575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x7 (16x7.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 0.0850 0.0358 0.003 0.190 0.178 2.253 0.022 0.790 35.753 0.06 30500. 0.5525
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0.31 0.0203 0.0471 0.0834 0.0360 0.003 0.191 0.174 2.262 0.022 0.774 34.908 0.06 30518. 0.5342
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0.62 0.0407 0.0920 0.0816 0.0361 0.003 0.192 0.170 2.270 0.022 0.758 34.059 0.06 30536. 0.5157
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0.92 0.0610 0.1345 0.0798 0.0362 0.003 0.192 0.167 2.276 0.022 0.741 33.206 0.06 30556. 0.4970
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1.23 0.0813 0.1747 0.0778 0.0362 0.003 0.193 0.163 2.279 0.022 0.723 32.351 0.06 30577. 0.4783
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1.54 0.1016 0.2126 0.0758 0.0362 0.003 0.193 0.158 2.279 0.022 0.704 31.493 0.06 30599. 0.4594
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1.85 0.1220 0.2482 0.0736 0.0362 0.003 0.192 0.154 2.276 0.022 0.684 30.633 0.06 30622. 0.4404
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2.16 0.1423 0.2814 0.0713 0.0361 0.003 0.192 0.149 2.269 0.022 0.663 29.770 0.06 30647. 0.4214
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2.46 0.1626 0.3122 0.0689 0.0359 0.003 0.191 0.144 2.259 0.022 0.640 28.903 0.06 30673. 0.4022
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2.77 0.1830 0.3407 0.0664 0.0357 0.003 0.190 0.139 2.245 0.021 0.617 28.031 0.06 30701. 0.3829
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3.08 0.2033 0.3667 0.0638 0.0354 0.003 0.188 0.133 2.227 0.021 0.593 27.154 0.06 30730. 0.3636
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3.39 0.2236 0.3902 0.0611 0.0350 0.003 0.186 0.128 2.205 0.021 0.568 26.269 0.06 30761. 0.3442
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3.70 0.2439 0.4112 0.0583 0.0346 0.003 0.184 0.122 2.178 0.021 0.542 25.375 0.06 30793. 0.3248
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4.00 0.2643 0.4295 0.0554 0.0341 0.003 0.181 0.116 2.146 0.020 0.515 24.469 0.06 30827. 0.3053
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4.31 0.2846 0.4451 0.0525 0.0335 0.003 0.178 0.110 2.110 0.020 0.487 23.547 0.06 30862. 0.2858
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4.62 0.3049 0.4579 0.0494 0.0329 0.003 0.175 0.103 2.070 0.020 0.459 22.607 0.06 30899. 0.2663
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4.93 0.3253 0.4676 0.0462 0.0322 0.003 0.171 0.097 2.024 0.019 0.430 21.643 0.06 30937. 0.2466
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5.24 0.3456 0.4740 0.0430 0.0314 0.003 0.167 0.090 1.973 0.019 0.400 20.649 0.06 30977. 0.2270
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5.54 0.3659 0.4768 0.0397 0.0305 0.003 0.162 0.083 1.917 0.018 0.369 19.619 0.06 31019. 0.2072
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5.85 0.3862 0.4758 0.0363 0.0295 0.002 0.157 0.076 1.856 0.018 0.338 18.545 0.06 31063. 0.1874
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6.16 0.4066 0.4703 0.0329 0.0284 0.002 0.151 0.069 1.790 0.017 0.306 17.414 0.06 31108. 0.1674
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6.47 0.4269 0.4598 0.0294 0.0273 0.002 0.145 0.061 1.718 0.016 0.273 16.215 0.06 31155. 0.1474
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6.78 0.4472 0.4435 0.0259 0.0261 0.002 0.139 0.054 1.641 0.016 0.240 14.929 0.06 31203. 0.1272
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7.08 0.4675 0.4203 0.0223 0.0248 0.002 0.132 0.046 1.558 0.015 0.207 13.533 0.06 31254. 0.1070
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7.39 0.4879 0.3888 0.0186 0.0234 0.002 0.124 0.039 1.470 0.014 0.173 11.998 0.06 31306. 0.0868
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7.70 0.5082 0.3471 0.0149 0.0219 0.002 0.116 0.031 1.376 0.013 0.139 10.283 0.06 31359. 0.0666
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8.01 0.5285 0.2925 0.0112 0.0203 0.002 0.108 0.023 1.277 0.012 0.104 8.332 0.06 31415. 0.0468
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8.32 0.5489 0.2211 0.0075 0.0186 0.002 0.099 0.016 1.173 0.011 0.070 6.065 0.06 31472. 0.0279
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8.62 0.5692 0.1272 0.0038 0.0169 0.001 0.090 0.008 1.064 0.010 0.035 3.363 0.06 31531. 0.0110
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8.93 0.5895 0.0014 0.0000 0.0151 0.001 0.080 0.000 0.949 0.009 0.000 0.035 0.06 31590. 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 0.0854 0.0314 0.021 0.669 0.714 15.824 0.076 3.175 20.460 0.13 61000. 0.6339
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0.62 0.0205 0.0542 0.0838 0.0316 0.021 0.673 0.700 15.919 0.076 3.113 19.943 0.13 61035. 0.6119
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1.24 0.0409 0.1056 0.0820 0.0318 0.021 0.676 0.685 15.998 0.076 3.048 19.429 0.13 61072. 0.5898
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1.86 0.0614 0.1542 0.0802 0.0319 0.022 0.679 0.670 16.058 0.077 2.979 18.917 0.13 61112. 0.5677
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2.48 0.0818 0.2001 0.0782 0.0320 0.022 0.680 0.653 16.098 0.077 2.906 18.408 0.13 61154. 0.5457
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3.10 0.1023 0.2432 0.0761 0.0320 0.022 0.681 0.636 16.115 0.077 2.829 17.903 0.13 61198. 0.5236
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3.72 0.1227 0.2837 0.0740 0.0320 0.022 0.681 0.618 16.106 0.077 2.748 17.401 0.13 61246. 0.5016
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4.34 0.1432 0.3215 0.0717 0.0319 0.022 0.679 0.599 16.068 0.077 2.663 16.902 0.13 61296. 0.4796
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4.96 0.1636 0.3566 0.0693 0.0318 0.021 0.676 0.579 15.999 0.076 2.574 16.406 0.13 61349. 0.4577
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5.58 0.1841 0.3891 0.0668 0.0316 0.021 0.672 0.558 15.897 0.076 2.481 15.913 0.13 61405. 0.4358
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6.20 0.2045 0.4190 0.0641 0.0313 0.021 0.666 0.536 15.760 0.075 2.383 15.422 0.13 61464. 0.4140
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6.82 0.2250 0.4463 0.0614 0.0310 0.021 0.659 0.513 15.586 0.074 2.282 14.932 0.13 61526. 0.3923
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7.44 0.2454 0.4709 0.0586 0.0305 0.021 0.650 0.490 15.374 0.073 2.177 14.442 0.13 61590. 0.3706
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8.06 0.2659 0.4927 0.0557 0.0300 0.020 0.639 0.465 15.124 0.072 2.069 13.951 0.13 61658. 0.3489
