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Four digit profiles
0006   0008   0010   0012   0015   0018   0021

Modified four digit profiles
0008-34   0010-34   0010-35   0010-64   0010-65   0010-66   0012-34   0012-64

16-series profiles
16-006   16-009   16-012   16-015   16-018   16-021

63 series profiles
63-006   63-008   63-009   63-010  
63-012   63-015   63-018   63-021

63A series profiles
63A-006   63A-000   63A-010   63A-012   63A-015

64 series profiles
64-006   64-008   64-009   64-010  
64-012   64-015   64-018   64-021

64A series profiles
64A-006   64A-008   64A-010   64A-012   64A-015

65 series profiles
65-006   65-008   65-009   65-010  
65-012   65-015   65-018   65-021

65A series profiles
65A-006   65A-008   65A-010   65A-012   65A-015

66 series profiles
66-006   66-008   66-009   66-010  
66-012   66-015   66-018   66-021

67 series profiles
67-012   67-015

NACA Profile 0006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.61070.5910
0.75000.74240.4749
1.25000.94700.3579
2.50001.30740.2387
5.00001.77730.1514
7.50002.10000.1104
10.00002.34140.0844
15.00002.67260.0509
20.00002.86880.0289
25.00002.97060.0126
30.00003.0009-0.0000
35.00002.9743-0.0102
40.00002.9015-0.0186
45.00002.7904-0.0256
50.00002.6470-0.0316
55.00002.4762-0.0366
60.00002.2817-0.0411
65.00002.0662-0.0450
70.00001.8320-0.0486
75.00001.5802-0.0521
80.00001.3116-0.0554
85.00001.0263-0.0587
90.00000.7239-0.0623
95.00000.4033-0.0660
100.00000.0630-0.0702
L.E. radius = 0.397 percent chord

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NACA Profile 0008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.81420.7880
0.75000.98990.6332
1.25001.26260.4772
2.50001.74310.3183
5.00002.36980.2019
7.50002.79990.1472
10.00003.12180.1125
15.00003.56340.0679
20.00003.82500.0385
25.00003.96080.0168
30.00004.0012-0.0001
35.00003.9657-0.0136
40.00003.8687-0.0248
45.00003.7205-0.0342
50.00003.5294-0.0421
55.00003.3016-0.0489
60.00003.0422-0.0548
65.00002.7550-0.0600
70.00002.4426-0.0649
75.00002.1069-0.0694
80.00001.7487-0.0738
85.00001.3684-0.0783
90.00000.9651-0.0830
95.00000.5377-0.0880
100.00000.0840-0.0935
L.E. radius = 0.705 percent chord

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NACA Profile 0010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.01780.9850
0.75001.23740.7915
1.25001.57830.5966
2.50002.17890.3979
5.00002.96220.2524
7.50003.49990.1840
10.00003.90230.1406
15.00004.45430.0848
20.00004.78130.0481
25.00004.95100.0210
30.00005.0014-0.0001
35.00004.9572-0.0171
40.00004.8358-0.0310
45.00004.6506-0.0427
50.00004.4117-0.0526
55.00004.1270-0.0611
60.00003.8028-0.0685
65.00003.4437-0.0750
70.00003.0533-0.0811
75.00002.6336-0.0868
80.00002.1859-0.0923
85.00001.7105-0.0979
90.00001.2064-0.1038
95.00000.6721-0.1100
100.00000.1050-0.1169
L.E. radius = 1.102 percent chord

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NACA Profile 0012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.22131.1819
0.75001.48490.9498
1.25001.89390.7159
2.50002.61470.4775
5.00003.55470.3029
7.50004.19990.2208
10.00004.68280.1687
15.00005.34520.1018
20.00005.73750.0577
25.00005.94120.0252
30.00006.0017-0.0001
35.00005.9486-0.0205
40.00005.8030-0.0372
45.00005.5807-0.0513
50.00005.2940-0.0631
55.00004.9524-0.0733
60.00004.5634-0.0822
65.00004.1325-0.0901
70.00003.6639-0.0973
75.00003.1603-0.1041
80.00002.6231-0.1108
85.00002.0526-0.1175
90.00001.4477-0.1245
95.00000.8066-0.1321
100.00000.1260-0.1403
L.E. radius = 1.587 percent chord

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NACA Profile 0015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.52661.4774
0.75001.85611.1872
1.25002.36740.8948
2.50003.26840.5969
5.00004.44340.3786
7.50005.24990.2760
10.00005.85350.2109
15.00006.68150.1272
20.00007.17190.0721
25.00007.42660.0315
30.00007.5022-0.0001
35.00007.4358-0.0256
40.00007.2538-0.0466
45.00006.9759-0.0641
50.00006.6175-0.0789
55.00006.1905-0.0916
60.00005.7042-0.1027
65.00005.1656-0.1126
70.00004.5799-0.1216
75.00003.9504-0.1301
80.00003.2789-0.1385
85.00002.5657-0.1469
90.00001.8096-0.1556
95.00001.0082-0.1651
100.00000.1575-0.1754
L.E. radius = 2.479 percent chord

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NACA Profile 0018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.83201.7729
0.75002.22731.4246
1.25002.84091.0738
2.50003.92210.7162
5.00005.33200.4543
7.50006.29990.3312
10.00007.02420.2531
15.00008.01770.1527
20.00008.60630.0866
25.00008.91190.0379
30.00009.0026-0.0001
35.00008.9229-0.0307
40.00008.7045-0.0559
45.00008.3711-0.0769
50.00007.9410-0.0947
55.00007.4286-0.1099
60.00006.8451-0.1232
65.00006.1987-0.1351
70.00005.4959-0.1459
75.00004.7405-0.1562
80.00003.9347-0.1661
85.00003.0788-0.1762
90.00002.1716-0.1868
95.00001.2098-0.1981
100.00000.1890-0.2105
L.E. radius = 3.570 percent chord

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NACA Profile 0021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50002.13732.0684
0.75002.59851.6621
1.25003.31431.2528
2.50004.57580.8356
5.00006.22070.5301
7.50007.34980.3863
10.00008.19480.2953
15.00009.35400.1781
20.000010.04070.1010
25.000010.39720.0442
30.000010.5030-0.0001
35.000010.4101-0.0358
40.000010.1553-0.0652
45.00009.7663-0.0897
50.00009.2645-0.1104
55.00008.6667-0.1282
60.00007.9859-0.1438
65.00007.2319-0.1576
70.00006.4118-0.1703
75.00005.5305-0.1822
80.00004.5905-0.1938
85.00003.5920-0.2056
90.00002.5335-0.2179
95.00001.4115-0.2311
100.00000.2205-0.2455
L.E. radius = 4.859 percent chord

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NACA Profile 0008-34
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.45780.4946
0.75000.57070.4164
1.25000.75660.3370
2.50001.11740.2538
5.00001.65830.1884
7.50002.08300.1540
10.00002.43640.1298
15.00002.99260.0947
20.00003.39690.0681
25.00003.68150.0464
30.00003.86690.0283
35.00003.96870.0129
40.00004.00000.0000
45.00003.97080.0117
50.00003.88380.0231
55.00003.74010.0343
60.00003.54090.0453
65.00003.28730.0561
70.00002.98030.0667
75.00002.62110.0770
80.00002.21070.0871
85.00001.75030.0970
90.00001.24100.1067
95.00000.68390.1161
100.00000.08000.1254
L.E. radius = 0.176 percent chord

