From 0d4f43d355de79178b1142e9735902cf641670b6 Mon Sep 17 00:00:00 2001 From: Dimitri Sokolyuk Date: Mon, 11 May 2009 00:27:49 +0000 Subject: Xfoil 6.97 --- runs/cp_060_050.387 | 57 +++++++++++++++++++++ runs/cp_100_040.387 | 58 +++++++++++++++++++++ runs/cp_250_040.203 | 48 ++++++++++++++++++ runs/cp_500_080.lnv | 44 ++++++++++++++++ runs/dae11.dat | 83 +++++++++++++++++++++++++++++++ runs/dae21.dat | 83 +++++++++++++++++++++++++++++++ runs/dae31.dat | 84 +++++++++++++++++++++++++++++++ runs/dae51.dat | 83 +++++++++++++++++++++++++++++++ runs/e387.dat | 62 +++++++++++++++++++++++ runs/e387_09.100 | 102 +++++++++++++++++++++++++++++++++++++ runs/e387_11.100 | 123 +++++++++++++++++++++++++++++++++++++++++++++ runs/la203.dat | 103 ++++++++++++++++++++++++++++++++++++++ runs/la203t.dat | 141 ++++++++++++++++++++++++++++++++++++++++++++++++++++ runs/lnv109a.dat | 102 +++++++++++++++++++++++++++++++++++++ runs/polref_100.387 | 82 ++++++++++++++++++++++++++++++ 15 files changed, 1255 insertions(+) create mode 100644 runs/cp_060_050.387 create mode 100644 runs/cp_100_040.387 create mode 100644 runs/cp_250_040.203 create mode 100644 runs/cp_500_080.lnv create mode 100644 runs/dae11.dat create mode 100644 runs/dae21.dat create mode 100644 runs/dae31.dat create mode 100644 runs/dae51.dat create mode 100644 runs/e387.dat create mode 100644 runs/e387_09.100 create mode 100644 runs/e387_11.100 create mode 100644 runs/la203.dat create mode 100644 runs/la203t.dat create mode 100644 runs/lnv109a.dat create mode 100644 runs/polref_100.387 (limited to 'runs') diff --git a/runs/cp_060_050.387 b/runs/cp_060_050.387 new file mode 100644 index 0000000..8c920e2 --- /dev/null +++ b/runs/cp_060_050.387 @@ -0,0 +1,57 @@ +0.950 -0.0370 | CL=0.838 (a=5 deg nominal) Re=60000 +0.900 -0.1214 +0.850 -0.2418 +0.800 -0.4137 +0.750 -0.5977 +0.700 -0.6307 +0.650 -0.6126 +0.600 -0.6075 +0.550 -0.5985 +0.500 -0.5990 +0.450 -0.6124 +0.400 -0.6330 +0.350 -0.6652 +0.300 -0.7310 +0.250 -0.8065 +0.200 -0.8648 +0.150 -0.9291 +0.100 -1.0042 +0.075 -1.0262 +0.060 -1.0360 +0.050 -1.0463 +0.040 -1.0469 +0.030 -1.0311 +0.025 -1.0353 +0.020 -1.0571 +0.015 -1.0064 +0.010 -0.9906 +0.005 -0.8359 +0.0 0.4274 +0.950 0.1178 +0.900 0.1461 +0.850 0.1603 +0.800 0.1754 +0.750 0.1786 +0.700 0.1837 +0.650 0.1912 +0.600 0.1977 +0.550 0.1983 +0.500 0.2044 +0.450 0.2144 +0.400 0.2156 +0.350 0.2243 +0.300 0.2354 +0.250 0.2380 +0.200 0.2570 +0.150 0.2817 +0.100 0.3200 +0.075 0.3595 +0.060 0.3932 +0.050 0.4291 +0.040 0.4701 +0.031 0.5370 +0.025 