686 lines
122 KiB
Plaintext
686 lines
122 KiB
Plaintext
13.5x10 (135x10.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 0.1085 0.0555 0.002 0.126 0.115 1.493 0.014 0.511 34.889 0.05 20941. 0.5139
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0.39 0.0308 0.0587 0.1075 0.0564 0.002 0.128 0.114 1.518 0.014 0.506 33.997 0.05 20958. 0.4984
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0.79 0.0617 0.1144 0.1063 0.0573 0.002 0.130 0.113 1.543 0.015 0.501 33.093 0.05 20978. 0.4826
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1.18 0.0925 0.1668 0.1050 0.0582 0.002 0.132 0.111 1.567 0.015 0.495 32.184 0.05 21000. 0.4664
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1.58 0.1233 0.2161 0.1036 0.0591 0.002 0.134 0.110 1.590 0.015 0.488 31.273 0.05 21024. 0.4501
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1.97 0.1541 0.2623 0.1019 0.0599 0.002 0.136 0.108 1.612 0.015 0.480 30.365 0.05 21050. 0.4335
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2.36 0.1850 0.3054 0.1001 0.0606 0.002 0.138 0.106 1.631 0.016 0.471 29.463 0.05 21080. 0.4169
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2.76 0.2158 0.3455 0.0981 0.0613 0.002 0.139 0.104 1.648 0.016 0.462 28.569 0.05 21111. 0.4001
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3.15 0.2466 0.3827 0.0958 0.0618 0.002 0.140 0.101 1.662 0.016 0.451 27.685 0.05 21146. 0.3832
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3.55 0.2775 0.4170 0.0933 0.0621 0.002 0.141 0.099 1.671 0.016 0.439 26.813 0.05 21183. 0.3663
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3.94 0.3083 0.4484 0.0906 0.0623 0.002 0.142 0.096 1.676 0.016 0.427 25.951 0.05 21223. 0.3493
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4.34 0.3391 0.4770 0.0876 0.0623 0.002 0.142 0.093 1.675 0.016 0.412 25.100 0.05 21266. 0.3322
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4.73 0.3700 0.5029 0.0843 0.0620 0.002 0.141 0.089 1.669 0.016 0.397 24.257 0.05 21311. 0.3150
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5.12 0.4008 0.5261 0.0808 0.0615 0.002 0.140 0.085 1.656 0.016 0.380 23.421 0.05 21360. 0.2976
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5.52 0.4316 0.5464 0.0769 0.0608 0.002 0.138 0.081 1.635 0.016 0.362 22.587 0.05 21411. 0.2801
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5.91 0.4624 0.5638 0.0728 0.0597 0.002 0.136 0.077 1.607 0.015 0.343 21.753 0.05 21465. 0.2625
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6.31 0.4933 0.5781 0.0685 0.0584 0.002 0.133 0.072 1.572 0.015 0.322 20.912 0.05 21522. 0.2447
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6.70 0.5241 0.5892 0.0639 0.0568 0.002 0.129 0.068 1.529 0.015 0.301 20.059 0.05 21582. 0.2267
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7.09 0.5549 0.5967 0.0591 0.0550 0.002 0.125 0.063 1.479 0.014 0.278 19.185 0.05 21645. 0.2086
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7.49 0.5858 0.6001 0.0542 0.0529 0.002 0.120 0.057 1.423 0.014 0.255 18.281 0.05 21711. 0.1903
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7.88 0.6166 0.5990 0.0491 0.0506 0.002 0.115 0.052 1.360 0.013 0.231 17.335 0.05 21779. 0.1718
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8.28 0.6474 0.5926 0.0439 0.0480 0.002 0.109 0.047 1.291 0.012 0.207 16.331 0.05 21850. 0.1531
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8.67 0.6782 0.5796 0.0386 0.0452 0.002 0.103 0.041 1.217 0.012 0.182 15.248 0.05 21924. 0.1340
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9.06 0.7091 0.5587 0.0333 0.0422 0.002 0.096 0.035 1.136 0.011 0.157 14.059 0.05 22001. 0.1147
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9.46 0.7399 0.5277 0.0278 0.0390 0.001 0.089 0.029 1.049 0.010 0.131 12.724 0.06 22080. 0.0949
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9.85 0.7707 0.4832 0.0223 0.0356 0.001 0.081 0.024 0.957 0.009 0.105 11.186 0.06 22163. 0.0747
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10.25 0.8016 0.4203 0.0168 0.0320 0.001 0.073 0.018 0.860 0.008 0.079 9.355 0.06 22248. 0.0542
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10.64 0.8324 0.3308 0.0112 0.0282 0.001 0.064 0.012 0.758 0.007 0.053 7.090 0.06 22335. 0.0335
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11.04 0.8632 0.2007 0.0056 0.0242 0.001 0.055 0.006 0.651 0.006 0.026 4.148 0.06 22426. 0.0139
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11.43 0.8941 0.0035 0.0001 0.0200 0.001 0.046 0.000 0.539 0.005 0.000 0.071 0.06 22518. 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 0.1090 0.0491 0.014 0.447 0.462 10.576 0.050 2.053 19.797 0.11 41881. 0.5846
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0.79 0.0311 0.0670 0.1080 0.0501 0.014 0.456 0.457 10.788 0.052 2.034 19.228 0.11 41917. 0.5652
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1.59 0.0621 0.1300 0.1069 0.0511 0.015 0.465 0.453 11.001 0.053 2.013 18.657 0.11 41956. 0.5455
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2.38 0.0932 0.1890 0.1056 0.0521 0.015 0.474 0.447 11.211 0.054 1.988 18.087 0.11 42000. 0.5256
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3.18 0.1243 0.2441 0.1041 0.0530 0.015 0.482 0.441 11.414 0.054 1.961 17.521 0.11 42049. 0.5057
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3.97 0.1553 0.2954 0.1025 0.0539 0.016 0.491 0.434 11.606 0.055 1.931 16.961 0.11 42103. 0.4857
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4.77 0.1864 0.3429 0.1007 0.0547 0.016 0.498 0.426 11.782 0.056 1.896 16.411 0.11 42162. 0.4657
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5.56 0.2175 0.3869 0.0987 0.0555 0.016 0.504 0.418 11.937 0.057 1.858 15.871 0.11 42226. 0.4458
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6.36 0.2486 0.4275 0.0964 0.0560 0.016 0.510 0.408 12.065 0.058 1.815 15.343 0.11 42296. 0.4260
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7.15 0.2796 0.4647 0.0939 0.0565 0.016 0.514 0.398 12.160 0.058 1.768 14.827 0.11 42371. 0.4063
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7.94 0.3107 0.4988 0.0911 0.0568 0.016 0.516 0.386 12.217 0.058 1.716 14.324 0.11 42452. 0.3867
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8.74 0.3418 0.5299 0.0881 0.0568 0.016 0.517 0.373 12.230 0.058 1.659 13.833 0.11 42539. 0.3672
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9.53 0.3728 0.5581 0.0848 0.0566 0.016 0.515 0.359 12.194 0.058 1.597 13.353 0.11 42631. 0.3477
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10.33 0.4039 0.5833 0.0812 0.0562 0.016 0.511 0.344 12.102 0.058 1.529 12.884 0.11 42729. 0.3283
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11.12 0.4350 0.6057 0.0773 0.0555 0.016 0.505 0.327 11.951 0.057 1.456 12.423 0.11 42834. 0.3089
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11.92 0.4660 0.6253 0.0731 0.0545 0.016 0.496 0.310 11.736 0.056 1.378 11.970 0.11 42944. 0.2895
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12.71 0.4971 0.6419 0.0687 0.0532 0.015 0.484 0.291 11.458 0.055 1.294 11.520 0.11 43059. 0.2701
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13.50 0.5282 0.6555 0.0641 0.0517 0.015 0.470 0.271 11.118 0.053 1.207 11.072 0.11 43181. 0.2507
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14.30 0.5593 0.6658 0.0593 0.0498 0.014 0.453 0.251 10.719 0.051 1.116 10.620 0.11 43308. 0.2313
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15.09 0.5903 0.6724 0.0543 0.0477 0.014 0.434 0.230 10.263 0.049 1.023 10.161 0.11 43441. 0.2118
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15.89 0.6214 0.6748 0.0492 0.0453 0.013 0.412 0.208 9.751 0.047 0.926 9.687 0.11 43580. 0.1922
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16.68 0.6525 0.6722 0.0440 0.0427 0.012 0.388 0.186 9.185 0.044 0.828 9.192 0.11 43724. 0.1724
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17.48 0.6835 0.6637 0.0386 0.0398 0.011 0.362 0.164 8.566 0.041 0.728 8.662 0.11 43874. 0.1523
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18.27 0.7146 0.6475 0.0332 0.0367 0.011 0.334 0.141 7.894 0.038 0.626 8.083 0.11 44030. 0.1318
