Appendix III - 6A-Series Sections

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Only a few of these 6A sections were published in the book. I have added those that I know were used on a production airplane.
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63A-series cambered airfoils

63A112	63A210	63A412	63A415
63A418	63A421	63A615

64- and 64A-series cambered airfoils

64A204	64A106	64A210	64A410
64A212	64A412	64A612	64A114
64A215	64A415	64A218	64A221

65- and 65A-series cambered airfoils

65A112	65A210	65A212	65A412
65A215	65A415	65A615	65A418
65A421

NACA 63A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.9481	0.5000	-0.7113
0.7500	1.1304	0.7500	-0.8649
1.2500	1.4288	1.2500	-1.0953
2.5000	1.9946	2.5000	-1.4974
5.0000	2.8123	5.0000	-2.0319
7.5000	3.4372	7.5000	-2.4155
10.0000	3.9478	10.0000	-2.7156
15.0000	4.7494	15.0000	-3.1612
20.0000	5.3430	20.0000	-3.4651
25.0000	5.7736	25.0000	-3.6605
30.0000	6.0671	30.0000	-3.7650
35.0000	6.2210	35.0000	-3.7725
40.0000	6.2466	40.0000	-3.6905
45.0000	6.1487	45.0000	-3.5224
50.0000	5.9411	50.0000	-3.2810
55.0000	5.6340	55.0000	-2.9804
60.0000	5.2413	60.0000	-2.6335
65.0000	4.7693	65.0000	-2.2528
70.0000	4.2280	70.0000	-1.8532
75.0000	3.6289	75.0000	-1.4568
80.0000	2.9823	80.0000	-1.0972
85.0000	2.2643	85.0000	-0.8077
90.0000	1.5264	90.0000	-0.5357
95.0000	0.7724	95.0000	-0.2760
100.0000	0.0155	100.0000	-0.0155
L.E. radius = 0.724 percent c
slope of mean line at LE = 0.0951

NACA 63A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4220	0.8771	0.5780	-0.7647
0.6628	1.0696	0.8372	-0.9115
1.1508	1.3748	1.3492	-1.1335
2.3838	1.9495	2.6162	-1.5276
4.8689	2.7755	5.1311	-2.0543
7.3635	3.4065	7.6365	-2.4338
9.8628	3.9222	10.1372	-2.7302
14.8693	4.7319	15.1307	-3.1705
19.8816	5.3311	20.1184	-3.4709
24.8975	5.7665	25.1025	-3.6636
29.9155	6.0632	30.0845	-3.7660
34.9351	6.2198	35.0649	-3.7720
39.9552	6.2470	40.0448	-3.6893
44.9752	6.1496	45.0248	-3.5212
49.9944	5.9411	50.0056	-3.2810
55.0121	5.6333	54.9879	-2.9810
60.0279	5.2388	59.9721	-2.6356
65.0413	4.7653	64.9587	-2.2559
70.0523	4.2224	69.9477	-1.8571
75.0613	3.6217	74.9387	-1.4613
80.0735	2.9716	79.9265	-1.1023
85.0718	2.2543	84.9282	-0.8115
90.0504	1.5192	89.9495	-0.5383
95.0256	0.7679	94.9744	-0.2775
100.0008	0.0155	99.9992	-0.0155
L.E. radius = 0.724 percent c
slope of mean line at LE = 0.0951

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NACA 63A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0435	0.5000	-0.9003
0.7500	1.2499	0.7500	-1.0978
1.2500	1.5877	1.2500	-1.3999
2.5000	2.2120	2.5000	-1.9447
5.0000	3.0982	5.0000	-2.6944
7.5000	3.7656	7.5000	-3.2455
10.0000	4.3079	10.0000	-3.6840
15.0000	5.1500	15.0000	-4.3495
20.0000	5.7607	20.0000	-4.8183
25.0000	6.1953	25.0000	-5.1367
30.0000	6.4794	30.0000	-5.3276
35.0000	6.6094	35.0000	-5.3850
40.0000	6.5976	40.0000	-5.3200
45.0000	6.4495	45.0000	-5.1371
50.0000	6.1835	50.0000	-4.8534
55.0000	5.8118	55.0000	-4.4856
60.0000	5.3531	60.0000	-4.0477
65.0000	4.8168	65.0000	-3.5557
70.0000	4.2163	70.0000	-3.0268
75.0000	3.5709	75.0000	-2.4814
80.0000	2.8978	80.0000	-1.9538
85.0000	2.1909	85.0000	-1.4601
90.0000	1.4740	90.0000	-0.9765
95.0000	0.7490	95.0000	-0.4991
100.0000	0.0189	100.0000	-0.0189
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.0475