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8.68 0.2863 0.5118 0.0527 0.0295 0.020 0.627 0.440 14.833 0.071 1.957 13.457 0.13 61730. 0.3274
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9.30 0.3068 0.5280 0.0496 0.0288 0.019 0.613 0.414 14.502 0.069 1.843 12.957 0.13 61804. 0.3058
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9.92 0.3272 0.5412 0.0464 0.0281 0.019 0.597 0.388 14.127 0.067 1.725 12.449 0.13 61882. 0.2843
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10.54 0.3477 0.5511 0.0432 0.0272 0.018 0.579 0.361 13.709 0.065 1.604 11.931 0.13 61963. 0.2628
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11.16 0.3681 0.5574 0.0398 0.0263 0.018 0.560 0.333 13.247 0.063 1.481 11.398 0.13 62047. 0.2412
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11.78 0.3886 0.5598 0.0365 0.0253 0.017 0.538 0.305 12.739 0.061 1.355 10.844 0.13 62135. 0.2195
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12.39 0.4090 0.5577 0.0330 0.0242 0.016 0.515 0.276 12.184 0.058 1.226 10.264 0.13 62226. 0.1976
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13.01 0.4295 0.5505 0.0295 0.0230 0.016 0.489 0.246 11.582 0.055 1.096 9.648 0.13 62321. 0.1756
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13.63 0.4499 0.5371 0.0259 0.0217 0.015 0.462 0.217 10.932 0.052 0.963 8.985 0.13 62419. 0.1533
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14.25 0.4704 0.5162 0.0223 0.0203 0.014 0.432 0.186 10.234 0.049 0.829 8.260 0.13 62521. 0.1308
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14.87 0.4908 0.4858 0.0187 0.0188 0.013 0.401 0.156 9.487 0.045 0.693 7.450 0.13 62627. 0.1078
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15.49 0.5113 0.4430 0.0150 0.0173 0.012 0.367 0.125 8.693 0.042 0.556 6.523 0.13 62735. 0.0846
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16.11 0.5317 0.3835 0.0112 0.0156 0.011 0.332 0.094 7.852 0.037 0.418 5.429 0.13 62848. 0.0610
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16.73 0.5522 0.3002 0.0075 0.0138 0.009 0.294 0.063 6.964 0.033 0.279 4.092 0.13 62964. 0.0376
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17.35 0.5726 0.1809 0.0038 0.0120 0.008 0.255 0.032 6.032 0.029 0.141 2.378 0.13 63083. 0.0155
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17.97 0.5931 0.0022 0.0000 0.0100 0.007 0.214 0.000 5.052 0.024 0.001 0.028 0.13 63199. 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 0.0858 0.0297 0.068 1.421 1.613 50.442 0.161 7.174 14.503 0.19 91498. 0.6755
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0.93 0.0205 0.0577 0.0841 0.0299 0.068 1.431 1.582 50.786 0.162 7.035 14.126 0.19 91551. 0.6515
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1.86 0.0410 0.1124 0.0824 0.0301 0.068 1.439 1.549 51.077 0.163 6.888 13.751 0.19 91607. 0.6275
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2.80 0.0615 0.1640 0.0805 0.0302 0.069 1.445 1.513 51.305 0.163 6.732 13.380 0.19 91666. 0.6037
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3.73 0.0820 0.2127 0.0786 0.0303 0.069 1.450 1.477 51.462 0.164 6.567 13.013 0.19 91730. 0.5799
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4.66 0.1025 0.2584 0.0765 0.0303 0.069 1.452 1.437 51.539 0.164 6.394 12.651 0.19 91797. 0.5562
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5.59 0.1230 0.3013 0.0743 0.0303 0.069 1.452 1.396 51.527 0.164 6.211 12.292 0.19 91869. 0.5327
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6.52 0.1435 0.3414 0.0720 0.0303 0.069 1.449 1.353 51.416 0.164 6.019 11.937 0.19 91944. 0.5092
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7.46 0.1640 0.3787 0.0696 0.0301 0.069 1.442 1.308 51.198 0.163 5.817 11.586 0.19 92024. 0.4859
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8.39 0.1845 0.4133 0.0671 0.0299 0.068 1.433 1.260 50.864 0.162 5.606 11.239 0.19 92108. 0.4627
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9.32 0.2050 0.4451 0.0644 0.0297 0.068 1.420 1.211 50.409 0.160 5.386 10.896 0.19 92197. 0.4397
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10.25 0.2255 0.4743 0.0617 0.0293 0.067 1.404 1.159 49.827 0.159 5.157 10.555 0.19 92290. 0.4168
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11.18 0.2460 0.5008 0.0588 0.0289 0.066 1.384 1.106 49.114 0.156 4.920 10.216 0.19 92388. 0.3940
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12.12 0.2665 0.5246 0.0559 0.0284 0.065 1.360 1.051 48.265 0.154 4.675 9.878 0.19 92490. 0.3714
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13.05 0.2870 0.5456 0.0529 0.0278 0.063 1.332 0.994 47.277 0.150 4.423 9.539 0.19 92598. 0.3488
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13.98 0.3075 0.5638 0.0498 0.0272 0.062 1.300 0.936 46.144 0.147 4.163 9.200 0.19 92710. 0.3264
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14.91 0.3280 0.5790 0.0466 0.0264 0.060 1.264 0.876 44.862 0.143 3.897 8.857 0.19 92827. 0.3040
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15.84 0.3485 0.5909 0.0433 0.0256 0.058 1.224 0.815 43.428 0.138 3.624 8.508 0.19 92949. 0.2816
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16.77 0.3690 0.5995 0.0400 0.0246 0.056 1.179 0.752 41.837 0.133 3.345 8.152 0.19 93077. 0.2592
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17.71 0.3895 0.6042 0.0366 0.0236 0.054 1.129 0.688 40.087 0.128 3.060 7.783 0.19 93209. 0.2367
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18.64 0.4100 0.6046 0.0331 0.0225 0.051 1.075 0.623 38.173 0.122 2.770 7.399 0.19 93346. 0.2141
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19.57 0.4306 0.5999 0.0296 0.0212 0.048 1.017 0.556 36.093 0.115 2.475 6.992 0.19 93489. 0.1912
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20.50 0.4511 0.5891 0.0260 0.0199 0.045 0.954 0.489 33.845 0.108 2.175 6.554 0.19 93637. 0.1681
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21.43 0.4716 0.5707 0.0224 0.0185 0.042 0.885 0.421 31.429 0.100 1.872 6.073 0.19 93791. 0.1445
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22.37 0.4921 0.5425 0.0187 0.0170 0.039 0.813 0.352 28.843 0.092 1.565 5.533 0.19 93949. 0.1204
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23.30 0.5126 0.5012 0.0150 0.0154 0.035 0.735 0.282 26.090 0.083 1.256 4.907 0.19 94114. 0.0956
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24.23 0.5331 0.4413 0.0113 0.0136 0.031 0.653 0.212 23.172 0.074 0.944 4.154 0.19 94283. 0.0702
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25.16 0.5536 0.3534 0.0076 0.0118 0.027 0.566 0.142 20.092 0.064 0.631 3.204 0.19 94457. 0.0443
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26.09 0.5741 0.2202 0.0038 0.0099 0.023 0.475 0.072 16.857 0.054 0.318 1.925 0.19 94636. 0.0189