0.5845 +0.020 0.6551 +0.015 0.7133 +0.010 0.8403 +0.005 0.9710 diff --git a/runs/cp_100_040.387 b/runs/cp_100_040.387 new file mode 100644 index 0000000..ef89416 --- /dev/null +++ b/runs/cp_100_040.387 @@ -0,0 +1,58 @@ +# Langley Cp data +0.950 0.0451 | CL=0.778 (a=4 deg nominal) Re=100000 +0.900 -.0008 +0.850 -.0410 +0.800 -.1223 +0.750 -.3670 +0.700 -.6230 +0.650 -.6383 +0.600 -.6343 +0.550 -.6327 +0.500 -.6351 +0.450 -.6557 +0.400 -.6849 +0.350 -.7470 +0.300 -.8061 +0.250 -.8481 +0.200 -.8876 +0.150 -.9254 +0.100 -.9656 +0.075 -.9831 +0.060 -.9826 +0.050 -.9700 +0.040 -.9659 +0.030 -.9529 +0.025 -.9409 +0.020 -.9137 +0.015 -.8654 +0.010 -.8129 +0.005 -.6744 +0.0 0.6121 +0.950 0.1352 +0.900 0.1558 +0.850 0.1623 +0.800 0.1692 +0.750 0.1688 +0.700 0.1743 +0.650 0.1755 +0.600 0.1795 +0.550 0.1787 +0.500 0.1851 +0.450 0.1902 +0.400 0.1894 +0.350 0.1963 +0.300 0.1978 +0.250 0.1970 +0.200 0.2121 +0.150 0.2204 +0.100 0.2585 +0.075 0.2879 +0.060 0.3143 +0.050 0.3489 +0.040 0.3891 +0.031 0.4545 +0.025 0.4966 +0.020 0.5466 +0.015 0.6190 +0.010 0.7428 +0.005 0.9269 diff --git a/runs/cp_250_040.203 b/runs/cp_250_040.203 new file mode 100644 index 0000000..340915c --- /dev/null +++ b/runs/cp_250_040.203 @@ -0,0 +1,48 @@ +1.000 0.088 | CL=1.08 (a=4 deg nominal) Re=250000 +0.950 -.051 +0.900 -.102 +0.850 -.196 +0.800 -.293 +0.750 -.386 +0.700 -.458 +0.675 -.481 +0.650 -.719 +0.625 -1.098 +0.600 -1.098 +0.575 -1.098 +0.550 -1.098 +0.525 -1.098 +0.500 -1.123 +0.475 -1.146 +0.450 -1.195 +0.425 -1.244 +0.400 -1.291 +0.375 -1.344 +0.350 -1.344 +0.325 -1.363 +0.300 -1.388 +0.250 -1.388 +0.200 -1.363 +0.150 -1.342 +0.100 -1.246 +0.075 -1.195 +0.050 -1.144 +0.025 -1.007 +0.012 -.811 +0.000 0.760 +0.012 0.430 +0.025 0.140 +0.050 0.189 +0.075 0.189 +0.100 0.189 +0.150 0.189 +0.200 0.160 +0.300 0.163 +0.400 0.140 +0.500 0.139 +0.600 0.189 +0.700 0.212 +0.800 0.212 +0.850 0.237 +0.900 0.330 +0.950 0.430 diff --git a/runs/cp_500_080.lnv b/runs/cp_500_080.lnv new file mode 100644 index 0000000..ab4ed18 --- /dev/null +++ b/runs/cp_500_080.lnv @@ -0,0 +1,44 @@ +1.000 0.055 | CL=1.234 (a=8 deg nominal) Re=500000 +0.950 0.050 +0.900 0.020 +0.850 0.000 +0.800 -.045 +0.750 -.105 +0.700 -.150 +0.650 -.222 +0.600 -.309 +0.550 -.418 +0.500 -.567 +0.450 -.743 +0.425 -.860 +0.400 -1.216 +0.375 -1.775 +0.350 -1.784 +0.325 -1.784 +0.300 -1.870 +0.275 -1.944 +0.250 -2.022 +0.225 -2.072 +0.200 -2.111 +0.150 -2.126 +0.100 -2.063 +0.075 -2.005 +0.050 -1.946 +0.025 -1.805 +0.012 -1.171 +0.000 0.202 +0.012 0.750 +0.025 0.486 +0.050 0.414 +0.075 0.400 +0.100 0.408 +0.150 0.400 +0.200 0.395 +0.300 0.336 +0.400 0.371 +0.500 0.357 +0.600 0.332 +0.700 0.250 +0.800 0.211 +0.900 0.152 +0.950 0.077 diff --git a/runs/dae11.dat b/runs/dae11.dat new file mode 100644 index 0000000..f0e6bd3 --- /dev/null +++ b/runs/dae11.dat @@ -0,0 +1,83 @@ +DAE 11 +# Daedalus wing center panel airfoil. Design Re = 500K + 1.000000 0.000000 + 0.986485 0.002537 + 0.970011 0.005613 + 0.947881 0.010041 + 0.918618 0.016374 + 0.887980 0.023556 + 0.857968 0.031118 + 0.827970 0.039139 + 0.797803 0.047590 + 0.767378 0.056399 + 0.736634 0.065482 + 0.705687 0.074715 + 0.675260 0.083695 + 0.645478 0.092177 + 0.616310 0.099961 + 0.587628 0.106875 + 0.559192 0.112804 + 0.530735 0.117738 + 0.502104 0.121740 + 0.473284 0.124848 + 0.444338 0.127068 + 0.415323 0.128391 + 0.386255 0.128806 + 0.357167 0.128336 + 0.328135 0.126996 + 0.299232 0.124754 + 0.270512 0.121609 + 0.242030 0.117536 + 0.213885 0.112508 + 0.186216 0.106500 + 0.159197 0.099489 + 0.133039 0.091476 + 0.108024 0.082466 + 0.084520 0.072514 + 0.062995 0.061754 + 0.044085 0.050490 + 0.028485 0.039251 + 0.016619 0.028679 + 0.008417 0.019287 + 0.003417 0.011421 + 0.000883 0.005097 + 0.000128 0.000182 + 0.000626 -0.003555 + 0.002138 -0.006473 + 0.004541 -0.008835 + 0.008212 -0.010744 + 0.014240 -0.012418 + 0.024697 -0.013921 + 0.041573 -0.014931 + 0.065014 -0.015107 + 0.092723 -0.014502 + 0.122696 -0.013331 + 0.153786 -0.011784 + 0.185487 -0.010003 + 0.217549 -0.008087 + 0.249834 -0.006102 + 0.282263 -0.004093 + 0.314698 -0.002099 + 0.347047 -0.000149 + 0.379318 0.001724 + 0.411508 0.003509 + 0.443624 0.005174 + 0.475671 0.006709 + 0.507637 0.008092 + 0.539527 0.009282 + 0.571366 0.010264 + 0.603162 0.011026 + 0.634928 0.011552 + 0.666677 0.011849 + 0.698414 0.011916 + 0.730135 0.011759 + 0.761819 0.011381 + 0.793447 0.010763 + 0.825020 0.009891 + 0.856580 0.008751 + 0.888343 0.007325 + 0.920025 0.005610 + 0.948000 0.003865 + 0.969655 0.002348 + 0.986285 0.001076 + 1.000000 0.000000 diff --git a/runs/dae21.dat b/runs/dae21.dat new file mode 100644 index 0000000..ef05e48 --- /dev/null +++ b/runs/dae21.dat @@ -0,0 +1,83 @@ +DAE 21 +# Daedalus outer panel break airfoil. Design Re = 375K + 1.000000 0.000000 + 0.986712 0.002418 + 0.970362 0.005492 + 0.947691 0.010083 + 0.917703 0.016743 + 0.887293 0.024120 + 0.857161 0.031966 + 0.826867 0.040283 + 0.796262 0.048982 + 0.765287 0.057938 + 0.734180 0.066919 + 0.703358 0.075625 + 0.672878 0.083860 + 0.642725 0.091437 + 0.612839 0.098204 + 0.583189 