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NACA Profile 0010-34
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.57220.6182
0.75000.71330.5205
1.25000.94570.4212
2.50001.39680.3173
5.00002.07280.2355
7.50002.60380.1925
10.00003.04550.1623
15.00003.74080.1183
20.00004.24610.0851
25.00004.60180.0580
30.00004.83360.0353
35.00004.96090.0161
40.00005.00000.0000
45.00004.96340.0146
50.00004.85470.0289
55.00004.67510.0429
60.00004.42610.0567
65.00004.10910.0701
70.00003.72540.0833
75.00003.27640.0962
80.00002.76340.1089
85.00002.18790.1213
90.00001.55130.1334
95.00000.85480.1452
100.00000.10000.1567
L.E. radius = 0.275 percent chord

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NACA Profile 0010-35
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.54570.5660
0.75000.67390.4692
1.25000.88100.3717
2.50001.27300.2722
5.00001.84690.1987
7.50002.29600.1636
10.00002.67480.1408
15.00003.29580.1098
20.00003.78700.0876
25.00004.17820.0694
30.00004.48440.0534
35.00004.71480.0389
40.00004.87500.0253
45.00004.96910.0124
50.00005.00000.0000
55.00004.96760.0133
60.00004.86310.0289
65.00004.67530.0466
70.00004.39320.0666
75.00004.00570.0888
80.00003.50180.1132
85.00002.87030.1398
90.00002.10030.1686
95.00001.18050.1997
100.00000.10000.2329
L.E. radius = 0.275 percent chord

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NACA Profile 0010-64
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.98800.9266
0.75001.19320.7345
1.25001.50620.5421
2.50002.04280.3497
5.00002.72050.2160
7.50003.18080.1583
10.00003.53150.1247
15.00004.04710.0855
20.00004.41150.0617
25.00004.67420.0440
30.00004.85560.0288
35.00004.96370.0145
40.00005.00000.0000
45.00004.96340.0146
50.00004.85470.0289
55.00004.67510.0429
60.00004.42610.0567
65.00004.10910.0701
70.00003.72540.0833
75.00003.27640.0962
80.00002.76340.1089
85.00002.18790.1213
90.00001.55130.1334
95.00000.85480.1452
100.00000.10000.1567
L.E. radius = 1.102 percent chord

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NACA Profile 0010-65
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.97280.8967
0.75001.17050.7049
1.25001.46900.5133
2.50001.97070.3229
5.00002.58620.1929
7.50002.99350.1390
10.00003.30050.1091
15.00003.75560.0769
20.00004.09380.0598
25.00004.36310.0485
30.00004.58200.0393
35.00004.75690.0306
40.00004.88770.0215
45.00004.97070.0115
50.00005.00000.0000
55.00004.96760.0133
60.00004.86310.0289
65.00004.67530.0466
70.00004.39320.0666
75.00004.00570.0888
80.00003.50180.1132
85.00002.87030.1398
90.00002.10030.1686
95.00001.18050.1997
100.00000.10000.2329
L.E. radius = 1.102 percent chord

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NACA Profile 0010-66
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.98200.9147
0.75001.18420.7224
1.25001.49120.5299
2.50002.01230.3372
5.00002.65800.2030
7.50003.08550.1452
10.00003.40360.1119
15.00003.85840.0743
20.00004.17350.0535
25.00004.40560.0402
30.00004.58230.0309
35.00004.71860.0239
40.00004.82340.0182
45.00004.90170.0132
50.00004.95650.0087
55.00004.98910.0044
60.00005.00000.0000
65.00004.98080.0093
70.00004.89050.0285
75.00004.67980.0575
80.00004.29960.0963
85.00003.70070.1449
90.00002.83390.2034
95.00001.65010.2717
100.00000.10000.3499
L.E. radius = 1.102 percent chord

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NACA Profile 0012-34
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.68670.7418
0.75000.85600.6246
1.25001.13480.5054
2.50001.67610.3807
5.00002.48740.2825
7.50003.12450.2310
10.00003.65460.1948
15.00004.48890.1420
20.00005.09530.1021
25.00005.52220.0696
30.00005.80030.0424
35.00005.95300.0194
40.00006.00000.0000
45.00005.95610.0175
50.00005.82560.0347
55.00005.61020.0515
60.00005.31140.0680
65.00004.93090.0841
70.00004.47040.1000
75.00003.93160.1155
80.00003.31610.1307
85.00002.62550.1455
90.00001.86150.1600
95.00001.02580.1742
100.00000.12000.1881
L.E. radius = 0.397 percent chord

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NACA Profile 0012-64
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.18551.1120
0.75001.43180.8813
1.25001.80740.6506
2.50002.45130.4197
5.00003.26470.2592
7.50003.81700.1900
10.00004.23780.1497
15.00004.85650.1027
20.00005.29380.0741
25.00005.60910.0528
30.00005.82670.0346
35.00005.95640.0173
40.00006.00000.0000
45.00005.95610.0175
50.00005.82560.0347
55.00005.61020.0515
60.00005.31140.0680
65.00004.93090.0841
70.00004.47040.1000
75.00003.93160.1155
80.00003.31610.1307
85.00002.62550.1455
90.00001.86150.1600
95.00001.02580.1742
100.00000.12000.1881
L.E. radius = 1.587 percent chord

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NACA Profile 16-006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.41280.4057
0.75000.50370.3287
1.25000.64620.2514
2.50000.90340.1734
5.00001.25600.1181
7.50001.51710.0932
10.00001.73000.0781
15.00002.06940.0593
20.00002.33360.0470
25.00002.54390.0374
30.00002.71020.0292
35.00002.83730.0217
40.00002.92760.0144
45.00002.98180.0073
50.00003.00000.0000
55.00002.98060.0080
60.00002.91780.0173
65.00002.80520.0280
70.00002.63590.0400
75.00002.40340.0533
80.00002.10110.0679
85.00001.72220.0839
90.00001.26020.1012
95.00000.70830.1198
100.00000.06000.1398
L.E. radius = 0.176 percent chord

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NACA Profile 16-009
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.61920.6086
0.75000.75550.4930
1.25000.96930.3770
2.50001.35500.2602
5.00001.88400.1771
7.50002.27560.1399
10.00002.59500.1172
15.00003.10420.0890
20.00003.50040.0705
25.00003.81580.0562
30.00004.06530.0438
35.00004.25590.0325
40.00004.39130.0217
45.00004.47270.0109
50.00004.50000.0000
55.00004.47090.0120
60.00004.37680.0260
65.00004.20780.0420
70.00003.95390.0599
75.00003.60520.0799
80.00003.15160.1019
85.00002.58330.1258
90.00001.89020.1518
95.00001.06250.1797
100.00000.09000.2096
L.E. radius = 0.397 percent chord