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27.03 0.5946 0.0032 0.0000 0.0079 0.018 0.379 0.001 13.447 0.043 0.004 0.027 0.19 94809. 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 0.0862 0.0288 0.155 2.449 2.882 115.901 0.277 12.817 11.277 0.25 121994. 0.7020
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1.25 0.0206 0.0599 0.0846 0.0290 0.157 2.467 2.826 116.751 0.279 12.569 10.978 0.25 122065. 0.6768
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2.49 0.0411 0.1167 0.0828 0.0292 0.158 2.482 2.767 117.473 0.280 12.306 10.682 0.25 122140. 0.6516
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3.74 0.0617 0.1702 0.0809 0.0293 0.158 2.494 2.704 118.044 0.282 12.028 10.390 0.25 122220. 0.6266
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4.98 0.0822 0.2206 0.0789 0.0294 0.159 2.503 2.638 118.443 0.283 11.734 10.102 0.25 122305. 0.6017
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6.23 0.1028 0.2680 0.0769 0.0295 0.159 2.507 2.568 118.649 0.283 11.423 9.818 0.25 122395. 0.5770
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7.47 0.1233 0.3125 0.0747 0.0295 0.159 2.507 2.495 118.640 0.283 11.097 9.538 0.25 122491. 0.5525
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8.72 0.1439 0.3540 0.0723 0.0294 0.159 2.502 2.417 118.393 0.283 10.753 9.261 0.25 122592. 0.5281
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9.96 0.1644 0.3927 0.0699 0.0293 0.158 2.491 2.336 117.887 0.281 10.392 8.989 0.25 122699. 0.5039
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11.21 0.1850 0.4286 0.0674 0.0291 0.157 2.474 2.252 117.101 0.280 10.015 8.721 0.25 122812. 0.4799
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12.46 0.2055 0.4617 0.0647 0.0288 0.156 2.452 2.163 116.021 0.277 9.621 8.456 0.25 122930. 0.4561
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13.70 0.2261 0.4922 0.0620 0.0285 0.154 2.422 2.071 114.634 0.274 9.211 8.194 0.25 123055. 0.4324
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14.95 0.2466 0.5199 0.0591 0.0280 0.151 2.386 1.976 112.930 0.270 8.787 7.935 0.25 123186. 0.4090
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16.19 0.2672 0.5449 0.0562 0.0275 0.149 2.343 1.877 110.896 0.265 8.349 7.677 0.25 123324. 0.3857
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17.44 0.2877 0.5672 0.0531 0.0269 0.146 2.293 1.775 108.522 0.259 7.897 7.420 0.25 123468. 0.3626
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18.68 0.3083 0.5867 0.0500 0.0263 0.142 2.236 1.671 105.798 0.253 7.432 7.163 0.26 123618. 0.3396
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19.93 0.3288 0.6032 0.0468 0.0255 0.138 2.170 1.564 102.713 0.245 6.955 6.905 0.26 123775. 0.3166
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21.17 0.3494 0.6167 0.0435 0.0246 0.133 2.097 1.454 99.257 0.237 6.467 6.643 0.26 123938. 0.2938
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22.42 0.3699 0.6268 0.0401 0.0237 0.128 2.016 1.342 95.419 0.228 5.967 6.377 0.26 124109. 0.2709
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23.66 0.3905 0.6331 0.0367 0.0226 0.122 1.927 1.227 91.193 0.218 5.458 6.103 0.26 124286. 0.2479
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24.91 0.4110 0.6353 0.0332 0.0215 0.116 1.829 1.110 86.570 0.207 4.939 5.817 0.26 124470. 0.2248
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26.16 0.4316 0.6325 0.0297 0.0202 0.109 1.723 0.992 81.543 0.195 4.411 5.516 0.26 124662. 0.2014
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27.40 0.4521 0.6237 0.0261 0.0189 0.102 1.608 0.871 76.108 0.182 3.875 5.192 0.26 124860. 0.1777
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28.65 0.4727 0.6074 0.0224 0.0174 0.094 1.485 0.749 70.262 0.168 3.332 4.836 0.26 125065. 0.1535
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29.89 0.4932 0.5812 0.0187 0.0159 0.086 1.352 0.626 64.005 0.153 2.784 4.435 0.26 125278. 0.1287
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31.14 0.5138 0.5414 0.0150 0.0142 0.077 1.212 0.501 57.341 0.137 2.230 3.966 0.26 125498. 0.1030
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32.38 0.5343 0.4817 0.0113 0.0125 0.067 1.062 0.376 50.275 0.120 1.673 3.393 0.26 125725. 0.0763
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33.63 0.5549 0.3911 0.0075 0.0106 0.057 0.905 0.250 42.819 0.102 1.114 2.653 0.26 125958. 0.0487
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34.87 0.5754 0.2471 0.0037 0.0087 0.047 0.739 0.125 34.985 0.084 0.555 1.616 0.26 126198. 0.0209
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36.12 0.5960 -0.0059 -0.0001 0.0066 0.036 0.564 -0.002 26.697 0.064 -0.010 -0.037 0.26 126421. 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 0.0867 0.0283 0.298 3.760 4.529 222.414 0.425 20.146 9.237 0.32 152487. 0.7209
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1.57 0.0208 0.0621 0.0851 0.0285 0.301 3.789 4.441 224.135 0.428 19.753 8.987 0.32 152577. 0.6945
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3.15 0.0416 0.1207 0.0833 0.0287 0.303 3.814 4.347 225.594 0.431 19.336 8.740 0.32 152672. 0.6683
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4.72 0.0624 0.1760 0.0814 0.0288 0.304 3.833 4.248 226.748 0.433 18.894 8.497 0.32 152773. 0.6422
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|
6.30 0.0832 0.2280 0.0793 0.0289 0.305 3.847 4.143 227.554 0.435 18.426 8.257 0.32 152881. 0.6163
|
|
7.87 0.1039 0.2769 0.0772 0.0290 0.306 3.854 4.032 227.966 0.435 17.933 8.021 0.32 152996. 0.5907
|
|
9.45 0.1247 0.3227 0.0750 0.0290 0.306 3.853 3.915 227.941 0.435 17.412 7.790 0.32 153118. 0.5652
|
|
11.02 0.1455 0.3655 0.0726 0.0289 0.305 3.845 3.792 227.431 0.434 16.865 7.562 0.32 153247. 0.5400
|
|
12.60 0.1663 0.4053 0.0701 0.0288 0.304 3.827 3.662 226.392 0.432 16.290 7.337 0.32 153383. 0.5149
|
|
14.17 0.1871 0.4422 0.0676 0.0286 0.301 3.800 3.527 224.785 0.429 15.688 7.117 0.32 153527. 0.4902
|
|
15.75 0.2079 0.4764 0.0648 0.0283 0.298 3.763 3.386 222.578 0.425 15.060 6.900 0.32 153678. 0.4656
|
|
17.32 0.2287 0.5078 0.0620 0.0279 0.295 3.715 3.239 219.747 0.420 14.407 6.685 0.32 153837. 0.4412
|
|
18.90 0.2495 0.5364 0.0591 0.0275 0.290 3.656 3.087 216.268 0.413 13.730 6.474 0.32 154004. 0.4171
|
|
20.47 0.2703 0.5623 0.0561 0.0270 0.284 3.586 2.930 212.118 0.405 13.030 6.264 0.32 154179. 0.3932
|
|
22.05 0.2911 0.5854 0.0530 0.0264 0.278 3.504 2.767 207.275 0.396 12.309 6.056 0.32 154363. 0.3694
|
|
23.62 0.3118 0.6056 0.0498 0.0256 0.271 3.410 2.601 201.717 0.385 11.568 5.848 0.32 154554. 0.3458
|
|
25.20 0.3326 0.6230 0.0465 0.0248 0.262 3.304 2.430 195.423 0.373 10.807 5.639 0.32 154754. 0.3223
