575 lines
102 KiB
Plaintext
575 lines
102 KiB
Plaintext
16x6E (16x6E.dat)
|
|
v2022-0915
|
|
Simulation Date: 09/22/2022
|
|
|
|
AIRFOIL AERO DATA GENERATED USING: POLAR DIAGRAMS
|
|
|
|
====== PERFORMANCE DATA (versus advance ratio and MPH) ======
|
|
|
|
DEFINITIONS:
|
|
J=V/nD (advance ratio)
|
|
Ct=T/(rho * n**2 * D**4) (thrust coef.)
|
|
Cp=P/(rho * n**3 * D**5) (power coef.)
|
|
Pe=Ct*J/Cp (efficiency)
|
|
V (model speed in MPH)
|
|
Mach (at prop tip)
|
|
Reyn (at 75% of span)
|
|
FOM (Figure of Merit)
|
|
|
|
|
|
PROP RPM = 1000
|
|
|
|
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 0.0685 0.0253 0.002 0.135 0.143 1.593 0.015 0.637 40.741 0.06 23855. 0.5653
|
|
0.27 0.0176 0.0464 0.0671 0.0254 0.002 0.135 0.140 1.598 0.015 0.624 39.806 0.06 23866. 0.5467
|
|
0.53 0.0351 0.0906 0.0657 0.0254 0.002 0.135 0.137 1.601 0.015 0.610 38.863 0.06 23877. 0.5279
|
|
0.80 0.0527 0.1326 0.0642 0.0255 0.002 0.136 0.134 1.603 0.015 0.596 37.912 0.06 23889. 0.5090
|
|
1.06 0.0702 0.1724 0.0626 0.0255 0.002 0.136 0.131 1.604 0.015 0.581 36.954 0.06 23902. 0.4898
|
|
1.33 0.0878 0.2098 0.0609 0.0255 0.002 0.135 0.127 1.602 0.015 0.565 35.989 0.06 23915. 0.4706
|
|
1.60 0.1053 0.2450 0.0591 0.0254 0.002 0.135 0.123 1.599 0.015 0.549 35.016 0.06 23930. 0.4512
|
|
1.86 0.1229 0.2778 0.0573 0.0253 0.002 0.135 0.120 1.594 0.015 0.532 34.034 0.06 23945. 0.4316
|
|
2.13 0.1404 0.3082 0.0553 0.0252 0.002 0.134 0.116 1.586 0.015 0.514 33.042 0.06 23960. 0.4119
|
|
2.39 0.1580 0.3362 0.0533 0.0251 0.002 0.133 0.111 1.577 0.015 0.495 32.038 0.06 23977. 0.3921
|
|
2.66 0.1756 0.3617 0.0512 0.0249 0.002 0.132 0.107 1.565 0.015 0.476 31.021 0.06 23995. 0.3721
|
|
2.93 0.1931 0.3846 0.0491 0.0246 0.002 0.131 0.102 1.550 0.015 0.456 29.987 0.06 24013. 0.3520
|
|
3.19 0.2107 0.4049 0.0468 0.0244 0.002 0.130 0.098 1.533 0.015 0.435 28.933 0.06 24032. 0.3318
|
|
3.46 0.2282 0.4223 0.0445 0.0240 0.002 0.128 0.093 1.512 0.014 0.413 27.856 0.06 24052. 0.3113
|
|
3.72 0.2458 0.4367 0.0420 0.0237 0.002 0.126 0.088 1.489 0.014 0.391 26.751 0.06 24074. 0.2907
|
|
3.99 0.2633 0.4480 0.0395 0.0232 0.002 0.124 0.083 1.463 0.014 0.367 25.614 0.06 24096. 0.2700
|
|
4.26 0.2809 0.4560 0.0370 0.0228 0.002 0.121 0.077 1.434 0.014 0.344 24.439 0.06 24119. 0.2491
|
|
4.52 0.2984 0.4603 0.0344 0.0223 0.002 0.118 0.072 1.402 0.013 0.319 23.220 0.06 24143. 0.2281
|
|
4.79 0.3160 0.4607 0.0317 0.0217 0.002 0.116 0.066 1.367 0.013 0.294 21.951 0.06 24167. 0.2070
|
|
5.05 0.3336 0.4569 0.0289 0.0211 0.002 0.112 0.060 1.329 0.013 0.269 20.621 0.06 24193. 0.1859
|
|
5.32 0.3511 0.4483 0.0261 0.0205 0.002 0.109 0.055 1.288 0.012 0.243 19.220 0.06 24220. 0.1647
|
|
5.59 0.3687 0.4344 0.0233 0.0198 0.002 0.105 0.049 1.245 0.012 0.217 17.737 0.06 24248. 0.1435
|
|
5.85 0.3862 0.4145 0.0204 0.0190 0.002 0.101 0.043 1.198 0.011 0.190 16.156 0.06 24277. 0.1224
|
|
6.12 0.4038 0.3878 0.0175 0.0183 0.002 0.097 0.037 1.149 0.011 0.163 14.459 0.06 24307. 0.1015
|
|
6.38 0.4213 0.3533 0.0146 0.0174 0.001 0.093 0.031 1.097 0.010 0.136 12.624 0.06 24338. 0.0809
|
|
6.65 0.4389 0.3097 0.0117 0.0166 0.001 0.088 0.024 1.043 0.010 0.109 10.624 0.06 24371. 0.0609
|
|
6.92 0.4564 0.2554 0.0088 0.0157 0.001 0.083 0.018 0.986 0.009 0.081 8.425 0.06 24404. 0.0418
|
|
7.18 0.4740 0.1884 0.0059 0.0147 0.001 0.078 0.012 0.927 0.009 0.054 5.985 0.06 24438. 0.0243
|
|
7.45 0.4916 0.1060 0.0030 0.0138 0.001 0.073 0.006 0.865 0.008 0.028 3.248 0.06 24473. 0.0094
|
|
7.71 0.5091 0.0044 0.0001 0.0127 0.001 0.068 0.000 0.802 0.008 0.001 0.130 0.06 24509. 0.0001
|
|
|
|
|
|
|
|
PROP RPM = 2000
|
|
|
|
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 0.0688 0.0227 0.015 0.483 0.575 11.423 0.055 2.556 22.817 0.13 47710. 0.6343
|
|
0.54 0.0177 0.0523 0.0674 0.0228 0.015 0.485 0.563 11.469 0.055 2.504 22.268 0.13 47731. 0.6128
|
|
1.07 0.0353 0.1019 0.0659 0.0229 0.015 0.486 0.551 11.504 0.055 2.450 21.717 0.13 47754. 0.5911
|
|
1.61 0.0530 0.1490 0.0644 0.0229 0.015 0.487 0.538 11.528 0.055 2.393 21.166 0.13 47778. 0.5693
|
|
2.14 0.0707 0.1935 0.0628 0.0229 0.015 0.488 0.524 11.538 0.055 2.333 20.615 0.13 47804. 0.5475
|
|
2.68 0.0883 0.2354 0.0611 0.0229 0.015 0.487 0.510 11.534 0.055 2.270 20.065 0.13 47831. 0.5256
|
|
3.21 0.1060 0.2748 0.0593 0.0229 0.015 0.487 0.495 11.514 0.055 2.204 19.515 0.13 47860. 0.5037
|
|
3.75 0.1237 0.3115 0.0574 0.0228 0.015 0.485 0.480 11.477 0.055 2.135 18.964 0.13 47890. 0.4818
|
|
4.28 0.1413 0.3457 0.0555 0.0227 0.015 0.483 0.464 11.422 0.055 2.062 18.413 0.13 47922. 0.4598
|
|
4.82 0.1590 0.3772 0.0535 0.0225 0.015 0.479 0.447 11.346 0.054 1.987 17.860 0.13 47956. 0.4378
|
|
5.35 0.1767 0.4061 0.0514 0.0223 0.015 0.475 0.429 11.249 0.054 1.909 17.304 0.13 47991. 0.4157
|
|
5.89 0.1943 0.4322 0.0492 0.0221 0.015 0.470 0.411 11.129 0.053 1.827 16.744 0.13 48028. 0.3936
|
|
6.42 0.2120 0.4556 0.0469 0.0218 0.015 0.464 0.392 10.986 0.052 1.743 16.178 0.13 48067. 0.3714
|
|
6.96 0.2297 0.4760 0.0445 0.0215 0.015 0.457 0.372 10.816 0.052 1.655 15.604 0.13 48108. 0.3491
|
|
7.49 0.2473 0.4935 0.0421 0.0211 0.014 0.449 0.352 10.621 0.051 1.564 15.019 0.13 48151. 0.3267
|
|
8.03 0.2650 0.5077 0.0396 0.0207 0.014 0.440 0.331 10.400 0.050 1.471 14.422 0.13 48195. 0.3042
|
|
8.57 0.2826 0.5185 0.0370 0.0202 0.014 0.429 0.309 10.153 0.048 1.375 13.809 0.13 48242. 0.2816
|
|
9.10 0.3003 0.5257 0.0344 0.0196 0.013 0.418 0.287 9.879 0.047 1.277 13.176 0.13 48290. 0.2589
|
|
9.64 0.3180 0.5288 0.0316 0.0190 0.013 0.405 0.264 9.580 0.046 1.176 12.518 0.13 48341. 0.2361
|
|
10.17 0.3356 0.5275 0.0289 0.0184 0.012 0.391 0.241 9.254 0.044 1.074 11.830 0.13 48393. 0.2131
|
|
10.71 0.3533 0.5212 0.0261 0.0177 0.012 0.376 0.218 8.902 0.043 0.969 11.105 0.13 48448. 0.1901
|
|
11.24 0.3710 0.5092 0.0232 0.0169 0.011 0.360 0.194 8.523 0.041 0.864 10.333 0.13 48504. 0.1670
|
|
11.78 0.3886 0.4907 0.0204 0.0161 0.011 0.343 0.170 8.118 0.039 0.757 9.504 0.13 48563. 0.1437