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NACA Profile 16-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.82560.8115
0.75001.00730.6573
1.25001.29240.5027
2.50001.80670.3469
5.00002.51200.2362
7.50003.03420.1865
10.00003.46000.1562
15.00004.13890.1186
20.00004.66710.0940
25.00005.08770.0749
30.00005.42030.0585
35.00005.67460.0434
40.00005.85510.0289
45.00005.96360.0145
50.00006.00000.0000
55.00005.96110.0160
60.00005.83570.0346
65.00005.61030.0559
70.00005.27180.0799
75.00004.80690.1065
80.00004.20220.1358
85.00003.44440.1677
90.00002.52030.2023
95.00001.41660.2396
100.00000.12000.2795
L.E. radius = 0.705 percent chord

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NACA Profile 16-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.03211.0144
0.75001.25910.8217
1.25001.61550.6284
2.50002.25840.4336
5.00003.14000.2952
7.50003.79270.2331
10.00004.32500.1953
15.00005.17360.1483
20.00005.83390.1175
25.00006.35970.0936
30.00006.77540.0731
35.00007.09320.0542
40.00007.31890.0361
45.00007.45450.0181
50.00007.50000.0000
55.00007.45140.0200
60.00007.29460.0433
65.00007.01290.0699
70.00006.58980.0999
75.00006.00860.1332
80.00005.25270.1698
85.00004.30550.2097
90.00003.15040.2529
95.00001.77080.2995
100.00000.15000.3494
L.E. radius = 1.102 percent chord

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NACA Profile 16-018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.23851.2172
0.75001.51100.9860
1.25001.93860.7541
2.50002.71010.5203
5.00003.76800.3542
7.50004.55130.2797
10.00005.19000.2343
15.00006.20830.1780
20.00007.00070.1410
25.00007.63160.1123
30.00008.13050.0877
35.00008.51190.0651
40.00008.78270.0433
45.00008.94540.0218
50.00009.00000.0000
55.00008.94170.0240
60.00008.75350.0520
65.00008.41550.0839
70.00007.90780.1199
75.00007.21030.1598
80.00006.30330.2037
85.00005.16660.2516
90.00003.78050.3035
95.00002.12490.3594
100.00000.18000.4193
L.E. radius = 1.587 percent chord

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NACA Profile 16-021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.44491.4201
0.75001.76281.1503
1.25002.26170.8797
2.50003.16180.6070
5.00004.39600.4133
7.50005.30980.3263
10.00006.05500.2734
15.00007.24300.2076
20.00008.16750.1645
25.00008.90360.1310
30.00009.48560.1023
35.00009.93050.0759
40.000010.24640.0505
45.000010.43630.0254
50.000010.50000.0000
55.000010.43200.0280
60.000010.21240.0606
65.00009.81810.0979
70.00009.22570.1398
75.00008.41200.1864
80.00007.35380.2377
85.00006.02770.2935
90.00004.41060.3541
95.00002.47910.4193
100.00000.21000.4891
L.E. radius = 2.160 percent chord

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NACA Profile 63-006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.50390.4762
0.75000.60940.3777
1.25000.77090.2809
2.50001.05680.1945
5.00001.46260.1383
7.50001.76660.1077
10.00002.01070.0890
15.00002.38720.0638
20.00002.65720.0451
25.00002.84240.0294
30.00002.95580.0154
35.00002.99900.0013
40.00002.9712-0.0124
45.00002.8764-0.0253
50.00002.7218-0.0364
55.00002.5161-0.0456
60.00002.2679-0.0536
65.00001.9844-0.0599
70.00001.6727-0.0646
75.00001.3433-0.0672
80.00001.0075-0.0671
85.00000.6806-0.0633
90.00000.3820-0.0555
95.00000.1371-0.0405
100.00000.0000-0.0008
L.E. radius = 0.267 percent chord

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NACA Profile 63-008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.66820.6340
0.75000.80870.5036
1.25001.02440.3755
2.50001.40730.2609
5.00001.95160.1854
7.50002.35880.1442
10.00002.68570.1191
15.00003.18950.0853
20.00003.55000.0599
25.00003.79640.0391
30.00003.94580.0201
35.00003.99980.0007
40.00003.9577-0.0176
45.00003.8252-0.0351
50.00003.6131-0.0498
55.00003.3336-0.0618
60.00002.9982-0.0722
65.00002.6172-0.0802
70.00002.2002-0.0858
75.00001.7616-0.0891
80.00001.3171-0.0882
85.00000.8871-0.0830
90.00000.4963-0.0725
95.00000.1777-0.0529
100.0000-0.0000-0.0011
L.E. radius = 0.471 percent chord

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NACA Profile 63-009
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.74890.7124
0.75000.90690.5665
1.25001.14970.4230
2.50001.58150.2944
5.00002.19580.2092
7.50002.65500.1627
10.00003.02370.1343
15.00003.59150.0959
20.00003.99740.0673
25.00004.27430.0439
30.00004.44140.0224
35.00004.50010.0005
40.00004.4499-0.0204
45.00004.2974-0.0402
50.00004.0556-0.0565
55.00003.7383-0.0701
60.00003.3586-0.0810
65.00002.9282-0.0904
70.00002.4585-0.0965
75.00001.9654-0.0997
80.00001.4674-0.0985
85.00000.9867-0.0925
90.00000.5512-0.0806
95.00000.1971-0.0589
100.00000.0000-0.0012
L.E. radius = 0.590 percent chord

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NACA Profile 63-010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.82850.7905
0.75001.00400.6293
1.25001.27390.4706
2.50001.75480.3281
5.00002.43960.2332
7.50002.95130.1812
10.00003.36190.1494
15.00003.99410.1066
20.00004.44540.0748
25.00004.75290.0488
30.00004.93740.0249
35.00005.00030.0003
40.00004.9414-0.0233
45.00004.7682-0.0452
50.00004.4959-0.0634
55.00004.1401-0.0784
60.00003.7158-0.0903
65.00003.2357-0.1007
70.00002.7131-0.1074
75.00002.1659-0.1101
80.00001.6146-0.1088
85.00001.0841-0.1018
90.00000.6047-0.0884
95.00000.2160-0.0648
100.00000.0000-0.0013
L.E. radius = 0.721 percent chord

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NACA Profile 63-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.98370.9453
0.75001.19380.7547
1.25001.51810.5663
2.50002.09800.3964
5.00002.92560.2817
7.50003.54320.2186
10.00004.03860.1800
15.00004.80030.1280
20.00005.34310.0899
25.00005.71150.0585
30.00005.93040.0295
35.00006.0005-0.0008
40.00005.9220-0.0299
45.00005.7051-0.0557
50.00005.3698-0.0777
55.00004.9354-0.0957
60.00004.4206-0.1100
65.00003.8398-0.1220
70.00003.2113-0.1294
75.00002.5567-0.1319
80.00001.9002-0.1298
85.00001.2724-0.1201
90.00000.7076-0.1038
95.00000.2521-0.0759
100.0000-0.0000-0.0016
L.E. radius = 1.004 percent chord