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19.07 0.7457 0.6212 0.0278 0.0333 0.010 0.303 0.118 7.173 0.034 0.523 7.432 0.11 44191. 0.1107
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19.86 0.7767 0.5808 0.0222 0.0297 0.009 0.271 0.094 6.402 0.031 0.419 6.670 0.11 44358. 0.0890
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20.65 0.8078 0.5196 0.0167 0.0259 0.007 0.236 0.071 5.584 0.027 0.314 5.738 0.11 44530. 0.0663
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21.45 0.8389 0.4253 0.0111 0.0219 0.006 0.200 0.047 4.721 0.023 0.209 4.523 0.11 44708. 0.0427
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22.24 0.8700 0.2731 0.0056 0.0177 0.005 0.161 0.024 3.818 0.018 0.105 2.801 0.11 44891. 0.0187
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23.04 0.9010 0.0035 0.0001 0.0134 0.004 0.122 0.000 2.877 0.014 0.001 0.035 0.11 45079. 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 0.1093 0.0465 0.045 0.952 1.042 33.808 0.108 4.633 13.974 0.16 62821. 0.6199
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1.20 0.0312 0.0710 0.1083 0.0476 0.046 0.973 1.032 34.545 0.110 4.591 13.551 0.16 62875. 0.5984
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2.39 0.0624 0.1376 0.1072 0.0486 0.047 0.994 1.021 35.289 0.112 4.543 13.127 0.16 62934. 0.5766
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3.59 0.0935 0.1998 0.1059 0.0496 0.048 1.015 1.009 36.025 0.115 4.489 12.706 0.16 63000. 0.5548
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4.78 0.1247 0.2577 0.1045 0.0506 0.049 1.035 0.995 36.740 0.117 4.428 12.290 0.16 63074. 0.5330
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5.98 0.1559 0.3114 0.1029 0.0515 0.050 1.054 0.980 37.418 0.119 4.359 11.880 0.16 63155. 0.5112
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7.17 0.1871 0.3610 0.1011 0.0524 0.051 1.072 0.963 38.042 0.121 4.282 11.479 0.16 63244. 0.4895
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8.37 0.2183 0.4068 0.0990 0.0531 0.052 1.087 0.943 38.593 0.123 4.196 11.087 0.16 63341. 0.4680
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9.57 0.2494 0.4490 0.0968 0.0538 0.052 1.100 0.922 39.054 0.124 4.100 10.705 0.16 63446. 0.4467
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10.76 0.2806 0.4876 0.0942 0.0542 0.053 1.110 0.898 39.405 0.125 3.994 10.335 0.16 63559. 0.4256
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11.96 0.3118 0.5229 0.0915 0.0545 0.053 1.116 0.871 39.625 0.126 3.876 9.975 0.16 63682. 0.4047
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13.15 0.3430 0.5551 0.0884 0.0546 0.053 1.118 0.842 39.695 0.126 3.747 9.627 0.16 63813. 0.3841
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14.35 0.3741 0.5843 0.0851 0.0545 0.053 1.116 0.811 39.595 0.126 3.607 9.288 0.16 63952. 0.3635
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15.55 0.4053 0.6106 0.0815 0.0541 0.053 1.107 0.776 39.305 0.125 3.453 8.959 0.16 64101. 0.3431
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16.74 0.4365 0.6340 0.0776 0.0534 0.052 1.093 0.739 38.808 0.124 3.288 8.639 0.16 64258. 0.3228
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17.94 0.4677 0.6547 0.0734 0.0524 0.051 1.073 0.699 38.094 0.121 3.110 8.325 0.16 64424. 0.3026
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19.13 0.4989 0.6725 0.0690 0.0512 0.050 1.047 0.657 37.161 0.118 2.922 8.018 0.16 64599. 0.2824
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20.33 0.5300 0.6874 0.0643 0.0496 0.048 1.015 0.612 36.013 0.115 2.724 7.714 0.16 64782. 0.2624
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21.52 0.5612 0.6992 0.0594 0.0477 0.046 0.976 0.566 34.659 0.110 2.519 7.410 0.16 64974. 0.2424
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22.72 0.5924 0.7076 0.0544 0.0456 0.044 0.933 0.519 33.104 0.105 2.306 7.105 0.16 65175. 0.2224
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23.92 0.6236 0.7122 0.0493 0.0432 0.042 0.883 0.470 31.354 0.100 2.089 6.792 0.16 65385. 0.2023
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25.11 0.6548 0.7121 0.0440 0.0405 0.039 0.829 0.419 29.414 0.094 1.866 6.468 0.16 65603. 0.1821
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26.31 0.6859 0.7064 0.0387 0.0376 0.037 0.769 0.369 27.287 0.087 1.639 6.125 0.16 65829. 0.1616
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27.50 0.7171 0.6936 0.0333 0.0344 0.033 0.704 0.317 24.978 0.080 1.409 5.752 0.16 66064. 0.1407
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28.70 0.7483 0.6710 0.0278 0.0310 0.030 0.634 0.264 22.490 0.072 1.176 5.334 0.17 66307. 0.1192
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29.89 0.7795 0.6346 0.0222 0.0273 0.027 0.559 0.212 19.829 0.063 0.942 4.842 0.17 66559. 0.0968
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31.09 0.8106 0.5769 0.0167 0.0234 0.023 0.479 0.159 17.002 0.054 0.706 4.233 0.17 66819. 0.0733
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32.29 0.8418 0.4834 0.0111 0.0193 0.019 0.395 0.106 14.019 0.045 0.470 3.416 0.17 67088. 0.0482
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33.48 0.8730 0.3217 0.0055 0.0150 0.015 0.307 0.053 10.891 0.035 0.234 2.192 0.17 67364. 0.0219
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34.68 0.9042 0.0008 0.0000 0.0105 0.010 0.215 0.000 7.634 0.024 0.000 0.005 0.17 67646. 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 0.1096 0.0451 0.104 1.642 1.857 77.696 0.185 8.259 10.839 0.21 83760. 0.6419
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1.60 0.0312 0.0735 0.1086 0.0462 0.107 1.680 1.840 79.482 0.190 8.184 10.500 0.21 83831. 0.6191
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3.20 0.0625 0.1423 0.1075 0.0472 0.109 1.718 1.821 81.285 0.194 8.101 10.162 0.21 83911. 0.5961
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4.79 0.0937 0.2065 0.1063 0.0482 0.111 1.755 1.800 83.073 0.198 8.005 9.827 0.21 84000. 0.5730
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6.39 0.1250 0.2660 0.1048 0.0493 0.114 1.792 1.776 84.813 0.202 7.898 9.496 0.21 84098. 0.5499
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7.99 0.1562 0.3212 0.1032 0.0502 0.116 1.827 1.748 86.466 0.206 7.776 9.171 0.21 84206. 0.5270
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9.59 0.1875 0.3721 0.1014 0.0511 0.118 1.859 1.718 87.993 0.210 7.640 8.854 0.21 84325. 0.5043
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11.18 0.2187 0.4189 0.0994 0.0519 0.120 1.888 1.683 89.348 0.213 7.487 8.545 0.21 84455. 0.4818
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12.78 0.2499 0.4620 0.0971 0.0525 0.121 1.912 1.645 90.487 0.216 7.317 8.245 0.21 84596. 0.4596
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14.38 0.2812 0.5014 0.0946 0.0531 0.123 1.931 1.602 91.362 0.218 7.127 7.955 0.22 84748. 0.4377
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15.98 0.3124 0.5375 0.0918 0.0534 0.123 1.942 1.555 91.926 0.219 6.918 7.675 0.22 84911. 0.4160
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17.57 0.3437 0.5704 0.0888 0.0535 0.124 1.947 1.504 92.129 0.220 6.689 7.403 0.22 85086. 0.3946
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19.17 0.3749 0.6002 0.0855 0.0534 0.123 1.942 1.447 91.923 0.219 6.438 7.141 0.22 85273. 0.3734
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20.77 0.4061 0.6271 0.0818 0.0530 0.122 1.928 1.386 91.261 0.218 6.164 6.887 0.22 85472. 0.3524
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22.37 0.4374 0.6512 0.0779 0.0523 0.121 1.904 1.319 90.102 0.215 5.868 6.641 0.22 85683. 0.3316
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23.96 0.4686 0.6726 0.0737 0.0513 0.119 1.868 1.248 88.419 0.211 5.551 6.402 0.22 85905. 0.3108
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25.56 0.4999 0.6912 0.0692 0.0501 0.116 1.822 1.172 86.207 0.206 5.214 6.168 0.22 86139. 0.2903
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27.16 0.5311 0.7070 0.0645 0.0485 0.112 1.764 1.093 83.478 0.199 4.861 5.938 0.22 86384. 0.2698
