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authorDimitri Sokolyuk <demon@dim13.org>2009-05-11 00:27:49 +0000
committerDimitri Sokolyuk <demon@dim13.org>2009-05-11 00:27:49 +0000
commit0d4f43d355de79178b1142e9735902cf641670b6 (patch)
tree2ced2323f6351db2a51090b3fd13eb11f69ff53f /runs
Xfoil 6.97
Diffstat (limited to 'runs')
-rw-r--r--runs/cp_060_050.38757
-rw-r--r--runs/cp_100_040.38758
-rw-r--r--runs/cp_250_040.20348
-rw-r--r--runs/cp_500_080.lnv44
-rw-r--r--runs/dae11.dat83
-rw-r--r--runs/dae21.dat83
-rw-r--r--runs/dae31.dat84
-rw-r--r--runs/dae51.dat83
-rw-r--r--runs/e387.dat62
-rw-r--r--runs/e387_09.100102
-rw-r--r--runs/e387_11.100123
-rw-r--r--runs/la203.dat103
-rw-r--r--runs/la203t.dat141
-rw-r--r--runs/lnv109a.dat102
-rw-r--r--runs/polref_100.38782
15 files changed, 1255 insertions, 0 deletions
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 0.2490 0.01398 0.00786 -0.0955 0.8547 1.0000
+ -1.500 0.2599 0.01406 0.00781 -0.0955 0.8505 1.0000
+ -1.400 0.2710 0.01411 0.00773 -0.0953 0.8474 1.0000
+ -1.200 0.2926 0.01429 0.00768 -0.0953 0.8397 1.0000
+ -1.000 0.3145 0.01440 0.00757 -0.0949 0.8337 1.0000
+ -0.800 0.3359 0.01461 0.00763 -0.0949 0.8258 1.0000
+ -0.600 0.3576 0.01473 0.00755 -0.0945 0.8204 1.0000
+ -0.400 0.3791 0.01498 0.00767 -0.0946 0.8125 1.0000
+ -0.200 0.4008 0.01510 0.00763 -0.0942 0.8075 1.0000
+ 0.000 0.4222 0.01538 0.00782 -0.0943 0.7998 1.0000
+ 0.200 0.4439 0.01551 0.00781 -0.0939 0.7950 1.0000
+ 0.400 0.4654 0.01581 0.00804 -0.0941 0.7874 1.0000
+ 0.600 0.4871 0.01596 0.00806 -0.0937 0.7827 1.0000
+ 0.800 0.5086 0.01628 0.00835 -0.0939 0.7755 1.0000
+ 1.000 0.5304 0.01644 0.00841 -0.0935 0.7706 1.0000
+ 1.200 0.5518 0.01678 0.00872 -0.0937 0.7638 1.0000
+ 1.400 0.5736 0.01697 0.00884 -0.0934 0.7588 1.0000
+ 1.600 0.5950 0.01730 0.00916 -0.0935 0.7525 1.0000
+ 1.800 0.6167 0.01754 0.00936 -0.0933 0.7471 1.0000
+ 2.000 0.6382 0.01784 0.00964 -0.0933 0.7416 1.0000
+ 2.200 0.6596 0.01813 0.00992 -0.0932 0.7355 1.0000
+ 2.400 0.6814 0.01834 0.01009 -0.0929 0.7311 1.0000
+ 2.600 0.7025 0.01875 0.01057 -0.0931 0.7240 1.0000
+ 2.800 0.7244 0.01891 0.01069 -0.0927 0.7198 1.0000
+ 3.000 0.7451 0.01938 0.01122 -0.0929 0.7124 1.0000
+ 3.200 0.7669 0.01953 0.01136 -0.0924 0.7077 1.0000
+ 3.400 0.7875 0.01998 0.01191 -0.0925 0.7003 1.0000
+ 3.600 0.8092 0.02011 0.01203 -0.0920 0.6953 1.0000
+ 3.800 0.8295 0.02053 0.01253 -0.0920 0.6875 1.0000
+ 4.000 0.8514 0.02053 0.01252 -0.0913 0.6820 1.0000