|
|
12.31 0.4063 0.4644 0.0175 0.0153 0.010 0.325 0.146 7.688 0.037 0.649 8.603 0.13 48623. 0.1205
|
|
12.85 0.4240 0.4288 0.0145 0.0144 0.010 0.306 0.121 7.234 0.035 0.540 7.613 0.13 48686. 0.0973
|
|
13.38 0.4416 0.3819 0.0116 0.0134 0.009 0.285 0.097 6.755 0.032 0.431 6.509 0.13 48751. 0.0743
|
|
13.92 0.4593 0.3208 0.0087 0.0124 0.008 0.264 0.073 6.255 0.030 0.322 5.257 0.13 48818. 0.0519
|
|
14.45 0.4770 0.2416 0.0058 0.0114 0.008 0.242 0.048 5.734 0.027 0.214 3.813 0.13 48888. 0.0307
|
|
14.99 0.4946 0.1387 0.0029 0.0103 0.007 0.220 0.024 5.194 0.025 0.107 2.110 0.13 48959. 0.0120
|
|
15.52 0.5123 0.0023 0.0000 0.0092 0.006 0.196 0.000 4.635 0.022 0.002 0.034 0.13 49030. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 3000
|
|
|
|
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 0.0690 0.0216 0.049 1.033 1.298 36.655 0.117 5.772 16.058 0.19 71564. 0.6709
|
|
0.81 0.0177 0.0553 0.0676 0.0217 0.049 1.037 1.271 36.822 0.117 5.655 15.662 0.19 71596. 0.6476
|
|
1.61 0.0355 0.1079 0.0662 0.0218 0.050 1.041 1.244 36.954 0.118 5.532 15.266 0.19 71631. 0.6244
|
|
2.42 0.0532 0.1576 0.0646 0.0218 0.050 1.044 1.215 37.045 0.118 5.403 14.872 0.19 71667. 0.6011
|
|
3.22 0.0709 0.2046 0.0630 0.0218 0.050 1.045 1.184 37.090 0.118 5.267 14.480 0.19 71706. 0.5778
|
|
4.03 0.0886 0.2489 0.0613 0.0218 0.050 1.045 1.152 37.085 0.118 5.124 14.089 0.19 71747. 0.5546
|
|
4.84 0.1064 0.2904 0.0595 0.0218 0.050 1.043 1.118 37.025 0.118 4.974 13.700 0.19 71790. 0.5313
|
|
5.64 0.1241 0.3292 0.0576 0.0217 0.049 1.040 1.083 36.904 0.117 4.818 13.313 0.19 71836. 0.5081
|
|
6.45 0.1418 0.3654 0.0557 0.0216 0.049 1.035 1.046 36.718 0.117 4.655 12.927 0.19 71884. 0.4849
|
|
7.25 0.1596 0.3988 0.0536 0.0215 0.049 1.027 1.008 36.462 0.116 4.484 12.541 0.19 71935. 0.4618
|
|
8.06 0.1773 0.4294 0.0515 0.0213 0.048 1.018 0.968 36.131 0.115 4.307 12.155 0.19 71989. 0.4386
|
|
8.86 0.1950 0.4573 0.0493 0.0210 0.048 1.006 0.927 35.720 0.114 4.122 11.768 0.19 72045. 0.4155
|
|
9.67 0.2128 0.4824 0.0470 0.0207 0.047 0.992 0.884 35.224 0.112 3.931 11.379 0.19 72103. 0.3923
|
|
10.48 0.2305 0.5046 0.0446 0.0204 0.046 0.976 0.839 34.638 0.110 3.732 10.986 0.19 72165. 0.3690
|
|
11.28 0.2482 0.5237 0.0422 0.0200 0.046 0.957 0.793 33.961 0.108 3.526 10.588 0.19 72229. 0.3457
|
|
12.09 0.2659 0.5397 0.0396 0.0195 0.045 0.935 0.745 33.191 0.106 3.315 10.183 0.19 72296. 0.3224
|
|
12.89 0.2837 0.5522 0.0370 0.0190 0.043 0.911 0.696 32.328 0.103 3.097 9.769 0.19 72367. 0.2989
|
|
13.70 0.3014 0.5611 0.0344 0.0185 0.042 0.884 0.646 31.372 0.100 2.874 9.343 0.19 72440. 0.2754
|
|
14.51 0.3191 0.5661 0.0317 0.0178 0.041 0.854 0.595 30.323 0.097 2.647 8.901 0.19 72516. 0.2518
|
|
15.31 0.3369 0.5665 0.0289 0.0172 0.039 0.822 0.543 29.179 0.093 2.415 8.439 0.19 72595. 0.2280
|
|
16.12 0.3546 0.5619 0.0261 0.0164 0.037 0.787 0.490 27.940 0.089 2.179 7.953 0.19 72677. 0.2041
|
|
16.92 0.3723 0.5516 0.0232 0.0157 0.036 0.750 0.436 26.608 0.085 1.940 7.434 0.19 72763. 0.1801
|
|
17.73 0.3901 0.5344 0.0203 0.0148 0.034 0.710 0.382 25.183 0.080 1.698 6.875 0.19 72851. 0.1558
|
|
18.54 0.4078 0.5091 0.0174 0.0139 0.032 0.667 0.327 23.666 0.075 1.454 6.265 0.19 72943. 0.1313
|
|
19.34 0.4255 0.4737 0.0145 0.0130 0.030 0.622 0.272 22.062 0.070 1.209 5.586 0.19 73038. 0.1068
|
|
20.15 0.4432 0.4257 0.0115 0.0120 0.027 0.574 0.216 20.373 0.065 0.963 4.819 0.19 73136. 0.0822
|
|
20.95 0.4610 0.3613 0.0086 0.0110 0.025 0.524 0.161 18.605 0.059 0.718 3.933 0.19 73237. 0.0579
|
|
21.76 0.4787 0.2750 0.0057 0.0099 0.022 0.472 0.107 16.765 0.053 0.474 2.883 0.19 73342. 0.0345
|
|
22.57 0.4964 0.1582 0.0028 0.0087 0.020 0.419 0.052 14.859 0.047 0.233 1.600 0.19 73449. 0.0134
|
|
23.37 0.5142 -0.0050 -0.0001 0.0076 0.017 0.363 -0.001 12.877 0.041 -0.006 -0.049 0.19 73555. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 4000
|
|
|
|
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 0.0693 0.0210 0.113 1.784 2.317 84.429 0.202 10.307 12.449 0.25 95417. 0.6949
|
|
1.08 0.0177 0.0572 0.0679 0.0211 0.114 1.793 2.270 84.843 0.203 10.099 12.137 0.25 95460. 0.6707
|
|
2.15 0.0355 0.1115 0.0665 0.0211 0.114 1.800 2.221 85.170 0.203 9.879 11.828 0.25 95506. 0.6464
|
|
3.23 0.0532 0.1629 0.0649 0.0212 0.115 1.805 2.169 85.400 0.204 9.648 11.520 0.25 95555. 0.6222
|
|
4.30 0.0710 0.2115 0.0633 0.0212 0.115 1.807 2.114 85.519 0.204 9.405 11.214 0.25 95607. 0.5980
|
|
5.38 0.0887 0.2572 0.0616 0.0212 0.115 1.807 2.057 85.517 0.204 9.150 10.911 0.25 95662. 0.5739
|
|
6.45 0.1065 0.3001 0.0598 0.0212 0.114 1.804 1.997 85.380 0.204 8.883 10.609 0.25 95720. 0.5498
|
|
7.53 0.1242 0.3402 0.0579 0.0211 0.114 1.798 1.934 85.098 0.203 8.604 10.310 0.25 95781. 0.5259
|
|
8.60 0.1419 0.3776 0.0559 0.0210 0.114 1.789 1.869 84.657 0.202 8.312 10.012 0.25 95845. 0.5019
|
|
9.68 0.1597 0.4122 0.0539 0.0209 0.113 1.776 1.800 84.045 0.201 8.008 9.716 0.25 95913. 0.4781
|
|
10.75 0.1774 0.4441 0.0517 0.0207 0.112 1.759 1.729 83.252 0.199 7.691 9.420 0.25 95984. 0.4543
|
|
11.83 0.1952 0.4732 0.0495 0.0204 0.110 1.738 1.655 82.266 0.196 7.362 9.125 0.25 96059. 0.4305
|
|
12.90 0.2129 0.4994 0.0472 0.0201 0.109 1.713 1.578 81.072 0.194 7.019 8.829 0.25 96138. 0.4067
|
|
13.98 0.2306 0.5228 0.0448 0.0198 0.107 1.683 1.498 79.659 0.190 6.664 8.531 0.25 96220. 0.3829
|
|
15.05 0.2484 0.5432 0.0424 0.0194 0.105 1.649 1.416 78.023 0.186 6.297 8.230 0.25 96306. 0.3591
|
|
16.13 0.2661 0.5604 0.0398 0.0189 0.102 1.609 1.331 76.162 0.182 5.919 7.925 0.25 96396. 0.3353
|
|
17.20 0.2839 0.5743 0.0372 0.0184 0.099 1.565 1.243 74.074 0.177 5.531 7.614 0.25 96490. 0.3114
|
|
18.28 0.3016 0.5846 0.0345 0.0178 0.096 1.516 1.154 71.759 0.171 5.133 7.295 0.26 96587. 0.2874
|
|
19.35 0.3194 0.5909 0.0318 0.0172 0.093 1.463 1.063 69.214 0.165 4.727 6.964 0.26 96689. 0.2633
|
|
20.43 0.3371 0.5929 0.0290 0.0165 0.089 1.404 0.970 66.437 0.159 4.313 6.620 0.26 96795. 0.2391