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28.76 0.5624 0.7199 0.0597 0.0466 0.108 1.696 1.010 80.247 0.192 4.494 5.710 0.22 86642. 0.2495
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30.35 0.5936 0.7295 0.0546 0.0444 0.103 1.617 0.925 76.531 0.183 4.115 5.482 0.22 86910. 0.2292
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31.95 0.6248 0.7355 0.0495 0.0420 0.097 1.529 0.837 72.342 0.173 3.725 5.251 0.22 87191. 0.2089
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33.55 0.6561 0.7372 0.0442 0.0393 0.091 1.430 0.748 67.690 0.162 3.327 5.013 0.22 87482. 0.1884
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35.15 0.6873 0.7337 0.0388 0.0363 0.084 1.322 0.657 62.584 0.149 2.922 4.762 0.22 87786. 0.1678
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36.74 0.7186 0.7234 0.0333 0.0331 0.076 1.205 0.565 57.033 0.136 2.512 4.490 0.22 88100. 0.1467
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38.34 0.7498 0.7038 0.0278 0.0296 0.068 1.079 0.471 51.048 0.122 2.096 4.187 0.22 88426. 0.1249
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39.94 0.7810 0.6708 0.0223 0.0259 0.060 0.943 0.377 44.642 0.107 1.677 3.831 0.22 88763. 0.1022
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41.54 0.8123 0.6166 0.0167 0.0220 0.051 0.799 0.282 37.832 0.090 1.256 3.386 0.22 89111. 0.0782
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43.14 0.8435 0.5255 0.0111 0.0178 0.041 0.647 0.188 30.642 0.073 0.835 2.779 0.22 89470. 0.0523
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44.73 0.8748 0.3595 0.0055 0.0134 0.031 0.488 0.093 23.102 0.055 0.415 1.833 0.22 89840. 0.0243
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46.33 0.9060 -0.0017 0.0000 0.0089 0.020 0.322 0.000 15.244 0.036 -0.001 -0.008 0.22 90217. 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 0.1099 0.0443 0.200 2.516 2.909 148.853 0.284 12.941 8.865 0.27 104698. 0.6572
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2.00 0.0313 0.0752 0.1090 0.0453 0.204 2.576 2.884 152.403 0.291 12.827 8.583 0.27 104787. 0.6335
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4.00 0.0626 0.1455 0.1079 0.0464 0.209 2.637 2.855 155.990 0.298 12.698 8.301 0.27 104887. 0.6096
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6.00 0.0938 0.2109 0.1066 0.0474 0.214 2.697 2.822 159.552 0.305 12.551 8.021 0.27 104998. 0.5856
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|
8.00 0.1251 0.2716 0.1052 0.0485 0.219 2.756 2.784 163.022 0.311 12.384 7.746 0.27 105121. 0.5618
|
|
10.00 0.1564 0.3277 0.1036 0.0495 0.223 2.812 2.742 166.327 0.318 12.196 7.477 0.27 105257. 0.5381
|
|
12.00 0.1877 0.3794 0.1018 0.0504 0.227 2.863 2.694 169.384 0.323 11.984 7.215 0.27 105405. 0.5147
|
|
14.00 0.2190 0.4270 0.0998 0.0512 0.231 2.909 2.641 172.106 0.329 11.746 6.960 0.27 105568. 0.4916
|
|
16.00 0.2502 0.4707 0.0975 0.0519 0.234 2.948 2.581 174.403 0.333 11.481 6.713 0.27 105744. 0.4687
|
|
18.00 0.2815 0.5107 0.0950 0.0524 0.236 2.978 2.515 176.180 0.336 11.185 6.474 0.27 105935. 0.4462
|
|
19.99 0.3128 0.5473 0.0923 0.0527 0.238 2.998 2.441 177.343 0.339 10.859 6.244 0.27 106140. 0.4240
|
|
21.99 0.3441 0.5806 0.0892 0.0529 0.238 3.006 2.360 177.793 0.340 10.499 6.022 0.27 106359. 0.4021
|
|
23.99 0.3754 0.6109 0.0859 0.0528 0.238 2.999 2.272 177.436 0.339 10.106 5.808 0.27 106594. 0.3805
|
|
25.99 0.4067 0.6383 0.0822 0.0524 0.236 2.978 2.176 176.178 0.336 9.677 5.601 0.27 106843. 0.3591
|
|
27.99 0.4379 0.6629 0.0783 0.0517 0.233 2.940 2.071 173.936 0.332 9.213 5.401 0.27 107107. 0.3379
|
|
29.99 0.4692 0.6847 0.0740 0.0507 0.229 2.885 1.959 170.656 0.326 8.715 5.208 0.27 107385. 0.3168
|
|
31.99 0.5005 0.7040 0.0696 0.0495 0.223 2.812 1.841 166.328 0.318 8.187 5.019 0.27 107678. 0.2960
|
|
33.99 0.5318 0.7205 0.0648 0.0479 0.216 2.721 1.716 160.973 0.307 7.632 4.835 0.27 107986. 0.2753
|
|
35.99 0.5631 0.7342 0.0599 0.0460 0.207 2.614 1.586 154.622 0.295 7.055 4.653 0.27 108309. 0.2547
|
|
37.99 0.5943 0.7448 0.0549 0.0438 0.198 2.490 1.452 147.305 0.281 6.460 4.472 0.27 108646. 0.2342
|
|
39.99 0.6256 0.7519 0.0497 0.0413 0.186 2.351 1.315 139.047 0.266 5.848 4.289 0.27 108997. 0.2137
|
|
41.99 0.6569 0.7550 0.0444 0.0386 0.174 2.195 1.174 129.868 0.248 5.223 4.101 0.27 109362. 0.1932
|
|
43.99 0.6882 0.7531 0.0390 0.0356 0.161 2.025 1.031 119.785 0.229 4.587 3.905 0.27 109742. 0.1724
|
|
45.99 0.7195 0.7448 0.0335 0.0324 0.146 1.839 0.886 108.816 0.208 3.942 3.694 0.27 110136. 0.1512
|
|
47.99 0.7507 0.7277 0.0279 0.0288 0.130 1.639 0.740 96.982 0.185 3.290 3.459 0.28 110544. 0.1293
|
|
49.99 0.7820 0.6976 0.0224 0.0251 0.113 1.425 0.592 84.308 0.161 2.632 3.183 0.28 110967. 0.1064
|
|
51.99 0.8133 0.6468 0.0167 0.0211 0.095 1.197 0.443 70.830 0.135 1.971 2.838 0.28 111403. 0.0821
|
|
53.99 0.8446 0.5586 0.0111 0.0168 0.076 0.957 0.295 56.594 0.108 1.310 2.360 0.28 111853. 0.0557
|
|
55.99 0.8759 0.3912 0.0055 0.0124 0.056 0.704 0.146 41.663 0.080 0.651 1.594 0.28 112316. 0.0265
|
|
57.99 0.9071 -0.0022 0.0000 0.0078 0.035 0.441 -0.001 26.098 0.050 -0.002 -0.009 0.28 112787. 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 0.1103 0.0437 0.341 3.579 4.203 254.092 0.404 18.695 7.503 0.32 125635. 0.6685
|
|
2.40 0.0313 0.0764 0.1093 0.0448 0.349 3.667 4.167 260.324 0.414 18.534 7.260 0.32 125741. 0.6441
|
|
4.80 0.0626 0.1478 0.1083 0.0459 0.358 3.756 4.126 266.629 0.424 18.351 7.018 0.32 125861. 0.6196
|
|
7.20 0.0939 0.2141 0.1070 0.0470 0.366 3.844 4.079 272.898 0.434 18.142 6.779 0.32 125994. 0.5951
|
|
9.61 0.1252 0.2756 0.1056 0.0480 0.374 3.930 4.026 279.014 0.444 17.906 6.544 0.32 126142. 0.5707
|
|
12.01 0.1565 0.3323 0.1041 0.0490 0.382 4.013 3.965 284.846 0.453 17.637 6.314 0.32 126305. 0.5465
|
|
14.41 0.1878 0.3847 0.1023 0.0499 0.389 4.089 3.897 290.250 0.462 17.334 6.090 0.32 126484. 0.5225
|
|
16.81 0.2191 0.4328 0.1003 0.0508 0.396 4.157 3.821 295.072 0.470 16.994 5.873 0.32 126679. 0.4989
|
|
19.21 0.2504 0.4769 0.0980 0.0515 0.401 4.214 3.735 299.154 0.476 16.612 5.663 0.32 126891. 0.4756
|
|
21.61 0.2818 0.5173 0.0955 0.0520 0.405 4.259 3.639 302.330 0.481 16.188 5.460 0.32 127121. 0.4527
|
|
24.01 0.3131 0.5543 0.0927 0.0524 0.408 4.289 3.534 304.432 0.485 15.718 5.265 0.32 127367. 0.4302
|
|
26.41 0.3444 0.5879 0.0897 0.0525 0.409 4.301 3.417 305.291 0.486 15.200 5.077 0.32 127631. 0.4079
|
|
28.82 0.3757 0.6186 0.0863 0.0524 0.409 4.293 3.290 304.737 0.485 14.633 4.896 0.32 127913. 0.3860
|
|
31.22 0.4070 0.6463 0.0827 0.0521 0.406 4.263 3.151 302.608 0.482 14.014 4.722 0.32 128213. 0.3643
|
|
33.62 0.4383 0.6712 0.0787 0.0514 0.401 4.209 3.000 298.757 0.475 13.343 4.554 0.32 128530. 0.3429
|
|
36.02 0.4696 0.6935 0.0745 0.0504 0.393 4.129 2.838 293.088 0.466 12.623 4.392 0.32 128865. 0.3216
|
|
38.42 0.5009 0.7132 0.0700 0.0491 0.383 4.023 2.666 285.582 0.455 11.859 4.234 0.33 129217. 0.3005
|
|
40.82 0.5322 0.7303 0.0652 0.0475 0.370 3.892 2.486 276.275 0.440 11.056 4.081 0.33 129588. 0.2796
|
|
43.22 0.5635 0.7446 0.0603 0.0456 0.356 3.736 2.298 265.221 0.422 10.221 3.930 0.33 129975. 0.2589
|
|
45.63 0.5948 0.7560 0.0552 0.0434 0.339 3.557 2.104 252.471 0.402 9.358 3.780 0.33 130380. 0.2383
|
|
48.03 0.6261 0.7641 0.0500 0.0410 0.319 3.354 1.905 238.068 0.379 8.473 3.629 0.33 130802. 0.2177
|
|
50.43 0.6574 0.7683 0.0446 0.0382 0.298 3.128 1.701 222.046 0.353 7.568 3.475 0.33 131242. 0.1970
|
|
52.83 0.6887 0.7678 0.0392 0.0352 0.274 2.880 1.494 204.436 0.325 6.647 3.315 0.33 131698. 0.1761
|
|
55.23 0.7200 0.7612 0.0337 0.0319 0.248 2.610 1.284 185.268 0.295 5.712 3.144 0.33 132172. 0.1548
|
|
57.63 0.7513 0.7462 0.0281 0.0283 0.221 2.318 1.072 164.580 0.262 4.767 2.953 0.33 132663. 0.1329
|
|
60.03 0.7827 0.7187 0.0225 0.0245 0.191 2.006 0.857 142.416 0.227 3.814 2.731 0.33 133170. 0.1099
|
|
62.43 0.8140 0.6710 0.0169 0.0204 0.159 1.674 0.642 118.839 0.189 2.857 2.451 0.33 133695. 0.0854
|
|
64.84 0.8453 0.5860 0.0112 0.0162 0.126 1.323 0.427 93.931 0.149 1.899 2.062 0.33 134236. 0.0586
|
|
67.24 0.8766 0.4190 0.0056 0.0117 0.091 0.955 0.212 67.802 0.108 0.945 1.421 0.33 134792. 0.0285
|
|