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NACA Profile 63-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.20391.1730
0.75001.46530.9414
1.25001.87120.7107
2.50002.60180.5010
5.00003.64880.3561
7.50004.42850.2757
10.00005.05310.2266
15.00006.01210.1606
20.00006.69340.1128
25.00007.15320.0728
30.00007.42220.0348
35.00007.4992-0.0039
40.00007.3860-0.0416
45.00007.0988-0.0733
50.00006.6640-0.0996
55.00006.1072-0.1219
60.00005.4529-0.1398
65.00004.7194-0.1530
70.00003.9318-0.1606
75.00003.1175-0.1636
80.00002.3072-0.1597
85.00001.5389-0.1474
90.00000.8524-0.1262
95.00000.3026-0.0912
100.00000.0000-0.0019
L.E. radius = 1.473 percent chord

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NACA Profile 63-018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.40501.3929
0.75001.71661.1259
1.25002.20410.8562
2.50003.08840.6086
5.00004.36200.4329
7.50005.30860.3344
10.00006.06570.2743
15.00007.22590.1941
20.00008.04780.1360
25.00008.59920.0864
30.00008.91620.0397
35.00008.9961-0.0075
40.00008.8419-0.0525
45.00008.4783-0.0910
50.00007.9382-0.1241
55.00007.2546-0.1488
60.00006.4567-0.1693
65.00005.5689-0.1843
70.00004.6226-0.1935
75.00003.6506-0.1945
80.00002.6909-0.1873
85.00001.7880-0.1713
90.00000.9866-0.1464
95.00000.3492-0.1050
100.00000.0000-0.0023
L.E. radius = 1.952 percent chord

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NACA Profile 63-021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.58291.6012
0.75001.94301.3061
1.25002.51161.0024
2.50003.55250.7196
5.00005.06150.5128
7.50006.18100.3948
10.00007.07440.3235
15.00008.44100.2287
20.00009.40590.1594
25.000010.04930.1001
30.000010.41290.0450
35.000010.4911-0.0135
40.000010.2906-0.0657
45.00009.8438-0.1114
50.00009.1921-0.1479
55.00008.3775-0.1766
60.00007.4333-0.1995
65.00006.3890-0.2162
70.00005.2835-0.2240
75.00004.1572-0.2241
80.00003.0531-0.2151
85.00002.0217-0.1959
90.00001.1116-0.1658
95.00000.3924-0.1179
100.0000-0.0000-0.0026
L.E. radius = 2.399 percent chord

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NACA Profile 63A006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.50660.4616
0.75000.60820.3643
1.25000.76630.2796
2.50001.05340.1951
5.00001.45360.1354
7.50001.75300.1067
10.00001.99440.0882
15.00002.36640.0625
20.00002.63430.0448
25.00002.82240.0310
30.00002.94330.0178
35.00002.99560.0038
40.00002.9838-0.0090
45.00002.9103-0.0207
50.00002.7816-0.0306
55.00002.6048-0.0399
60.00002.3870-0.0470
65.00002.1341-0.0531
70.00001.8528-0.0588
75.00001.5523-0.0613
80.00001.2455-0.0618
85.00000.9382-0.0614
90.00000.6308-0.0623
95.00000.3187-0.0573
100.0000-0.0000-2.3633
L.E. radius = 0.279 percent chord

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NACA Profile 63A008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.66870.6119
0.75000.80370.4856
1.25001.01520.3748
2.50001.40040.2618
5.00001.93720.1816
7.50002.33840.1429
10.00002.66170.1181
15.00003.15950.0836
20.00003.51750.0598
25.00003.76840.0409
30.00003.92860.0231
35.00003.99570.0049
40.00003.9766-0.0121
45.00003.8745-0.0282
50.00003.6988-0.0422
55.00003.4594-0.0539
60.00003.1662-0.0639
65.00002.8271-0.0718
70.00002.4509-0.0782
75.00002.0514-0.0815
80.00001.6455-0.0812
85.00001.2391-0.0811
90.00000.8325-0.0827
95.00000.4216-0.0748
100.0000-0.0000-3.8447
L.E. radius = 0.483 percent chord

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NACA Profile 63A010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.82450.7591
0.75000.99250.6064
1.25001.25770.4713
2.50001.74250.3298
5.00002.41840.2284
7.50002.92280.1795
10.00003.32900.1482
15.00003.95370.1051
20.00004.40250.0750
25.00004.71620.0508
30.00004.91540.0279
35.00004.99630.0054
40.00004.9683-0.0158
45.00004.8355-0.0363
50.00004.6109-0.0533
55.00004.3073-0.0678
60.00003.9371-0.0805
65.00003.5109-0.0908
70.00003.0403-0.0970
75.00002.5423-0.1009
80.00002.0387-0.1006
85.00001.5347-0.1005
90.00001.0302-0.1032
95.00000.5233-0.0916
100.0000-0.0000-6.1087
L.E. radius = 0.724 percent chord

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NACA Profile 63A012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.97230.9023
0.75001.17250.7259
1.25001.49190.5693
2.50002.07820.3991
5.00002.89570.2760
7.50003.50510.2167
10.00003.99530.1786
15.00004.74840.1270
20.00005.28870.0903
25.00005.66570.0609
30.00005.90320.0322
35.00005.99710.0052
40.00005.9588-0.0204
45.00005.7934-0.0446
50.00005.5183-0.0645
55.00005.1489-0.0820
60.00004.7004-0.0968
65.00004.1862-0.1084
70.00003.6212-0.1167
75.00003.0256-0.1197
80.00002.4255-0.1200
85.00001.8254-0.1197
90.00001.2240-0.1235
95.00000.6238-0.1077
100.0000-0.0000-9.4867
L.E. radius = 0.990 percent chord

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NACA Profile 63A015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.17541.1071
0.75001.42210.9004
1.25001.82280.7195
2.50002.56570.5062
5.00003.60180.3494
7.50004.37230.2738
10.00004.99120.2249
15.00005.94040.1606
20.00006.61970.1138
25.00007.09240.0771
30.00007.38670.0391
35.00007.49830.0050
40.00007.4417-0.0279
45.00007.2244-0.0577
50.00006.8703-0.0838
55.00006.3998-0.1043
60.00005.8320-0.1214
65.00005.1845-0.1363
70.00004.4772-0.1460
75.00003.7376-0.1487
80.00002.9946-0.1491
85.00002.2529-0.1479
90.00001.5083-0.1531
95.00000.7730-0.1309
100.0000-0.0000-19.2242
L.E. radius = 1.406 percent chord

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NACA Profile 64-006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.49180.4693
0.75000.59540.3689
1.25000.75170.2693
2.50001.02160.1822
5.00001.40220.1300
7.50001.68970.1025
10.00001.92370.0860
15.00002.29310.0635
20.00002.56750.0471
25.00002.76750.0332
30.00002.90200.0207
35.00002.97610.0090
40.00002.9855-0.0061
45.00002.9133-0.0223
50.00002.7685-0.0348
55.00002.5688-0.0448
60.00002.3244-0.0528
65.00002.0441-0.0593
70.00001.7359-0.0640
75.00001.4078-0.0671
80.00001.0697-0.0678
85.00000.7351-0.0654
90.00000.4226-0.0589
95.00000.1568-0.0458
100.00000.0000-0.0010
L.E. radius = 0.249 percent chord