|
|
21.51 0.3548 0.5899 0.0262 0.0158 0.085 1.340 0.875 63.429 0.151 3.892 6.257 0.26 96904. 0.2146
|
|
22.58 0.3726 0.5811 0.0233 0.0149 0.081 1.272 0.779 60.191 0.144 3.465 5.871 0.26 97018. 0.1900
|
|
23.66 0.3903 0.5655 0.0204 0.0141 0.076 1.199 0.682 56.725 0.135 3.034 5.453 0.26 97137. 0.1652
|
|
24.73 0.4081 0.5416 0.0175 0.0132 0.071 1.121 0.584 53.036 0.127 2.598 4.996 0.26 97259. 0.1400
|
|
25.81 0.4258 0.5073 0.0145 0.0122 0.066 1.038 0.486 49.130 0.117 2.161 4.484 0.26 97386. 0.1146
|
|
26.88 0.4436 0.4597 0.0116 0.0112 0.060 0.951 0.387 45.018 0.107 1.722 3.901 0.26 97517. 0.0890
|
|
27.96 0.4613 0.3945 0.0086 0.0101 0.055 0.860 0.289 40.712 0.097 1.285 3.219 0.26 97652. 0.0634
|
|
29.03 0.4790 0.3048 0.0057 0.0090 0.049 0.766 0.191 36.230 0.086 0.851 2.395 0.26 97792. 0.0384
|
|
30.11 0.4968 0.1796 0.0028 0.0078 0.042 0.667 0.095 31.588 0.075 0.422 1.361 0.26 97935. 0.0154
|
|
31.18 0.5145 -0.0027 0.0000 0.0066 0.036 0.565 -0.001 26.755 0.064 -0.005 -0.020 0.26 98076. 0.0000
|
|
|
|
|
|
|
|
PROP RPM = 5000
|
|
|
|
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 0.0697 0.0206 0.217 2.741 3.640 162.119 0.310 16.192 10.185 0.32 119268. 0.7126
|
|
1.36 0.0180 0.0592 0.0683 0.0207 0.219 2.755 3.566 162.954 0.311 15.861 9.925 0.32 119323. 0.6873
|
|
2.72 0.0359 0.1153 0.0668 0.0208 0.219 2.766 3.487 163.613 0.312 15.512 9.668 0.32 119381. 0.6621
|
|
4.08 0.0539 0.1684 0.0652 0.0209 0.220 2.774 3.405 164.074 0.313 15.144 9.412 0.32 119443. 0.6369
|
|
5.44 0.0718 0.2185 0.0635 0.0209 0.220 2.778 3.318 164.309 0.314 14.757 9.159 0.32 119509. 0.6118
|
|
6.80 0.0898 0.2656 0.0618 0.0209 0.220 2.777 3.227 164.295 0.314 14.352 8.908 0.32 119579. 0.5868
|
|
8.16 0.1077 0.3098 0.0600 0.0209 0.220 2.772 3.131 164.007 0.313 13.926 8.659 0.32 119653. 0.5619
|
|
9.52 0.1257 0.3511 0.0580 0.0208 0.219 2.763 3.031 163.420 0.312 13.481 8.412 0.32 119731. 0.5371
|
|
10.88 0.1436 0.3896 0.0560 0.0207 0.218 2.747 2.926 162.508 0.310 13.016 8.167 0.32 119813. 0.5124
|
|
12.24 0.1616 0.4253 0.0540 0.0205 0.216 2.726 2.817 161.247 0.308 12.531 7.924 0.32 119899. 0.4878
|
|
13.60 0.1795 0.4581 0.0518 0.0203 0.214 2.698 2.703 159.614 0.305 12.025 7.682 0.32 119990. 0.4632
|
|
14.96 0.1975 0.4881 0.0495 0.0200 0.211 2.664 2.585 157.582 0.301 11.499 7.441 0.32 120085. 0.4387
|
|
16.32 0.2155 0.5152 0.0472 0.0197 0.208 2.622 2.462 155.125 0.296 10.952 7.199 0.32 120186. 0.4143
|
|
17.68 0.2334 0.5393 0.0447 0.0194 0.204 2.573 2.335 152.219 0.291 10.385 6.957 0.32 120290. 0.3898
|
|
19.04 0.2514 0.5604 0.0422 0.0189 0.200 2.516 2.203 148.856 0.284 9.799 6.712 0.32 120400. 0.3654
|
|
20.40 0.2693 0.5783 0.0396 0.0184 0.194 2.452 2.067 145.034 0.277 9.195 6.465 0.32 120515. 0.3409
|
|
21.76 0.2873 0.5927 0.0369 0.0179 0.189 2.379 1.928 140.748 0.269 8.575 6.213 0.32 120634. 0.3163
|
|
23.12 0.3052 0.6035 0.0342 0.0173 0.182 2.299 1.785 135.994 0.260 7.940 5.954 0.32 120759. 0.2917
|
|
24.48 0.3232 0.6103 0.0314 0.0166 0.175 2.211 1.639 130.769 0.250 7.292 5.686 0.32 120889. 0.2670
|
|
25.84 0.3411 0.6126 0.0286 0.0159 0.168 2.114 1.491 125.070 0.239 6.631 5.407 0.32 121024. 0.2421
|
|
27.20 0.3591 0.6096 0.0257 0.0151 0.159 2.010 1.340 118.898 0.227 5.960 5.112 0.32 121164. 0.2170
|
|
28.56 0.3771 0.6006 0.0227 0.0143 0.151 1.898 1.187 112.254 0.214 5.280 4.796 0.32 121310. 0.1916
|
|
29.92 0.3950 0.5843 0.0198 0.0134 0.141 1.777 1.032 105.146 0.201 4.592 4.454 0.32 121460. 0.1660
|
|
31.28 0.4130 0.5589 0.0168 0.0124 0.131 1.650 0.877 97.583 0.186 3.900 4.075 0.32 121617. 0.1399
|
|
32.65 0.4309 0.5220 0.0138 0.0114 0.120 1.514 0.720 89.581 0.171 3.204 3.647 0.32 121779. 0.1135
|
|
34.01 0.4489 0.4697 0.0108 0.0103 0.109 1.372 0.564 81.164 0.155 2.508 3.151 0.32 121946. 0.0868
|
|
35.37 0.4668 0.3965 0.0078 0.0092 0.097 1.223 0.408 72.361 0.138 1.815 2.557 0.32 122119. 0.0599
|
|
36.73 0.4848 0.2928 0.0049 0.0080 0.085 1.068 0.253 63.207 0.121 1.127 1.819 0.32 122298. 0.0336
|
|
38.09 0.5027 0.1422 0.0019 0.0068 0.072 0.908 0.101 53.736 0.103 0.449 0.852 0.32 122480. 0.0099
|
|
39.45 0.5207
|
|
|
|
|
|
|
|
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 0.0702 0.0204 0.372 3.909 5.277 277.523 0.442 23.470 8.624 0.38 143117. 0.7265
|
|
1.63 0.0179 0.0599 0.0688 0.0205 0.374 3.930 5.169 278.977 0.444 22.993 8.404 0.38 143183. 0.7007
|
|
3.25 0.0358 0.1167 0.0672 0.0206 0.376 3.946 5.056 280.126 0.446 22.489 8.186 0.38 143253. 0.6751
|
|
4.88 0.0536 0.1704 0.0657 0.0207 0.377 3.957 4.937 280.926 0.447 21.959 7.971 0.38 143327. 0.6495
|
|
6.50 0.0715 0.2211 0.0640 0.0207 0.377 3.963 4.812 281.336 0.448 21.402 7.757 0.38 143406. 0.6240
|
|
8.13 0.0894 0.2689 0.0622 0.0207 0.377 3.963 4.680 281.313 0.448 20.817 7.546 0.38 143490. 0.5987
|
|
9.75 0.1073 0.3137 0.0604 0.0207 0.377 3.956 4.542 280.811 0.447 20.205 7.337 0.38 143578. 0.5735
|
|
11.38 0.1252 0.3557 0.0585 0.0206 0.375 3.941 4.398 279.789 0.445 19.563 7.130 0.38 143671. 0.5484
|
|
13.00 0.1430 0.3948 0.0565 0.0205 0.373 3.919 4.247 278.203 0.443 18.893 6.925 0.38 143769. 0.5234
|
|
14.63 0.1609 0.4311 0.0544 0.0203 0.370 3.888 4.090 276.010 0.439 18.193 6.721 0.38 143873. 0.4985
|
|
16.25 0.1788 0.4646 0.0522 0.0201 0.366 3.848 3.926 273.169 0.435 17.464 6.519 0.38 143981. 0.4737
|
|
17.88 0.1967 0.4953 0.0500 0.0198 0.362 3.798 3.756 269.636 0.429 16.707 6.318 0.38 144095. 0.4490
|
|
19.51 0.2146 0.5231 0.0476 0.0195 0.356 3.738 3.579 265.364 0.422 15.919 6.117 0.38 144215. 0.4244
|
|
21.13 0.2324 0.5480 0.0452 0.0192 0.349 3.667 3.395 260.311 0.414 15.102 5.916 0.38 144340. 0.3998
|
|
22.76 0.2503 0.5700 0.0426 0.0187 0.341 3.585 3.205 254.460 0.405 14.257 5.713 0.38 144471. 0.3751
|
|
24.38 0.2682 0.5888 0.0400 0.0182 0.332 3.491 3.010 247.808 0.394 13.387 5.509 0.38 144608. 0.3505
|
|
26.01 0.2861 0.6044 0.0374 0.0177 0.322 3.386 2.809 240.346 0.383 12.494 5.301 0.38 144751. 0.3258