69.64 0.9079 -0.0011 0.0000 0.0070 0.054 0.571 0.000 40.556 0.065 -0.001 -0.004 0.33 135357. 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 0.1107 0.0434 0.537 4.836 5.741 400.511 0.546 25.537 6.502 0.37 146569. 0.6771
|
|
2.80 0.0313 0.0773 0.1098 0.0445 0.551 4.957 5.693 410.569 0.560 25.324 6.290 0.37 146694. 0.6523
|
|
5.61 0.0627 0.1494 0.1087 0.0456 0.564 5.080 5.638 420.757 0.574 25.080 6.078 0.37 146833. 0.6273
|
|
8.41 0.0940 0.2164 0.1075 0.0467 0.578 5.203 5.576 430.899 0.588 24.801 5.869 0.38 146989. 0.6024
|
|
11.22 0.1253 0.2785 0.1061 0.0478 0.591 5.323 5.504 440.805 0.601 24.483 5.664 0.38 147162. 0.5775
|
|
14.02 0.1567 0.3357 0.1046 0.0488 0.604 5.437 5.423 450.262 0.614 24.122 5.463 0.38 147352. 0.5530
|
|
16.82 0.1880 0.3885 0.1028 0.0497 0.616 5.543 5.331 459.038 0.626 23.714 5.268 0.38 147561. 0.5287
|
|
19.63 0.2193 0.4370 0.1008 0.0506 0.626 5.637 5.228 466.886 0.637 23.253 5.079 0.38 147789. 0.5047
|
|
22.43 0.2506 0.4814 0.0986 0.0513 0.635 5.718 5.112 473.545 0.646 22.737 4.896 0.38 148037. 0.4811
|
|
25.23 0.2820 0.5222 0.0961 0.0519 0.642 5.781 4.982 478.749 0.653 22.161 4.720 0.38 148305. 0.4579
|
|
28.04 0.3133 0.5594 0.0933 0.0522 0.647 5.823 4.839 482.226 0.658 21.522 4.551 0.38 148593. 0.4351
|
|
30.84 0.3446 0.5934 0.0902 0.0524 0.649 5.841 4.680 483.703 0.660 20.817 4.388 0.38 148902. 0.4126
|
|
33.65 0.3760 0.6243 0.0869 0.0523 0.648 5.831 4.506 482.906 0.659 20.043 4.232 0.38 149232. 0.3905
|
|
36.45 0.4073 0.6523 0.0832 0.0520 0.643 5.791 4.316 479.574 0.654 19.198 4.082 0.38 149582. 0.3686
|
|
39.25 0.4386 0.6775 0.0792 0.0513 0.635 5.717 4.110 473.470 0.646 18.282 3.937 0.38 149953. 0.3469
|
|
42.06 0.4700 0.7002 0.0750 0.0503 0.623 5.608 3.889 464.438 0.634 17.297 3.798 0.38 150345. 0.3255
|
|
44.86 0.5013 0.7203 0.0704 0.0490 0.607 5.463 3.654 452.445 0.617 16.251 3.663 0.38 150757. 0.3043
|
|
47.66 0.5326 0.7379 0.0657 0.0474 0.587 5.283 3.406 437.547 0.597 15.152 3.531 0.38 151190. 0.2833
|
|
50.47 0.5640 0.7527 0.0607 0.0455 0.563 5.069 3.149 419.832 0.573 14.008 3.402 0.38 151643. 0.2624
|
|
53.27 0.5953 0.7648 0.0556 0.0433 0.536 4.822 2.884 399.380 0.545 12.826 3.275 0.38 152116. 0.2417
|
|
56.08 0.6266 0.7736 0.0503 0.0408 0.505 4.543 2.611 376.261 0.513 11.612 3.147 0.38 152610. 0.2210
|
|
58.88 0.6579 0.7788 0.0450 0.0380 0.470 4.233 2.332 350.530 0.478 10.372 3.017 0.38 153123. 0.2003
|
|
61.68 0.6893 0.7795 0.0395 0.0349 0.432 3.891 2.048 322.236 0.440 9.109 2.883 0.38 153657. 0.1793
|
|
64.49 0.7206 0.7743 0.0339 0.0316 0.391 3.519 1.760 291.429 0.398 7.828 2.739 0.38 154211. 0.1579
|
|
67.29 0.7519 0.7611 0.0283 0.0280 0.346 3.117 1.468 258.168 0.352 6.532 2.580 0.39 154784. 0.1359
|
|
70.09 0.7833 0.7358 0.0226 0.0241 0.298 2.687 1.175 222.525 0.304 5.225 2.394 0.39 155377. 0.1128
|
|
72.90 0.8146 0.6908 0.0170 0.0200 0.248 2.229 0.880 184.601 0.252 3.913 2.161 0.39 155990. 0.0881
|
|
75.70 0.8459 0.6087 0.0113 0.0157 0.194 1.745 0.584 144.532 0.197 2.600 1.834 0.39 156622. 0.0609
|
|
78.51 0.8773 0.4421 0.0056 0.0111 0.137 1.238 0.290 102.494 0.140 1.291 1.285 0.39 157272. 0.0301
|
|
81.31 0.9086 -0.0043 0.0000 0.0064 0.079 0.708 -0.002 58.647 0.080 -0.007 -0.012 0.39 157931. 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 0.1111 0.0432 0.799 6.292 7.529 595.579 0.711 33.489 5.734 0.43 167502. 0.6838
|
|
3.21 0.0313 0.0779 0.1102 0.0443 0.819 6.454 7.468 610.847 0.729 33.219 5.545 0.43 167644. 0.6587
|
|
6.41 0.0627 0.1506 0.1092 0.0455 0.840 6.617 7.398 626.330 0.748 32.908 5.358 0.43 167803. 0.6334
|
|
9.62 0.0940 0.2180 0.1080 0.0466 0.861 6.780 7.318 641.763 0.766 32.552 5.172 0.43 167981. 0.6082
|
|
12.82 0.1254 0.2805 0.1067 0.0477 0.881 6.940 7.227 656.857 0.784 32.146 4.990 0.43 168178. 0.5831
|
|
16.03 0.1567 0.3381 0.1051 0.0487 0.900 7.092 7.123 671.286 0.801 31.681 4.813 0.43 168396. 0.5582
|
|
19.23 0.1880 0.3912 0.1034 0.0497 0.918 7.234 7.004 684.697 0.817 31.154 4.640 0.43 168635. 0.5337
|
|
22.44 0.2194 0.4399 0.1014 0.0506 0.934 7.361 6.870 696.712 0.832 30.559 4.473 0.43 168896. 0.5095
|
|
25.64 0.2507 0.4847 0.0992 0.0513 0.948 7.469 6.720 706.934 0.844 29.889 4.311 0.43 169180. 0.4858
|
|
28.85 0.2821 0.5256 0.0967 0.0519 0.959 7.554 6.551 714.956 0.853 29.140 4.156 0.43 169487. 0.4624
|
|
32.05 0.3134 0.5631 0.0939 0.0523 0.966 7.611 6.364 720.366 0.860 28.307 4.007 0.43 169817. 0.4394
|
|
35.26 0.3447 0.5972 0.0909 0.0525 0.969 7.636 6.157 722.750 0.863 27.387 3.864 0.43 170170. 0.4167
|
|
38.46 0.3761 0.6284 0.0875 0.0524 0.968 7.625 5.930 721.694 0.861 26.375 3.727 0.43 170547. 0.3944
|
|
41.67 0.4074 0.6566 0.0839 0.0520 0.961 7.573 5.681 716.799 0.856 25.269 3.595 0.43 170948. 0.3724
|
|
44.87 0.4388 0.6822 0.0799 0.0514 0.949 7.477 5.411 707.711 0.845 24.068 3.468 0.43 171373. 0.3506
|
|
48.08 0.4701 0.7052 0.0756 0.0504 0.931 7.334 5.121 694.187 0.829 22.776 3.346 0.43 171821. 0.3291
|
|
51.28 0.5014 0.7257 0.0710 0.0491 0.907 7.144 4.812 676.175 0.807 21.403 3.228 0.43 172293. 0.3077
|
|
54.49 0.5328 0.7436 0.0662 0.0475 0.877 6.907 4.487 653.758 0.780 19.958 3.113 0.43 172788. 0.2866
|
|
57.69 0.5641 0.7590 0.0612 0.0455 0.841 6.625 4.149 627.068 0.749 18.454 3.001 0.44 173307. 0.2657
|
|
60.90 0.5955 0.7717 0.0561 0.0433 0.800 6.299 3.799 596.229 0.712 16.900 2.890 0.44 173848. 0.2449
|
|
64.10 0.6268 0.7813 0.0508 0.0407 0.753 5.931 3.440 561.346 0.670 15.303 2.780 0.44 174413. 0.2241
|
|
67.31 0.6581 0.7873 0.0454 0.0379 0.701 5.520 3.073 522.503 0.624 13.671 2.668 0.44 175001. 0.2033
|
|
70.52 0.6895 0.7890 0.0399 0.0348 0.643 5.069 2.700 479.775 0.573 12.009 2.552 0.44 175611. 0.1823
|
|
73.72 0.7208 0.7852 0.0343 0.0314 0.581 4.577 2.321 433.238 0.517 10.322 2.429 0.44 176244. 0.1609
|
|
76.93 0.7522 0.7736 0.0286 0.0278 0.514 4.046 1.937 382.979 0.457 8.615 2.294 0.44 176900. 0.1388
|
|
80.13 0.7835 0.7504 0.0229 0.0239 0.441 3.477 1.550 329.110 0.393 6.895 2.136 0.44 177579. 0.1156
|
|
83.34 0.8148 0.7081 0.0171 0.0197 0.364 2.871 1.161 271.781 0.324 5.166 1.938 0.44 178279. 0.0908
|
|
86.54 0.8462 0.6293 0.0114 0.0153 0.283 2.231 0.772 211.199 0.252 3.436 1.659 0.44 179002. 0.0634
|
|
89.75 0.8775 0.4652 0.0057 0.0107 0.198 1.560 0.385 147.633 0.176 1.712 1.182 0.44 179746. 0.0319
|
|
92.95 0.9089 0.0006 0.0000 0.0059 0.109 0.859 0.000 81.319 0.097 0.001 0.001 0.45 180498. 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 0.1116 0.0432 1.136 7.957 9.572 847.230 0.899 42.574 5.124 0.48 188432. 0.6890
|
|
3.61 0.0314 0.0784 0.1108 0.0443 1.166 8.165 9.497 869.372 0.922 42.244 4.955 0.48 188591. 0.6637
|
|
7.22 0.0627 0.1514 0.1098 0.0455 1.196 8.376 9.412 891.860 0.946 41.864 4.787 0.48 188770. 0.6383
|
|
10.82 0.0941 0.2192 0.1086 0.0466 1.226 8.587 9.313 914.307 0.970 41.426 4.620 0.48 188971. 0.6128
|
|
14.43 0.1254 0.2820 0.1073 0.0477 1.256 8.793 9.200 936.294 0.993 40.923 4.457 0.48 189193. 0.5876
|
|
18.04 0.1568 0.3399 0.1058 0.0488 1.284 8.991 9.071 957.343 1.016 40.347 4.298 0.48 189438. 0.5626
|
|
21.65 0.1881 0.3932 0.1041 0.0498 1.310 9.175 8.923 976.934 1.037 39.690 4.143 0.48 189707. 0.5379
|
|
25.26 0.2195 0.4421 0.1021 0.0507 1.334 9.340 8.756 994.516 1.055 38.944 3.993 0.48 190001. 0.5136
|
|
28.86 0.2509 0.4870 0.0999 0.0515 1.354 9.481 8.566 1009.510 1.071 38.104 3.849 0.48 190321. 0.4896
|
|
32.47 0.2822 0.5282 0.0974 0.0521 1.370 9.592 8.354 1021.324 1.084 37.161 3.710 0.48 190667. 0.4661
|
|
36.08 0.3136 0.5658 0.0947 0.0525 1.380 9.667 8.118 1029.355 1.092 36.109 3.577 0.48 191039. 0.4430
|
|
39.69 0.3449 0.6002 0.0916 0.0527 1.385 9.701 7.856 1033.003 1.096 34.945 3.450 0.48 191437. 0.4202
|
|
43.30 0.3763 0.6315 0.0883 0.0526 1.383 9.689 7.568 1031.670 1.095 33.662 3.327 0.49 191862. 0.3978
|
|
46.90 0.4077 0.6600 0.0846 0.0522 1.374 9.624 7.252 1024.780 1.087 32.258 3.210 0.49 192314. 0.3757
|
|
50.51 0.4390 0.6858 0.0806 0.0516 1.357 9.502 6.909 1011.819 1.074 30.732 3.097 0.49 192793. 0.3538
|
|
54.12 0.4704 0.7091 0.0763 0.0506 1.331 9.320 6.540 992.433 1.053 29.088 2.989 0.49 193299. 0.3322
|
|
57.73 0.5017 0.7299 0.0717 0.0493 1.296 9.077 6.146 966.542 1.026 27.338 2.884 0.49 193830. 0.3108