+ 4.100 0.8607 0.02079 0.01286 -0.0912 0.6764 1.0000
+ 4.200 0.8712 0.02078 0.01286 -0.0908 0.6724 1.0000
+ 4.300 0.8823 0.02067 0.01275 -0.0903 0.6695 1.0000
+ 4.400 0.8916 0.02091 0.01307 -0.0902 0.6636 1.0000
+ 4.500 0.9021 0.02088 0.01305 -0.0898 0.6596 1.0000
+ 4.600 0.9133 0.02079 0.01293 -0.0893 0.6568 1.0000
+ 4.700 0.9226 0.02106 0.01330 -0.0893 0.6512 1.0000
+ 4.800 0.9332 0.02110 0.01337 -0.0890 0.6475 1.0000
+ 4.900 0.9444 0.02106 0.01333 -0.0886 0.6448 1.0000
+ 5.000 0.9540 0.02130 0.01366 -0.0885 0.6400 1.0000
+ 5.100 0.9643 0.02140 0.01381 -0.0883 0.6358 1.0000
+ 5.200 0.9754 0.02136 0.01378 -0.0880 0.6328 1.0000
+ 5.300 0.9854 0.02152 0.01400 -0.0878 0.6284 1.0000
+ 5.400 0.9954 0.02162 0.01420 -0.0875 0.6234 1.0000
+ 5.500 1.0066 0.02145 0.01402 -0.0870 0.6197 1.0000
+ 5.600 1.0157 0.02157 0.01424 -0.0867 0.6130 1.0000
+ 5.700 1.0266 0.02137 0.01403 -0.0861 0.6079 1.0000
+ 5.800 1.0360 0.02136 0.01410 -0.0856 0.6009 1.0000
+ 5.900 1.0468 0.02109 0.01382 -0.0849 0.5951 1.0000
+ 6.000 1.0560 0.02107 0.01389 -0.0844 0.5873 1.0000
+ 6.100 1.0671 0.02078 0.01357 -0.0838 0.5817 1.0000
+ 6.200 1.0760 0.02080 0.01370 -0.0834 0.5735 1.0000
+ 6.300 1.0870 0.02056 0.01344 -0.0828 0.5676 1.0000
+ 6.400 1.0961 0.02053 0.01356 -0.0823 0.5593 1.0000
+ 6.500 1.1060 0.02045 0.01353 -0.0818 0.5519 1.0000
+ 6.600 1.1163 0.02029 0.01341 -0.0813 0.5450 1.0000
+ 6.700 1.1255 0.02029 0.01352 -0.0808 0.5365 1.0000
+ 6.800 1.1358 0.02015 0.01341 -0.0803 0.5292 1.0000
+ 6.900 1.1453 0.02008 0.01342 -0.0798 0.5203 1.0000
+ 7.000 1.1544 0.02003 0.01348 -0.0793 0.5104 1.0000
+ 7.100 1.1637 0.01995 0.01348 -0.0787 0.4999 1.0000
+ 7.200 1.1728 0.01985 0.01346 -0.0781 0.4882 1.0000
+ 7.300 1.1816 0.01977 0.01346 -0.0775 0.4749 1.0000
+ 7.400 1.1903 0.01971 0.01347 -0.0768 0.4599 1.0000
+ 7.500 1.1984 0.01965 0.01346 -0.0761 0.4411 1.0000
+ 7.600 1.2055 0.01965 0.01347 -0.0753 0.4143 1.0000
+ 7.700 1.2113 0.01978 0.01352 -0.0743 0.3772 1.0000
+ 7.800 1.2151 0.02018 0.01362 -0.0731 0.3296 1.0000
+ 7.900 1.2166 0.02093 0.01397 -0.0719 0.2827 1.0000
+ 8.000 1.2176 0.02184 0.01455 -0.0708 0.2438 1.0000
+ 8.100 1.2191 0.02276 0.01522 -0.0698 0.2131 1.0000
+ 8.200 1.2206 0.02367 0.01595 -0.0688 0.1885 1.0000
+ 8.300 1.2220 0.02459 0.01671 -0.0678 0.1669 1.0000
+ 8.400 1.2224 0.02557 0.01750 -0.0667 0.1477 1.0000
+ 8.500 1.2228 0.02655 0.01835 -0.0655 0.1267 1.0000
+ 8.600 1.2212 0.02767 0.01929 -0.0642 0.1086 1.0000
diff --git a/runs/e387_11.100 b/runs/e387_11.100