NACA 63A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4539	0.9968	0.5461	-0.9406
0.6985	1.2102	0.8015	-1.1311
1.1911	1.5508	1.3089	-1.4301
2.4307	2.1813	2.5693	-1.9704
4.9214	3.0748	5.0786	-2.7142
7.4181	3.7470	7.5819	-3.2607
9.9176	4.2924	10.0824	-3.6964
14.9214	5.1388	15.0786	-4.3582
19.9289	5.7537	20.0711	-4.8235
24.9384	6.1911	25.0616	-5.1397
29.9493	6.4774	30.0507	-5.3288
34.9610	6.6089	35.0390	-5.3850
39.9731	6.5981	40.0269	-5.3192
44.9852	6.4503	45.0148	-5.1361
49.9966	6.1835	50.0034	-4.8534
55.0072	5.8118	54.9928	-4.4856
60.0166	5.3512	59.9834	-4.0496
65.0246	4.8134	64.9754	-3.5587
70.0312	4.2126	69.9688	-3.0300
75.0365	3.5658	74.9635	-2.4856
80.0437	2.8924	79.9563	-1.9577
85.0427	2.1853	84.9573	-1.4639
90.0300	1.4698	89.9700	-0.9793
95.0153	0.7462	94.9847	-0.5010
100.0005	0.0189	99.9995	-0.0189
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.0475

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NACA 63A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.2647	0.5000	-0.7125
0.7500	1.4942	0.7500	-0.8825
1.2500	1.8867	1.2500	-1.1350
2.5000	2.6269	2.5000	-1.5634
5.0000	3.7192	5.0000	-2.1042
7.5000	4.5622	7.5000	-2.4761
10.0000	5.2592	10.0000	-2.7571
15.0000	6.3600	15.0000	-3.1579
20.0000	7.1822	20.0000	-3.4105
25.0000	7.7886	25.0000	-3.5530
30.0000	8.2107	30.0000	-3.6028
35.0000	8.4477	35.0000	-3.5504
40.0000	8.5152	40.0000	-3.4041
45.0000	8.4193	45.0000	-3.1678
50.0000	8.1779	50.0000	-2.8590
55.0000	7.8035	55.0000	-2.4941
60.0000	7.3107	60.0000	-2.0911
65.0000	6.7073	65.0000	-1.6673
70.0000	6.0038	70.0000	-1.2436
75.0000	5.2073	75.0000	-0.8514
80.0000	4.3224	80.0000	-0.5415
85.0000	3.2952	85.0000	-0.3696
90.0000	2.2251	90.0000	-0.2354
95.0000	1.1241	95.0000	-0.1291
100.0000	0.0188	100.0000	-0.0188
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.1902

NACA 63A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3188	1.0652	0.6812	-0.8403
0.5469	1.3122	0.9531	-0.9960
1.0170	1.7146	1.4830	-1.2321
2.2249	2.4806	2.7751	-1.6369
4.6874	3.5999	5.3126	-2.1574
7.1737	4.4623	7.8263	-2.5169
9.6716	5.1738	10.3284	-2.7897
14.6864	6.3002	15.3136	-3.1774
19.7158	7.1417	20.2842	-3.4212
24.7538	7.7632	25.2462	-3.5575
29.7972	8.1969	30.2028	-3.6027
34.8442	8.4429	35.1558	-3.5472
39.8926	8.5155	40.1074	-3.4000
44.9407	8.4213	45.0593	-3.1646
49.9866	8.1785	50.0134	-2.8583
55.0289	7.8009	54.9711	-2.4963
60.0665	7.3031	59.9335	-2.0968
65.0985	6.6944	64.9015	-1.6756
70.1246	5.9845	69.8754	-1.2540
75.1458	5.1827	74.8542	-0.8621
80.1745	4.2885	79.8255	-0.5498
85.1703	3.2600	84.8297	-0.3744
90.1196	2.1999	89.8804	-0.2382
95.0609	1.1112	94.9391	-0.1304
100.0018	0.0188	99.9982	-0.0188
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.1902

