|
34.08 0.1817 0.4700 0.0680 0.0263 5.321 30.491 27.524 3968.179 3.445 122.428 3.146 0.79 331176. 0.5380
|
|
37.86 0.2019 0.5077 0.0655 0.0260 5.269 30.190 26.495 3929.003 3.411 117.851 3.059 0.79 331489. 0.5132
|
|
41.65 0.2221 0.5427 0.0628 0.0257 5.200 29.796 25.414 3877.766 3.366 113.040 2.973 0.79 331819. 0.4885
|
|
45.43 0.2423 0.5752 0.0600 0.0253 5.114 29.302 24.279 3813.456 3.311 107.991 2.888 0.79 332165. 0.4638
|
|
49.22 0.2625 0.6050 0.0570 0.0247 5.009 28.701 23.090 3735.188 3.243 102.703 2.804 0.79 332528. 0.4392
|
|
53.01 0.2827 0.6323 0.0540 0.0241 4.885 27.989 21.850 3642.562 3.162 97.189 2.721 0.79 332908. 0.4146
|
|
56.79 0.3029 0.6569 0.0508 0.0234 4.741 27.166 20.564 3535.417 3.069 91.469 2.638 0.79 333305. 0.3900
|
|
60.58 0.3231 0.6787 0.0475 0.0226 4.578 26.231 19.235 3413.756 2.964 85.559 2.556 0.79 333719. 0.3654
|
|
64.37 0.3433 0.6977 0.0441 0.0217 4.395 25.185 17.868 3277.691 2.845 79.476 2.473 0.79 334151. 0.3407
|
|
68.15 0.3635 0.7135 0.0407 0.0207 4.194 24.030 16.465 3127.328 2.715 73.236 2.388 0.79 334600. 0.3159
|
|
71.94 0.3837 0.7257 0.0371 0.0196 3.973 22.766 15.031 2962.869 2.572 66.856 2.301 0.79 335068. 0.2908
|
|
75.72 0.4039 0.7337 0.0335 0.0185 3.734 21.397 13.568 2784.618 2.417 60.352 2.210 0.79 335553. 0.2654
|
|
79.51 0.4241 0.7367 0.0298 0.0172 3.477 19.924 12.082 2593.023 2.251 53.741 2.113 0.79 336056. 0.2395
|
|
83.30 0.4442 0.7334 0.0261 0.0158 3.203 18.354 10.576 2388.660 2.074 47.043 2.008 0.79 336577. 0.2129
|
|
87.08 0.4644 0.7218 0.0224 0.0144 2.913 16.692 9.056 2172.311 1.886 40.279 1.891 0.79 337117. 0.1855
|
|
90.87 0.4846 0.6991 0.0186 0.0129 2.608 14.945 7.526 1944.988 1.688 33.474 1.755 0.79 337676. 0.1569
|
|
94.65 0.5048 0.6603 0.0148 0.0113 2.290 13.124 5.992 1707.958 1.483 26.652 1.591 0.80 338253. 0.1270
|
|
98.44 0.5250 0.5971 0.0110 0.0097 1.962 11.240 4.462 1462.773 1.270 19.847 1.384 0.80 338848. 0.0953
|
|
102.23 0.5452 0.4939 0.0073 0.0080 1.624 9.307 2.943 1211.282 1.052 13.091 1.102 0.80 339463. 0.0616
|
|
106.01 0.5654 0.3185 0.0036 0.0063 1.281 7.342 1.444 955.527 0.830 6.422 0.685 0.80 340095. 0.0268
|
|
109.80 0.5856 -0.0144 -0.0001 0.0046 0.930 5.326 -0.046 693.204 0.602 -0.204 -0.030 0.80 340705. 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 0.0873 0.0290 7.620 40.023 42.052 5682.277 4.522 187.046 3.357 0.86 358890. 0.7096
|
|
4.13 0.0202 0.0597 0.0858 0.0290 7.627 40.057 41.349 5687.112 4.526 183.922 3.298 0.86 359091. 0.6913
|
|
8.26 0.0404 0.1172 0.0843 0.0290 7.625 40.051 40.593 5686.243 4.525 180.559 3.238 0.86 359305. 0.6725
|
|
12.39 0.0606 0.1726 0.0826 0.0290 7.615 39.999 39.782 5678.846 4.519 176.951 3.177 0.86 359535. 0.6533
|
|
16.52 0.0808 0.2257 0.0808 0.0289 7.596 39.895 38.913 5664.125 4.507 173.087 3.116 0.86 359779. 0.6337
|
|
20.65 0.1009 0.2765 0.0789 0.0288 7.565 39.734 37.985 5641.258 4.489 168.958 3.054 0.86 360040. 0.6136
|
|