|
|
27.63 0.3040 0.6164 0.0346 0.0171 0.311 3.269 2.603 232.067 0.369 11.579 5.088 0.38 144899. 0.3011
|
|
29.26 0.3218 0.6244 0.0318 0.0164 0.299 3.141 2.393 222.965 0.355 10.645 4.868 0.38 145054. 0.2762
|
|
30.88 0.3397 0.6282 0.0290 0.0157 0.286 3.001 2.179 213.034 0.339 9.693 4.640 0.38 145215. 0.2512
|
|
32.51 0.3576 0.6269 0.0261 0.0149 0.271 2.849 1.962 202.276 0.322 8.725 4.398 0.38 145382. 0.2259
|
|
34.13 0.3755 0.6197 0.0232 0.0140 0.256 2.686 1.741 190.693 0.303 7.744 4.141 0.38 145556. 0.2004
|
|
35.76 0.3934 0.6055 0.0202 0.0131 0.239 2.512 1.518 178.295 0.284 6.753 3.862 0.38 145736. 0.1745
|
|
37.39 0.4112 0.5824 0.0172 0.0121 0.221 2.326 1.293 165.102 0.263 5.753 3.553 0.38 145922. 0.1482
|
|
39.01 0.4291 0.5480 0.0142 0.0111 0.203 2.129 1.068 151.139 0.241 4.749 3.204 0.38 146115. 0.1214
|
|
40.64 0.4470 0.4986 0.0112 0.0100 0.183 1.922 0.842 136.445 0.217 3.745 2.799 0.38 146314. 0.0942
|
|
42.26 0.4649 0.4281 0.0082 0.0089 0.162 1.706 0.617 121.070 0.193 2.744 2.311 0.38 146520. 0.0666
|
|
43.89 0.4828 0.3269 0.0052 0.0077 0.141 1.480 0.394 105.078 0.167 1.751 1.699 0.39 146733. 0.0391
|
|
45.51 0.5006 0.1770 0.0023 0.0065 0.119 1.247 0.173 88.528 0.141 0.770 0.887 0.39 146950. 0.0135
|
|
47.14 0.5185
|
|
|
|
|
|
|
|
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 0.0707 0.0203 0.589 5.302 7.239 439.086 0.599 32.197 7.477 0.44 166963. 0.7378
|
|
1.88 0.0178 0.0602 0.0693 0.0205 0.592 5.330 7.093 441.389 0.602 31.548 7.288 0.44 167040. 0.7118
|
|
3.77 0.0355 0.1172 0.0678 0.0205 0.594 5.352 6.939 443.206 0.605 30.863 7.101 0.44 167121. 0.6860
|
|
5.65 0.0533 0.1713 0.0662 0.0206 0.596 5.367 6.777 444.467 0.606 30.143 6.915 0.44 167208. 0.6602
|
|
7.53 0.0710 0.2223 0.0646 0.0206 0.597 5.374 6.606 445.107 0.607 29.385 6.732 0.44 167300. 0.6346
|
|
9.42 0.0888 0.2704 0.0628 0.0206 0.597 5.374 6.428 445.057 0.607 28.591 6.551 0.44 167396. 0.6091
|
|
11.30 0.1065 0.3156 0.0610 0.0206 0.596 5.364 6.240 444.248 0.606 27.758 6.371 0.44 167499. 0.5837
|
|
13.18 0.1243 0.3579 0.0591 0.0205 0.594 5.344 6.045 442.611 0.604 26.886 6.194 0.44 167607. 0.5585
|
|
15.06 0.1420 0.3975 0.0571 0.0204 0.590 5.314 5.840 440.079 0.600 25.975 6.019 0.44 167721. 0.5334
|
|
16.95 0.1598 0.4343 0.0550 0.0202 0.585 5.272 5.626 436.584 0.596 25.025 5.845 0.44 167840. 0.5084
|
|
18.83 0.1775 0.4683 0.0528 0.0200 0.579 5.217 5.404 432.062 0.589 24.035 5.673 0.44 167966. 0.4836
|
|
20.71 0.1953 0.4995 0.0505 0.0198 0.572 5.149 5.172 426.442 0.582 23.005 5.501 0.45 168098. 0.4588
|
|
22.60 0.2131 0.5280 0.0482 0.0194 0.563 5.067 4.932 419.653 0.572 21.936 5.330 0.45 168236. 0.4341
|
|
24.48 0.2308 0.5537 0.0458 0.0191 0.552 4.970 4.682 411.624 0.562 20.826 5.159 0.45 168381. 0.4094
|
|
26.36 0.2486 0.5764 0.0432 0.0186 0.540 4.858 4.424 402.326 0.549 19.679 4.988 0.45 168532. 0.3847
|
|
28.25 0.2663 0.5962 0.0406 0.0182 0.525 4.730 4.158 391.751 0.534 18.497 4.815 0.45 168690. 0.3601
|
|
30.13 0.2841 0.6128 0.0380 0.0176 0.509 4.587 3.886 379.886 0.518 17.283 4.639 0.45 168855. 0.3354
|
|
32.01 0.3018 0.6259 0.0352 0.0170 0.492 4.428 3.606 366.721 0.500 16.040 4.460 0.45 169027. 0.3106
|
|
33.89 0.3196 0.6353 0.0324 0.0163 0.472 4.253 3.320 352.244 0.481 14.770 4.276 0.45 169205. 0.2857
|
|
35.78 0.3373 0.6406 0.0296 0.0156 0.451 4.062 3.029 336.448 0.459 13.475 4.084 0.45 169391. 0.2607
|
|
37.66 0.3551 0.6411 0.0267 0.0148 0.428 3.856 2.734 319.330 0.436 12.159 3.883 0.45 169584. 0.2354
|
|
39.54 0.3728 0.6360 0.0238 0.0139 0.404 3.633 2.434 300.897 0.410 10.825 3.668 0.45 169784. 0.2099
|
|
41.43 0.3906 0.6241 0.0208 0.0130 0.377 3.395 2.130 281.162 0.384 9.476 3.437 0.45 169991. 0.1839
|
|
43.31 0.4083 0.6039 0.0178 0.0121 0.349 3.141 1.824 260.153 0.355 8.115 3.181 0.45 170206. 0.1576
|
|
45.19 0.4261 0.5730 0.0148 0.0110 0.319 2.873 1.517 237.909 0.325 6.748 2.892 0.45 170428. 0.1306
|
|
47.08 0.4439 0.5277 0.0118 0.0099 0.288 2.590 1.209 214.488 0.293 5.378 2.557 0.45 170658. 0.1031
|
|
48.96 0.4616 0.4623 0.0088 0.0088 0.255 2.294 0.902 189.968 0.259 4.013 2.154 0.45 170896. 0.0750
|
|
50.84 0.4794 0.3672 0.0058 0.0076 0.221 1.986 0.597 164.446 0.224 2.657 1.648 0.45 171140. 0.0467
|
|
52.72 0.4971 0.2249 0.0029 0.0064 0.185 1.667 0.296 138.025 0.188 1.317 0.973 0.45 171392. 0.0194
|
|
54.61 0.5149 -0.0046 0.0000 0.0051 0.148 1.333 -0.005 110.400 0.151 -0.021 -0.019 0.45 171632. 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 0.0714 0.0204 0.880 6.933 9.543 656.172 0.783 42.448 6.597 0.51 190806. 0.7473
|
|
2.15 0.0178 0.0607 0.0700 0.0205 0.885 6.969 9.351 659.604 0.787 41.593 6.430 0.51 190894. 0.7211
|
|
4.31 0.0355 0.1183 0.0684 0.0206 0.888 6.997 9.148 662.294 0.791 40.690 6.265 0.51 190988. 0.6949
|
|
6.46 0.0533 0.1728 0.0668 0.0206 0.891 7.017 8.934 664.135 0.793 39.740 6.102 0.51 191087. 0.6689
|
|
8.61 0.0711 0.2243 0.0652 0.0206 0.892 7.026 8.710 665.025 0.794 38.742 5.940 0.51 191193. 0.6429
|
|
10.77 0.0888 0.2729 0.0634 0.0206 0.892 7.024 8.474 664.863 0.794 37.694 5.781 0.51 191304. 0.6172
|
|
12.92 0.1066 0.3186 0.0616 0.0206 0.890 7.011 8.227 663.544 0.792 36.595 5.624 0.51 191422. 0.5916
|
|
15.07 0.1244 0.3614 0.0596 0.0205 0.886 6.983 7.969 660.962 0.789 35.445 5.468 0.51 191546. 0.5661
|
|
17.23 0.1421 0.4014 0.0576 0.0204 0.881 6.942 7.699 657.016 0.784 34.244 5.315 0.51 191676. 0.5408
|
|
19.38 0.1599 0.4387 0.0555 0.0202 0.874 6.884 7.417 651.604 0.778 32.990 5.163 0.51 191814. 0.5156
|
|
21.53 0.1777 0.4732 0.0533 0.0200 0.864 6.811 7.123 644.626 0.769 31.683 5.012 0.51 191958. 0.4905
|
|
23.69 0.1954 0.5049 0.0510 0.0197 0.853 6.719 6.818 635.980 0.759 30.325 4.862 0.51 192109. 0.4656
|
|
25.84 0.2132 0.5340 0.0486 0.0194 0.839 6.609 6.500 625.555 0.747 28.913 4.713 0.51 192268. 0.4407
|
|
28.00 0.2310 0.5602 0.0462 0.0190 0.822 6.479 6.171 613.243 0.732 27.448 4.564 0.51 192434. 0.4158
|
|