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NACA Profile 64-008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.65500.6242
0.75000.79280.4906
1.25001.00080.3590
2.50001.36150.2441
5.00001.87190.1743
7.50002.25700.1372
10.00002.57060.1152
15.00003.06540.0850
20.00003.43250.0630
25.00003.69950.0443
30.00003.87810.0271
35.00003.97540.0114
40.00003.9831-0.0091
45.00003.8794-0.0313
50.00003.6797-0.0475
55.00003.4077-0.0606
60.00003.0773-0.0710
65.00002.7001-0.0793
70.00002.2875-0.0854
75.00001.8501-0.0888
80.00001.4015-0.0898
85.00000.9601-0.0861
90.00000.5499-0.0774
95.00000.2032-0.0597
100.0000-0.0000-0.0013
L.E. radius = 0.446 percent chord

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NACA Profile 64-009
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.73600.7010
0.75000.89070.5510
1.25001.12450.4036
2.50001.53060.2752
5.00002.10640.1966
7.50002.54080.1547
10.00002.89460.1299
15.00003.45250.0958
20.00003.86610.0709
25.00004.16680.0498
30.00004.36730.0304
35.00004.47580.0125
40.00004.4817-0.0110
45.00004.3608-0.0361
50.00004.1326-0.0542
55.00003.8234-0.0687
60.00003.4492-0.0804
65.00003.0232-0.0893
70.00002.5581-0.0961
75.00002.0661-0.0999
80.00001.5628-0.1006
85.00001.0689-0.0962
90.00000.6112-0.0861
95.00000.2254-0.0663
100.00000.0000-0.0014
L.E. radius = 0.566 percent chord

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NACA Profile 64-010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.81650.7772
0.75000.98800.6110
1.25001.24740.4482
2.50001.69910.3065
5.00002.34060.2191
7.50002.82460.1723
10.00003.21860.1446
15.00003.84000.1067
20.00004.30040.0789
25.00004.63460.0553
30.00004.85700.0337
35.00004.97660.0135
40.00004.9800-0.0133
45.00004.8409-0.0410
50.00004.5834-0.0610
55.00004.2365-0.0771
60.00003.8181-0.0899
65.00003.3429-0.0994
70.00002.8252-0.1068
75.00002.2788-0.1112
80.00001.7211-0.1112
85.00001.1754-0.1061
90.00000.6710-0.0945
95.00000.2470-0.0728
100.0000-0.0000-0.0016
L.E. radius = 0.701 percent chord

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NACA Profile 64-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.97550.9276
0.75001.18020.7295
1.25001.49040.5368
2.50002.03310.3695
5.00002.80750.2645
7.50003.39140.2079
10.00003.86680.1743
15.00004.61590.1285
20.00005.17040.0950
25.00005.57210.0664
30.00005.83810.0407
35.00005.97890.0151
40.00005.9752-0.0186
45.00005.7972-0.0511
50.00005.4788-0.0752
55.00005.0545-0.0942
60.00004.5462-0.1092
65.00003.9721-0.1201
70.00003.3488-0.1284
75.00002.6938-0.1331
80.00002.0289-0.1323
85.00001.3815-0.1254
90.00000.7862-0.1110
95.00000.2883-0.0851
100.00000.0000-0.0019
L.E. radius = 1.004 percent chord

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NACA Profile 64-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.20771.1469
0.75001.46080.9030
1.25001.84580.6681
2.50002.52500.4649
5.00003.50190.3337
7.50004.23820.2621
10.00004.83740.2195
15.00005.78080.1616
20.00006.47800.1192
25.00006.98140.0831
30.00007.31250.0505
35.00007.48320.0171
40.00007.4629-0.0275
45.00007.2202-0.0682
50.00006.8050-0.0971
55.00006.2609-0.1195
60.00005.6145-0.1376
65.00004.8898-0.1513
70.00004.1079-0.1608
75.00003.2917-0.1647
80.00002.4688-0.1633
85.00001.6740-0.1536
90.00000.9484-0.1354
95.00000.3459-0.1023
100.00000.0000-0.0023
L.E. radius = 1.556 percent chord

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NACA Profile 64-018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.43001.3568
0.75001.72971.0699
1.25002.18720.7969
2.50003.00260.5615
5.00004.18620.4047
7.50005.07840.3174
10.00005.80410.2656
15.00006.94530.1952
20.00007.78730.1436
25.00008.39330.0998
30.00008.78910.0591
35.00008.98730.0182
40.00008.9432-0.0372
45.00008.6277-0.0862
50.00008.1107-0.1195
55.00007.4420-0.1463
60.00006.6541-0.1674
65.00005.7770-0.1830
70.00004.8364-0.1924
75.00003.8609-0.1964
80.00002.8841-0.1926
85.00001.9477-0.1802
90.00001.0988-0.1572
95.00000.3988-0.1186
100.00000.0000-0.0027
L.E. radius = 2.206 percent chord

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NACA Profile 64-021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.63991.5554
0.75001.98391.2290
1.25002.51130.9224
2.50003.46170.6591
5.00004.85720.4776
7.50005.90940.3742
10.00006.76450.3128
15.00008.10780.2295
20.00009.09710.1683
25.00009.80680.1163
30.000010.26690.0680
35.000010.49030.0180
40.000010.4155-0.0487
45.000010.0198-0.1044
50.00009.3950-0.1436
55.00008.5971-0.1746
60.00007.6648-0.1972
65.00006.6334-0.2140
70.00005.5351-0.2243
75.00004.4025-0.2274
80.00003.2762-0.2217
85.00002.2043-0.2054
90.00001.2386-0.1783
95.00000.4474-0.1335
100.0000-0.0000-0.0031
L.E. radius = 2.937 percent chord

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NACA Profile 64A006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.50150.4570
0.75000.60180.3569
1.25000.75430.2661
2.50001.02670.1843
5.00001.40410.1274
7.50001.68700.1018
10.00001.92080.0858
15.00002.28640.0627
20.00002.55920.0469
25.00002.75920.0333
30.00002.89670.0214
35.00002.97670.0103
40.00002.9978-0.0027
45.00002.9439-0.0179
50.00002.8245-0.0295
55.00002.6522-0.0391
60.00002.4371-0.0470
65.00002.1857-0.0537
70.00001.9034-0.0592
75.00001.5997-0.0621
80.00001.2850-0.0633
85.00000.9678-0.0629
90.00000.6512-0.0650
95.00000.3290-0.0595
100.0000-0.0000-2.3550
L.E. radius = 0.277 percent chord

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NACA Profile 64A008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.66140.6055
0.75000.79450.4749
1.25000.99810.3560
2.50001.36310.2471
5.00001.86920.1706
7.50002.24840.1364
10.00002.56150.1148
15.00003.05080.0839
20.00003.41570.0628
25.00003.68260.0443
30.00003.86570.0288
35.00003.97150.0139
40.00003.9965-0.0046
45.00003.9194-0.0249
50.00003.7558-0.0399
55.00003.5222-0.0528
60.00003.2325-0.0630
65.00002.8951-0.0719
70.00002.5177-0.0787
75.00002.1138-0.0825
80.00001.6967-0.0840
85.00001.2777-0.0831
90.00000.8587-0.0858
95.00000.4349-0.0777
100.0000-0.0000-3.8241
L.E. radius = 0.485 percent chord