new file mode 100644
index 0000000..9c5a2b4
--- /dev/null
+++ b/runs/e387_11.100
@@ -0,0 +1,123 @@
+
+ XFOIL Version 6.90
+
+ Calculated polar for: Eppler 387
+
+ 1 1 Reynolds number fixed Mach number fixed
+
+ xtrf = 1.000 (top) 1.000 (bottom)
+ Mach = 0.000 Re = 0.100 e 6 Ncrit = 11.000
+
+ alpha CL CD CDp CM Top Xtr Bot Xtr
+ ------- -------- --------- --------- -------- ------- -------
+ -3.000 0.0560 0.02350 0.01498 -0.0988 0.9417 0.0994
+ -2.900 0.0725 0.02284 0.01431 -0.0997 0.9384 0.1034
+ -2.800 0.0920 0.02213 0.01360 -0.1013 0.9361 0.1128
+ -2.700 0.1121 0.02138 0.01290 -0.1029 0.9341 0.1252
+ -2.600 0.1330 0.02070 0.01217 -0.1045 0.9324 0.1443
+ -2.400 0.1588 0.01962 0.01143 -0.1054 0.9245 0.1926
+ -2.100 0.1963 0.01636 0.01058 -0.1056 0.9170 0.6517
+ -1.900 0.2190 0.01570 0.01026 -0.1033 0.9104 1.0000
+ -1.800 0.2368 0.01571 0.01006 -0.1045 0.9079 1.0000
+ -1.700 0.2458 0.01589 0.01010 -0.1043 0.9028 1.0000
+ -1.600 0.2595 0.01597 0.01003 -0.1048 0.8992 1.0000
+ -1.500 0.2750 0.01599 0.00990 -0.1055 0.8965 1.0000
+ -1.400 0.2863 0.01613 0.00992 -0.1057 0.8925 1.0000
+ -1.300 0.2970 0.01627 0.00996 -0.1057 0.8882 1.0000
+ -1.200 0.3107 0.01633 0.00990 -0.1061 0.8852 1.0000
+ -1.100 0.3251 0.01635 0.00982 -0.1065 0.8829 1.0000
+ -1.000 0.3331 0.01660 0.01000 -0.1063 0.8778 1.0000
+ -0.900 0.3449 0.01670 0.01001 -0.1064 0.8743 1.0000
+ -0.800 0.3581 0.01675 0.00997 -0.1066 0.8717 1.0000
+ -0.700 0.3688 0.01690 0.01005 -0.1066 0.8682 1.0000
+ -0.600 0.3785 0.01710 0.01017 -0.1066 0.8639 1.0000
+ -0.500 0.3905 0.01718 0.01018 -0.1066 0.8609 1.0000
+ -0.400 0.4031 0.01722 0.01015 -0.1066 0.8586 1.0000
+ -0.300 0.4123 0.01748 0.01035 -0.1066 0.8543 1.0000
+ -0.200 0.4227 0.01764 0.01047 -0.1066 0.8507 1.0000
+ -0.100 0.4345 0.01772 0.01048 -0.1065 0.8479 1.0000
+ 0.000 0.4466 0.01777 0.01047 -0.1064 0.8458 1.0000
+ 0.100 0.4554 0.01808 0.01075 -0.1065 0.8412 1.0000
+ 0.200 0.4660 0.01824 0.01086 -0.1064 0.8378 1.0000
+ 0.300 0.4775 0.01832 0.01089 -0.1063 0.8353 1.0000
+ 0.400 0.4894 0.01837 0.01089 -0.1062 0.8333 1.0000
+ 0.500 0.4982 0.01873 0.01123 -0.1063 0.8286 1.0000
+ 0.600 0.5087 0.01890 0.01136 -0.1063 0.8254 1.0000
+ 0.700 0.5201 0.01898 0.01140 -0.1061 0.8229 1.0000
+ 0.800 0.5316 0.01903 0.01141 -0.1059 0.8209 1.0000
+ 0.900 0.5406 0.01942 0.01179 -0.1061 0.8164 1.0000
+ 1.000 0.5510 0.01961 0.01196 -0.1061 0.8132 1.0000
+ 1.100 0.5622 0.01970 0.01202 -0.1059 0.8107 1.0000
+ 1.200 0.5736 0.01976 0.01204 -0.1056 0.8087 1.0000