30.15 0.2487 0.5835 0.0436 0.0186 0.803 6.329 5.830 599.002 0.715 25.934 4.415 0.51 192607. 0.3909
|
|
32.30 0.2665 0.6039 0.0410 0.0181 0.782 6.158 5.480 582.816 0.696 24.373 4.264 0.51 192788. 0.3661
|
|
34.46 0.2843 0.6211 0.0383 0.0175 0.757 5.966 5.119 564.669 0.674 22.770 4.112 0.51 192977. 0.3412
|
|
36.61 0.3020 0.6350 0.0355 0.0169 0.730 5.753 4.750 544.542 0.650 21.129 3.957 0.51 193174. 0.3162
|
|
38.76 0.3198 0.6452 0.0327 0.0162 0.701 5.520 4.373 522.420 0.624 19.451 3.797 0.51 193379. 0.2912
|
|
40.92 0.3376 0.6513 0.0298 0.0155 0.668 5.265 3.989 498.291 0.595 17.742 3.631 0.51 193591. 0.2659
|
|
43.07 0.3553 0.6526 0.0269 0.0147 0.633 4.988 3.598 472.152 0.564 16.004 3.456 0.51 193812. 0.2404
|
|
45.22 0.3731 0.6485 0.0240 0.0138 0.595 4.691 3.202 444.011 0.530 14.242 3.271 0.51 194041. 0.2146
|
|
47.38 0.3909 0.6376 0.0210 0.0128 0.555 4.373 2.801 413.892 0.494 12.460 3.070 0.51 194279. 0.1884
|
|
49.53 0.4086 0.6184 0.0179 0.0119 0.512 4.034 2.397 381.835 0.456 10.664 2.848 0.51 194525. 0.1617
|
|
51.68 0.4264 0.5883 0.0149 0.0108 0.467 3.676 1.991 347.903 0.415 8.858 2.596 0.51 194779. 0.1344
|
|
53.84 0.4442 0.5435 0.0119 0.0097 0.419 3.298 1.585 312.184 0.373 7.049 2.303 0.51 195042. 0.1063
|
|
55.99 0.4619 0.4779 0.0088 0.0085 0.369 2.903 1.179 274.798 0.328 5.246 1.947 0.51 195314. 0.0775
|
|
58.14 0.4797 0.3808 0.0058 0.0073 0.316 2.492 0.777 235.894 0.282 3.456 1.494 0.51 195594. 0.0483
|
|
60.30 0.4975 0.2325 0.0028 0.0061 0.262 2.067 0.379 195.630 0.234 1.688 0.880 0.51 195882. 0.0199
|
|
62.45 0.5152 -0.0158 -0.0001 0.0048 0.206 1.620 -0.019 153.334 0.183 -0.087 -0.058 0.51 196150. 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 0.0722 0.0205 1.260 8.823 12.211 939.445 0.997 54.317 5.896 0.57 214645. 0.7556
|
|
2.45 0.0180 0.0618 0.0707 0.0206 1.266 8.869 11.963 944.350 1.002 53.211 5.746 0.57 214746. 0.7288
|
|
4.90 0.0360 0.1203 0.0692 0.0207 1.271 8.904 11.700 948.140 1.006 52.042 5.597 0.57 214853. 0.7021
|
|
7.35 0.0539 0.1757 0.0675 0.0207 1.275 8.928 11.424 950.656 1.009 50.812 5.450 0.57 214967. 0.6756
|
|
9.81 0.0719 0.2281 0.0658 0.0207 1.276 8.938 11.133 951.750 1.010 49.518 5.305 0.57 215088. 0.6492
|
|
12.26 0.0899 0.2774 0.0640 0.0207 1.276 8.934 10.827 951.262 1.009 48.158 5.162 0.57 215216. 0.6229
|
|
14.71 0.1079 0.3238 0.0621 0.0207 1.273 8.913 10.506 949.039 1.007 46.732 5.021 0.57 215351. 0.5969
|
|
17.16 0.1259 0.3673 0.0601 0.0206 1.267 8.874 10.170 944.924 1.003 45.238 4.882 0.57 215493. 0.5710
|
|
19.61 0.1438 0.4079 0.0580 0.0205 1.259 8.816 9.819 938.766 0.996 43.676 4.744 0.57 215643. 0.5452
|
|
22.06 0.1618 0.4457 0.0559 0.0203 1.248 8.738 9.453 930.412 0.987 42.046 4.608 0.57 215801. 0.5196
|
|
24.52 0.1798 0.4808 0.0536 0.0201 1.233 8.637 9.071 919.714 0.976 40.346 4.473 0.57 215967. 0.4941
|
|
26.97 0.1978 0.5130 0.0513 0.0198 1.216 8.513 8.673 906.518 0.962 38.578 4.340 0.57 216141. 0.4687
|
|
29.42 0.2157 0.5425 0.0488 0.0194 1.194 8.365 8.260 890.658 0.945 36.740 4.206 0.57 216323. 0.4433
|
|
31.87 0.2337 0.5691 0.0463 0.0190 1.169 8.189 7.831 871.983 0.925 34.832 4.073 0.57 216514. 0.4180
|
|
34.32 0.2517 0.5929 0.0437 0.0185 1.140 7.987 7.388 850.437 0.902 32.860 3.940 0.57 216713. 0.3927
|
|
36.77 0.2697 0.6136 0.0410 0.0180 1.108 7.757 6.931 825.998 0.876 30.828 3.806 0.57 216921. 0.3674
|
|
39.23 0.2877 0.6311 0.0382 0.0174 1.071 7.500 6.462 798.641 0.847 28.741 3.670 0.57 217138. 0.3421
|
|
41.68 0.3056 0.6451 0.0354 0.0168 1.030 7.216 5.981 768.342 0.815 26.604 3.531 0.57 217365. 0.3167
|
|
44.13 0.3236 0.6554 0.0325 0.0160 0.986 6.903 5.490 735.076 0.780 24.420 3.388 0.57 217600. 0.2911
|
|
46.58 0.3416 0.6614 0.0295 0.0152 0.937 6.563 4.990 698.828 0.741 22.196 3.239 0.57 217844. 0.2653
|
|
49.03 0.3596 0.6625 0.0265 0.0144 0.885 6.195 4.482 659.599 0.700 19.935 3.082 0.57 218098. 0.2393
|
|
51.48 0.3776 0.6577 0.0234 0.0135 0.828 5.798 3.967 617.407 0.655 17.644 2.914 0.58 218362. 0.2128
|
|
53.94 0.3955 0.6458 0.0204 0.0125 0.767 5.375 3.446 572.292 0.607 15.328 2.731 0.58 218635. 0.1859
|
|
56.39 0.4135 0.6247 0.0173 0.0114 0.703 4.924 2.921 524.324 0.556 12.994 2.527 0.58 218918. 0.1584
|
|
58.84 0.4315 0.5915 0.0142 0.0103 0.635 4.448 2.394 473.608 0.503 10.650 2.293 0.58 219210. 0.1301
|
|
61.29 0.4495 0.5415 0.0110 0.0092 0.564 3.947 1.867 420.290 0.446 8.306 2.015 0.58 219513. 0.1010
|
|
63.74 0.4674 0.4668 0.0079 0.0079 0.489 3.424 1.343 364.565 0.387 5.972 1.670 0.58 219825. 0.0710
|
|
66.19 0.4854 0.3530 0.0049 0.0067 0.411 2.880 0.822 306.671 0.325 3.658 1.216 0.58 220147. 0.0405
|
|
68.65 0.5034 0.1709 0.0018 0.0054 0.331 2.318 0.309 246.801 0.262 1.374 0.568 0.58 220476. 0.0116
|
|
71.10 0.5214
|
|
|
|
|
|
|
|
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 0.0731 0.0207 1.745 11.000 15.272 1301.440 1.243 67.929 5.322 0.63 238478. 0.7628
|
|
2.69 0.0177 0.0611 0.0717 0.0208 1.754 11.056 14.966 1308.006 1.249 66.568 5.190 0.63 238589. 0.7362
|
|
5.37 0.0355 0.1192 0.0701 0.0209 1.761 11.098 14.643 1313.040 1.254 65.130 5.058 0.63 238708. 0.7098
|
|
8.06 0.0532 0.1742 0.0685 0.0209 1.765 11.126 14.302 1316.329 1.257 63.617 4.928 0.63 238833. 0.6835
|
|
10.75 0.0709 0.2262 0.0668 0.0209 1.767 11.137 13.945 1317.671 1.258 62.026 4.800 0.63 238966. 0.6573
|
|
13.44 0.0887 0.2753 0.0650 0.0209 1.766 11.130 13.569 1316.858 1.258 60.355 4.674 0.63 239107. 0.6314
|
|
16.12 0.1064 0.3215 0.0631 0.0209 1.762 11.104 13.175 1313.681 1.254 58.603 4.549 0.64 239255. 0.6055
|
|
18.81 0.1242 0.3650 0.0611 0.0208 1.754 11.055 12.763 1307.934 1.249 56.768 4.426 0.64 239411. 0.5798
|
|
21.50 0.1419 0.4057 0.0590 0.0207 1.743 10.983 12.331 1299.412 1.241 54.850 4.304 0.64 239576. 0.5543
|
|
24.19 0.1596 0.4436 0.0569 0.0205 1.727 10.886 11.881 1287.912 1.230 52.848 4.184 0.64 239748. 0.5289
|
|
26.87 0.1774 0.4789 0.0546 0.0202 1.707 10.762 11.412 1273.240 1.216 50.762 4.065 0.64 239930. 0.5037
|
|