24.78 0.1211 0.3250 0.0768 0.0286 7.522 39.510 36.996 5609.349 4.464 164.557 2.991 0.86 360316. 0.5931
|
|
28.91 0.1413 0.3711 0.0746 0.0284 7.466 39.215 35.944 5567.488 4.430 159.877 2.928 0.86 360609. 0.5723
|
|
33.04 0.1615 0.4149 0.0723 0.0281 7.395 38.843 34.828 5514.723 4.388 154.913 2.864 0.86 360919. 0.5511
|
|
37.17 0.1817 0.4563 0.0698 0.0278 7.309 38.388 33.647 5450.088 4.337 149.662 2.800 0.86 361246. 0.5295
|
|
41.30 0.2019 0.4952 0.0673 0.0274 7.205 37.842 32.401 5372.593 4.275 144.121 2.735 0.86 361590. 0.5076
|
|
45.43 0.2221 0.5318 0.0645 0.0270 7.082 37.198 31.090 5281.173 4.203 138.289 2.670 0.86 361952. 0.4853
|
|
49.56 0.2423 0.5658 0.0617 0.0264 6.939 36.448 29.712 5174.604 4.118 132.161 2.604 0.86 362333. 0.4628
|
|
53.69 0.2625 0.5974 0.0587 0.0258 6.774 35.581 28.268 5051.626 4.020 125.735 2.538 0.86 362731. 0.4399
|
|
57.82 0.2827 0.6262 0.0555 0.0251 6.588 34.602 26.759 4912.634 3.909 119.026 2.471 0.86 363148. 0.4166
|
|
61.95 0.3028 0.6519 0.0523 0.0243 6.383 33.526 25.192 4759.781 3.788 112.056 2.401 0.86 363584. 0.3928
|
|
66.08 0.3230 0.6743 0.0489 0.0234 6.159 32.348 23.572 4592.559 3.655 104.847 2.328 0.86 364038. 0.3684
|
|
70.20 0.3432 0.6932 0.0455 0.0225 5.915 31.069 21.902 4410.936 3.510 97.420 2.252 0.86 364512. 0.3436
|
|
74.33 0.3634 0.7076 0.0419 0.0215 5.655 29.702 20.188 4216.971 3.356 89.794 2.171 0.86 365004. 0.3180
|
|
78.46 0.3836 0.7176 0.0383 0.0205 5.374 28.228 18.434 4007.600 3.189 81.992 2.086 0.86 365515. 0.2920
|
|
82.59 0.4038 0.7226 0.0346 0.0193 5.073 26.646 16.644 3783.075 3.010 74.034 1.996 0.86 366046. 0.2654
|
|
86.72 0.4240 0.7212 0.0308 0.0181 4.753 24.966 14.825 3544.586 2.821 65.943 1.897 0.86 366597. 0.2381
|
|
90.85 0.4442 0.7120 0.0269 0.0168 4.417 23.200 12.981 3293.796 2.621 57.740 1.788 0.87 367167. 0.2099
|
|
94.98 0.4644 0.6925 0.0231 0.0155 4.066 21.357 11.118 3032.147 2.413 49.454 1.663 0.87 367757. 0.1808
|
|
99.11 0.4846 0.6596 0.0192 0.0141 3.703 19.451 9.243 2761.596 2.198 41.114 1.518 0.87 368367. 0.1505
|
|
103.24 0.5047 0.6085 0.0153 0.0127 3.332 17.499 7.364 2484.409 1.977 32.753 1.344 0.87 368997. 0.1189
|
|
107.37 0.5249 0.5318 0.0114 0.0112 2.954 15.518 5.488 2203.159 1.753 24.410 1.130 0.87 369647. 0.0863
|
|
111.50 0.5451 0.4186 0.0075 0.0098 2.576 13.528 3.626 1920.619 1.528 16.129 0.856 0.87 370317. 0.0532
|
|
115.63 0.5653 0.2509 0.0037 0.0084 2.199 11.548 1.789 1639.583 1.305 7.958 0.495 0.87 371007. 0.0216
|
|
119.76 0.5855 -0.0058 -0.0001 0.0069 1.818 9.546 -0.033 1355.335 1.079 -0.146 -0.011 0.87 371687. 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 0.0887 0.0349 11.649 56.478 50.168 8686.563 6.381 223.148 2.620 0.93 388748. 0.6048
|
|
4.51 0.0203 0.0512 0.0873 0.0347 11.599 56.236 49.385 8649.371 6.353 219.665 2.590 0.93 388965. 0.5933
|
|
9.01 0.0407 0.1011 0.0858 0.0345 11.533 55.914 48.534 8599.801 6.317 215.880 2.560 0.93 389199. 0.5813
|
|