+ 1.300 0.5828 0.02015 0.01243 -0.1059 0.8045 1.0000
+ 1.400 0.5930 0.02037 0.01264 -0.1059 0.8011 1.0000
+ 1.500 0.6041 0.02048 0.01273 -0.1057 0.7986 1.0000
+ 1.600 0.6154 0.02054 0.01276 -0.1054 0.7966 1.0000
+ 1.700 0.6248 0.02092 0.01314 -0.1056 0.7928 1.0000
+ 1.800 0.6348 0.02119 0.01341 -0.1057 0.7893 1.0000
+ 1.900 0.6457 0.02131 0.01354 -0.1055 0.7867 1.0000
+ 2.000 0.6570 0.02137 0.01357 -0.1052 0.7846 1.0000
+ 2.100 0.6667 0.02171 0.01391 -0.1053 0.7812 1.0000
+ 2.200 0.6763 0.02204 0.01426 -0.1054 0.7774 1.0000
+ 2.300 0.6871 0.02218 0.01439 -0.1052 0.7746 1.0000
+ 2.400 0.6983 0.02223 0.01443 -0.1049 0.7725 1.0000
+ 2.500 0.7083 0.02250 0.01471 -0.1049 0.7695 1.0000
+ 2.600 0.7175 0.02292 0.01515 -0.1051 0.7653 1.0000
+ 2.700 0.7282 0.02305 0.01529 -0.1049 0.7625 1.0000
+ 2.800 0.7394 0.02309 0.01531 -0.1045 0.7603 1.0000
+ 2.900 0.7494 0.02335 0.01562 -0.1044 0.7572 1.0000
+ 3.000 0.7584 0.02378 0.01609 -0.1046 0.7528 1.0000
+ 3.100 0.7691 0.02389 0.01620 -0.1043 0.7499 1.0000
+ 3.200 0.7804 0.02389 0.01619 -0.1038 0.7476 1.0000
+ 3.300 0.7896 0.02428 0.01661 -0.1039 0.7437 1.0000
+ 3.400 0.7990 0.02461 0.01697 -0.1039 0.7396 1.0000
+ 3.500 0.8099 0.02464 0.01701 -0.1034 0.7368 1.0000
+ 3.600 0.8213 0.02456 0.01692 -0.1028 0.7346 1.0000
+ 3.700 0.8292 0.02516 0.01758 -0.1031 0.7292 1.0000
+ 3.800 0.8396 0.02523 0.01767 -0.1027 0.7255 1.0000
+ 3.900 0.8510 0.02505 0.01752 -0.1019 0.7228 1.0000
+ 4.000 0.8591 0.02546 0.01799 -0.1018 0.7172 1.0000
+ 4.100 0.8695 0.02542 0.01796 -0.1012 0.7129 1.0000
+ 4.200 0.8810 0.02512 0.01764 -0.1002 0.7100 1.0000
+ 4.300 0.8887 0.02559 0.01818 -0.1002 0.7036 1.0000
+ 4.400 0.8995 0.02546 0.01806 -0.0994 0.6998 1.0000
+ 4.500 0.9112 0.02517 0.01775 -0.0985 0.6972 1.0000
+ 4.600 0.9187 0.02575 0.01842 -0.0987 0.6906 1.0000
+ 4.700 0.9296 0.02564 0.01834 -0.0980 0.6871 1.0000
+ 4.800 0.9414 0.02542 0.01811 -0.0973 0.6848 1.0000
+ 5.000 0.9598 0.02594 0.01875 -0.0969 0.6748 1.0000
+ 5.100 0.9717 0.02568 0.01853 -0.0961 0.6724 1.0000
+ 5.300 0.9903 0.02610 0.01908 -0.0955 0.6620 1.0000
+ 5.400 0.9998 0.02619 0.01923 -0.0950 0.6569 1.0000
+ 5.500 1.0096 0.02612 0.01921 -0.0943 0.6511 1.0000
+ 5.600 1.0221 0.02551 0.01855 -0.0931 0.6476 1.0000
+ 5.700 1.0295 0.02575 0.01891 -0.0927 0.6392 1.0000
+ 5.800 1.0413 0.02518 0.01830 -0.0915 0.6343 1.0000
+ 5.900 1.0499 0.02511 0.01832 -0.0908 0.6261 1.0000
+ 6.000 1.0598 0.02484 0.01808 -0.0899 0.6194 1.0000
+ 6.100 1.0705 0.02445 0.01769 -0.0890 0.6128 1.0000