|
|
26.77 0.3534 0.6371 0.0432 0.0239 0.253 3.184 2.254 188.371 0.360 10.027 5.428 0.32 154963. 0.2989
|
|
28.35 0.3742 0.6480 0.0397 0.0230 0.242 3.052 2.075 180.543 0.345 9.231 5.214 0.32 155181. 0.2754
|
|
29.92 0.3950 0.6550 0.0362 0.0219 0.231 2.906 1.893 171.921 0.328 8.418 4.993 0.32 155407. 0.2519
|
|
31.50 0.4158 0.6578 0.0327 0.0207 0.218 2.747 1.706 162.490 0.310 7.590 4.763 0.32 155642. 0.2282
|
|
33.07 0.4366 0.6554 0.0291 0.0194 0.204 2.573 1.517 152.237 0.291 6.748 4.520 0.32 155886. 0.2042
|
|
34.65 0.4574 0.6468 0.0254 0.0179 0.189 2.386 1.325 141.154 0.270 5.894 4.258 0.32 156139. 0.1798
|
|
36.22 0.4782 0.6302 0.0217 0.0164 0.173 2.185 1.131 129.235 0.247 5.030 3.969 0.32 156402. 0.1548
|
|
37.80 0.4989 0.6028 0.0179 0.0148 0.156 1.969 0.934 116.484 0.222 4.156 3.638 0.32 156673. 0.1290
|
|
39.37 0.5197 0.5601 0.0141 0.0131 0.138 1.740 0.736 102.907 0.197 3.274 3.245 0.32 156953. 0.1021
|
|
40.95 0.5405 0.4939 0.0103 0.0113 0.119 1.496 0.537 88.521 0.169 2.388 2.751 0.32 157243. 0.0739
|
|
42.52 0.5613 0.3887 0.0065 0.0093 0.098 1.240 0.337 73.350 0.140 1.500 2.085 0.32 157541. 0.0444
|
|
44.10 0.5821 0.2098 0.0026 0.0073 0.077 0.971 0.137 57.413 0.110 0.611 1.085 0.32 157845. 0.0148
|
|
45.67 0.6029
|
|
|
|
|
|
|
|
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 0.0874 0.0280 0.511 5.366 6.569 380.902 0.606 29.220 7.823 0.38 182977. 0.7353
|
|
1.87 0.0206 0.0625 0.0857 0.0282 0.515 5.408 6.443 383.904 0.611 28.657 7.612 0.38 183083. 0.7085
|
|
3.75 0.0412 0.1216 0.0839 0.0284 0.518 5.444 6.308 386.457 0.615 28.059 7.404 0.38 183197. 0.6819
|
|
5.62 0.0618 0.1774 0.0820 0.0286 0.521 5.473 6.166 388.484 0.618 27.426 7.199 0.38 183318. 0.6556
|
|
7.49 0.0824 0.2299 0.0800 0.0287 0.523 5.493 6.015 389.912 0.621 26.757 6.997 0.38 183446. 0.6294
|
|
9.37 0.1031 0.2793 0.0779 0.0287 0.524 5.503 5.857 390.667 0.622 26.050 6.800 0.38 183583. 0.6035
|
|
11.24 0.1237 0.3255 0.0757 0.0287 0.524 5.503 5.689 390.671 0.622 25.305 6.605 0.38 183728. 0.5778
|
|
13.12 0.1443 0.3688 0.0733 0.0287 0.523 5.492 5.513 389.846 0.620 24.522 6.414 0.38 183881. 0.5523
|
|
14.99 0.1649 0.4092 0.0709 0.0286 0.520 5.467 5.328 388.113 0.618 23.699 6.227 0.38 184043. 0.5271
|
|
16.86 0.1855 0.4467 0.0683 0.0284 0.517 5.429 5.134 385.407 0.613 22.837 6.042 0.38 184214. 0.5021
|
|
18.74 0.2061 0.4815 0.0656 0.0281 0.512 5.377 4.932 381.671 0.607 21.938 5.861 0.38 184393. 0.4774
|
|
20.61 0.2267 0.5135 0.0628 0.0277 0.505 5.309 4.722 376.863 0.600 21.004 5.683 0.38 184582. 0.4529
|
|
22.48 0.2473 0.5429 0.0599 0.0273 0.497 5.225 4.504 370.943 0.590 20.034 5.507 0.38 184780. 0.4286
|
|
24.36 0.2679 0.5696 0.0569 0.0268 0.488 5.126 4.279 363.871 0.579 19.033 5.334 0.38 184988. 0.4046
|
|
26.23 0.2885 0.5936 0.0538 0.0262 0.477 5.009 4.047 355.610 0.566 18.000 5.162 0.38 185205. 0.3808
|
|
28.11 0.3092 0.6149 0.0506 0.0255 0.464 4.876 3.808 346.121 0.551 16.938 4.990 0.38 185433. 0.3571
|
|
29.98 0.3298 0.6333 0.0474 0.0247 0.450 4.724 3.563 335.369 0.534 15.849 4.819 0.38 185670. 0.3336
|
|
31.85 0.3504 0.6488 0.0441 0.0238 0.434 4.555 3.312 323.318 0.515 14.732 4.646 0.38 185917. 0.3101
|
|
33.73 0.3710 0.6612 0.0406 0.0228 0.416 4.366 3.056 309.935 0.493 13.591 4.472 0.38 186174. 0.2867
|
|
35.60 0.3916 0.6700 0.0372 0.0217 0.396 4.158 2.794 295.188 0.470 12.427 4.293 0.38 186442. 0.2631
|
|
37.47 0.4122 0.6748 0.0336 0.0205 0.374 3.931 2.527 279.052 0.444 11.240 4.107 0.38 186720. 0.2395
|
|
39.35 0.4328 0.6749 0.0300 0.0192 0.351 3.684 2.256 261.504 0.416 10.034 3.913 0.38 187009. 0.2155
|
|
41.22 0.4534 0.6694 0.0263 0.0178 0.325 3.416 1.981 242.527 0.386 8.810 3.704 0.38 187308. 0.1912
|
|
43.09 0.4740 0.6565 0.0226 0.0163 0.298 3.129 1.702 222.113 0.354 7.570 3.475 0.39 187618. 0.1663
|
|
44.97 0.4947 0.6340 0.0189 0.0147 0.269 2.821 1.420 200.262 0.319 6.316 3.216 0.39 187939. 0.1405
|
|
46.84 0.5153 0.5976 0.0151 0.0130 0.237 2.493 1.136 176.986 0.282 5.051 2.910 0.39 188270. 0.1137
|
|
48.72 0.5359 0.5402 0.0113 0.0112 0.204 2.146 0.849 152.309 0.242 3.778 2.530 0.39 188613. 0.0855
|
|
50.59 0.5565 0.4480 0.0075 0.0093 0.169 1.779 0.562 126.269 0.201 2.501 2.020 0.39 188965. 0.0556
|
|
52.46 0.5771 0.2901 0.0037 0.0073 0.133 1.393 0.275 98.910 0.157 1.224 1.261 0.39 189326. 0.0243
|
|
54.34 0.5977 -0.0277 -0.0002 0.0051 0.093 0.981 -0.018 69.625 0.111 -0.079 -0.116 0.39 189624. 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 0.0881 0.0280 0.809 7.285 9.019 603.321 0.823 40.115 6.780 0.44 213461. 0.7467
|
|
2.18 0.0206 0.0631 0.0864 0.0282 0.816 7.343 8.846 608.148 0.830 39.346 6.597 0.44 213585. 0.7196
|
|
4.37 0.0412 0.1228 0.0846 0.0284 0.821 7.393 8.662 612.249 0.835 38.529 6.417 0.44 213718. 0.6926
|
|
6.55 0.0618 0.1792 0.0827 0.0285 0.825 7.432 8.467 615.503 0.840 37.663 6.240 0.44 213860. 0.6659
|
|
8.73 0.0823 0.2322 0.0807 0.0286 0.828 7.460 8.262 617.795 0.843 36.748 6.066 0.44 214010. 0.6394
|
|
10.92 0.1029 0.2821 0.0786 0.0287 0.830 7.474 8.044 619.003 0.844 35.782 5.895 0.44 214170. 0.6131
|
|
13.10 0.1235 0.3289 0.0764 0.0287 0.830 7.474 7.815 619.002 0.844 34.763 5.727 0.44 214340. 0.5871
|
|
15.28 0.1441 0.3727 0.0740 0.0286 0.828 7.458 7.575 617.670 0.843 33.692 5.562 0.44 214519. 0.5614
|
|
17.47 0.1647 0.4135 0.0715 0.0285 0.825 7.424 7.321 614.880 0.839 32.566 5.401 0.44 214708. 0.5359
|
|
19.65 0.1853 0.4516 0.0690 0.0283 0.819 7.372 7.056 610.523 0.833 31.387 5.242 0.45 214907. 0.5107
|
|
21.83 0.2058 0.4869 0.0662 0.0280 0.811 7.299 6.780 604.514 0.825 30.156 5.087 0.45 215117. 0.4857
|
|
24.02 0.2264 0.5195 0.0634 0.0277 0.800 7.206 6.492 596.781 0.814 28.877 4.934 0.45 215337. 0.4610
|
|
26.20 0.2470 0.5494 0.0605 0.0272 0.788 7.091 6.194 587.259 0.801 27.550 4.784 0.45 215569. 0.4366
|
|
28.38 0.2676 0.5768 0.0575 0.0267 0.772 6.954 5.885 575.887 0.786 26.178 4.635 0.45 215811. 0.4124
|
|
30.56 0.2882 0.6014 0.0544 0.0261 0.754 6.793 5.568 562.606 0.767 24.764 4.489 0.45 216065. 0.3884
|
|
32.75 0.3088 0.6235 0.0512 0.0254 0.734 6.609 5.241 547.354 0.747 23.310 4.343 0.45 216329. 0.3646
|
|
34.93 0.3294 0.6427 0.0479 0.0246 0.711 6.400 4.905 530.074 0.723 21.817 4.197 0.45 216606. 0.3409
|
|
37.11 0.3499 0.6591 0.0446 0.0237 0.685 6.167 4.561 510.710 0.697 20.288 4.051 0.45 216894. 0.3173
|
|
39.30 0.3705 0.6724 0.0411 0.0227 0.656 5.907 4.210 489.208 0.667 18.725 3.903 0.45 217194. 0.2937
|
|
41.48 0.3911 0.6823 0.0376 0.0216 0.624 5.621 3.851 465.518 0.635 17.129 3.752 0.45 217506. 0.2700
|
|
43.66 0.4117 0.6884 0.0341 0.0204 0.590 5.308 3.486 439.598 0.600 15.504 3.596 0.45 217830. 0.2462
|
|