|
|
61.33 0.5331 0.7483 0.0669 0.0476 1.253 8.774 5.732 934.269 0.991 25.496 2.783 0.49 194389. 0.2896
|
|
64.94 0.5644 0.7641 0.0618 0.0457 1.201 8.413 5.301 895.803 0.950 23.577 2.684 0.49 194973. 0.2686
|
|
68.55 0.5958 0.7773 0.0566 0.0434 1.142 7.995 4.855 851.328 0.903 21.593 2.586 0.49 195584. 0.2477
|
|
72.16 0.6272 0.7875 0.0513 0.0408 1.074 7.522 4.396 800.995 0.850 19.555 2.489 0.49 196220. 0.2269
|
|
75.77 0.6585 0.7943 0.0458 0.0380 0.999 6.996 3.928 744.930 0.790 17.470 2.391 0.49 196882. 0.2060
|
|
79.37 0.6899 0.7970 0.0402 0.0348 0.916 6.417 3.450 683.242 0.725 15.346 2.290 0.49 197570. 0.1849
|
|
82.98 0.7212 0.7943 0.0346 0.0314 0.826 5.785 2.965 616.038 0.654 13.190 2.183 0.49 198283. 0.1634
|
|
86.59 0.7526 0.7841 0.0289 0.0277 0.729 5.104 2.475 543.446 0.577 11.009 2.066 0.50 199022. 0.1412
|
|
90.20 0.7839 0.7628 0.0231 0.0237 0.624 4.373 1.980 465.628 0.494 8.809 1.929 0.50 199786. 0.1180
|
|
93.81 0.8153 0.7228 0.0173 0.0195 0.513 3.595 1.483 382.802 0.406 6.598 1.758 0.50 200576. 0.0930
|
|
97.41 0.8467 0.6467 0.0115 0.0151 0.396 2.773 0.986 295.266 0.313 4.385 1.514 0.50 201390. 0.0653
|
|
101.02 0.8780 0.4839 0.0057 0.0104 0.273 1.910 0.490 203.415 0.216 2.180 1.093 0.50 202227. 0.0332
|
|
104.63 0.9094 -0.0041 0.0000 0.0055 0.144 1.010 -0.002 107.568 0.114 -0.009 -0.009 0.50 203072. 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 0.1122 0.0433 1.561 9.838 11.875 1163.952 1.111 52.819 4.627 0.54 209359. 0.6931
|
|
4.01 0.0314 0.0787 0.1114 0.0444 1.602 10.100 11.787 1194.940 1.141 52.430 4.474 0.54 209536. 0.6677
|
|
8.02 0.0627 0.1520 0.1104 0.0456 1.645 10.366 11.686 1226.470 1.171 51.979 4.322 0.54 209735. 0.6421
|
|
12.03 0.0941 0.2200 0.1093 0.0468 1.687 10.633 11.569 1257.996 1.201 51.457 4.171 0.54 209957. 0.6166
|
|
16.04 0.1255 0.2829 0.1080 0.0479 1.728 10.894 11.433 1288.926 1.231 50.854 4.023 0.54 210204. 0.5913
|
|
20.05 0.1568 0.3410 0.1065 0.0490 1.768 11.145 11.277 1318.586 1.259 50.160 3.879 0.54 210476. 0.5662
|
|
24.06 0.1882 0.3944 0.1048 0.0500 1.805 11.379 11.098 1346.241 1.286 49.365 3.739 0.54 210776. 0.5414
|
|
28.07 0.2196 0.4435 0.1029 0.0510 1.839 11.589 10.894 1371.108 1.309 48.458 3.604 0.54 211103. 0.5170
|
|
32.08 0.2510 0.4886 0.1007 0.0517 1.867 11.769 10.664 1392.369 1.330 47.431 3.474 0.54 211459. 0.4930
|
|
36.09 0.2823 0.5298 0.0983 0.0524 1.890 11.911 10.404 1409.188 1.346 46.276 3.349 0.54 211843. 0.4694
|
|
40.10 0.3137 0.5676 0.0955 0.0528 1.905 12.008 10.113 1420.722 1.357 44.983 3.229 0.54 212257. 0.4463
|
|
44.11 0.3451 0.6022 0.0925 0.0530 1.912 12.054 9.790 1426.124 1.362 43.547 3.114 0.54 212701. 0.4235
|
|
48.12 0.3764 0.6337 0.0891 0.0529 1.910 12.041 9.434 1424.565 1.360 41.962 3.004 0.54 213174. 0.4010
|
|
52.13 0.4078 0.6624 0.0854 0.0526 1.898 11.962 9.043 1415.241 1.351 40.224 2.898 0.54 213678. 0.3788
|
|
56.14 0.4392 0.6885 0.0814 0.0519 1.874 11.811 8.618 1397.433 1.334 38.332 2.797 0.54 214211. 0.3569
|
|
60.15 0.4705 0.7120 0.0771 0.0509 1.838 11.585 8.159 1370.648 1.309 36.291 2.700 0.54 214773. 0.3352
|
|
64.16 0.5019 0.7331 0.0725 0.0496 1.790 11.282 7.670 1334.763 1.275 34.115 2.606 0.54 215365. 0.3137
|
|
68.17 0.5333 0.7519 0.0676 0.0479 1.730 10.903 7.155 1289.950 1.232 31.823 2.516 0.54 215987. 0.2925
|
|
72.18 0.5646 0.7681 0.0625 0.0460 1.658 10.451 6.617 1236.480 1.181 29.433 2.427 0.54 216637. 0.2714
|
|
76.19 0.5960 0.7818 0.0573 0.0437 1.575 9.928 6.061 1174.613 1.122 26.961 2.341 0.55 217316. 0.2505
|
|
80.20 0.6274 0.7927 0.0519 0.0411 1.481 9.336 5.490 1104.565 1.055 24.419 2.254 0.55 218025. 0.2296
|
|
84.22 0.6587 0.8002 0.0463 0.0381 1.377 8.676 4.905 1026.515 0.980 21.818 2.167 0.55 218761. 0.2086
|
|
88.23 0.6901 0.8037 0.0407 0.0350 1.261 7.950 4.309 940.615 0.898 19.168 2.078 0.55 219527. 0.1875
|
|
92.24 0.7215 0.8021 0.0350 0.0315 1.136 7.159 3.704 847.017 0.809 16.477 1.984 0.55 220320. 0.1659
|
|
96.25 0.7529 0.7933 0.0292 0.0277 1.000 6.305 3.092 745.898 0.712 13.753 1.880 0.55 221142. 0.1437
|
|
100.26 0.7842 0.7737 0.0234 0.0237 0.855 5.388 2.474 637.483 0.609 11.006 1.760 0.55 221992. 0.1204
|
|
104.27 0.8156 0.7360 0.0175 0.0194 0.700 4.413 1.853 522.077 0.499 8.243 1.610 0.55 222870. 0.0953
|
|
108.28 0.8470 0.6627 0.0116 0.0149 0.537 3.382 1.232 400.095 0.382 5.478 1.396 0.55 223775. 0.0673
|
|
112.29 0.8783 0.5021 0.0058 0.0101 0.365 2.300 0.612 272.092 0.260 2.722 1.020 0.56 224706. 0.0347
|
|
116.30 0.9097 -0.0058 0.0000 0.0051 0.186 1.171 -0.004 138.488 0.132 -0.016 -0.011 0.56 225643. 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 0.1128 0.0434 2.085 11.948 14.445 1554.899 1.350 64.251 4.214 0.59 230282. 0.6961
|
|
4.41 0.0314 0.0788 0.1120 0.0446 2.142 12.272 14.345 1597.067 1.386 63.808 4.074 0.59 230477. 0.6707
|
|
8.83 0.0628 0.1522 0.1111 0.0458 2.199 12.602 14.229 1640.067 1.424 63.290 3.935 0.59 230695. 0.6452
|
|
13.24 0.0941 0.2204 0.1100 0.0470 2.257 12.933 14.093 1683.159 1.461 62.686 3.798 0.59 230939. 0.6197
|
|
17.65 0.1255 0.2834 0.1088 0.0482 2.314 13.259 13.935 1725.523 1.498 61.983 3.663 0.59 231211. 0.5943
|
|
22.06 0.1569 0.3416 0.1074 0.0493 2.369 13.571 13.752 1766.228 1.533 61.169 3.532 0.59 231511. 0.5692
|
|
26.48 0.1883 0.3951 0.1057 0.0504 2.420 13.864 13.541 1804.256 1.566 60.230 3.404 0.59 231840. 0.5444
|
|
30.89 0.2197 0.4443 0.1038 0.0513 2.466 14.127 13.299 1838.530 1.596 59.154 3.281 0.59 232201. 0.5200
|
|
35.30 0.2510 0.4894 0.1017 0.0522 2.505 14.353 13.024 1867.913 1.622 57.929 3.162 0.59 232592. 0.4960
|
|
39.71 0.2824 0.5308 0.0993 0.0528 2.536 14.532 12.712 1891.262 1.642 56.544 3.049 0.59 233016. 0.4724
|
|
44.13 0.3138 0.5687 0.0965 0.0533 2.558 14.656 12.363 1907.417 1.656 54.989 2.940 0.59 233473. 0.4493
|
|
48.54 0.3452 0.6034 0.0935 0.0535 2.568 14.716 11.973 1915.228 1.663 53.256 2.835 0.59 233962. 0.4264
|
|
52.95 0.3766 0.6351 0.0901 0.0534 2.566 14.704 11.542 1913.566 1.661 51.338 2.736 0.59 234484. 0.4040
|
|
57.37 0.4079 0.6640 0.0864 0.0531 2.550 14.610 11.068 1901.341 1.651 49.229 2.640 0.59 235038. 0.3818
|
|
61.78 0.4393 0.6903 0.0824 0.0524 2.518 14.427 10.551 1877.587 1.630 46.929 2.549 0.59 235626. 0.3598
|
|
66.19 0.4707 0.7141 0.0780 0.0514 2.470 14.151 9.992 1841.625 1.599 44.443 2.461 0.60 236246. 0.3381
|
|
70.60 0.5021 0.7355 0.0734 0.0501 2.405 13.779 9.395 1793.284 1.557 41.790 2.376 0.60 236899. 0.3166
|
|
75.02 0.5335 0.7546 0.0684 0.0484 2.324 13.315 8.766 1732.796 1.504 38.992 2.295 0.60 237583. 0.2953
|
|
79.43 0.5648 0.7713 0.0633 0.0464 2.227 12.759 8.109 1660.536 1.442 36.071 2.215 0.60 238300. 0.2742
|
|
83.84 0.5962 0.7855 0.0580 0.0440 2.115 12.116 7.430 1576.867 1.369 33.047 2.137 0.60 239049. 0.2532
|
|
88.25 0.6276 0.7969 0.0525 0.0414 1.988 11.388 6.730 1482.095 1.287 29.936 2.060 0.60 239829. 0.2322
|
|
92.67 0.6590 0.8051 0.0470 0.0384 1.846 10.577 6.014 1376.463 1.195 26.752 1.982 0.60 240641. 0.2112
|
|
97.08 0.6903 0.8095 0.0413 0.0352 1.690 9.683 5.285 1260.184 1.094 23.506 1.902 0.60 241483. 0.1900
|
|
101.49 0.7217 0.8089 0.0355 0.0316 1.520 8.709 4.543 1133.466 0.984 20.208 1.818 0.60 242358. 0.1684
|
|
105.91 0.7531 0.8014 0.0296 0.0278 1.336 7.657 3.793 996.543 0.865 16.869 1.726 0.61 243263. 0.1461
|
|
110.32 0.7845 0.7835 0.0237 0.0237 1.139 6.529 3.035 849.724 0.738 13.500 1.620 0.61 244198. 0.1227
|
|
114.73 0.8159 0.7479 0.0177 0.0194 0.930 5.328 2.273 693.418 0.602 10.111 1.487 0.61 245165. 0.0974
|
|
119.14 0.8472 0.6774 0.0118 0.0147 0.708 4.059 1.510 528.192 0.459 6.717 1.297 0.61 246161. 0.0693
|
|
123.56 0.8786 0.5190 0.0059 0.0099 0.476 2.726 0.750 354.798 0.308 3.334 0.958 0.61 247187. 0.0361
|
|
127.97 0.9100 -0.0092 0.0000 0.0049 0.233 1.335 -0.006 173.769 0.151 -0.028 -0.016 0.61 248214. 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 0.1134 0.0437 2.725 14.313 17.289 2032.140 1.617 76.900 3.859 0.64 251203. 0.6974
|
|
4.81 0.0314 0.0787 0.1127 0.0449 2.800 14.705 17.179 2087.751 1.661 76.410 3.732 0.64 251414. 0.6723
|
|
9.63 0.0627 0.1522 0.1119 0.0461 2.876 15.106 17.049 2144.661 1.707 75.834 3.606 0.64 251651. 0.6471