29.56 0.1951 0.5116 0.0523 0.0199 1.683 10.609 10.924 1255.190 1.199 48.591 3.948 0.64 240120. 0.4785
|
|
32.25 0.2128 0.5415 0.0499 0.0196 1.654 10.426 10.417 1233.548 1.178 46.336 3.830 0.64 240319. 0.4534
|
|
34.93 0.2306 0.5687 0.0474 0.0192 1.620 10.211 9.891 1208.099 1.154 43.995 3.713 0.64 240527. 0.4283
|
|
37.62 0.2483 0.5932 0.0448 0.0187 1.581 9.963 9.347 1178.746 1.126 41.574 3.597 0.64 240745. 0.4032
|
|
40.31 0.2660 0.6148 0.0421 0.0182 1.536 9.682 8.786 1145.457 1.094 39.079 3.479 0.64 240972. 0.3782
|
|
43.00 0.2838 0.6333 0.0393 0.0176 1.486 9.367 8.209 1108.205 1.058 36.515 3.360 0.64 241208. 0.3530
|
|
45.68 0.3015 0.6486 0.0365 0.0170 1.431 9.018 7.619 1066.954 1.019 33.888 3.239 0.64 241455. 0.3278
|
|
48.37 0.3192 0.6604 0.0336 0.0162 1.370 8.635 7.015 1021.673 0.976 31.204 3.114 0.64 241711. 0.3025
|
|
51.06 0.3370 0.6683 0.0306 0.0155 1.304 8.218 6.400 972.341 0.929 28.468 2.986 0.64 241976. 0.2770
|
|
53.75 0.3547 0.6716 0.0276 0.0146 1.232 7.767 5.775 918.954 0.878 25.686 2.850 0.64 242253. 0.2512
|
|
56.43 0.3725 0.6695 0.0246 0.0137 1.155 7.282 5.140 861.528 0.823 22.864 2.706 0.64 242539. 0.2250
|
|
59.12 0.3902 0.6609 0.0215 0.0127 1.073 6.763 4.499 800.110 0.764 20.010 2.550 0.64 242835. 0.1984
|
|
61.81 0.4079 0.6442 0.0184 0.0117 0.985 6.211 3.851 734.783 0.702 17.131 2.377 0.64 243142. 0.1711
|
|
64.49 0.4257 0.6166 0.0153 0.0106 0.893 5.626 3.201 665.673 0.636 14.237 2.181 0.64 243460. 0.1431
|
|
67.18 0.4434 0.5742 0.0122 0.0094 0.795 5.012 2.549 592.959 0.566 11.338 1.950 0.64 243788. 0.1142
|
|
69.87 0.4611 0.5104 0.0091 0.0082 0.693 4.369 1.899 516.883 0.494 8.446 1.666 0.64 244127. 0.0842
|
|
72.56 0.4789 0.4131 0.0060 0.0070 0.587 3.700 1.253 437.751 0.418 5.575 1.299 0.64 244476. 0.0533
|
|
75.24 0.4966 0.2587 0.0029 0.0057 0.477 3.008 0.615 355.887 0.340 2.737 0.784 0.64 244835. 0.0226
|
|
77.93 0.5143 -0.0146 -0.0001 0.0043 0.362 2.281 -0.025 269.840 0.258 -0.113 -0.043 0.64 245166. 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 0.0742 0.0210 2.357 13.505 18.761 1757.572 1.526 83.450 4.842 0.70 262304. 0.7691
|
|
2.97 0.0178 0.0614 0.0728 0.0211 2.368 13.571 18.385 1766.170 1.533 81.776 4.721 0.70 262428. 0.7424
|
|
5.93 0.0356 0.1197 0.0712 0.0212 2.377 13.621 17.987 1772.635 1.539 80.008 4.602 0.70 262560. 0.7158
|
|
8.90 0.0534 0.1750 0.0695 0.0212 2.383 13.652 17.568 1776.680 1.542 78.145 4.485 0.70 262700. 0.6894
|
|
11.87 0.0712 0.2273 0.0678 0.0212 2.384 13.662 17.128 1778.022 1.544 76.184 4.369 0.70 262848. 0.6631
|
|
14.83 0.0890 0.2767 0.0659 0.0212 2.382 13.649 16.665 1776.383 1.542 74.125 4.255 0.70 263004. 0.6370
|
|
17.80 0.1068 0.3233 0.0640 0.0212 2.376 13.612 16.179 1771.474 1.538 71.964 4.142 0.70 263169. 0.6111
|
|
20.77 0.1246 0.3671 0.0620 0.0211 2.364 13.547 15.670 1763.013 1.531 69.700 4.031 0.70 263343. 0.5852
|
|
23.74 0.1424 0.4081 0.0599 0.0209 2.348 13.452 15.138 1750.722 1.520 67.333 3.922 0.70 263526. 0.5596
|
|
26.70 0.1602 0.4464 0.0577 0.0207 2.326 13.326 14.582 1734.322 1.506 64.860 3.814 0.70 263718. 0.5340
|
|
29.67 0.1780 0.4821 0.0554 0.0205 2.298 13.167 14.003 1713.553 1.488 62.284 3.706 0.70 263920. 0.5086
|
|
32.64 0.1958 0.5151 0.0530 0.0202 2.264 12.971 13.400 1688.138 1.466 59.602 3.600 0.70 264131. 0.4833
|
|
35.60 0.2136 0.5455 0.0505 0.0198 2.223 12.738 12.773 1657.787 1.439 56.815 3.495 0.70 264352. 0.4580
|
|
38.57 0.2314 0.5731 0.0480 0.0194 2.175 12.465 12.123 1622.205 1.408 53.922 3.390 0.70 264584. 0.4328
|
|
41.54 0.2492 0.5981 0.0453 0.0189 2.121 12.150 11.450 1581.267 1.373 50.929 3.284 0.70 264826. 0.4075
|
|
44.50 0.2670 0.6201 0.0426 0.0183 2.058 11.794 10.756 1534.934 1.333 47.843 3.178 0.70 265078. 0.3823
|
|
47.47 0.2848 0.6392 0.0397 0.0177 1.989 11.396 10.043 1483.166 1.288 44.673 3.071 0.70 265340. 0.3570
|
|
50.44 0.3026 0.6550 0.0369 0.0170 1.912 10.957 9.313 1425.920 1.238 41.425 2.962 0.70 265613. 0.3315
|
|
53.41 0.3204 0.6674 0.0339 0.0163 1.828 10.474 8.567 1363.158 1.183 38.105 2.850 0.70 265897. 0.3060
|
|
56.37 0.3382 0.6757 0.0309 0.0155 1.736 9.949 7.806 1294.853 1.124 34.721 2.734 0.70 266192. 0.2802
|
|
59.34 0.3560 0.6796 0.0278 0.0146 1.637 9.382 7.032 1221.005 1.060 31.280 2.612 0.70 266498. 0.2540
|
|
62.31 0.3738 0.6780 0.0247 0.0136 1.531 8.772 6.248 1141.646 0.991 27.789 2.482 0.70 266816. 0.2275
|
|
65.27 0.3916 0.6698 0.0216 0.0126 1.417 8.121 5.454 1056.860 0.917 24.259 2.341 0.70 267145. 0.2005
|
|
68.24 0.4094 0.6531 0.0184 0.0115 1.296 7.429 4.653 966.780 0.839 20.698 2.183 0.70 267485. 0.1727
|
|
71.21 0.4272 0.6252 0.0152 0.0104 1.169 6.697 3.849 871.606 0.757 17.120 2.003 0.70 267837. 0.1441
|
|
74.17 0.4450 0.5817 0.0120 0.0092 1.035 5.929 3.043 771.622 0.670 13.536 1.789 0.71 268201. 0.1144
|
|
77.14 0.4628 0.5149 0.0089 0.0080 0.895 5.127 2.240 667.205 0.579 9.962 1.522 0.71 268576. 0.0836
|
|
80.11 0.4806 0.4111 0.0057 0.0067 0.749 4.294 1.442 558.835 0.485 6.415 1.171 0.71 268963. 0.0516
|
|
83.07 0.4984 0.2418 0.0026 0.0053 0.599 3.435 0.654 446.997 0.388 2.910 0.664 0.71 269359. 0.0197
|
|
86.04 0.5163
|
|
|
|
|
|
|
|
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 0.0756 0.0214 3.126 16.419 22.731 2331.113 1.855 101.107 4.423 0.76 286120. 0.7733
|
|
3.24 0.0178 0.0612 0.0741 0.0215 3.139 16.489 22.277 2341.040 1.863 99.087 4.316 0.76 286258. 0.7471
|
|
6.47 0.0356 0.1195 0.0725 0.0216 3.149 16.540 21.797 2348.276 1.869 96.951 4.210 0.76 286403. 0.7208
|
|
9.71 0.0534 0.1748 0.0708 0.0216 3.155 16.569 21.290 2352.412 1.872 94.700 4.105 0.76 286557. 0.6946
|
|
12.95 0.0712 0.2271 0.0690 0.0216 3.156 16.574 20.758 2353.059 1.873 92.330 4.001 0.76 286720. 0.6685
|
|
16.19 0.0890 0.2766 0.0672 0.0216 3.151 16.551 20.197 2349.818 1.870 89.838 3.899 0.76 286892. 0.6425
|
|
19.42 0.1068 0.3233 0.0652 0.0215 3.141 16.498 19.609 2342.279 1.864 87.223 3.797 0.76 287074. 0.6167
|
|
22.66 0.1246 0.3673 0.0632 0.0214 3.125 16.412 18.993 2330.039 1.854 84.482 3.697 0.76 287265. 0.5909
