ファイルインデックス名　: File Index Name        : 3046        .A  
翼型整理番号　　　　　　: Airfoil Serial No.     : M03-0001-1
翼型名　　　　　　　　　: Airfoil Name           : Martin M1
翼型ファイル番号　　　　: Airfoil File No.       : 3046
翼型情報　　　　　　　　: Airfoil Information    : Original

算出前縁半径　　　　　　: Computed L.E.R.        : ?
算出前縁傾斜　　　　　　: Computed Slope of L.E. : ?
算出プログラム番号　　　: Computed Program No.   : X68eB03-C01G2


座標　　　　　　　　　　: Plot Ordinates         :

 X             Y

 1.00000, 0.00000
 0.98671, 0.00172
 0.97362, 0.00332
 0.96072, 0.00481
 0.94801, 0.00622
 0.93549, 0.00753
 0.92315, 0.00878
 0.91099, 0.00996
 0.89900, 0.01110
 0.88719, 0.01224
 0.87554, 0.01334
 0.86406, 0.01441
 0.85274, 0.01545
 0.84158, 0.01645
 0.83058, 0.01742
 0.81973, 0.01835
 0.80903, 0.01926
 0.79848, 0.02012
 0.78808, 0.02091
 0.77781, 0.02167
 0.76769, 0.02240
 0.75770, 0.02310
 0.74785, 0.02379
 0.73814, 0.02445
 0.72855, 0.02510
 0.71909, 0.02573
 0.70976, 0.02635
 0.70055, 0.02696
 0.69146, 0.02761
 0.68249, 0.02825
 0.67363, 0.02888
 0.66490, 0.02950
 0.65627, 0.03011
 0.64776, 0.03071
 0.63935, 0.03130
 0.63106, 0.03188
 0.62287, 0.03244
 0.61478, 0.03300
 0.60680, 0.03354
 0.59891, 0.03408
 0.59112, 0.03461
 0.58344, 0.03513
 0.57584, 0.03563
 0.56834, 0.03612
 0.56094, 0.03660
 0.55362, 0.03706
 0.54639, 0.03750
 0.53925, 0.03792
 0.53220, 0.03833
 0.52523, 0.03872
 0.51835, 0.03909
 0.51155, 0.03944
 0.50483, 0.03977
 0.49819, 0.04006
 0.49163, 0.04028
 0.48514, 0.04048
 0.47874, 0.04066
 0.47240, 0.04082
 0.46614, 0.04097
 0.45996, 0.04111
 0.45384, 0.04123
 0.44780, 0.04134
 0.44182, 0.04145
 0.43591, 0.04154
 0.43007, 0.04163
 0.42430, 0.04171
 0.41859, 0.04178
 0.41295, 0.04185
 0.40737, 0.04192
 0.40185, 0.04198
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 0.39099, 0.04226
 0.38566, 0.04242
 0.38038, 0.04257
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 0.36489, 0.04299
 0.35984, 0.04312
 0.35484, 0.04325
 0.34990, 0.04337
 0.34501, 0.04347
 0.34017, 0.04358
 0.33538, 0.04367
 0.33065, 0.04375
 0.32596, 0.04382
 0.32133, 0.04388
 0.31674, 0.04393
 0.31220, 0.04396
 0.30771, 0.04399
 0.30326, 0.04400
 0.29887, 0.04397
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 0.28594, 0.04358
 0.28172, 0.04342
 0.27754, 0.04325
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 0.25728, 0.04225
 0.25334, 0.04202
 0.24945, 0.04179
 0.24560, 0.04154
 0.24178, 0.04129
 0.23800, 0.04103
 0.23426, 0.04077
 0.23056, 0.04050
 0.22689, 0.04023
 0.22326, 0.03995
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 0.21257, 0.03909
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 0.20561, 0.03849
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 0.19879, 0.03790
 0.19542, 0.03761
 0.19209, 0.03733
 0.18879, 0.03703
 0.18552, 0.03674
 0.18228, 0.03645
 0.17908, 0.03615
 0.17590, 0.03585
 0.17275, 0.03554
 0.16963, 0.03524
 0.16654, 0.03493
 0.16348, 0.03462
 0.16044, 0.03431
 0.15743, 0.03400
 0.15445, 0.03368
 0.15150, 0.03336
 0.14858, 0.03305
 0.14568, 0.03273
 0.14280, 0.03241
 0.13996, 0.03209
 0.13713, 0.03177
 0.13434, 0.03145
 0.13157, 0.03112
 0.12882, 0.03080
 0.12610, 0.03047
 0.12340, 0.03013
 0.12072, 0.02980
 0.11807, 0.02946
 0.11544, 0.02912
 0.11283, 0.02878
 0.11025, 0.02843
 0.10769, 0.02808
 0.10515, 0.02773
 0.10264, 0.02738
 0.10014, 0.02702
 0.09767, 0.02664
 0.09521, 0.02626
 0.09278, 0.02588
 0.09037, 0.02550
 0.08798, 0.02512
 0.08561, 0.02474
 0.08326, 0.02435
 0.08093, 0.02397
 0.07862, 0.02360
 0.07633, 0.02322
 0.07405, 0.02285
 0.07180, 0.02249
 0.06956, 0.02213
 0.06735, 0.02178
 0.06515, 0.02142
 0.06297, 0.02108
 0.06081, 0.02073
 0.05866, 0.02039
 0.05653, 0.02004
 0.05442, 0.01971
 0.05233, 0.01937
 0.05026, 0.01904
 0.04820, 0.01873
 0.04615, 0.01842
 0.04413, 0.01812
 0.04212, 0.01782
 0.04012, 0.01752
 0.03815, 0.01721
 0.03618, 0.01691
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 0.03231, 0.01629
 0.03039, 0.01596
 0.02849, 0.01564
 0.02660, 0.01530
 0.02473, 0.01495
 0.02287, 0.01459
 0.02103, 0.01421
 0.01920, 0.01381
 0.01739, 0.01338
 0.01559, 0.01292
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 0.01027, 0.01121
 0.00853, 0.01049
 0.00680, 0.00964
 0.00508, 0.00861
 0.00337, 0.00729
 0.00168, 0.00541
 0.00056, 0.00328
 0.00000, 0.00000
 0.00000, 0.00000
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 0.11025,-0.02843
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 1.00000, 0.00000