|
|
14.44 0.0941 0.2203 0.1109 0.0474 2.953 15.509 16.897 2201.899 1.752 75.156 3.481 0.64 251917. 0.6218
|
|
19.25 0.1255 0.2834 0.1097 0.0486 3.029 15.907 16.718 2258.379 1.797 74.360 3.358 0.64 252212. 0.5967
|
|
24.06 0.1569 0.3415 0.1083 0.0497 3.102 16.291 16.509 2312.854 1.841 73.431 3.237 0.64 252539. 0.5717
|
|
28.88 0.1882 0.3951 0.1067 0.0508 3.170 16.651 16.266 2363.944 1.881 72.350 3.121 0.64 252899. 0.5471
|
|
33.69 0.2196 0.4443 0.1049 0.0518 3.232 16.976 15.985 2410.178 1.918 71.102 3.008 0.64 253292. 0.5228
|
|
38.50 0.2510 0.4895 0.1028 0.0527 3.286 17.257 15.664 2450.005 1.950 69.673 2.900 0.64 253719. 0.4988
|
|
43.32 0.2824 0.5309 0.1004 0.0534 3.328 17.481 15.298 2481.845 1.975 68.047 2.796 0.65 254182. 0.4753
|
|
48.13 0.3137 0.5689 0.0977 0.0539 3.358 17.638 14.886 2504.127 1.993 66.214 2.696 0.65 254681. 0.4522
|
|
52.94 0.3451 0.6037 0.0946 0.0541 3.373 17.717 14.425 2515.309 2.002 64.162 2.601 0.65 255215. 0.4294
|
|
57.75 0.3765 0.6355 0.0913 0.0541 3.371 17.707 13.912 2513.886 2.000 61.883 2.510 0.65 255785. 0.4069
|
|
62.57 0.4078 0.6646 0.0876 0.0537 3.350 17.598 13.348 2498.429 1.988 59.370 2.423 0.65 256391. 0.3848
|
|
67.38 0.4392 0.6912 0.0835 0.0531 3.309 17.381 12.730 2467.654 1.964 56.623 2.340 0.65 257033. 0.3628
|
|
72.19 0.4706 0.7152 0.0791 0.0521 3.246 17.050 12.061 2420.658 1.926 53.648 2.260 0.65 257711. 0.3411
|
|
77.00 0.5020 0.7370 0.0744 0.0507 3.161 16.603 11.346 2357.199 1.876 50.466 2.183 0.65 258423. 0.3196
|
|
81.82 0.5333 0.7565 0.0695 0.0490 3.054 16.042 10.590 2277.585 1.812 47.105 2.109 0.65 259171. 0.2983
|
|
86.63 0.5647 0.7736 0.0643 0.0469 2.927 15.371 9.801 2182.328 1.737 43.593 2.037 0.65 259954. 0.2772
|
|
91.44 0.5961 0.7883 0.0589 0.0446 2.779 14.594 8.982 2071.927 1.649 39.954 1.966 0.65 260771. 0.2561
|
|
96.26 0.6274 0.8003 0.0534 0.0419 2.611 13.712 8.140 1946.800 1.549 36.207 1.896 0.66 261623. 0.2352
|
|
101.07 0.6588 0.8092 0.0477 0.0389 2.424 12.730 7.277 1807.283 1.438 32.369 1.826 0.66 262509. 0.2141
|
|
105.88 0.6902 0.8144 0.0420 0.0356 2.218 11.648 6.397 1653.663 1.316 28.454 1.755 0.66 263429. 0.1929
|
|
110.69 0.7216 0.8149 0.0361 0.0320 1.993 10.468 5.502 1486.215 1.183 24.475 1.679 0.66 264383. 0.1712
|
|
115.51 0.7529 0.8088 0.0302 0.0281 1.750 9.194 4.596 1305.253 1.039 20.444 1.597 0.66 265370. 0.1488
|
|
120.32 0.7843 0.7926 0.0242 0.0239 1.490 7.827 3.681 1111.175 0.884 16.374 1.503 0.66 266391. 0.1253
|
|
125.13 0.8157 0.7594 0.0181 0.0195 1.213 6.371 2.761 904.524 0.720 12.280 1.384 0.66 267445. 0.1000
|
|
129.95 0.8471 0.6923 0.0121 0.0148 0.920 4.832 1.838 686.058 0.546 8.176 1.215 0.67 268532. 0.0716
|
|
134.76 0.8784 0.5386 0.0060 0.0098 0.613 3.218 0.918 456.827 0.364 4.084 0.912 0.67 269651. 0.0380
|
|
139.57 0.9098 0.0046 0.0000 0.0047 0.292 1.533 0.004 217.650 0.173 0.016 0.008 0.67 270772. 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 0.1141 0.0444 3.522 17.076 20.410 2626.308 1.929 90.783 3.525 0.70 272120. 0.6921
|
|
5.22 0.0314 0.0780 0.1134 0.0456 3.617 17.534 20.292 2696.887 1.981 90.261 3.413 0.70 272347. 0.6682
|
|
10.43 0.0628 0.1509 0.1127 0.0468 3.714 18.005 20.153 2769.221 2.034 89.640 3.301 0.70 272603. 0.6441
|
|
15.65 0.0941 0.2188 0.1117 0.0481 3.811 18.478 19.987 2842.067 2.088 88.903 3.190 0.70 272890. 0.6198
|
|
20.86 0.1255 0.2817 0.1106 0.0493 3.908 18.946 19.791 2914.039 2.141 88.029 3.080 0.70 273210. 0.5956
|
|
26.08 0.1569 0.3399 0.1093 0.0505 4.001 19.398 19.558 2983.559 2.192 86.996 2.973 0.70 273563. 0.5715
|
|
31.29 0.1883 0.3936 0.1078 0.0516 4.089 19.823 19.286 3048.885 2.240 85.782 2.869 0.70 273953. 0.5476
|
|
36.51 0.2197 0.4430 0.1060 0.0526 4.168 20.208 18.967 3108.147 2.283 84.367 2.768 0.70 274379. 0.5239
|
|
41.72 0.2511 0.4884 0.1040 0.0534 4.237 20.542 18.600 3159.395 2.321 82.732 2.670 0.70 274843. 0.5005
|
|
46.94 0.2824 0.5301 0.1016 0.0541 4.292 20.809 18.179 3200.603 2.351 80.859 2.576 0.70 275345. 0.4774
|
|
52.15 0.3138 0.5684 0.0989 0.0546 4.331 20.999 17.701 3229.722 2.372 78.733 2.486 0.70 275886. 0.4546
|
|
57.37 0.3452 0.6034 0.0959 0.0549 4.351 21.096 17.163 3244.710 2.383 76.340 2.399 0.70 276466. 0.4320
|
|
62.59 0.3766 0.6355 0.0926 0.0549 4.350 21.089 16.562 3243.525 2.383 73.670 2.316 0.70 277085. 0.4097
|
|
67.80 0.4080 0.6648 0.0889 0.0545 4.324 20.963 15.898 3224.207 2.368 70.716 2.237 0.70 277744. 0.3876
|
|
73.02 0.4393 0.6915 0.0848 0.0539 4.271 20.708 15.170 3184.990 2.340 67.476 2.160 0.70 278441. 0.3657
|
|
78.23 0.4707 0.7159 0.0804 0.0529 4.190 20.315 14.379 3124.589 2.295 63.958 2.087 0.70 279177. 0.3440
|
|
83.45 0.5021 0.7379 0.0756 0.0515 4.080 19.782 13.532 3042.646 2.235 60.188 2.017 0.70 279951. 0.3225
|
|
88.66 0.5335 0.7578 0.0706 0.0497 3.942 19.112 12.635 2939.564 2.159 56.199 1.950 0.71 280763. 0.3012
|
|
93.88 0.5649 0.7753 0.0654 0.0476 3.776 18.309 11.696 2816.039 2.069 52.025 1.884 0.71 281613. 0.2800
|
|
99.09 0.5963 0.7905 0.0599 0.0452 3.584 17.377 10.723 2672.745 1.963 47.695 1.820 0.71 282500. 0.2590
|
|
104.31 0.6276 0.8031 0.0543 0.0425 3.366 16.321 9.720 2510.258 1.844 43.232 1.756 0.71 283425. 0.2380
|
|
109.52 0.6590 0.8127 0.0486 0.0394 3.123 15.143 8.691 2329.028 1.711 38.658 1.693 0.71 284386. 0.2169
|
|
114.74 0.6904 0.8187 0.0427 0.0360 2.856 13.845 7.642 2129.443 1.564 33.990 1.628 0.71 285384. 0.1956
|
|
119.95 0.7218 0.8202 0.0367 0.0323 2.564 12.430 6.574 1911.867 1.404 29.242 1.560 0.71 286419. 0.1738
|
|
125.17 0.7532 0.8152 0.0307 0.0284 2.249 10.902 5.492 1676.748 1.232 24.429 1.486 0.72 287490. 0.1513
|
|
130.39 0.7845 0.8005 0.0246 0.0241 1.911 9.263 4.399 1424.692 1.047 19.566 1.400 0.72 288598. 0.1277
|
|
135.60 0.8159 0.7690 0.0184 0.0196 1.551 7.520 3.298 1156.558 0.850 14.671 1.294 0.72 289741. 0.1021
|
|
140.82 0.8473 0.7035 0.0123 0.0148 1.171 5.680 2.195 873.565 0.642 9.762 1.140 0.72 290919. 0.0734
|
|
146.03 0.8787 0.5499 0.0061 0.0098 0.774 3.754 1.093 577.384 0.424 4.864 0.859 0.72 292132. 0.0390
|
|
151.25 0.9101 -0.0029 0.0000 0.0046 0.361 1.752 -0.003 269.395 0.198 -0.011 -0.004 0.72 293342. 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 0.1148 0.0461 4.569 20.571 23.807 3407.286 2.324 105.895 3.169 0.75 293033. 0.6721
|
|
5.62 0.0314 0.0757 0.1142 0.0473 4.685 21.094 23.687 3493.925 2.383 105.360 3.075 0.75 293276. 0.6505
|
|
11.23 0.0628 0.1468 0.1135 0.0485 4.804 21.629 23.543 3582.509 2.444 104.718 2.981 0.75 293551. 0.6286
|
|
16.85 0.0941 0.2132 0.1126 0.0497 4.923 22.165 23.369 3671.380 2.504 103.947 2.887 0.75 293858. 0.6066
|
|
22.46 0.1255 0.2752 0.1116 0.0509 5.041 22.693 23.161 3758.710 2.564 103.019 2.795 0.75 294201. 0.5846
|
|
28.08 0.1569 0.3329 0.1104 0.0520 5.153 23.198 22.911 3842.469 2.621 101.908 2.704 0.75 294580. 0.5626
|
|
33.70 0.1883 0.3865 0.1090 0.0531 5.257 23.669 22.613 3920.465 2.674 100.585 2.616 0.75 294999. 0.5407
|
|
39.31 0.2196 0.4361 0.1073 0.0540 5.351 24.091 22.262 3990.422 2.722 99.023 2.530 0.75 295457. 0.5189
|
|
44.93 0.2510 0.4820 0.1053 0.0549 5.431 24.451 21.852 4049.997 2.762 97.198 2.447 0.75 295957. 0.4972
|
|
50.54 0.2824 0.5244 0.1030 0.0555 5.494 24.734 21.377 4096.841 2.794 95.085 2.367 0.75 296498. 0.4756
|
|
56.16 0.3138 0.5635 0.1004 0.0559 5.537 24.926 20.833 4128.576 2.816 92.667 2.289 0.75 297082. 0.4541
|
|
61.78 0.3452 0.5994 0.0974 0.0561 5.556 25.012 20.217 4142.822 2.826 89.925 2.213 0.75 297708. 0.4326
|
|
67.39 0.3765 0.6324 0.0941 0.0560 5.548 24.977 19.525 4137.174 2.822 86.848 2.141 0.76 298376. 0.4111
|
|
73.01 0.4079 0.6626 0.0904 0.0557 5.511 24.809 18.756 4109.273 2.803 83.426 2.070 0.76 299087. 0.3897
|
|
78.62 0.4393 0.6901 0.0863 0.0549 5.440 24.493 17.909 4056.914 2.767 79.657 2.002 0.76 299839. 0.3683
|
|
84.24 0.4707 0.7151 0.0819 0.0539 5.335 24.019 16.986 3978.396 2.714 75.552 1.936 0.76 300634. 0.3469
|
|
89.86 0.5020 0.7378 0.0771 0.0525 5.194 23.383 15.993 3873.047 2.642 71.138 1.873 0.76 301469. 0.3256
|
|
95.47 0.5334 0.7581 0.0720 0.0507 5.017 22.586 14.941 3741.132 2.552 66.457 1.811 0.76 302345. 0.3043
|
|