0.104141 + 0.553743 0.109238 + 0.524452 0.113495 + 0.495245 0.116921 + 0.466044 0.119541 + 0.436797 0.121383 + 0.407512 0.122444 + 0.378226 0.122715 + 0.348985 0.122181 + 0.319838 0.120829 + 0.290842 0.118635 + 0.262053 0.115583 + 0.233558 0.111651 + 0.205468 0.106814 + 0.177922 0.101046 + 0.151092 0.094310 + 0.125176 0.086572 + 0.100450 0.077840 + 0.077317 0.068163 + 0.056331 0.057700 + 0.038181 0.046773 + 0.023556 0.035891 + 0.012848 0.025735 + 0.005879 0.016869 + 0.001956 0.009449 + 0.000266 0.003383 + 0.000061 -0.001451 + 0.000768 -0.005145 + 0.002174 -0.007971 + 0.004373 -0.010203 + 0.007802 -0.012025 + 0.013654 -0.013482 + 0.024269 -0.014572 + 0.041672 -0.014985 + 0.065976 -0.014369 + 0.094566 -0.012972 + 0.125275 -0.011034 + 0.156913 -0.008816 + 0.189022 -0.006461 + 0.221380 -0.004063 + 0.253714 -0.001687 + 0.285949 0.000632 + 0.318102 0.002874 + 0.350185 0.005015 + 0.382195 0.007039 + 0.414128 0.008920 + 0.445987 0.010630 + 0.477768 0.012157 + 0.509472 0.013465 + 0.541126 0.014532 + 0.572758 0.015351 + 0.604367 0.015925 + 0.635947 0.016240 + 0.667511 0.016282 + 0.699072 0.016053 + 0.730622 0.015565 + 0.762134 0.014807 + 0.793605 0.013763 + 0.825056 0.012422 + 0.856541 0.010783 + 0.888226 0.008848 + 0.920042 0.006634 + 0.948501 0.004447 + 0.970227 0.002643 + 0.986570 0.001203 + 1.000000 0.000000 diff --git a/runs/dae31.dat b/runs/dae31.dat new file mode 100644 index 0000000..79af6f9 --- /dev/null +++ b/runs/dae31.dat @@ -0,0 +1,84 @@ +DAE 31 +# Daedalus tip panel airfoil (4ft from tip). Design Re = 250K + 1.000000 0.000000 + 0.983670 0.003678 + 0.964831 0.008217 + 0.942298 0.013939 + 0.915136 0.021198 + 0.884751 0.029762 + 0.854418 0.038671 + 0.823963 0.047867 + 0.793343 0.057188 + 0.763399 0.066115 + 0.734041 0.074433 + 0.705002 0.082031 + 0.676045 0.088917 + 0.647058 0.095104 + 0.617978 0.100577 + 0.588755 0.105349 + 0.559366 0.109434 + 0.529812 0.112852 + 0.500123 0.115621 + 0.470348 0.117747 + 0.440557 0.119235 + 0.410816 0.120061 + 0.381154 0.120198 + 0.351603 0.119637 + 0.322220 0.118356 + 0.293057 0.116321 + 0.264162 0.113501 + 0.235612 0.109876 + 0.207525 0.105414 + 0.180030 0.100065 + 0.153293 0.093810 + 0.127559 0.086629 + 0.103134 0.078508 + 0.080386 0.069477 + 0.059755 0.059645 + 0.041713 0.049168 + 0.026721 0.038403 + 0.015173 0.027944 + 0.007269 0.018571 + 0.002584 0.010709 + 0.000358 0.004518 + 0.000025 -0.000558 + 0.000189 -0.002800 + 0.001175 -0.006664 + 0.002966 -0.009596 + 0.005693 -0.011873 + 0.009988 -0.013595 + 0.017247 -0.014838 + 0.029729 -0.015535 + 0.049021 -0.015193 + 0.074285 -0.013756 + 0.102957 -0.011523 + 0.133315 -0.008820 + 0.164511 -0.005908 + 0.196175 -0.002926 + 0.228118 0.000031 + 0.260168 0.002902 + 0.292125 0.005647 + 0.323993 0.008244 + 0.355786 0.010669 + 0.387504 0.012911 + 0.419145 0.014938 + 0.450717 0.016729 + 0.482216 0.018267 + 0.513641 0.019520 + 0.545019 0.020458 + 0.576374 0.021089 + 0.607695 0.021417 + 0.638977 0.021429 + 0.670233 0.021125 + 0.701474 0.020513 + 0.732690 0.019612 + 0.763858 0.018421 + 0.794976 0.016921 + 0.826072 0.015114 + 0.857232 0.012998 + 0.888815 0.010562 + 0.919284 0.007958 + 0.945604 0.005528 + 0.967071 0.003429 + 0.984882 0.001590 + 1.000000 0.000000 diff --git a/runs/dae51.dat b/runs/dae51.dat new file mode 100644 index 0000000..6b32ee9 --- /dev/null +++ b/runs/dae51.dat @@ -0,0 +1,83 @@ +DAE 51 +# Daedalus propeller airfoil + 1.000000 -0.000051 + 0.989166 0.001996 + 0.975819 0.004501 + 0.957448 0.007991 + 0.931599 0.013004 + 0.901654 0.018957 + 0.870818 0.025167 + 0.839998 0.031363 + 0.809336 0.037430 + 0.778839 0.043301 + 0.748503 0.048933 + 0.718326 0.054243 + 0.688314 0.059175 + 0.658443 0.063716 + 0.628653 0.067839 + 0.598855 0.071530 + 0.569004 0.074792 + 0.539074 0.077652 + 0.509071 0.080095 + 0.479015 0.082100 + 0.448934 0.083641 + 0.418877 0.084690 + 0.388863 0.085217 + 0.358908 0.085197 + 0.329049 0.084600 + 0.299321 0.083399 + 0.269760 0.081570 + 0.240419 0.079081 + 0.211388 0.075895 + 0.182766 0.071967 + 0.154699 0.067243 + 0.127404 0.061670 + 0.101193 0.055204 + 0.076503 0.047832 + 0.054060 0.039675 + 0.034881 0.031085 + 0.020059 0.022737 + 0.010052 0.015405 + 0.004208 0.009557 + 0.001251 0.005050 + 0.000113 0.001479 + 0.000123 -0.001494 + 0.001002 -0.004085 + 0.002793 -0.006422 + 0.006019 -0.008524 + 0.011960 -0.010609 + 0.022698 -0.012727 + 0.040333 -0.014554 + 0.064233 -0.015717 + 0.091882 -0.016173 + 0.121305 -0.016067 + 0.151560 -0.015570 + 0.182231 -0.014790 + 0.213149 -0.013797 + 0.244240 -0.012649 + 0.275464 -0.011392 + 0.306798 -0.010061 + 0.338230 -0.008690 + 0.369725 -0.007318 + 0.401184 -0.005962 + 0.432597 -0.004640 + 0.463976 -0.003366 + 0.495325 -0.002147 + 0.526644 -0.000994 + 0.557930 0.000082 + 0.589182 0.001071 + 0.620390 0.001960 + 0.651547 0.002731 + 0.682648 0.003367 + 0.713694 0.003847 + 0.744690 0.004152 + 0.775644 0.004269 + 0.806546 0.004190 + 0.837373 0.003898 + 0.868134 0.003359 + 0.898985 0.002532 + 0.929868 0.001410 + 0.956572 0.000219 + 0.975393 -0.000742 + 0.988983 -0.001472 + 1.000000 -0.002051 diff --git a/runs/e387.dat