45.85 0.4323 0.6900 0.0304 0.0191 0.552 4.968 3.114 411.413 0.561 13.851 3.433 0.45 218167. 0.2222
|
|
48.03 0.4529 0.6861 0.0267 0.0177 0.511 4.600 2.737 380.935 0.520 12.173 3.258 0.45 218515. 0.1977
|
|
50.21 0.4734 0.6752 0.0230 0.0161 0.467 4.204 2.354 348.149 0.475 10.473 3.067 0.45 218876. 0.1726
|
|
52.40 0.4940 0.6550 0.0192 0.0145 0.420 3.780 1.968 313.057 0.427 8.754 2.851 0.45 219250. 0.1467
|
|
54.58 0.5146 0.6213 0.0154 0.0128 0.370 3.329 1.578 275.675 0.376 7.020 2.597 0.45 219636. 0.1196
|
|
56.76 0.5352 0.5670 0.0116 0.0109 0.317 2.850 1.186 236.042 0.322 5.275 2.279 0.45 220034. 0.0910
|
|
58.95 0.5558 0.4780 0.0077 0.0090 0.260 2.345 0.792 194.220 0.265 3.523 1.850 0.45 220445. 0.0604
|
|
61.13 0.5764 0.3220 0.0039 0.0070 0.202 1.815 0.398 150.279 0.205 1.771 1.201 0.45 220865. 0.0278
|
|
63.31 0.5970 -0.0014 0.0000 0.0048 0.139 1.251 -0.001 103.570 0.141 -0.005 -0.005 0.45 221238. 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 0.0890 0.0280 1.211 9.541 11.899 903.080 1.078 52.929 5.976 0.51 243938. 0.7561
|
|
2.50 0.0206 0.0637 0.0873 0.0283 1.221 9.618 11.672 910.372 1.087 51.917 5.815 0.51 244082. 0.7286
|
|
4.99 0.0412 0.1239 0.0855 0.0285 1.229 9.684 11.430 916.557 1.094 50.842 5.656 0.51 244235. 0.7013
|
|
7.49 0.0618 0.1806 0.0836 0.0286 1.236 9.735 11.174 921.447 1.100 49.703 5.500 0.51 244397. 0.6743
|
|
9.99 0.0824 0.2342 0.0816 0.0287 1.240 9.772 10.903 924.867 1.104 48.499 5.347 0.51 244571. 0.6475
|
|
12.49 0.1030 0.2845 0.0794 0.0288 1.243 9.790 10.617 926.636 1.106 47.226 5.197 0.51 244754. 0.6210
|
|
14.98 0.1236 0.3317 0.0772 0.0288 1.243 9.789 10.316 926.565 1.106 45.884 5.050 0.51 244949. 0.5948
|
|
17.48 0.1442 0.3759 0.0748 0.0287 1.240 9.767 9.998 924.464 1.103 44.471 4.905 0.51 245155. 0.5688
|
|
19.98 0.1648 0.4172 0.0723 0.0286 1.234 9.722 9.664 920.147 1.098 42.987 4.764 0.51 245372. 0.5431
|
|
22.47 0.1854 0.4557 0.0697 0.0284 1.225 9.651 9.315 913.445 1.090 41.432 4.625 0.51 245601. 0.5177
|
|
24.97 0.2060 0.4915 0.0670 0.0281 1.213 9.553 8.950 904.229 1.079 39.809 4.489 0.51 245842. 0.4925
|
|
27.47 0.2266 0.5246 0.0641 0.0277 1.197 9.428 8.570 892.390 1.065 38.120 4.356 0.51 246095. 0.4676
|
|
29.97 0.2472 0.5550 0.0612 0.0272 1.177 9.275 8.176 877.833 1.048 36.369 4.225 0.51 246360. 0.4430
|
|
32.46 0.2678 0.5829 0.0581 0.0267 1.154 9.091 7.769 860.465 1.027 34.558 4.095 0.51 246638. 0.4186
|
|
34.96 0.2884 0.6081 0.0550 0.0261 1.127 8.877 7.350 840.197 1.003 32.692 3.968 0.51 246929. 0.3945
|
|
37.46 0.3090 0.6307 0.0518 0.0254 1.096 8.631 6.918 816.938 0.975 30.771 3.841 0.51 247233. 0.3705
|
|
39.96 0.3296 0.6507 0.0484 0.0245 1.060 8.353 6.475 790.602 0.944 28.800 3.715 0.51 247550. 0.3466
|
|
42.45 0.3502 0.6678 0.0450 0.0236 1.021 8.041 6.021 761.103 0.909 26.780 3.588 0.51 247880. 0.3229
|
|
44.95 0.3708 0.6819 0.0416 0.0226 0.977 7.695 5.557 728.362 0.869 24.716 3.460 0.51 248224. 0.2991
|
|
47.45 0.3914 0.6927 0.0380 0.0215 0.928 7.314 5.083 692.305 0.826 22.608 3.330 0.51 248582. 0.2753
|
|
49.94 0.4120 0.6997 0.0344 0.0203 0.876 6.898 4.600 652.866 0.779 20.461 3.196 0.51 248953. 0.2514
|
|
52.44 0.4326 0.7024 0.0307 0.0189 0.818 6.445 4.109 609.992 0.728 18.277 3.055 0.51 249338. 0.2271
|
|
54.94 0.4532 0.6998 0.0270 0.0175 0.756 5.955 3.611 563.642 0.673 16.060 2.906 0.51 249738. 0.2025
|
|
57.44 0.4738 0.6903 0.0232 0.0159 0.689 5.428 3.106 513.795 0.613 13.814 2.742 0.51 250152. 0.1772
|
|
59.93 0.4944 0.6716 0.0194 0.0143 0.617 4.865 2.595 460.451 0.550 11.543 2.556 0.51 250579. 0.1510
|
|
62.43 0.5150 0.6396 0.0156 0.0125 0.541 4.265 2.080 403.637 0.482 9.251 2.337 0.51 251022. 0.1236
|
|
64.93 0.5357 0.5869 0.0117 0.0107 0.461 3.628 1.561 343.414 0.410 6.945 2.062 0.52 251478. 0.0945
|
|
67.42 0.5563 0.4986 0.0078 0.0087 0.375 2.957 1.041 279.874 0.334 4.630 1.687 0.52 251948. 0.0631
|
|
69.92 0.5769 0.3392 0.0039 0.0066 0.286 2.252 0.520 213.124 0.254 2.313 1.107 0.52 252429. 0.0293
|
|
72.42 0.5975 -0.0100 -0.0001 0.0044 0.190 1.499 -0.010 141.878 0.169 -0.044 -0.032 0.52 252835. 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 0.0901 0.0282 1.737 12.168 15.240 1295.611 1.375 67.789 5.335 0.57 274408. 0.7638
|
|
2.81 0.0206 0.0640 0.0884 0.0285 1.752 12.266 14.950 1306.111 1.386 66.500 5.192 0.57 274570. 0.7362
|
|
5.62 0.0412 0.1245 0.0866 0.0287 1.763 12.350 14.642 1314.984 1.395 65.128 5.050 0.57 274744. 0.7087
|
|
8.43 0.0618 0.1816 0.0846 0.0288 1.773 12.415 14.315 1321.969 1.403 63.675 4.912 0.57 274928. 0.6815
|
|
11.24 0.0824 0.2354 0.0826 0.0289 1.779 12.461 13.970 1326.806 1.408 62.137 4.776 0.57 275124. 0.6546
|
|
14.05 0.1031 0.2860 0.0804 0.0290 1.783 12.483 13.604 1329.233 1.410 60.511 4.642 0.57 275332. 0.6279
|
|
16.86 0.1237 0.3335 0.0781 0.0290 1.782 12.481 13.219 1328.983 1.410 58.796 4.511 0.57 275552. 0.6015
|
|
19.67 0.1443 0.3781 0.0757 0.0289 1.778 12.451 12.812 1325.780 1.407 56.990 4.383 0.57 275785. 0.5754
|
|
22.49 0.1649 0.4197 0.0732 0.0288 1.769 12.391 12.386 1319.353 1.400 55.092 4.258 0.57 276031. 0.5496
|
|
25.30 0.1855 0.4586 0.0706 0.0285 1.756 12.298 11.939 1309.460 1.389 53.103 4.135 0.57 276289. 0.5240
|
|
28.11 0.2061 0.4947 0.0678 0.0283 1.738 12.170 11.471 1295.913 1.375 51.025 4.015 0.57 276562. 0.4987
|
|
30.92 0.2267 0.5282 0.0649 0.0279 1.715 12.007 10.985 1278.556 1.357 48.863 3.897 0.57 276848. 0.4737
|
|
33.73 0.2473 0.5591 0.0620 0.0274 1.686 11.807 10.481 1257.253 1.334 46.621 3.781 0.57 277147. 0.4489
|
|
36.54 0.2680 0.5874 0.0589 0.0269 1.652 11.569 9.960 1231.874 1.307 44.302 3.667 0.57 277461. 0.4244
|
|
39.35 0.2886 0.6132 0.0557 0.0262 1.612 11.291 9.422 1202.291 1.276 41.911 3.555 0.57 277790. 0.4001
|
|
42.16 0.3092 0.6364 0.0524 0.0255 1.567 10.973 8.869 1168.376 1.240 39.450 3.443 0.57 278133. 0.3760
|
|
44.97 0.3298 0.6569 0.0491 0.0246 1.515 10.612 8.301 1130.007 1.199 36.925 3.332 0.57 278490. 0.3521
|
|
47.78 0.3504 0.6747 0.0456 0.0237 1.458 10.209 7.720 1087.061 1.153 34.337 3.221 0.57 278863. 0.3282
|
|
50.59 0.3710 0.6896 0.0421 0.0227 1.394 9.762 7.125 1039.423 1.103 31.690 3.109 0.58 279251. 0.3043
|
|
53.40 0.3916 0.7012 0.0385 0.0215 1.324 9.269 6.517 986.990 1.047 28.989 2.995 0.58 279654. 0.2804
|
|
56.21 0.4122 0.7092 0.0349 0.0203 1.247 8.731 5.899 929.666 0.986 26.237 2.878 0.58 280073. 0.2563
|
|
59.02 0.4328 0.7130 0.0311 0.0189 1.163 8.146 5.269 867.375 0.920 23.437 2.755 0.58 280508. 0.2319
|
|
61.84 0.4535 0.7116 0.0274 0.0174 1.073 7.514 4.630 800.059 0.849 20.594 2.625 0.58 280958. 0.2071
|
|
64.65 0.4741 0.7035 0.0235 0.0159 0.976 6.834 3.982 727.686 0.772 17.714 2.482 0.58 281424. 0.1817
|
|
67.46 0.4947 0.6864 0.0197 0.0142 0.872 6.107 3.327 650.258 0.690 14.800 2.321 0.58 281906. 0.1553