101.09 0.5648 0.7762 0.0667 0.0485 4.805 21.634 13.838 3583.317 2.444 61.550 1.752 0.76 303262. 0.2832
|
|
106.70 0.5962 0.7919 0.0612 0.0461 4.560 20.529 12.692 3400.291 2.319 56.452 1.693 0.76 304220. 0.2621
|
|
112.32 0.6276 0.8051 0.0555 0.0432 4.281 19.275 11.509 3192.663 2.178 51.193 1.635 0.76 305216. 0.2411
|
|
117.93 0.6589 0.8154 0.0496 0.0401 3.971 17.877 10.296 2961.060 2.020 45.797 1.577 0.77 306253. 0.2200
|
|
123.55 0.6903 0.8222 0.0437 0.0367 3.629 16.338 9.057 2706.118 1.846 40.285 1.518 0.77 307329. 0.1986
|
|
129.17 0.7217 0.8244 0.0376 0.0329 3.257 14.662 7.795 2428.530 1.656 34.674 1.456 0.77 308445. 0.1767
|
|
134.78 0.7531 0.8202 0.0314 0.0288 2.855 12.854 6.516 2129.171 1.452 28.982 1.388 0.77 309599. 0.1540
|
|
140.40 0.7844 0.8057 0.0252 0.0245 2.426 10.923 5.222 1809.215 1.234 23.225 1.309 0.77 310792. 0.1300
|
|
146.01 0.8158 0.7735 0.0189 0.0199 1.972 8.877 3.917 1470.277 1.003 17.424 1.208 0.77 312023. 0.1040
|
|
151.63 0.8472 0.7055 0.0126 0.0151 1.495 6.729 2.608 1114.525 0.760 11.599 1.061 0.78 313293. 0.0745
|
|
157.25 0.8786 0.5454 0.0063 0.0101 0.999 4.497 1.299 744.789 0.508 5.779 0.791 0.78 314598. 0.0392
|
|
162.86 0.9100 -0.0046 0.0000 0.0049 0.488 2.195 -0.005 363.641 0.248 -0.023 -0.006 0.78 315901. 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 0.1154 0.0496 6.041 25.383 27.473 4504.725 2.868 122.198 2.766 0.80 313943. 0.6302
|
|
6.02 0.0314 0.0710 0.1149 0.0508 6.181 25.973 27.354 4609.409 2.934 121.672 2.692 0.80 314201. 0.6119
|
|
12.03 0.0628 0.1381 0.1143 0.0519 6.324 26.573 27.211 4715.908 3.002 121.036 2.617 0.80 314493. 0.5934
|
|
18.05 0.0941 0.2013 0.1135 0.0531 6.466 27.170 27.037 4821.834 3.070 120.262 2.543 0.80 314821. 0.5748
|
|
24.07 0.1255 0.2607 0.1126 0.0542 6.604 27.749 26.825 4924.520 3.135 119.317 2.471 0.80 315186. 0.5562
|
|
30.08 0.1569 0.3165 0.1115 0.0553 6.733 28.293 26.566 5021.074 3.197 118.167 2.400 0.80 315591. 0.5376
|
|
36.10 0.1883 0.3689 0.1102 0.0563 6.851 28.785 26.253 5108.477 3.252 116.774 2.331 0.80 316038. 0.5191
|
|
42.12 0.2196 0.4181 0.1087 0.0571 6.952 29.210 25.877 5183.795 3.300 115.103 2.264 0.81 316528. 0.5006
|
|
48.13 0.2510 0.4642 0.1068 0.0577 7.033 29.550 25.432 5244.228 3.339 113.119 2.200 0.81 317063. 0.4821
|
|
54.15 0.2824 0.5073 0.1046 0.0582 7.090 29.792 24.909 5287.149 3.366 110.794 2.137 0.81 317643. 0.4635
|
|
60.17 0.3138 0.5476 0.1020 0.0585 7.121 29.921 24.303 5310.099 3.381 108.099 2.076 0.81 318269. 0.4448
|
|
66.19 0.3451 0.5851 0.0991 0.0585 7.122 29.925 23.610 5310.682 3.381 105.015 2.016 0.81 318941. 0.4258
|
|
72.20 0.3765 0.6199 0.0958 0.0582 7.089 29.789 22.825 5286.545 3.366 101.525 1.958 0.81 319659. 0.4066
|
|
78.22 0.4079 0.6520 0.0921 0.0576 7.021 29.500 21.947 5235.307 3.333 97.618 1.901 0.81 320422. 0.3872
|
|
84.24 0.4393 0.6815 0.0881 0.0568 6.913 29.046 20.974 5154.691 3.282 93.291 1.846 0.81 321231. 0.3674
|
|
90.25 0.4707 0.7085 0.0836 0.0555 6.763 28.416 19.909 5042.893 3.210 88.555 1.791 0.81 322084. 0.3473
|
|
96.27 0.5020 0.7330 0.0788 0.0539 6.570 27.606 18.760 4899.231 3.119 83.444 1.737 0.81 322982. 0.3270
|
|
102.29 0.5334 0.7550 0.0736 0.0520 6.335 26.620 17.537 4724.119 3.007 78.005 1.684 0.81 323924. 0.3065
|
|
108.30 0.5648 0.7746 0.0682 0.0498 6.059 25.460 16.252 4518.370 2.876 72.290 1.631 0.82 324908. 0.2859
|
|
114.32 0.5962 0.7916 0.0626 0.0472 5.743 24.132 14.915 4282.714 2.726 66.341 1.580 0.82 325936. 0.2651
|
|
120.34 0.6275 0.8060 0.0568 0.0442 5.388 22.639 13.533 4017.767 2.558 60.194 1.528 0.82 327006. 0.2443
|
|
126.35 0.6589 0.8169 0.0509 0.0410 4.996 20.992 12.113 3725.486 2.372 53.878 1.475 0.82 328119. 0.2231
|
|
132.37 0.6903 0.8238 0.0448 0.0375 4.567 19.192 10.660 3405.955 2.168 47.417 1.420 0.82 329274. 0.2015
|
|
138.39 0.7217 0.8256 0.0385 0.0337 4.103 17.242 9.180 3059.814 1.948 40.834 1.361 0.82 330470. 0.1792
|
|
144.40 0.7530 0.8198 0.0322 0.0296 3.606 15.151 7.677 2688.829 1.712 34.148 1.295 0.83 331708. 0.1560
|
|
150.42 0.7844 0.8021 0.0258 0.0253 3.078 12.934 6.155 2295.427 1.461 27.379 1.216 0.83 332988. 0.1312
|
|
156.44 0.8158 0.7633 0.0194 0.0207 2.525 10.608 4.620 1882.664 1.199 20.550 1.113 0.83 334308. 0.1040
|
|
162.45 0.8472 0.6834 0.0129 0.0160 1.950 8.195 3.077 1454.347 0.926 13.685 0.960 0.83 335668. 0.0732
|
|
168.47 0.8785 0.5058 0.0064 0.0112 1.361 5.720 1.533 1015.116 0.646 6.817 0.685 0.83 337068. 0.0368
|
|
174.49 0.9099 -0.0041 0.0000 0.0063 0.764 3.208 -0.007 569.380 0.362 -0.030 -0.005 0.84 338472. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 16000
|
|
|
|
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 0.1156 0.0552 8.154 32.120 31.338 6080.269 3.629 139.390 2.338 0.86 334857. 0.5688
|
|
6.43 0.0314 0.0643 0.1152 0.0563 8.326 32.797 31.226 6208.341 3.705 138.892 2.281 0.86 335130. 0.5541
|
|
12.85 0.0628 0.1253 0.1147 0.0575 8.501 33.487 31.091 6338.969 3.783 138.291 2.225 0.86 335439. 0.5391
|
|
19.28 0.0942 0.1833 0.1141 0.0587 8.675 34.172 30.925 6468.667 3.861 137.555 2.168 0.86 335785. 0.5241
|
|
25.70 0.1257 0.2381 0.1134 0.0598 8.842 34.830 30.721 6593.283 3.935 136.646 2.113 0.86 336172. 0.5091
|
|
32.13 0.1571 0.2902 0.1124 0.0609 8.996 35.436 30.467 6708.068 4.004 135.518 2.060 0.86 336601. 0.4942
|
|
38.55 0.1885 0.3396 0.1113 0.0618 9.130 35.964 30.154 6808.011 4.063 134.124 2.009 0.86 337076. 0.4795
|
|
44.98 0.2199 0.3865 0.1099 0.0625 9.237 36.389 29.769 6888.304 4.111 132.414 1.960 0.86 337597. 0.4649
|
|
51.41 0.2513 0.4313 0.1081 0.0630 9.313 36.686 29.303 6944.690 4.145 130.342 1.914 0.86 338167. 0.4503
|
|
57.83 0.2827 0.4740 0.1061 0.0633 9.352 36.840 28.746 6973.729 4.162 127.864 1.870 0.86 338786. 0.4357
|
|
64.26 0.3142 0.5148 0.1037 0.0633 9.350 36.833 28.090 6972.506 4.161 124.943 1.827 0.86 339456. 0.4209
|
|
70.68 0.3456 0.5535 0.1008 0.0630 9.306 36.658 27.327 6939.337 4.142 121.551 1.786 0.86 340175. 0.4058
|
|
77.11 0.3770 0.5902 0.0976 0.0624 9.216 36.306 26.454 6872.687 4.102 117.666 1.746 0.86 340944. 0.3903
|
|
83.54 0.4084 0.6247 0.0940 0.0614 9.080 35.769 25.467 6771.009 4.041 113.275 1.706 0.86 341762. 0.3742
|
|
89.96 0.4398 0.6571 0.0899 0.0602 8.895 35.039 24.365 6632.826 3.959 108.374 1.666 0.87 342629. 0.3575
|
|
96.39 0.4712 0.6872 0.0854 0.0586 8.659 34.110 23.151 6457.075 3.854 102.974 1.626 0.87 343544. 0.3401
|
|
102.81 0.5026 0.7149 0.0806 0.0567 8.373 32.984 21.834 6243.833 3.727 97.116 1.586 0.87 344507. 0.3221
|
|
109.24 0.5341 0.7402 0.0754 0.0544 8.039 31.666 20.426 5994.345 3.578 90.856 1.546 0.87 345516. 0.3036
|
|
115.66 0.5655 0.7630 0.0699 0.0518 7.657 30.164 18.942 5710.087 3.408 84.254 1.505 0.87 346572. 0.2846
|
|
122.09 0.5969 0.7831 0.0642 0.0489 7.231 28.486 17.393 5392.410 3.218 77.365 1.463 0.87 347674. 0.2652
|
|
128.52 0.6283 0.8003 0.0583 0.0457 6.762 26.636 15.790 5042.125 3.009 70.233 1.420 0.87 348821. 0.2453
|
|
134.94 0.6597 0.8136 0.0522 0.0423 6.254 24.635 14.139 4663.323 2.783 62.891 1.375 0.88 350013. 0.2248
|
|
141.37 0.6911 0.8207 0.0459 0.0387 5.717 22.520 12.447 4263.044 2.544 55.365 1.324 0.88 351250. 0.2031
|
|
147.79 0.7225 0.8193 0.0396 0.0349 5.156 20.311 10.719 3844.818 2.295 47.677 1.264 0.88 352531. 0.1799
|
|
154.22 0.7540 0.8078 0.0331 0.0309 4.562 17.972 8.962 3402.034 2.030 39.862 1.195 0.88 353856. 0.1555
|
|
160.65 0.7854 0.7805 0.0265 0.0267 3.941 15.527 7.182 2939.172 1.754 31.944 1.108 0.88 355225. 0.1291
|
|
167.07 0.8168 0.7268 0.0199 0.0223 3.301 13.003 5.385 2461.527 1.469 23.954 0.992 0.89 356638. 0.1001
|
|
173.50 0.8482 0.6255 0.0132 0.0179 2.649 10.433 3.581 1975.043 1.179 15.928 0.822 0.89 358093. 0.0676
|
|
179.92 0.8796 0.4282 0.0066 0.0135 1.993 7.852 1.779 1486.299 0.887 7.913 0.543 0.89 359591. 0.0315
|
|
186.35 0.9110 -0.0035 0.0000 0.0091 1.342 5.287 -0.009 1000.916 0.597 -0.042 -0.004 0.89 361106. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 17000
|
|
|
|
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 0.1146 0.0609 10.796 40.028 35.050 8050.750 4.522 155.904 1.975 0.91 355812. 0.5081
|
|
6.86 0.0316 0.0581 0.1142 0.0620 10.996 40.770 34.940 8199.974 4.606 155.413 1.933 0.91 356102. 0.4965