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NACA Profile 64A010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.81480.7509
0.75000.98030.5920
1.25001.23510.4467
2.50001.69380.3110
5.00002.33070.2145
7.50002.80750.1713
10.00003.20100.1441
15.00003.81520.1053
20.00004.27310.0788
25.00004.60730.0555
30.00004.83610.0361
35.00004.96720.0173
40.00004.9946-0.0073
45.00004.8920-0.0321
50.00004.6822-0.0509
55.00004.3855-0.0664
60.00004.0198-0.0792
65.00003.5954-0.0903
70.00003.1228-0.0982
75.00002.6192-0.1027
80.00002.1010-0.1042
85.00001.5817-0.1040
90.00001.0620-0.1061
95.00000.5393-0.0950
100.0000-0.0000-6.0681
L.E. radius = 0.735 percent chord

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NACA Profile 64A012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.95990.8924
0.75001.15710.7078
1.25001.46320.5383
2.50002.01730.3761
5.00002.78740.2592
7.50003.36330.2068
10.00003.83830.1738
15.00004.57900.1269
20.00005.13090.0950
25.00005.53290.0667
30.00005.80770.0435
35.00005.96380.0201
40.00005.9916-0.0106
45.00005.8615-0.0399
50.00005.6034-0.0627
55.00005.2423-0.0808
60.00004.7994-0.0956
65.00004.2870-0.1089
70.00003.7191-0.1176
75.00003.1163-0.1230
80.00002.4983-0.1240
85.00001.8801-0.1237
90.00001.2613-0.1263
95.00000.6424-0.1117
100.0000-0.0000-9.4336
L.E. radius = 1.021 percent chord

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NACA Profile 64A015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.15861.0949
0.75001.40150.8775
1.25001.78440.6772
2.50002.48450.4765
5.00003.46010.3280
7.50004.18830.2613
10.00004.78820.2192
15.00005.72230.1600
20.00006.41740.1193
25.00006.92240.0840
30.00007.26680.0542
35.00007.45970.0235
40.00007.4852-0.0161
45.00007.3100-0.0527
50.00006.9761-0.0806
55.00006.5154-0.1029
60.00005.9546-0.1214
65.00005.3091-0.1356
70.00004.5981-0.1470
75.00003.8476-0.1525
80.00003.0824-0.1531
85.00002.3189-0.1510
90.00001.5532-0.1567
95.00000.7951-0.1356
100.0000-0.0000-19.1581
L.E. radius = 1.481 percent chord

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NACA Profile 65-006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.46800.4374
0.75000.56390.3385
1.25000.70520.2420
2.50000.95200.1691
5.00001.31100.1245
7.50001.59050.1013
10.00001.82430.0862
15.00002.19770.0646
20.00002.48140.0494
25.00002.69570.0368
30.00002.85100.0255
35.00002.95050.0144
40.00002.99710.0035
45.00002.9818-0.0099
50.00002.8978-0.0238
55.00002.7413-0.0383
60.00002.5198-0.0498
65.00002.2475-0.0585
70.00001.9345-0.0665
75.00001.5921-0.0704
80.00001.2311-0.0734
85.00000.8633-0.0729
90.00000.5069-0.0686
95.00000.1892-0.0558
100.00000.0000-0.0008
L.E. radius = 0.230 percent chord

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NACA Profile 65-008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.62050.5804
0.75000.74770.4492
1.25000.93550.3225
2.50001.26530.2265
5.00001.74640.1668
7.50002.12040.1355
10.00002.43330.1153
15.00002.93270.0864
20.00003.31200.0660
25.00003.59810.0492
30.00003.80500.0337
35.00003.93700.0192
40.00003.99750.0042
45.00003.9733-0.0140
50.00003.8556-0.0332
55.00003.6401-0.0524
60.00003.3388-0.0671
65.00002.9714-0.0792
70.00002.5508-0.0882
75.00002.0943-0.0937
80.00001.6145-0.0974
85.00001.1286-0.0962
90.00000.6602-0.0902
95.00000.2463-0.0723
100.00000.0000-0.0011
L.E. radius = 0.406 percent chord

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NACA Profile 65-009
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.69550.6511
0.75000.83830.5039
1.25001.04920.3626
2.50001.42060.2554
5.00001.96320.1881
7.50002.38500.1528
10.00002.73770.1299
15.00003.30040.0973
20.00003.72760.0743
25.00004.04990.0554
30.00004.28260.0378
35.00004.43070.0217
40.00004.49780.0045
45.00004.4684-0.0162
50.00004.3329-0.0382
55.00004.0865-0.0596
60.00003.7443-0.0761
65.00003.3284-0.0897
70.00002.8539-0.0989
75.00002.3402-0.1053
80.00001.8014-0.1094
85.00001.2573-0.1078
90.00000.7342-0.1005
95.00000.2739-0.0802
100.00000.0000-0.0012
L.E. radius = 0.510 percent chord

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NACA Profile 65-010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.76970.7211
0.75000.92780.5583
1.25001.16160.4026
2.50001.57470.2844
5.00002.17940.2096
7.50002.64910.1701
10.00003.04180.1446
15.00003.66810.1083
20.00004.14350.0827
25.00004.50200.0616
30.00004.76050.0418
35.00004.92470.0240
40.00004.99810.0047
45.00004.9631-0.0184
50.00004.8089-0.0434
55.00004.5309-0.0670
60.00004.1471-0.0853
65.00003.6823-0.1000
70.00003.1537-0.1102
75.00002.5828-0.1172
80.00001.9850-0.1213
85.00001.3834-0.1191
90.00000.8064-0.1105
95.00000.3010-0.0878
100.00000.0000-0.0014
L.E. radius = 0.624 percent chord

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NACA Profile 65-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.91470.8590
0.75001.10310.6655
1.25001.38240.4823
2.50001.87920.3430
5.00002.60910.2529
7.50003.17560.2052
10.00003.64900.1742
15.00004.40350.1304
20.00004.97580.0995
25.00005.40700.0741
30.00005.71720.0500
35.00005.91350.0287
40.00005.99900.0048
45.00005.9512-0.0235
50.00005.7573-0.0545
55.00005.4137-0.0821
60.00004.9445-0.1044
65.00004.3806-0.1207
70.00003.7427-0.1342
75.00003.0576-0.1408
80.00002.3433-0.1440
85.00001.6282-0.1411
90.00000.9461-0.1298
95.00000.3533-0.1025
100.00000.0000-0.0016
L.E. radius = 0.876 percent chord