|
|
70.27 0.5153 0.6561 0.0158 0.0124 0.761 5.333 2.667 567.814 0.602 11.861 2.130 0.58 282404. 0.1276
|
|
73.08 0.5359 0.6053 0.0118 0.0105 0.644 4.512 2.001 480.440 0.510 8.902 1.889 0.58 282918. 0.0980
|
|
75.89 0.5565 0.5183 0.0079 0.0085 0.521 3.646 1.334 388.275 0.412 5.932 1.558 0.58 283448. 0.0660
|
|
78.70 0.5771 0.3571 0.0039 0.0064 0.391 2.737 0.665 291.473 0.309 2.959 1.035 0.58 283989. 0.0310
|
|
81.51 0.5977 -0.0149 -0.0001 0.0041 0.252 1.764 -0.017 187.792 0.199 -0.077 -0.042 0.58 284426. 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 0.0913 0.0286 2.413 15.208 19.078 1799.229 1.718 84.861 4.809 0.63 304868. 0.7704
|
|
3.12 0.0206 0.0641 0.0896 0.0288 2.432 15.331 18.718 1813.786 1.732 83.256 4.681 0.63 305050. 0.7426
|
|
6.25 0.0412 0.1247 0.0878 0.0290 2.449 15.434 18.334 1826.040 1.744 81.549 4.554 0.63 305244. 0.7151
|
|
9.37 0.0619 0.1820 0.0858 0.0292 2.462 15.515 17.927 1835.624 1.753 79.738 4.430 0.63 305450. 0.6878
|
|
12.50 0.0825 0.2360 0.0838 0.0293 2.470 15.570 17.495 1842.173 1.759 77.820 4.308 0.63 305669. 0.6608
|
|
15.62 0.1031 0.2868 0.0816 0.0293 2.475 15.597 17.039 1845.326 1.762 75.791 4.188 0.64 305902. 0.6340
|
|
18.75 0.1237 0.3346 0.0793 0.0293 2.474 15.592 16.558 1844.703 1.762 73.651 4.071 0.64 306148. 0.6075
|
|
21.87 0.1443 0.3794 0.0769 0.0292 2.467 15.552 16.051 1839.928 1.757 71.395 3.957 0.64 306408. 0.5814
|
|
24.99 0.1650 0.4213 0.0743 0.0291 2.455 15.473 15.518 1830.625 1.748 69.024 3.845 0.64 306683. 0.5554
|
|
28.12 0.1856 0.4604 0.0716 0.0289 2.436 15.353 14.959 1816.453 1.735 66.537 3.735 0.64 306972. 0.5298
|
|
31.24 0.2062 0.4969 0.0688 0.0286 2.410 15.190 14.375 1797.148 1.716 63.939 3.628 0.64 307276. 0.5044
|
|
34.37 0.2268 0.5307 0.0659 0.0282 2.377 14.982 13.767 1772.500 1.693 61.235 3.523 0.64 307596. 0.4793
|
|
37.49 0.2474 0.5620 0.0629 0.0277 2.336 14.727 13.136 1742.320 1.664 58.429 3.420 0.64 307930. 0.4545
|
|
40.61 0.2681 0.5908 0.0598 0.0271 2.288 14.423 12.483 1706.432 1.630 55.526 3.318 0.64 308281. 0.4299
|
|
43.74 0.2887 0.6170 0.0565 0.0265 2.232 14.070 11.810 1664.664 1.590 52.532 3.218 0.64 308647. 0.4056
|
|
46.86 0.3093 0.6407 0.0532 0.0257 2.168 13.666 11.118 1616.841 1.544 49.451 3.119 0.64 309030. 0.3814
|
|
49.99 0.3299 0.6619 0.0498 0.0248 2.096 13.209 10.406 1562.796 1.492 46.288 3.020 0.64 309429. 0.3573
|
|
53.11 0.3505 0.6803 0.0463 0.0239 2.015 12.698 9.678 1502.364 1.435 43.047 2.922 0.64 309844. 0.3333
|
|
56.24 0.3712 0.6959 0.0428 0.0228 1.925 12.132 8.932 1435.384 1.371 39.731 2.823 0.64 310276. 0.3094
|
|
59.36 0.3918 0.7083 0.0391 0.0216 1.826 11.510 8.172 1361.712 1.300 36.347 2.722 0.64 310726. 0.2853
|
|
62.48 0.4124 0.7172 0.0354 0.0204 1.718 10.829 7.396 1281.222 1.223 32.898 2.618 0.64 311192. 0.2611
|
|
65.61 0.4330 0.7220 0.0316 0.0190 1.601 10.090 6.607 1193.804 1.140 29.389 2.510 0.64 311676. 0.2366
|
|
68.73 0.4536 0.7218 0.0278 0.0175 1.474 9.292 5.806 1099.380 1.050 25.825 2.395 0.64 312177. 0.2117
|
|
71.86 0.4743 0.7151 0.0239 0.0159 1.338 8.435 4.994 997.905 0.953 22.214 2.270 0.64 312696. 0.1860
|
|
74.98 0.4949 0.6995 0.0200 0.0141 1.193 7.517 4.173 889.382 0.849 18.560 2.128 0.64 313233. 0.1594
|
|
78.10 0.5155 0.6711 0.0160 0.0123 1.038 6.541 3.344 773.865 0.739 14.873 1.960 0.64 313787. 0.1314
|
|
81.23 0.5361 0.6221 0.0120 0.0104 0.874 5.506 2.509 651.476 0.622 11.162 1.747 0.64 314359. 0.1015
|
|
84.35 0.5567 0.5367 0.0080 0.0083 0.701 4.416 1.672 522.410 0.499 7.435 1.451 0.64 314947. 0.0688
|
|
87.48 0.5774 0.3745 0.0040 0.0061 0.519 3.270 0.833 386.890 0.369 3.705 0.976 0.65 315550. 0.0327
|
|
90.60 0.5980 -0.0202 -0.0001 0.0038 0.323 2.038 -0.027 241.174 0.230 -0.120 -0.051 0.65 316008. 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 0.0928 0.0291 3.268 18.723 23.462 2436.661 2.115 104.361 4.367 0.70 335315. 0.7758
|
|
3.44 0.0206 0.0641 0.0911 0.0293 3.294 18.873 23.022 2456.169 2.132 102.404 4.251 0.70 335516. 0.7481
|
|
6.88 0.0413 0.1247 0.0892 0.0295 3.316 18.999 22.554 2472.539 2.146 100.318 4.137 0.70 335732. 0.7206
|
|
10.31 0.0619 0.1820 0.0873 0.0297 3.333 19.096 22.056 2485.241 2.157 98.104 4.025 0.70 335961. 0.6933
|
|
13.75 0.0825 0.2360 0.0852 0.0298 3.344 19.162 21.528 2493.782 2.165 95.757 3.916 0.70 336204. 0.6663
|
|
17.19 0.1031 0.2870 0.0830 0.0298 3.349 19.192 20.970 2497.645 2.168 93.274 3.808 0.70 336462. 0.6395
|
|
20.63 0.1238 0.3348 0.0806 0.0298 3.348 19.181 20.380 2496.335 2.167 90.651 3.703 0.70 336735. 0.6130
|
|
24.06 0.1444 0.3798 0.0782 0.0297 3.338 19.128 19.758 2489.335 2.161 87.885 3.600 0.70 337023. 0.5869
|
|
27.50 0.1650 0.4219 0.0756 0.0296 3.321 19.026 19.104 2476.135 2.150 84.976 3.499 0.70 337327. 0.5609
|
|
30.94 0.1856 0.4613 0.0729 0.0293 3.294 18.874 18.418 2456.281 2.132 81.924 3.401 0.70 337647. 0.5353
|
|
34.38 0.2063 0.4980 0.0700 0.0290 3.258 18.667 17.701 2429.404 2.109 78.734 3.305 0.70 337984. 0.5099
|
|
37.81 0.2269 0.5322 0.0671 0.0286 3.212 18.405 16.954 2395.227 2.079 75.411 3.210 0.70 338337. 0.4848
|
|
41.25 0.2475 0.5639 0.0640 0.0281 3.156 18.084 16.178 2353.505 2.043 71.962 3.118 0.70 338708. 0.4599
|
|
44.69 0.2681 0.5930 0.0608 0.0275 3.090 17.704 15.376 2304.005 2.000 68.393 3.027 0.70 339095. 0.4353
|
|
48.13 0.2888 0.6197 0.0576 0.0268 3.013 17.262 14.548 2246.508 1.950 64.711 2.937 0.70 339500. 0.4109
|
|
51.56 0.3094 0.6440 0.0542 0.0260 2.924 16.757 13.696 2180.781 1.893 60.922 2.849 0.70 339923. 0.3866
|
|
55.00 0.3300 0.6656 0.0507 0.0252 2.825 16.187 12.821 2106.604 1.829 57.030 2.761 0.70 340363. 0.3625
|
|
58.44 0.3506 0.6847 0.0472 0.0242 2.714 15.550 11.925 2023.758 1.757 53.041 2.673 0.70 340822. 0.3385
|
|
61.88 0.3713 0.7010 0.0436 0.0231 2.591 14.845 11.007 1932.035 1.677 48.960 2.584 0.70 341299. 0.3144
|
|
65.32 0.3919 0.7142 0.0398 0.0219 2.456 14.071 10.071 1831.240 1.590 44.794 2.494 0.70 341795. 0.2903
|
|
68.75 0.4125 0.7240 0.0361 0.0206 2.308 13.225 9.116 1721.201 1.494 40.547 2.402 0.70 342309. 0.2660
|
|
72.19 0.4331 0.7299 0.0322 0.0191 2.148 12.308 8.144 1601.785 1.391 36.225 2.306 0.70 342843. 0.2414
|
|
75.63 0.4538 0.7308 0.0283 0.0176 1.975 11.318 7.157 1472.895 1.279 31.836 2.204 0.71 343395. 0.2162
|
|
79.07 0.4744 0.7254 0.0244 0.0159 1.790 10.254 6.157 1334.501 1.159 27.386 2.093 0.71 343967. 0.1904
|
|
82.50 0.4950 0.7113 0.0204 0.0142 1.591 9.118 5.145 1186.636 1.030 22.884 1.966 0.71 344558. 0.1636
|
|
85.94 0.5156 0.6844 0.0163 0.0123 1.380 7.910 4.123 1029.427 0.894 18.339 1.817 0.71 345169. 0.1353
|
|
89.38 0.5363 0.6371 0.0122 0.0103 1.157 6.632 3.094 863.103 0.749 13.762 1.626 0.71 345799. 0.1049
|
|