|
|
25.90 0.1424 0.4085 0.0610 0.0213 3.101 16.290 18.349 2312.702 1.840 81.614 3.599 0.76 287466. 0.5653
|
|
29.13 0.1602 0.4471 0.0588 0.0211 3.071 16.129 17.675 2289.889 1.822 78.619 3.501 0.76 287677. 0.5398
|
|
32.37 0.1780 0.4831 0.0564 0.0208 3.032 15.927 16.973 2261.235 1.799 75.496 3.405 0.76 287898. 0.5144
|
|
35.61 0.1958 0.5165 0.0540 0.0205 2.986 15.682 16.242 2226.401 1.772 72.245 3.309 0.76 288131. 0.4890
|
|
38.84 0.2136 0.5473 0.0515 0.0201 2.930 15.390 15.482 2185.011 1.739 68.865 3.214 0.76 288373. 0.4638
|
|
42.08 0.2314 0.5754 0.0489 0.0197 2.865 15.050 14.693 2136.689 1.700 65.355 3.119 0.76 288627. 0.4385
|
|
45.32 0.2493 0.6008 0.0461 0.0191 2.791 14.660 13.877 2081.280 1.656 61.723 3.024 0.76 288892. 0.4131
|
|
48.56 0.2671 0.6234 0.0433 0.0186 2.707 14.219 13.035 2018.757 1.606 57.979 2.929 0.76 289168. 0.3878
|
|
51.79 0.2849 0.6430 0.0405 0.0179 2.614 13.729 12.170 1949.098 1.551 54.131 2.832 0.76 289456. 0.3623
|
|
55.03 0.3027 0.6594 0.0375 0.0172 2.511 13.188 11.283 1872.287 1.490 50.187 2.733 0.77 289755. 0.3367
|
|
58.27 0.3205 0.6723 0.0345 0.0164 2.398 12.596 10.377 1788.312 1.423 46.155 2.632 0.77 290066. 0.3109
|
|
61.50 0.3383 0.6811 0.0314 0.0156 2.276 11.954 9.452 1697.202 1.351 42.044 2.526 0.77 290388. 0.2848
|
|
64.74 0.3561 0.6853 0.0283 0.0147 2.144 11.263 8.512 1599.024 1.272 37.863 2.415 0.77 290723. 0.2584
|
|
67.98 0.3739 0.6839 0.0251 0.0137 2.003 10.522 7.559 1493.906 1.189 33.621 2.295 0.77 291070. 0.2314
|
|
71.21 0.3917 0.6756 0.0219 0.0127 1.853 9.735 6.594 1382.048 1.100 29.330 2.164 0.77 291430. 0.2038
|
|
74.45 0.4095 0.6584 0.0187 0.0116 1.695 8.901 5.621 1263.738 1.006 25.000 2.017 0.77 291801. 0.1754
|
|
77.69 0.4273 0.6294 0.0154 0.0105 1.528 8.025 4.642 1139.370 0.907 20.648 1.848 0.77 292186. 0.1460
|
|
80.93 0.4451 0.5837 0.0122 0.0093 1.354 7.110 3.662 1009.459 0.803 16.288 1.645 0.77 292583. 0.1155
|
|
84.16 0.4629 0.5135 0.0089 0.0080 1.173 6.161 2.684 874.655 0.696 11.938 1.392 0.77 292993. 0.0836
|
|
87.40 0.4807 0.4047 0.0057 0.0068 0.987 5.182 1.713 735.741 0.585 7.620 1.056 0.77 293415. 0.0507
|
|
90.64 0.4985 0.2289 0.0025 0.0055 0.796 4.180 0.754 593.482 0.472 3.353 0.576 0.77 293848. 0.0183
|
|
93.87 0.5163
|
|
|
|
|
|
|
|
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 0.0772 0.0225 4.180 20.265 27.250 3116.789 2.289 121.208 3.966 0.83 309925. 0.7592
|
|
3.50 0.0178 0.0596 0.0757 0.0226 4.183 20.282 26.711 3119.488 2.291 118.809 3.884 0.83 310075. 0.7361
|
|
7.00 0.0355 0.1166 0.0741 0.0226 4.183 20.280 26.140 3119.101 2.291 116.271 3.801 0.83 310234. 0.7127
|
|
10.49 0.0533 0.1711 0.0724 0.0225 4.178 20.254 25.538 3115.199 2.288 113.593 3.718 0.83 310402. 0.6891
|
|
13.99 0.0710 0.2230 0.0706 0.0225 4.167 20.203 24.904 3107.328 2.283 110.772 3.635 0.83 310580. 0.6653
|
|
17.49 0.0888 0.2723 0.0687 0.0224 4.151 20.123 24.237 3095.033 2.273 107.805 3.552 0.83 310768. 0.6413
|
|
20.99 0.1065 0.3191 0.0667 0.0223 4.127 20.011 23.536 3077.824 2.261 104.688 3.468 0.83 310966. 0.6171
|
|
24.48 0.1243 0.3633 0.0646 0.0221 4.097 19.864 22.801 3055.212 2.244 101.421 3.385 0.83 311174. 0.5928
|
|
27.98 0.1421 0.4050 0.0624 0.0219 4.059 19.679 22.032 3026.707 2.223 98.000 3.302 0.83 311393. 0.5683
|
|
31.48 0.1598 0.4442 0.0601 0.0216 4.012 19.452 21.229 2991.787 2.198 94.426 3.218 0.83 311623. 0.5438
|
|
34.98 0.1776 0.4807 0.0578 0.0213 3.957 19.183 20.391 2950.482 2.167 90.697 3.135 0.83 311864. 0.5191
|
|
38.48 0.1953 0.5145 0.0553 0.0210 3.892 18.869 19.518 2902.079 2.132 86.814 3.050 0.83 312116. 0.4942
|
|
41.97 0.2131 0.5457 0.0527 0.0206 3.817 18.505 18.610 2846.202 2.091 82.776 2.966 0.83 312380. 0.4692
|
|
45.47 0.2309 0.5741 0.0501 0.0201 3.731 18.089 17.667 2782.217 2.044 78.581 2.880 0.83 312656. 0.4439
|
|
48.97 0.2486 0.5997 0.0473 0.0196 3.634 17.620 16.690 2709.983 1.991 74.238 2.793 0.83 312943. 0.4185
|
|
52.47 0.2664 0.6223 0.0444 0.0190 3.526 17.096 15.683 2629.407 1.931 69.759 2.705 0.83 313242. 0.3929
|
|
55.96 0.2841 0.6417 0.0415 0.0184 3.407 16.516 14.648 2540.312 1.866 65.153 2.615 0.83 313554. 0.3671
|
|
59.46 0.3019 0.6576 0.0385 0.0177 3.276 15.883 13.586 2442.844 1.794 60.431 2.523 0.83 313878. 0.3410
|
|
62.96 0.3196 0.6697 0.0354 0.0169 3.134 15.195 12.501 2337.016 1.717 55.603 2.426 0.83 314215. 0.3146
|
|
66.46 0.3374 0.6773 0.0323 0.0161 2.981 14.454 11.394 2223.041 1.633 50.678 2.325 0.83 314564. 0.2878
|
|
69.96 0.3552 0.6797 0.0291 0.0152 2.818 13.661 10.267 2101.208 1.543 45.667 2.216 0.83 314926. 0.2604
|
|
73.45 0.3729 0.6758 0.0258 0.0143 2.644 12.821 9.124 1971.944 1.449 40.581 2.099 0.83 315301. 0.2325
|
|
76.95 0.3907 0.6640 0.0226 0.0133 2.462 11.935 7.966 1835.714 1.348 35.433 1.968 0.83 315690. 0.2037
|
|
80.45 0.4084 0.6423 0.0193 0.0122 2.270 11.008 6.798 1693.095 1.244 30.238 1.821 0.83 316092. 0.1741
|
|
83.95 0.4262 0.6076 0.0159 0.0112 2.072 10.044 5.623 1544.826 1.135 25.011 1.651 0.83 316507. 0.1436
|
|
87.44 0.4439 0.5553 0.0126 0.0101 1.866 9.049 4.445 1391.818 1.022 19.773 1.449 0.83 316935. 0.1120
|
|
90.94 0.4617 0.4787 0.0093 0.0089 1.656 8.030 3.270 1235.098 0.907 14.544 1.201 0.83 317378. 0.0796
|
|
94.44 0.4795 0.3669 0.0060 0.0078 1.443 6.995 2.102 1075.827 0.790 9.350 0.886 0.83 317834. 0.0471
|
|
97.94 0.4972 0.2016 0.0027 0.0066 1.227 5.950 0.947 915.070 0.672 4.213 0.469 0.84 318301. 0.0168
|
|
101.44 0.5150
|
|
|
|
|
|
|
|
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 0.0790 0.0253 5.865 26.405 32.334 4373.674 2.983 143.822 3.353 0.89 333716. 0.6992
|
|
3.76 0.0177 0.0544 0.0775 0.0252 5.834 26.266 31.708 4350.529 2.967 141.036 3.306 0.89 333879. 0.6826
|
|
7.51 0.0354 0.1073 0.0758 0.0250 5.798 26.102 31.044 4323.437 2.949 138.083 3.257 0.89 334052. 0.6655
|
|
11.27 0.0531 0.1584 0.0741 0.0249 5.756 25.912 30.342 4292.041 2.928 134.963 3.206 0.89 334235. 0.6477
|
|