13.52 0.0610 0.1499 0.0842 0.0343 11.449 55.507 47.613 8537.223 6.271 211.783 2.530 0.93 389450. 0.5690
|
|
18.02 0.0813 0.1975 0.0825 0.0340 11.346 55.011 46.619 8461.038 6.215 207.361 2.499 0.93 389718. 0.5562
|
|
22.53 0.1017 0.2438 0.0806 0.0336 11.225 54.424 45.549 8370.680 6.149 202.600 2.468 0.93 390003. 0.5430
|
|
27.04 0.1220 0.2888 0.0785 0.0332 11.084 53.741 44.400 8265.608 6.072 197.492 2.436 0.93 390307. 0.5292
|
|
31.54 0.1424 0.3324 0.0764 0.0327 10.923 52.959 43.171 8145.328 5.983 192.026 2.404 0.93 390629. 0.5149
|
|
36.05 0.1627 0.3746 0.0740 0.0322 10.741 52.075 41.861 8009.355 5.883 186.197 2.371 0.93 390969. 0.5000
|
|
40.56 0.1830 0.4153 0.0716 0.0315 10.537 51.085 40.467 7857.165 5.772 179.999 2.336 0.93 391330. 0.4844
|
|
45.06 0.2034 0.4544 0.0690 0.0309 10.310 49.986 38.991 7688.142 5.647 173.431 2.300 0.93 391709. 0.4682
|
|
49.57 0.2237 0.4918 0.0662 0.0301 10.060 48.773 37.430 7501.601 5.510 166.489 2.263 0.93 392109. 0.4513
|
|
54.07 0.2440 0.5273 0.0633 0.0293 9.785 47.441 35.785 7296.728 5.360 159.171 2.224 0.93 392528. 0.4338
|
|
58.58 0.2644 0.5609 0.0602 0.0284 9.485 45.984 34.055 7072.596 5.195 151.475 2.184 0.93 392967. 0.4155
|
|
63.09 0.2847 0.5923 0.0570 0.0274 9.158 44.400 32.244 6828.981 5.016 143.422 2.142 0.93 393427. 0.3964
|
|
67.59 0.3050 0.6212 0.0537 0.0264 8.809 42.708 30.360 6568.671 4.825 135.040 2.096 0.93 393907. 0.3765
|
|
72.10 0.3254 0.6461 0.0502 0.0253 8.453 40.982 28.407 6303.243 4.630 126.355 2.044 0.93 394408. 0.3552
|
|
76.61 0.3457 0.6664 0.0467 0.0242 8.090 39.225 26.393 6033.027 4.432 117.394 1.984 0.93 394930. 0.3323
|
|
81.11 0.3660 0.6810 0.0430 0.0231 7.724 37.451 24.322 5760.113 4.231 108.182 1.915 0.93 395472. 0.3079
|
|
85.62 0.3864 0.6852 0.0393 0.0221 7.396 35.858 22.196 5515.118 4.051 98.729 1.825 0.94 396035. 0.2804
|
|
90.12 0.4067 0.6815 0.0354 0.0211 7.062 34.240 20.027 5266.230 3.868 89.082 1.725 0.94 396619. 0.2516
|
|
94.63 0.4271 0.6698 0.0315 0.0201 6.715 32.555 17.823 5007.184 3.678 79.275 1.614 0.94 397225. 0.2222
|
|
99.14 0.4474 0.6483 0.0276 0.0190 6.357 30.822 15.590 4740.641 3.482 69.343 1.492 0.94 397852. 0.1920
|
|
103.64 0.4677 0.6149 0.0236 0.0179 5.994 29.062 13.337 4469.944 3.283 59.323 1.353 0.94 398500. 0.1611
|
|
108.15 0.4881 0.5673 0.0196 0.0169 5.629 27.292 11.074 4197.723 3.083 49.258 1.197 0.94 399171. 0.1298
|
|
112.66 0.5084 0.5028 0.0156 0.0158 5.266 25.530 8.813 3926.631 2.884 39.199 1.018 0.94 399863. 0.0985
|
|
117.16 0.5287 0.4179 0.0116 0.0147 4.908 23.793 6.565 3659.548 2.688 29.201 0.814 0.94 400577. 0.0680
|
|
121.67 0.5491 0.3093 0.0077 0.0136 4.558 22.100 4.345 3399.081 2.497 19.328 0.580 0.94 401314. 0.0394
|
|
126.17 0.5694 0.1728 0.0038 0.0126 4.220 20.460 2.167 3146.797 2.312 9.640 0.312 0.94 402073. 0.0150
|
|
130.68 0.5897 0.0009 0.0000 0.0116 3.871 18.768 0.010 2886.562 2.120 0.043 0.002 0.94 402851. 0.0000
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