92.82 0.5569 0.5528 0.0082 0.0082 0.923 5.287 2.061 688.019 0.597 9.167 1.359 0.71 346447. 0.0715
|
|
96.25 0.5775 0.3892 0.0041 0.0060 0.677 3.877 1.026 504.582 0.438 4.564 0.922 0.71 347110. 0.0343
|
|
99.69 0.5982 -0.0261 -0.0002 0.0037 0.412 2.358 -0.040 306.902 0.266 -0.180 -0.060 0.71 347575. 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 0.0946 0.0300 4.373 22.968 28.457 3260.885 2.595 126.576 3.958 0.76 365745. 0.7743
|
|
3.75 0.0206 0.0635 0.0929 0.0302 4.401 23.116 27.929 3281.854 2.612 124.228 3.860 0.76 365967. 0.7481
|
|
7.50 0.0413 0.1237 0.0910 0.0303 4.424 23.237 27.366 3299.054 2.625 121.724 3.762 0.76 366204. 0.7218
|
|
11.25 0.0619 0.1808 0.0890 0.0305 4.441 23.327 26.767 3311.840 2.635 119.061 3.666 0.76 366456. 0.6955
|
|
15.00 0.0825 0.2348 0.0869 0.0305 4.452 23.381 26.132 3319.560 2.642 116.235 3.571 0.76 366724. 0.6694
|
|
18.75 0.1031 0.2858 0.0847 0.0305 4.454 23.395 25.459 3321.534 2.643 113.241 3.477 0.76 367008. 0.6433
|
|
22.50 0.1238 0.3338 0.0823 0.0305 4.448 23.364 24.747 3317.067 2.640 110.076 3.384 0.76 367308. 0.6173
|
|
26.25 0.1444 0.3790 0.0798 0.0304 4.433 23.282 23.997 3305.433 2.630 106.737 3.293 0.76 367626. 0.5915
|
|
30.00 0.1650 0.4213 0.0772 0.0302 4.406 23.144 23.206 3285.913 2.615 103.221 3.203 0.76 367960. 0.5659
|
|
33.75 0.1856 0.4610 0.0744 0.0300 4.369 22.947 22.376 3257.822 2.592 99.530 3.115 0.76 368312. 0.5404
|
|
37.50 0.2063 0.4980 0.0715 0.0296 4.319 22.684 21.508 3220.605 2.563 95.669 3.029 0.76 368682. 0.5152
|
|
41.25 0.2269 0.5325 0.0685 0.0292 4.256 22.355 20.603 3173.822 2.526 91.644 2.944 0.76 369070. 0.4901
|
|
45.00 0.2475 0.5645 0.0654 0.0287 4.180 21.955 19.664 3117.093 2.481 87.465 2.861 0.76 369476. 0.4653
|
|
48.75 0.2682 0.5941 0.0621 0.0281 4.090 21.483 18.691 3050.068 2.427 83.139 2.780 0.76 369901. 0.4407
|
|
52.51 0.2888 0.6213 0.0588 0.0273 3.986 20.936 17.688 2972.421 2.365 78.674 2.699 0.76 370345. 0.4163
|
|
56.26 0.3094 0.6460 0.0554 0.0265 3.867 20.313 16.654 2883.866 2.295 74.077 2.619 0.77 370808. 0.3920
|
|
60.01 0.3300 0.6682 0.0518 0.0256 3.734 19.610 15.592 2784.138 2.216 69.355 2.540 0.77 371291. 0.3678
|
|
63.76 0.3507 0.6879 0.0482 0.0246 3.585 18.827 14.504 2672.993 2.127 64.514 2.461 0.77 371794. 0.3437
|
|
67.51 0.3713 0.7048 0.0445 0.0235 3.420 17.962 13.390 2550.210 2.029 59.560 2.382 0.77 372316. 0.3196
|
|
71.26 0.3919 0.7187 0.0407 0.0222 3.239 17.014 12.253 2415.604 1.922 54.501 2.301 0.77 372859. 0.2953
|
|
75.01 0.4125 0.7292 0.0369 0.0209 3.043 15.982 11.093 2269.036 1.806 49.343 2.217 0.77 373421. 0.2709
|
|
78.76 0.4332 0.7356 0.0330 0.0194 2.830 14.865 9.913 2110.438 1.679 44.093 2.130 0.77 374005. 0.2460
|
|
82.51 0.4538 0.7370 0.0290 0.0178 2.601 13.663 8.714 1939.824 1.544 38.758 2.037 0.77 374609. 0.2206
|
|
86.26 0.4744 0.7318 0.0249 0.0162 2.357 12.378 7.497 1757.307 1.398 33.348 1.935 0.77 375234. 0.1943
|
|
90.01 0.4951 0.7175 0.0208 0.0144 2.096 11.010 6.266 1563.119 1.244 27.872 1.818 0.77 375880. 0.1669
|
|
93.76 0.5157 0.6898 0.0167 0.0125 1.821 9.563 5.023 1357.645 1.080 22.342 1.678 0.77 376547. 0.1379
|
|
97.51 0.5363 0.6404 0.0125 0.0105 1.531 8.040 3.770 1141.433 0.908 16.770 1.498 0.77 377234. 0.1067
|
|
101.26 0.5569 0.5525 0.0084 0.0084 1.227 6.446 2.512 915.219 0.728 11.171 1.245 0.77 377942. 0.0723
|
|
105.01 0.5776 0.3840 0.0042 0.0063 0.912 4.788 1.250 679.835 0.541 5.561 0.834 0.77 378665. 0.0342
|
|
108.76 0.5982 -0.0263 -0.0002 0.0039 0.573 3.011 -0.052 427.519 0.340 -0.231 -0.055 0.78 379158. 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 0.0967 0.0323 5.984 29.011 34.139 4462.050 3.278 151.849 3.470 0.83 396152. 0.7436
|
|
4.06 0.0206 0.0606 0.0950 0.0323 5.993 29.058 33.516 4469.326 3.283 149.080 3.401 0.83 396395. 0.7221
|
|
8.13 0.0413 0.1187 0.0931 0.0323 5.997 29.076 32.850 4471.989 3.285 146.118 3.332 0.83 396655. 0.7003
|
|
12.19 0.0619 0.1744 0.0911 0.0323 5.994 29.059 32.141 4469.394 3.283 142.963 3.262 0.83 396931. 0.6782
|
|
16.26 0.0825 0.2275 0.0889 0.0323 5.982 29.003 31.386 4460.862 3.277 139.607 3.191 0.83 397225. 0.6557
|
|
20.32 0.1032 0.2780 0.0867 0.0322 5.962 28.904 30.586 4445.664 3.266 136.047 3.121 0.83 397536. 0.6329
|
|
24.39 0.1238 0.3260 0.0843 0.0320 5.931 28.757 29.739 4423.030 3.249 132.277 3.050 0.83 397865. 0.6099
|
|
28.45 0.1444 0.3715 0.0817 0.0318 5.890 28.557 28.843 4392.168 3.226 128.295 2.979 0.83 398212. 0.5866
|
|
32.52 0.1651 0.4145 0.0790 0.0315 5.836 28.297 27.900 4352.229 3.197 124.099 2.908 0.83 398578. 0.5632
|
|
36.58 0.1857 0.4549 0.0762 0.0311 5.770 27.973 26.908 4302.406 3.160 119.688 2.837 0.83 398964. 0.5396
|
|
40.65 0.2064 0.4929 0.0733 0.0307 5.689 27.580 25.870 4242.016 3.116 115.069 2.766 0.83 399368. 0.5159
|
|
44.71 0.2270 0.5284 0.0702 0.0302 5.593 27.115 24.786 4170.479 3.063 110.250 2.696 0.83 399792. 0.4922
|
|
48.77 0.2476 0.5614 0.0670 0.0296 5.481 26.574 23.661 4087.287 3.002 105.243 2.626 0.83 400236. 0.4684
|
|
52.84 0.2683 0.5921 0.0637 0.0289 5.353 25.955 22.494 3991.949 2.932 100.056 2.556 0.83 400700. 0.4445
|
|
56.90 0.2889 0.6202 0.0603 0.0281 5.209 25.254 21.290 3884.266 2.853 94.698 2.486 0.83 401184. 0.4207
|
|
60.97 0.3095 0.6457 0.0568 0.0272 5.048 24.474 20.049 3764.296 2.765 89.179 2.416 0.83 401689. 0.3967
|
|
65.03 0.3302 0.6685 0.0532 0.0263 4.870 23.612 18.774 3631.639 2.668 83.508 2.345 0.83 402216. 0.3726
|
|
69.10 0.3508 0.6884 0.0495 0.0252 4.675 22.664 17.466 3485.869 2.561 77.691 2.273 0.83 402763. 0.3483
|
|
73.16 0.3714 0.7053 0.0457 0.0241 4.461 21.630 16.128 3326.810 2.444 71.737 2.199 0.83 403332. 0.3238
|
|
77.23 0.3921 0.7187 0.0418 0.0228 4.229 20.505 14.760 3153.746 2.317 65.654 2.123 0.83 403922. 0.2991
|
|
81.29 0.4127 0.7282 0.0379 0.0215 3.978 19.288 13.365 2966.640 2.179 59.450 2.043 0.83 404534. 0.2740
|
|
85.36 0.4333 0.7331 0.0338 0.0200 3.709 17.982 11.945 2765.697 2.032 53.133 1.959 0.83 405169. 0.2483
|
|
89.42 0.4540 0.7319 0.0298 0.0185 3.421 16.588 10.502 2551.307 1.874 46.712 1.867 0.83 405825. 0.2219
|
|
93.48 0.4746 0.7228 0.0256 0.0168 3.117 15.110 9.037 2324.038 1.707 40.198 1.764 0.83 406505. 0.1944
|
|
97.55 0.4953 0.7029 0.0214 0.0151 2.795 13.553 7.554 2084.600 1.531 33.601 1.644 0.84 407206. 0.1657
|
|
101.61 0.5159 0.6672 0.0172 0.0133 2.459 11.924 6.056 1833.940 1.347 26.936 1.498 0.84 407930. 0.1352
|
|
105.68 0.5365 0.6071 0.0129 0.0114 2.110 10.229 4.546 1573.227 1.156 20.219 1.311 0.84 408677. 0.1025
|
|
109.74 0.5572 0.5067 0.0086 0.0094 1.749 8.477 3.028 1303.861 0.958 13.466 1.053 0.84 409445. 0.0672
|
|
113.81 0.5778 0.3317 0.0043 0.0074 1.378 6.679 1.506 1027.337 0.755 6.699 0.665 0.84 410230. 0.0299
|
|