|
|
13.72 0.0631 0.1137 0.1138 0.0632 11.204 41.539 34.810 8354.722 4.693 154.834 1.890 0.91 356428. 0.4846
|
|
20.58 0.0947 0.1666 0.1133 0.0644 11.414 42.318 34.653 8511.417 4.781 154.136 1.847 0.91 356795. 0.4725
|
|
27.44 0.1263 0.2170 0.1127 0.0656 11.621 43.085 34.461 8665.595 4.868 153.281 1.804 0.91 357204. 0.4602
|
|
34.30 0.1578 0.2649 0.1119 0.0667 11.817 43.812 34.223 8811.825 4.950 152.224 1.762 0.91 357658. 0.4479
|
|
41.16 0.1894 0.3104 0.1109 0.0677 11.994 44.468 33.928 8943.862 5.024 150.911 1.721 0.91 358160. 0.4356
|
|
48.02 0.2209 0.3539 0.1097 0.0685 12.143 45.020 33.562 9054.860 5.086 149.285 1.681 0.91 358712. 0.4233
|
|
54.88 0.2525 0.3954 0.1082 0.0691 12.254 45.431 33.113 9137.608 5.133 147.285 1.644 0.91 359315. 0.4111
|
|
61.74 0.2841 0.4352 0.1065 0.0695 12.317 45.666 32.565 9184.835 5.159 144.849 1.608 0.91 359972. 0.3989
|
|
68.59 0.3156 0.4736 0.1043 0.0695 12.323 45.690 31.905 9189.553 5.162 141.916 1.575 0.91 360683. 0.3866
|
|
75.45 0.3472 0.5106 0.1017 0.0692 12.264 45.471 31.122 9145.582 5.137 138.429 1.543 0.92 361449. 0.3742
|
|
82.31 0.3788 0.5464 0.0987 0.0684 12.133 44.983 30.202 9047.388 5.082 134.340 1.514 0.92 362269. 0.3617
|
|
89.17 0.4103 0.5810 0.0953 0.0673 11.926 44.216 29.141 8893.195 4.996 129.620 1.486 0.92 363144. 0.3487
|
|
96.03 0.4419 0.6144 0.0913 0.0657 11.643 43.167 27.935 8682.185 4.877 124.256 1.459 0.92 364072. 0.3353
|
|
102.89 0.4734 0.6464 0.0869 0.0637 11.285 41.841 26.587 8415.527 4.727 118.260 1.433 0.92 365054. 0.3211
|
|
109.75 0.5050 0.6768 0.0821 0.0612 10.858 40.255 25.108 8096.525 4.548 111.680 1.407 0.92 366087. 0.3063
|
|
116.61 0.5366 0.7053 0.0769 0.0585 10.366 38.432 23.513 7729.926 4.342 104.587 1.380 0.92 367171. 0.2908
|
|
123.47 0.5681 0.7318 0.0713 0.0554 9.817 36.397 21.821 7320.457 4.112 97.059 1.352 0.93 368305. 0.2745
|
|
130.33 0.5997 0.7560 0.0655 0.0520 9.215 34.167 20.045 6871.922 3.860 89.162 1.323 0.93 369488. 0.2575
|
|
137.19 0.6313 0.7773 0.0595 0.0483 8.565 31.756 18.200 6387.115 3.588 80.955 1.292 0.93 370720. 0.2397
|
|
144.05 0.6628 0.7955 0.0533 0.0444 7.869 29.175 16.296 5867.900 3.296 72.486 1.260 0.93 372000. 0.2210
|
|
150.91 0.6944 0.8059 0.0469 0.0404 7.160 26.546 14.339 5339.244 2.999 63.779 1.218 0.93 373328. 0.2005
|
|
157.77 0.7259 0.7993 0.0403 0.0366 6.488 24.056 12.328 4838.445 2.718 54.836 1.156 0.93 374703. 0.1764
|
|
164.63 0.7575 0.7761 0.0336 0.0328 5.814 21.557 10.280 4335.797 2.436 45.724 1.075 0.94 376125. 0.1499
|
|
171.49 0.7891 0.7322 0.0268 0.0289 5.125 19.002 8.206 3821.935 2.147 36.502 0.974 0.94 377594. 0.1213
|
|
178.35 0.8206 0.6569 0.0200 0.0250 4.431 16.429 6.121 3304.343 1.856 27.225 0.840 0.94 379109. 0.0903
|
|
185.21 0.8522 0.5332 0.0132 0.0211 3.742 13.873 4.040 2790.282 1.567 17.968 0.657 0.94 380669. 0.0574
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192.07 0.8838 0.3313 0.0065 0.0173 3.066 11.367 1.983 2286.163 1.284 8.820 0.393 0.95 382274. 0.0241
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198.93 0.9153 -0.0071 -0.0001 0.0136 2.408 8.927 -0.032 1795.539 1.009 -0.144 -0.008 0.95 383908. 0.0000
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PROP RPM = 18000
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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 0.1120 0.0664 13.968 48.911 38.413 10416.183 5.526 170.862 1.673 0.96 376833. 0.4506
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7.33 0.0319 0.0528 0.1117 0.0674 14.180 49.652 38.294 10573.936 5.610 170.331 1.643 0.96 377141. 0.4418
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14.66 0.0637 0.1036 0.1113 0.0684 14.403 50.432 38.157 10739.994 5.698 169.721 1.611 0.96 377488. 0.4326
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21.99 0.0956 0.1523 0.1108 0.0695 14.632 51.234 37.996 10910.818 5.788 169.004 1.580 0.96 377878. 0.4232
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29.32 0.1274 0.1989 0.1102 0.0706 14.861 52.037 37.802 11081.896 5.879 168.144 1.547 0.96 378312. 0.4135
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36.66 0.1593 0.2434 0.1095 0.0717 15.083 52.815 37.566 11247.601 5.967 167.096 1.515 0.97 378794. 0.4036
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43.99 0.1912 0.2860 0.1087 0.0727 15.289 53.537 37.276 11401.274 6.049 165.806 1.483 0.97 379326. 0.3935
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51.32 0.2230 0.3266 0.1076 0.0735 15.469 54.167 36.919 11535.502 6.120 164.215 1.452 0.97 379911. 0.3834
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58.65 0.2549 0.3654 0.1064 0.0742 15.613 54.669 36.479 11642.363 6.176 162.257 1.421 0.97 380551. 0.3731
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65.98 0.2867 0.4025 0.1048 0.0746 15.708 55.004 35.941 11713.744 6.214 159.865 1.392 0.97 381248. 0.3626
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|
73.31 0.3186 0.4381 0.1029 0.0748 15.746 55.135 35.290 11741.586 6.229 156.970 1.363 0.97 382002. 0.3520
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|
80.64 0.3504 0.4723 0.1006 0.0747 15.714 55.024 34.511 11718.045 6.217 153.507 1.336 0.97 382816. 0.3411
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|
87.97 0.3823 0.5050 0.0979 0.0741 15.604 54.637 33.591 11635.563 6.173 149.413 1.309 0.97 383689. 0.3299
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95.30 0.4142 0.5365 0.0948 0.0732 15.404 53.938 32.517 11486.780 6.094 144.634 1.284 0.97 384621. 0.3182
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|
102.63 0.4460 0.5667 0.0912 0.0718 15.106 52.895 31.279 11264.523 5.976 139.128 1.259 0.97 385612. 0.3062
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|
109.97 0.4779 0.5958 0.0871 0.0699 14.701 51.475 29.872 10962.220 5.816 132.871 1.236 0.97 386661. 0.2936
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|
117.30 0.5097 0.6241 0.0825 0.0674 14.182 49.661 28.300 10575.798 5.611 125.879 1.214 0.98 387768. 0.2806
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|
124.63 0.5416 0.6516 0.0775 0.0644 13.553 47.458 26.576 10106.816 5.362 118.208 1.193 0.98 388932. 0.2672
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|
131.96 0.5735 0.6783 0.0721 0.0609 12.821 44.893 24.714 9560.403 5.072 109.928 1.172 0.98 390151. 0.2533
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|
139.29 0.6053 0.7039 0.0663 0.0570 11.996 42.004 22.733 8945.244 4.746 101.114 1.153 0.98 391426. 0.2389
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|
146.62 0.6372 0.7278 0.0602 0.0527 11.093 38.843 20.650 8272.092 4.388 91.849 1.132 0.98 392754. 0.2236
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|
153.95 0.6690 0.7493 0.0539 0.0481 10.127 35.459 18.483 7551.358 4.006 82.211 1.110 0.99 394134. 0.2074
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|
161.28 0.7009 0.7662 0.0474 0.0433 9.119 31.933 16.247 6800.399 3.608 72.267 1.084 0.99 395566. 0.1898
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|
168.61 0.7327 0.7601 0.0406 0.0392 8.243 28.864 13.934 6146.823 3.261 61.980 1.028 0.99 397049. 0.1668
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|
175.95 0.7646 0.7201 0.0337 0.0358 7.530 26.366 11.557 5614.948 2.979 51.408 0.934 0.99 398582. 0.1380
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|
183.28 0.7965 0.6570 0.0267 0.0324 6.821 23.886 9.170 5086.691 2.699 40.787 0.818 0.99 400165. 0.1076
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|
190.61 0.8283 0.5642 0.0198 0.0291 6.127 21.453 6.801 4568.591 2.424 30.252 0.675 1.00 401796. 0.0765
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|
197.94 0.8602 0.4330 0.0130 0.0259 5.454 19.097 4.475 4067.007 2.158 19.903 0.499 1.00 403476. 0.0459
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205.27 0.8920 0.2510 0.0064 0.0229 4.812 16.851 2.207 3588.662 1.904 9.816 0.279 1.00 405204. 0.0180
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|
212.60 0.9239 0.0006 0.0000 0.0200 4.199 14.703 0.004 3131.208 1.661 0.019 0.001 1.00 406983. 0.0000
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