15.03 0.0708 0.2078 0.0723 0.0246 5.707 25.694 29.602 4255.910 2.903 131.670 3.155 0.89 334428. 0.6295
|
|
18.78 0.0885 0.2554 0.0704 0.0244 5.652 25.445 28.822 4214.611 2.875 128.201 3.102 0.89 334631. 0.6107
|
|
22.54 0.1063 0.3011 0.0684 0.0241 5.589 25.162 28.002 4167.704 2.843 124.552 3.047 0.89 334846. 0.5914
|
|
26.30 0.1240 0.3449 0.0663 0.0238 5.518 24.842 27.141 4114.730 2.807 120.721 2.992 0.89 335072. 0.5716
|
|
30.05 0.1417 0.3866 0.0641 0.0235 5.438 24.483 26.238 4055.243 2.766 116.707 2.935 0.89 335309. 0.5513
|
|
33.81 0.1594 0.4263 0.0618 0.0231 5.349 24.081 25.294 3988.768 2.721 112.508 2.876 0.89 335558. 0.5305
|
|
37.57 0.1771 0.4638 0.0594 0.0227 5.250 23.635 24.309 3914.819 2.670 108.125 2.816 0.89 335819. 0.5092
|
|
41.32 0.1948 0.4989 0.0569 0.0222 5.142 23.150 23.282 3834.426 2.615 103.557 2.754 0.89 336091. 0.4873
|
|
45.08 0.2125 0.5312 0.0543 0.0217 5.027 22.631 22.213 3748.488 2.557 98.803 2.688 0.89 336377. 0.4646
|
|
48.83 0.2302 0.5606 0.0516 0.0212 4.901 22.067 21.102 3655.044 2.493 93.863 2.619 0.89 336674. 0.4412
|
|
52.59 0.2479 0.5869 0.0487 0.0206 4.767 21.463 19.952 3555.067 2.425 88.745 2.546 0.89 336984. 0.4170
|
|
56.35 0.2656 0.6097 0.0458 0.0200 4.624 20.818 18.764 3448.175 2.352 83.461 2.468 0.89 337307. 0.3921
|
|
60.10 0.2833 0.6281 0.0429 0.0193 4.476 20.150 17.541 3337.594 2.277 78.024 2.384 0.89 337643. 0.3661
|
|
63.86 0.3011 0.6414 0.0398 0.0187 4.324 19.468 16.287 3224.680 2.200 72.445 2.291 0.89 337992. 0.3391
|
|
67.62 0.3188 0.6499 0.0367 0.0180 4.163 18.741 15.004 3104.188 2.117 66.738 2.192 0.89 338355. 0.3114
|
|
71.37 0.3365 0.6531 0.0335 0.0172 3.991 17.967 13.695 2976.012 2.030 60.916 2.087 0.89 338731. 0.2833
|
|
75.13 0.3542 0.6502 0.0302 0.0165 3.810 17.151 12.363 2840.794 1.938 54.991 1.974 0.89 339120. 0.2545
|
|
78.89 0.3719 0.6399 0.0269 0.0156 3.620 16.297 11.011 2699.322 1.841 48.977 1.850 0.89 339524. 0.2252
|
|
82.64 0.3896 0.6208 0.0236 0.0148 3.423 15.411 9.643 2552.580 1.741 42.891 1.713 0.90 339941. 0.1951
|
|
86.40 0.4073 0.5910 0.0202 0.0139 3.221 14.500 8.262 2401.716 1.638 36.748 1.560 0.90 340372. 0.1645
|
|
90.16 0.4250 0.5482 0.0168 0.0130 3.014 13.570 6.873 2247.631 1.533 30.571 1.387 0.90 340818. 0.1333
|
|
93.91 0.4427 0.4894 0.0134 0.0121 2.805 12.627 5.481 2091.567 1.427 24.381 1.189 0.90 341278. 0.1021
|
|
97.67 0.4604 0.4108 0.0100 0.0112 2.595 11.681 4.093 1934.874 1.320 18.206 0.959 0.90 341753. 0.0712
|
|
101.43 0.4782 0.3078 0.0066 0.0103 2.386 10.740 2.715 1778.980 1.213 12.075 0.692 0.90 342242. 0.0418
|
|
105.18 0.4959 0.1741 0.0033 0.0094 2.179 9.810 1.353 1624.814 1.108 6.016 0.378 0.90 342744. 0.0161
|
|
108.94 0.5136 -0.0016 0.0000 0.0085 1.963 8.836 -0.011 1463.606 0.998 -0.049 -0.003 0.90 343233. 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 0.0803 0.0303 8.637 36.292 37.715 6440.733 4.100 167.756 2.656 0.95 357513. 0.5982
|
|
4.22 0.0185 0.0486 0.0787 0.0300 8.553 35.939 36.993 6378.019 4.060 164.545 2.631 0.95 357695. 0.5868
|
|
8.43 0.0371 0.0963 0.0771 0.0297 8.457 35.537 36.220 6306.613 4.015 161.107 2.605 0.95 357890. 0.5749
|
|
12.65 0.0556 0.1430 0.0753 0.0293 8.350 35.084 35.396 6226.326 3.964 157.440 2.578 0.95 358096. 0.5626
|
|
16.86 0.0742 0.1886 0.0735 0.0289 8.230 34.580 34.518 6136.920 3.907 153.538 2.551 0.95 358316. 0.5497
|
|
21.08 0.0927 0.2331 0.0715 0.0284 8.097 34.024 33.587 6038.218 3.844 149.396 2.523 0.95 358548. 0.5362
|
|
25.29 0.1113 0.2765 0.0694 0.0279 7.952 33.415 32.601 5930.105 3.775 145.010 2.494 0.95 358793. 0.5221
|
|
29.51 0.1298 0.3186 0.0672 0.0274 7.795 32.752 31.560 5812.445 3.700 140.377 2.463 0.95 359052. 0.5074
|
|
33.72 0.1484 0.3593 0.0648 0.0268 7.624 32.035 30.462 5685.090 3.619 135.496 2.430 0.95 359324. 0.4919
|
|
37.94 0.1669 0.3986 0.0624 0.0261 7.440 31.261 29.309 5547.906 3.532 130.368 2.396 0.95 359610. 0.4757
|
|
42.16 0.1855 0.4362 0.0598 0.0254 7.242 30.432 28.101 5400.677 3.438 124.993 2.360 0.95 359911. 0.4588
|
|
46.37 0.2040 0.4720 0.0571 0.0247 7.031 29.544 26.838 5243.094 3.338 119.373 2.322 0.95 360226. 0.4411
|
|
50.59 0.2226 0.5051 0.0543 0.0239 6.815 28.635 25.518 5081.797 3.235 113.504 2.278 0.95 360555. 0.4219
|
|
54.80 0.2411 0.5353 0.0514 0.0231 6.591 27.696 24.143 4915.155 3.129 107.389 2.228 0.95 360899. 0.4015
|
|
59.02 0.2597 0.5617 0.0483 0.0223 6.364 26.743 22.717 4745.949 3.021 101.047 2.171 0.96 361259. 0.3795
|
|
63.23 0.2782 0.5842 0.0452 0.0215 6.132 25.764 21.245 4572.317 2.911 94.497 2.107 0.96 361633. 0.3562
|
|
67.45 0.2968 0.6007 0.0420 0.0207 5.907 24.819 19.729 4404.562 2.804 87.754 2.032 0.96 362023. 0.3309
|
|
71.67 0.3153 0.6055 0.0387 0.0201 5.734 24.094 18.170 4275.927 2.722 80.820 1.927 0.96 362428. 0.3013
|
|
75.88 0.3339 0.6029 0.0353 0.0195 5.563 23.375 16.576 4148.326 2.641 73.731 1.812 0.96 362849. 0.2706
|
|
80.10 0.3524 0.5928 0.0318 0.0189 5.387 22.637 14.953 4017.338 2.558 66.512 1.688 0.96 363285. 0.2394
|
|
84.31 0.3710 0.5745 0.0283 0.0183 5.207 21.879 13.306 3882.796 2.472 59.185 1.554 0.96 363738. 0.2079
|
|
88.53 0.3895 0.5470 0.0248 0.0176 5.024 21.109 11.640 3746.079 2.385 51.773 1.409 0.96 364207. 0.1763
|
|
92.74 0.4081 0.5091 0.0212 0.0170 4.839 20.333 9.961 3608.495 2.297 44.306 1.252 0.96 364692. 0.1449
|
|
96.96 0.4266 0.4597 0.0176 0.0163 4.655 19.561 8.277 3471.468 2.210 36.816 1.081 0.96 365194. 0.1141
|
|
101.17 0.4452 0.3977 0.0140 0.0157 4.474 18.801 6.596 3336.612 2.124 29.340 0.897 0.96 365713. 0.0845
|
|
105.39 0.4637 0.3223 0.0105 0.0151 4.297 18.056 4.928 3204.394 2.040 21.920 0.698 0.96 366249. 0.0568
|
|
109.61 0.4823 0.2326 0.0070 0.0145 4.124 17.330 3.283 3075.485 1.958 14.601 0.484 0.96 366803. 0.0322
|
|
113.82 0.5008 0.1279 0.0035 0.0139 3.955 16.617 1.666 2949.049 1.877 7.412 0.256 0.96 367376. 0.0121
|
|
118.04 0.5194 0.0034 0.0001 0.0132 3.761 15.802 0.040 2804.322 1.785 0.180 0.007 0.96 367976. 0.0000
|
|
122.25 0.5379
|
|
|
|
|
|
|