b/runs/e387.dat new file mode 100644 index 0000000..58abadd --- /dev/null +++ b/runs/e387.dat @@ -0,0 +1,62 @@ +E387 + 1.00000 0.00000 + 0.99677 0.00043 + 0.98729 0.00180 + 0.97198 0.00423 + 0.95128 0.00763 + 0.92554 0.01184 + 0.89510 0.01679 + 0.86035 0.02242 + 0.82183 0.02866 + 0.78007 0.03540 + 0.73567 0.04249 + 0.68922 0.04975 + 0.64136 0.05696 + 0.59272 0.06390 + 0.54394 0.07020 + 0.49549 0.07546 + 0.44767 0.07936 + 0.40077 0.08173 + 0.35505 0.08247 + 0.31078 0.08156 + 0.26813 0.07908 + 0.22742 0.07529 + 0.18906 0.07037 + 0.15345 0.06448 + 0.12094 0.05775 + 0.09185 0.05033 + 0.06643 0.04238 + 0.04493 0.03408 + 0.02748 0.02562 + 0.01423 0.01726 + 0.00519 0.00931 + 0.00044 0.00234 + 0.00091 -0.00286 + 0.00717 -0.00682 + 0.01890 -0.01017 + 0.03596 -0.01265 + 0.05827 -0.01425 + 0.08569 -0.01500 + 0.11800 -0.01502 + 0.15490 -0.01441 + 0.19599 -0.01329 + 0.24083 -0.01177 + 0.28892 -0.00998 + 0.33968 -0.00804 + 0.39252 -0.00605 + 0.44679 -0.00410 + 0.50182 -0.00228 + 0.55694 -0.00065 + 0.61147 0.00074 + 0.66472 0.00186 + 0.71602 0.00268 + 0.76475 0.00320 + 0.81027 0.00342 + 0.85202 0.00337 + 0.88944 0.00307 + 0.92205 0.00258 + 0.94942 0.00196 + 0.97118 0.00132 + 0.98705 0.00071 + 0.99674 0.00021 + 1.00000 0.00000 diff --git a/runs/e387_09.100 b/runs/e387_09.100 new file mode 100644 index 0000000..04cc8b8 --- /dev/null +++ b/runs/e387_09.100 @@ -0,0 +1,102 @@ + + XFOIL Version 6.90 + + Calculated polar for: Eppler 387 1 elements + + 1 1 Reynolds number fixed Mach number fixed + + xtrf = 1.000 (top) 1.000 (bottom) element 1 + Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000 + + alpha CL CD CDp CM Top Xtr Bot Xtr + ------- -------- --------- --------- -------- ------- ------- + -3.000 0.1048 0.01946 0.01072 -0.1011 0.9086 0.0922 + -2.900 0.1145 0.01905 0.01039 -0.1009 0.9029 0.0999 + -2.800 0.1271 0.01856 0.00992 -0.1010 0.8993 0.1103 + -2.700 0.1402 0.01812 0.00956 -0.1013 0.8964 0.1268 + -2.600 0.1505 0.01776 0.00923 -0.1010 0.8914 0.1446 + -2.500 0.1617 0.01730 0.00895 -0.1011 0.8875 0.1717 + -2.400 0.1736 0.01670 0.00860 -0.1011 0.8845 0.2145 + -2.300 0.1837 0.01611 0.00840 -0.1011 0.8804 0.2881 + -2.200 0.1924 0.01544 0.00832 -0.1008 0.8761 0.4082 + -2.100 0.2001 0.01482 0.00828 -0.0998 0.8729 0.5607 + -2.000 0.2043 0.01437 0.00830 -0.0974 0.8701 0.7026 + -1.900 0.2064 0.01411 0.00836 -0.0945 0.8652 0.8362 + -1.800 0.2267 0.01386 0.00804 -0.0956 0.8620 1.0000 + -1.700 0.2383 0.01389 0.00790 -0.0955 0.8590 1.0000 + -1.600 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