+ 6.200 1.0796 0.02434 0.01765 -0.0883 0.6050 1.0000
+ 6.300 1.0913 0.02379 0.01712 -0.0873 0.5992 1.0000
+ 6.400 1.0999 0.02374 0.01718 -0.0866 0.5905 1.0000
+ 6.500 1.1110 0.02333 0.01676 -0.0858 0.5843 1.0000
+ 6.600 1.1205 0.02315 0.01665 -0.0851 0.5761 1.0000
+ 6.700 1.1298 0.02301 0.01659 -0.0844 0.5678 1.0000
+ 6.800 1.1417 0.02253 0.01609 -0.0836 0.5615 1.0000
+ 6.900 1.1502 0.02244 0.01612 -0.0829 0.5516 1.0000
+ 7.000 1.1595 0.02224 0.01601 -0.0822 0.5420 1.0000
+ 7.100 1.1693 0.02193 0.01575 -0.0814 0.5321 1.0000
+ 7.200 1.1789 0.02159 0.01545 -0.0805 0.5213 1.0000
+ 7.300 1.1880 0.02127 0.01521 -0.0796 0.5087 1.0000
+ 7.400 1.1965 0.02097 0.01499 -0.0787 0.4940 1.0000
+ 7.500 1.2050 0.02057 0.01461 -0.0777 0.4767 1.0000
+ 7.600 1.2118 0.02025 0.01440 -0.0765 0.4529 1.0000
+ 7.700 1.2175 0.02003 0.01418 -0.0752 0.4195 1.0000
+ 7.800 1.2217 0.02007 0.01403 -0.0738 0.3744 1.0000
+ 7.900 1.2234 0.02059 0.01418 -0.0724 0.3208 1.0000
+ 8.000 1.2233 0.02152 0.01468 -0.0710 0.2748 1.0000
+ 8.100 1.2227 0.02261 0.01542 -0.0696 0.2392 1.0000
+ 8.200 1.2222 0.02371 0.01625 -0.0683 0.2104 1.0000
+ 8.300 1.2217 0.02480 0.01712 -0.0670 0.1860 1.0000
+ 8.400 1.2208 0.02592 0.01804 -0.0657 0.1637 1.0000
+ 8.500 1.2186 0.02714 0.01906 -0.0641 0.1423 1.0000
+ 9.000 1.2117 0.03330 0.02451 -0.0564 0.0811 1.0000
diff --git a/runs/la203.dat b/runs/la203.dat
new file mode 100644
index 0000000..2fc3b0f
--- /dev/null
+++ b/runs/la203.dat
@@ -0,0 +1,103 @@
+LA203A
+ 1.000000 0.000000
+ 0.993938 0.003044
+ 0.986151 0.005883
+ 0.976665 0.008985
+ 0.965516 0.012408
+ 0.952740 0.016162
+ 0.938385 0.020258
+ 0.922500 0.024700
+ 0.905141 0.029490
+ 0.886369 0.034630
+ 0.866250 0.040113
+ 0.844856 0.045936
+ 0.822261 0.052086
+ 0.798545 0.058545
+ 0.773791 0.065291
+ 0.748087 0.072292
+ 0.721524 0.079495
+ 0.694194 0.086797
+ 0.666193 0.094063
+ 0.637621 0.101087
+ 0.608579 0.107640
+ 0.579167 0.113566
+ 0.549490 0.118770
+ 0.519653 0.123176
+ 0.489759 0.126743
+ 0.459916 0.129436
+ 0.430226 0.131219
+ 0.400796 0.132090
+ 0.371729 0.132075
+ 0.343127 0.131182
+ 0.315090 0.129435
+ 0.287716 0.126854
+ 0.261106 0.123424
+ 0.235350 0.119234
+ 0.210538 0.114389
+ 0.186758 0.108970
+ 0.164095 0.103048
+ 0.142628 0.096688
+ 0.122432 0.089956
+ 0.103579 0.082919
+ 0.086135 0.075641
+ 0.070162 0.068190
+ 0.055715 0.060636
+ 0.042846 0.053047
+ 0.031599 0.045492
+ 0.022015 0.038031
+ 0.014127 0.030677
+ 0.007963 0.023336
+ 0.003544 0.015836
+ 0.000887 0.008000