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NACA Profile 65-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.12221.0592
0.75001.35480.8223
1.25001.70120.6006
2.50002.32400.4323
5.00003.24540.3192
7.50003.95980.2586
10.00004.55620.2194
15.00005.50550.1640
20.00006.22490.1250
25.00006.76620.0928
30.00007.15430.0626
35.00007.39850.0352
40.00007.50040.0041
45.00007.4295-0.0333
50.00007.1704-0.0709
55.00006.7225-0.1065
60.00006.1200-0.1335
65.00005.4045-0.1532
70.00004.6011-0.1664
75.00003.7453-0.1752
80.00002.8588-0.1780
85.00001.9777-0.1732
90.00001.1444-0.1576
95.00000.4281-0.1237
100.0000-0.0000-0.0020
L.E. radius = 1.299 percent chord

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NACA Profile 65-018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.31521.2496
0.75001.59000.9735
1.25002.00180.7165
2.50002.75070.5233
5.00003.86870.3873
7.50004.73490.3133
10.00005.45700.2655
15.00006.60500.1983
20.00007.47380.1508
25.00008.12670.1117
30.00008.59340.0756
35.00008.88540.0416
40.00009.00160.0028
45.00008.9025-0.0429
50.00008.5722-0.0897
55.00008.0118-0.1323
60.00007.2713-0.1622
65.00006.4011-0.1846
70.00005.4316-0.1999
75.00004.4047-0.2097
80.00003.3493-0.2107
85.00002.3072-0.2042
90.00001.3305-0.1838
95.00000.4987-0.1440
100.00000.0000-0.0024
L.E. radius = 1.753 percent chord

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NACA Profile 65-021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.49091.4278
0.75001.80581.1178
1.25002.28050.8291
2.50003.15510.6160
5.00004.47550.4575
7.50005.49800.3695
10.00006.34930.3127
15.00007.70050.2333
20.00008.72160.1771
25.00009.48800.1307
30.000010.03440.0883
35.000010.37400.0480
40.000010.50250.0008
45.000010.3711-0.0524
50.00009.9609-0.1119
55.00009.2823-0.1578
60.00008.3992-0.1915
65.00007.3699-0.2198
70.00006.2331-0.2360
75.00005.0374-0.2428
80.00003.8165-0.2435
85.00002.6181-0.2338
90.00001.5056-0.2083
95.00000.5655-0.1630
100.0000-0.0000-0.0028
L.E. radius = 2.210 percent chord

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NACA Profile 65A006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.47850.4384
0.75000.57570.3509
1.25000.72790.2661
2.50000.98900.1677
5.00001.31990.1156
7.50001.59580.1025
10.00001.82820.0852
15.00002.19620.0637
20.00002.47540.0484
25.00002.68720.0362
30.00002.84150.0259
35.00002.94390.0157
40.00002.99490.0049
45.00002.9908-0.0064
50.00002.9247-0.0196
55.00002.7931-0.0326
60.00002.6014-0.0437
65.00002.3631-0.0519
70.00002.0859-0.0591
75.00001.7752-0.0651
80.00001.4389-0.0692
85.00001.0858-0.0713
90.00000.7307-0.0720
95.00000.3693-0.0677
100.0000-0.0000-2.3274
L.E. radius = 0.253 percent chord

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NACA Profile 65A008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.63020.5824
0.75000.75970.4686
1.25000.96330.3560
2.50001.31240.2240
5.00001.75560.1552
7.50002.12560.1371
10.00002.43650.1140
15.00002.92890.0852
20.00003.30220.0648
25.00003.58510.0484
30.00003.79100.0344
35.00003.92730.0208
40.00003.99420.0063
45.00003.9866-0.0093
50.00003.8946-0.0271
55.00003.7143-0.0447
60.00003.4545-0.0587
65.00003.1338-0.0697
70.00002.7623-0.0792
75.00002.3473-0.0868
80.00001.8997-0.0927
85.00001.4320-0.0937
90.00000.9627-0.0957
95.00000.4873-0.0886
100.0000-0.0000-3.7972
L.E. radius = 0.437 percent chord

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NACA Profile 65A010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.77530.7243
0.75000.93680.5866
1.25001.19230.4471
2.50001.63030.2809
5.00002.18720.1953
7.50002.65250.1721
10.00003.04290.1432
15.00003.66070.1069
20.00004.12880.0812
25.00004.48340.0608
30.00004.74130.0427
35.00004.91140.0256
40.00004.99380.0075
45.00004.9816-0.0126
50.00004.8618-0.0353
55.00004.6306-0.0572
60.00004.3010-0.0739
65.00003.8966-0.0876
70.00003.4298-0.0994
75.00002.9104-0.1081
80.00002.3518-0.1149
85.00001.7714-0.1158
90.00001.1893-0.1188
95.00000.6033-0.1089
100.0000-0.0000-6.0658
L.E. radius = 0.654 percent chord

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NACA Profile 65A012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.91200.8634
0.75001.10520.7046
1.25001.41330.5398
2.50001.94150.3385
5.00002.61340.2360
7.50003.17550.2077
10.00003.64650.1726
15.00004.39110.1288
20.00004.95500.0979
25.00005.38190.0733
30.00005.69200.0512
35.00005.89610.0304
40.00005.99370.0087
45.00005.9758-0.0163
50.00005.8264-0.0435
55.00005.5421-0.0698
60.00005.1411-0.0896
65.00004.6518-0.1054
70.00004.0889-0.1190
75.00003.4650-0.1291
80.00002.7959-0.1367
85.00002.1042-0.1379
90.00001.4110-0.1410
95.00000.7173-0.1284
100.0000-0.0000-9.4742
L.E. radius = 0.891 percent chord

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NACA Profile 65A015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.09791.0636
0.75001.33750.8799
1.25001.72560.6825
2.50002.39210.4268
5.00003.23990.2980
7.50003.95010.2624
10.00004.54440.2177
15.00005.48260.1622
20.00006.19220.1232
25.00006.72910.0925
30.00007.11850.0639
35.00007.37380.0375
40.00007.49380.0099
45.00007.4655-0.0224
50.00007.2686-0.0560
55.00006.9009-0.0889
60.00006.3898-0.1141
65.00005.7712-0.1327
70.00005.0631-0.1489
75.00004.2819-0.1620
80.00003.4477-0.1710
85.00002.5920-0.1710
90.00001.7352-0.1742
95.00000.8854-0.1559
100.0000-0.0000-19.0341
L.E. radius = 1.251 percent chord

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NACA Profile 66-006
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.45920.4300
0.75000.55290.3295
1.25000.68960.2309
2.50000.91740.1553
5.00001.25620.1199
7.50001.52550.0975
10.00001.75110.0840
15.00002.11870.0641
20.00002.39990.0492
25.00002.61710.0378
30.00002.78100.0279
35.00002.89730.0190
40.00002.96960.0100
45.00002.99860.0013
50.00002.9839-0.0074
55.00002.9229-0.0172
60.00002.8083-0.0296
65.00002.6116-0.0504
70.00002.3136-0.0676
75.00001.9511-0.0773
80.00001.5436-0.0853
85.00001.1066-0.0884
90.00000.6681-0.0862
95.00000.2625-0.0732
100.00000.0000-0.0009
L.E. radius = 0.218 percent chord