117.87 0.5984 -0.0163 -0.0001 0.0053 0.987 4.784 -0.051 735.861 0.541 -0.228 -0.032 0.84 410843. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 14000
|
|
|
|
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 0.0989 0.0373 8.642 38.907 40.496 6444.490 4.396 180.127 2.850 0.89 426537. 0.6652
|
|
4.39 0.0207 0.0542 0.0972 0.0371 8.600 38.718 39.782 6413.104 4.374 176.952 2.814 0.89 426802. 0.6508
|
|
8.78 0.0414 0.1069 0.0953 0.0369 8.548 38.483 39.015 6374.196 4.348 173.539 2.776 0.89 427085. 0.6359
|
|
13.18 0.0621 0.1582 0.0933 0.0366 8.485 38.200 38.194 6327.360 4.316 169.885 2.738 0.89 427387. 0.6205
|
|
17.57 0.0828 0.2079 0.0912 0.0363 8.411 37.867 37.316 6272.104 4.278 165.983 2.699 0.89 427708. 0.6045
|
|
21.96 0.1035 0.2559 0.0889 0.0360 8.325 37.479 36.381 6207.853 4.234 161.825 2.658 0.89 428048. 0.5880
|
|
26.35 0.1242 0.3023 0.0864 0.0355 8.226 37.033 35.388 6134.017 4.184 157.406 2.617 0.89 428408. 0.5709
|
|
30.75 0.1449 0.3470 0.0839 0.0350 8.113 36.526 34.335 6050.021 4.127 152.724 2.574 0.89 428788. 0.5532
|
|
35.14 0.1657 0.3898 0.0812 0.0345 7.986 35.954 33.223 5955.230 4.062 147.776 2.530 0.89 429188. 0.5349
|
|
39.53 0.1864 0.4307 0.0783 0.0339 7.844 35.312 32.051 5849.038 3.990 142.563 2.485 0.89 429609. 0.5160
|
|
43.92 0.2071 0.4697 0.0753 0.0332 7.685 34.599 30.821 5730.912 3.909 137.092 2.439 0.89 430051. 0.4966
|
|
48.32 0.2278 0.5067 0.0722 0.0324 7.510 33.812 29.536 5600.467 3.820 131.376 2.392 0.89 430514. 0.4768
|
|
52.71 0.2485 0.5416 0.0689 0.0316 7.318 32.948 28.199 5457.351 3.722 125.428 2.344 0.89 430999. 0.4564
|
|
57.10 0.2692 0.5743 0.0655 0.0307 7.109 32.005 26.812 5301.148 3.616 119.260 2.294 0.89 431505. 0.4356
|
|
61.49 0.2899 0.6047 0.0620 0.0297 6.881 30.980 25.379 5131.382 3.500 112.884 2.243 0.89 432034. 0.4144
|
|
65.89 0.3106 0.6327 0.0584 0.0287 6.636 29.878 23.901 4948.805 3.376 106.312 2.191 0.89 432585. 0.3927
|
|
70.28 0.3313 0.6576 0.0547 0.0275 6.378 28.714 22.381 4756.042 3.244 99.552 2.134 0.89 433158. 0.3703
|
|
74.67 0.3520 0.6790 0.0509 0.0264 6.106 27.489 20.821 4553.209 3.106 92.613 2.074 0.89 433755. 0.3471
|
|
79.06 0.3727 0.6960 0.0470 0.0251 5.822 26.212 19.223 4341.697 2.961 85.503 2.008 0.89 434374. 0.3229
|
|
83.46 0.3934 0.7068 0.0430 0.0239 5.537 24.929 17.587 4129.210 2.817 78.228 1.932 0.90 435017. 0.2971
|
|
87.85 0.4141 0.7118 0.0389 0.0226 5.239 23.585 15.918 3906.590 2.665 70.804 1.848 0.90 435683. 0.2704
|
|
92.24 0.4348 0.7104 0.0347 0.0213 4.923 22.163 14.219 3670.985 2.504 63.245 1.757 0.90 436373. 0.2429
|
|
96.63 0.4556 0.7011 0.0305 0.0198 4.591 20.668 12.491 3423.386 2.335 55.561 1.655 0.90 437086. 0.2145
|
|
101.02 0.4763 0.6816 0.0262 0.0183 4.244 19.109 10.739 3165.107 2.159 47.767 1.539 0.90 437824. 0.1849
|
|
105.42 0.4970 0.6485 0.0219 0.0168 3.886 17.495 8.966 2897.734 1.977 39.879 1.403 0.90 438586. 0.1541
|
|
109.81 0.5177 0.5973 0.0175 0.0152 3.517 15.835 7.175 2622.864 1.789 31.915 1.241 0.90 439372. 0.1219
|
|
114.20 0.5384 0.5209 0.0131 0.0136 3.141 14.141 5.373 2342.339 1.598 23.899 1.040 0.90 440182. 0.0884
|
|
118.59 0.5591 0.4085 0.0087 0.0119 2.760 12.425 3.565 2058.109 1.404 15.857 0.786 0.90 441016. 0.0544
|
|
122.99 0.5798 0.2426 0.0043 0.0103 2.376 10.697 1.758 1771.844 1.209 7.819 0.450 0.90 441869. 0.0219
|
|
127.38 0.6005 -0.0128 -0.0002 0.0085 1.974 8.889 -0.075 1472.290 1.004 -0.332 -0.023 0.90 442616. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 15000
|
|
|
|
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 0.0998 0.0443 12.626 53.051 46.885 9414.901 5.994 208.546 2.259 0.95 456965. 0.5672
|
|
4.81 0.0212 0.0470 0.0982 0.0442 12.575 52.840 46.147 9377.413 5.970 205.262 2.232 0.95 457248. 0.5561
|
|
9.62 0.0423 0.0930 0.0965 0.0439 12.502 52.530 45.340 9322.386 5.935 201.672 2.206 0.95 457552. 0.5447
|
|
14.42 0.0635 0.1379 0.0946 0.0435 12.402 52.111 44.460 9247.954 5.887 197.759 2.181 0.95 457878. 0.5332
|
|
19.23 0.0846 0.1818 0.0926 0.0431 12.274 51.574 43.505 9152.647 5.827 193.509 2.156 0.95 458226. 0.5215
|
|
24.04 0.1058 0.2247 0.0904 0.0425 12.117 50.914 42.470 9035.510 5.752 188.907 2.132 0.95 458598. 0.5095
|
|
28.85 0.1269 0.2666 0.0880 0.0419 11.930 50.128 41.354 8896.157 5.663 183.945 2.108 0.95 458993. 0.4972
|
|
33.65 0.1481 0.3076 0.0855 0.0411 11.713 49.219 40.157 8734.740 5.561 178.616 2.085 0.95 459411. 0.4846
|
|
38.46 0.1692 0.3477 0.0827 0.0403 11.468 48.187 38.876 8551.709 5.444 172.921 2.062 0.95 459854. 0.4715
|
|
43.27 0.1904 0.3866 0.0798 0.0393 11.194 47.038 37.514 8347.732 5.314 166.861 2.038 0.95 460320. 0.4578
|
|
48.08 0.2115 0.4245 0.0768 0.0383 10.894 45.776 36.073 8123.741 5.172 160.452 2.014 0.95 460812. 0.4436
|
|
52.88 0.2327 0.4611 0.0735 0.0371 10.568 44.407 34.557 7880.750 5.017 153.710 1.989 0.95 461327. 0.4288
|
|
57.69 0.2538 0.4964 0.0702 0.0359 10.218 42.936 32.971 7619.711 4.851 146.656 1.963 0.96 461867. 0.4133
|
|
62.50 0.2750 0.5302 0.0666 0.0346 9.845 41.366 31.319 7341.184 4.674 139.308 1.935 0.96 462432. 0.3971
|
|
67.31 0.2961 0.5624 0.0630 0.0332 9.448 39.700 29.605 7045.439 4.485 131.682 1.906 0.96 463022. 0.3803
|
|
72.11 0.3173 0.5928 0.0592 0.0317 9.029 37.939 27.832 6733.025 4.286 123.799 1.875 0.96 463637. 0.3627
|
|
76.92 0.3385 0.6207 0.0553 0.0302 8.593 36.108 26.006 6408.058 4.079 115.673 1.841 0.96 464277. 0.3442
|
|
81.73 0.3596 0.6448 0.0513 0.0286 8.154 34.263 24.127 6080.652 3.871 107.318 1.800 0.96 464943. 0.3242
|
|
86.54 0.3808 0.6640 0.0472 0.0271 7.715 32.419 22.201 5753.339 3.663 98.749 1.750 0.96 465634. 0.3024
|
|
91.34 0.4019 0.6735 0.0430 0.0257 7.315 30.738 20.226 5455.085 3.473 89.966 1.682 0.96 466352. 0.2774
|
|
96.15 0.4231 0.6675 0.0387 0.0246 6.992 29.380 18.203 5213.992 3.319 80.966 1.583 0.96 467095. 0.2478
|
|
100.96 0.4442 0.6527 0.0344 0.0234 6.659 27.980 16.144 4965.625 3.161 71.809 1.475 0.96 467865. 0.2173
|
|
105.77 0.4654 0.6274 0.0299 0.0222 6.318 26.549 14.055 4711.512 2.999 62.519 1.353 0.96 468661. 0.1860
|
|
110.58 0.4865 0.5897 0.0254 0.0210 5.972 25.093 11.944 4453.218 2.835 53.127 1.217 0.96 469483. 0.1542
|
|
115.38 0.5077 0.5373 0.0209 0.0197 5.622 23.623 9.818 4192.242 2.669 43.671 1.062 0.96 470333. 0.1221
|
|
120.19 0.5288 0.4675 0.0164 0.0185 5.270 22.144 7.688 3929.840 2.502 34.195 0.887 0.97 471208. 0.0902
|
|
125.00 0.5500 0.3771 0.0118 0.0173 4.918 20.664 5.563 3667.116 2.335 24.745 0.688 0.97 472111. 0.0595
|
|
129.81 0.5711 0.2618 0.0073 0.0160 4.567 19.188 3.454 3405.292 2.168 15.362 0.460 0.97 473038. 0.0314
|
|
134.61 0.5923 0.1161 0.0029 0.0148 4.216 17.715 1.364 3143.812 2.001 6.066 0.197 0.97 473985. 0.0084
|
|
139.42 0.6135
|
|
|
|
|
|
|