+ 0.000000 0.000000
+ 0.000887 -0.008018
+ 0.003544 -0.015138
+ 0.007963 -0.021544
+ 0.014127 -0.026519
+ 0.022015 -0.029639
+ 0.031599 -0.031320
+ 0.042846 -0.032209
+ 0.055715 -0.032676
+ 0.070162 -0.032868
+ 0.086135 -0.032857
+ 0.103579 -0.032693
+ 0.122432 -0.032408
+ 0.142628 -0.032024
+ 0.164095 -0.031556
+ 0.186758 -0.031016
+ 0.210538 -0.030405
+ 0.235350 -0.029724
+ 0.261106 -0.028966
+ 0.287716 -0.028124
+ 0.315090 -0.027183
+ 0.343127 -0.026124
+ 0.371729 -0.024919
+ 0.400796 -0.023512
+ 0.430226 -0.021827
+ 0.459916 -0.019830
+ 0.489759 -0.017533
+ 0.519653 -0.014948
+ 0.549490 -0.012098
+ 0.579167 -0.009052
+ 0.608579 -0.005918
+ 0.637621 -0.002821
+ 0.666193 0.000143
+ 0.694194 0.002917
+ 0.721524 0.005447
+ 0.748087 0.007686
+ 0.773791 0.009595
+ 0.798545 0.011145
+ 0.822261 0.012312
+ 0.844856 0.013088
+ 0.866250 0.013463
+ 0.886369 0.013448
+ 0.905141 0.013056
+ 0.922500 0.012302
+ 0.938385 0.011218
+ 0.952740 0.009838
+ 0.965516 0.008212
+ 0.976665 0.006393
+ 0.986151 0.004425
+ 0.993938 0.002384
+ 1.000000 0.000000
+
diff --git a/runs/la203t.dat b/runs/la203t.dat
new file mode 100644
index 0000000..95cc377
--- /dev/null
+++ b/runs/la203t.dat
@@ -0,0 +1,141 @@
+LA230A blunt TE
+ 1.000455 0.000895
+ 0.993427 0.004332
+ 0.981492 0.008450
+ 0.967879 0.012697
+ 0.952291 0.017269
+ 0.934612 0.022276
+ 0.914876 0.027744
+ 0.893349 0.033633
+ 0.870451 0.039856
+ 0.846614 0.046320
+ 0.822246 0.052928
+ 0.797640 0.059604
+ 0.773000 0.066294
+ 0.748527 0.072935
+ 0.724456 0.079441
+ 0.700950 0.085719
+ 0.678100 0.091696
+ 0.655966 0.097294
+ 0.634488 0.102460
+ 0.613509 0.107185
+ 0.592872 0.111482
+ 0.572474 0.115369
+ 0.552260 0.118854
+ 0.532181 0.121940
+ 0.512197 0.124633
+ 0.492299 0.126938
+ 0.472493 0.128851
+ 0.452778 0.130366
+ 0.433139 0.131481
+ 0.413556 0.132197
+ 0.394032 0.132519
+ 0.374603 0.132449
+ 0.355296 0.131983
+ 0.336122 0.131120
+ 0.317102 0.129862
+ 0.298297 0.128215
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diff --git a/runs/lnv109a.dat b/runs/lnv109a.dat
new file mode 100644
index 0000000..43a8df7
--- /dev/null
+++ b/runs/lnv109a.dat
@@ -0,0 +1,102 @@
+LNV-109A
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diff --git a/runs/polref_100.387 b/runs/polref_100.387
new file mode 100644
index 0000000..d450076
--- /dev/null
+++ b/runs/polref_100.387
@@ -0,0 +1,82 @@
+# Langley LTPT
+0.0201 0.098 | Eppler 387 polar Re=100000 Langley LTPT
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