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NACA Profile 66-008
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.60980.5690
0.75000.73380.4357
1.25000.91470.3062
2.50001.21820.2079
5.00001.67190.1605
7.50002.03200.1303
10.00002.33370.1123
15.00002.82480.0857
20.00003.20030.0658
25.00003.49030.0505
30.00003.70910.0372
35.00003.86420.0253
40.00003.96040.0131
45.00003.99840.0016
50.00003.9777-0.0102
55.00003.8946-0.0236
60.00003.7378-0.0408
65.00003.4657-0.0694
70.00003.0592-0.0915
75.00002.5714-0.1039
80.00002.0258-0.1137
85.00001.4453-0.1169
90.00000.8674-0.1131
95.00000.3381-0.0952
100.00000.0000-0.0011
L.E. radius = 0.389 percent chord

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NACA Profile 66-009
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.68430.6373
0.75000.82320.4878
1.25001.02590.3435
2.50001.36720.2343
5.00001.87870.1809
7.50002.28450.1468
10.00002.62440.1266
15.00003.17760.0965
20.00003.60040.0741
25.00003.92700.0569
30.00004.17330.0419
35.00004.34780.0284
40.00004.45580.0147
45.00004.49830.0018
50.00004.4745-0.0117
55.00004.3799-0.0268
60.00004.2012-0.0468
65.00003.8895-0.0789
70.00003.4272-0.1034
75.00002.8760-0.1172
80.00002.2609-0.1280
85.00001.6093-0.1309
90.00000.9631-0.1260
95.00000.3739-0.1057
100.00000.0000-0.0013
L.E. radius = 0.492 percent chord

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NACA Profile 66-010
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.75830.7046
0.75000.91160.5393
1.25001.13600.3805
2.50001.51500.2609
5.00002.08460.2014
7.50002.53640.1634
10.00002.91460.1408
15.00003.53010.1073
20.00004.00030.0824
25.00004.36350.0634
30.00004.63740.0466
35.00004.83140.0315
40.00004.95130.0163
45.00004.99830.0019
50.00004.9712-0.0132
55.00004.8649-0.0300
60.00004.6636-0.0530
65.00004.3111-0.0887
70.00003.7920-0.1154
75.00003.1768-0.1305
80.00002.4922-0.1423
85.00001.7699-0.1449
90.00001.0561-0.1388
95.00000.4084-0.1158
100.00000.0000-0.0014
L.E. radius = 0.607 percent chord

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NACA Profile 66-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.90380.8364
0.75001.08590.6399
1.25001.35250.4534
2.50001.80670.3142
5.00002.49360.2428
7.50003.03780.1968
10.00003.49330.1696
15.00004.23400.1292
20.00004.79960.0991
25.00005.23640.0763
30.00005.56560.0560
35.00005.79870.0376
40.00005.94240.0197
45.00005.99810.0022
50.00005.9642-0.0163
55.00005.8339-0.0366
60.00005.5857-0.0659
65.00005.1477-0.1097
70.00004.5122-0.1398
75.00003.7677-0.1571
80.00002.9432-0.1706
85.00002.0807-0.1723
90.00001.2346-0.1643
95.00000.4738-0.1352
100.00000.0000-0.0016
L.E. radius = 0.870 percent chord

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NACA Profile 66-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.11571.0250
0.75001.33860.7843
1.25001.66660.5600
2.50002.23260.3948
5.00003.09800.3059
7.50003.78310.2476
10.00004.35580.2132
15.00005.28630.1622
20.00005.99630.1245
25.00006.54440.0959
30.00006.95730.0701
35.00007.24940.0467
40.00007.42910.0251
45.00007.49790.0027
50.00007.4531-0.0208
55.00007.2853-0.0468
60.00006.9613-0.0867
65.00006.3846-0.1441
70.00005.5686-0.1781
75.00004.6263-0.1992
80.00003.5911-0.2134
85.00002.5222-0.2125
90.00001.4839-0.2004
95.00000.5635-0.1619
100.00000.0000-0.0020
L.E. radius = 1.345 percent chord

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NACA Profile 66-018
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.31791.2013
0.75001.57910.9195
1.25001.96520.6626
2.50002.64130.4758
5.00003.68860.3704
7.50004.51760.2993
10.00005.20970.2575
15.00006.33310.1957
20.00007.18930.1502
25.00007.85020.1157
30.00008.34770.0844
35.00008.69950.0561
40.00008.91590.0305
45.00008.99770.0031
50.00008.9415-0.0250
55.00008.7343-0.0579
60.00008.3274-0.1101
65.00007.5989-0.1800
70.00006.5958-0.2169
75.00005.4522-0.2400
80.00004.2058-0.2540
85.00002.9351-0.2516
90.00001.7130-0.2334
95.00000.6441-0.1860
100.00000.0000-0.0023
L.E. radius = 1.905 percent chord

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NACA Profile 66-021
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.50861.3639
0.75001.80511.0446
1.25002.24570.7602
2.50003.02940.5567
5.00004.26240.4366
7.50005.23890.3522
10.00006.05290.3027
15.00007.37260.2298
20.00008.37730.1763
25.00009.15270.1359
30.00009.73610.0989
35.000010.14870.0661
40.000010.40250.0355
45.000010.49760.0034
50.000010.4297-0.0298
55.000010.1809-0.0700
60.00009.6829-0.1354
65.00008.7908-0.2154
70.00007.5948-0.2551
75.00006.2451-0.2838
80.00004.7886-0.2961
85.00003.3208-0.2893
90.00001.9235-0.2653
95.00000.7166-0.2083
100.00000.0000-0.0026
L.E. radius = 2.537 percent chord

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NACA Profile 67-012
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50000.95040.8500
0.75001.13720.6774
1.25001.43550.5217
2.50001.94120.3300
5.00002.61740.2313
7.50003.13770.1867
10.00003.56170.1550
15.00004.23790.1179
20.00004.76060.0919
25.00005.16980.0717
30.00005.48780.0550
35.00005.72710.0399
40.00005.88910.0251
45.00005.98040.0111
50.00005.9972-0.0042
55.00005.9368-0.0206
60.00005.7860-0.0404
65.00005.5292-0.0634
70.00005.1376-0.0965
75.00004.5357-0.1462
80.00003.6903-0.1849
85.00002.7246-0.2018
90.00001.6745-0.2137
95.00000.6565-0.1842
100.0000-0.0000-0.0030
L.E. radius = 1.012 percent chord

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NACA Profile 67-015
(Stations and ordinates given
in per cent of airfoil chord)
xydy/dx
0.00000.0000********
0.50001.16491.0305
0.75001.39220.8322
1.25001.76260.6506
2.50002.39400.4134
5.00003.24430.2913
7.50003.89950.2350
10.00004.43290.1949
15.00005.28290.1481
20.00005.93980.1155
25.00006.45390.0902
30.00006.85390.0696
35.00007.15500.0501
40.00007.35930.0317
45.00007.47500.0143
50.00007.4969-0.0046
55.00007.4214-0.0262
60.00007.2309-0.0513
65.00006.9052-0.0805
70.00006.4023-0.1249
75.00005.6213-0.1886
80.00004.5401-0.2336
85.00003.3271-0.2539
90.00002.0210-0.2618
95.00000.7880-0.2209
100.00000.0000-0.0037
L.E. radius = 1.570 percent chord

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