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NACA 63A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.5572	0.5000	-0.8428
0.7500	1.8292	0.7500	-1.0623
1.2500	2.2982	1.2500	-1.4026
2.5000	3.1826	2.5000	-1.9957
5.0000	4.4783	5.0000	-2.7657
7.5000	5.4738	7.5000	-3.3062
10.0000	6.2923	10.0000	-3.7230
15.0000	7.5758	15.0000	-4.3285
20.0000	8.5283	20.0000	-4.7272
25.0000	9.2247	25.0000	-4.9722
30.0000	9.6982	30.0000	-5.0833
35.0000	9.9495	35.0000	-5.0518
40.0000	9.9969	40.0000	-4.8890
45.0000	9.8492	45.0000	-4.6010
50.0000	9.5286	50.0000	-4.2117
55.0000	9.0560	55.0000	-3.7432
60.0000	8.4453	60.0000	-3.2188
65.0000	7.7108	65.0000	-2.6590
70.0000	6.8681	70.0000	-2.0921
75.0000	5.9282	75.0000	-1.5543
80.0000	4.9035	80.0000	-1.1011
85.0000	3.7366	85.0000	-0.7885
90.0000	2.5177	90.0000	-0.5129
95.0000	1.2791	95.0000	-0.2753
100.0000	0.0241	100.0000	-0.0241
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.1902

NACA 63A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2811	1.2635	0.7189	-1.0386
0.5037	1.5572	0.9963	-1.2410
0.9650	2.0434	1.5350	-1.5609
2.1601	2.9655	2.8399	-2.1217
4.6111	4.3026	5.3889	-2.8602
7.0929	5.3261	7.9071	-3.3807
9.5897	6.1671	10.4103	-3.7830
14.6077	7.4887	15.3923	-4.3659
19.6443	8.4700	20.3557	-4.7495
24.6918	9.1886	25.3082	-4.9830
29.7462	9.6794	30.2538	-5.0852
34.8052	9.9436	35.1948	-5.0479
39.8659	9.9983	40.1341	-4.8828
44.9260	9.8524	45.0740	-4.5957
49.9833	9.5302	50.0167	-4.2100
55.0359	9.0517	54.9641	-3.7471
60.0825	8.4347	59.9175	-3.2283
65.1220	7.6921	64.8780	-2.6734
70.1541	6.8400	69.8459	-2.1095
75.1801	5.8938	74.8199	-1.5731
80.2155	4.8560	79.7845	-1.1173
85.2102	3.6859	84.7898	-0.8003
90.1472	2.4821	89.8527	-0.5205
95.0755	1.2599	94.9245	-0.2791
100.0024	0.0241	99.9976	-0.0241
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.1902

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NACA 63A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.7550	0.5000	-0.7106
0.7500	2.0502	0.7500	-0.9066
1.2500	2.5457	1.2500	-1.2106
2.5000	3.5051	2.5000	-1.7270
5.0000	4.9316	5.0000	-2.3631
7.5000	6.0376	7.5000	-2.7869
10.0000	6.9520	10.0000	-3.1005
15.0000	8.4028	15.0000	-3.5317
20.0000	9.4896	20.0000	-3.7882
25.0000	10.2962	25.0000	-3.9169
30.0000	10.8563	30.0000	-3.9348
35.0000	11.1766	35.0000	-3.8304
40.0000	11.2754	40.0000	-3.6135
45.0000	11.1616	45.0000	-3.2895
50.0000	10.8579	50.0000	-2.8824
55.0000	10.3832	55.0000	-2.4152
60.0000	9.7537	60.0000	-1.9132
65.0000	8.9768	65.0000	-1.3980
70.0000	8.0646	70.0000	-0.9015
75.0000	7.0276	75.0000	-0.4662
80.0000	5.8639	80.0000	-0.1605
85.0000	4.4864	85.0000	-0.0631
90.0000	3.0287	90.0000	-0.0206
95.0000	1.5351	95.0000	-0.0295
100.0000	0.0239	100.0000	-0.0239
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.2852

NACA 63A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.1786	1.2955	0.8214	-0.9581
0.3874	1.6107	1.1126	-1.1364
0.8289	2.1371	1.6711	-1.4134
1.9957	3.1490	3.0043	-1.8833
4.4208	4.6374	5.5792	-2.4738
6.8926	5.7890	8.1074	-2.8710
9.3871	6.7423	10.6129	-3.1661
14.4132	8.2533	15.5868	-3.5692
19.4675	9.3882	20.5325	-3.8075
24.5383	10.2317	25.4617	-3.9232
29.6196	10.8226	30.3804	-3.9312
34.7079	11.1643	35.2921	-3.8208
39.7989	11.2757	40.2011	-3.6024
44.8891	11.1661	45.1109	-3.2810
49.9750	10.8602	50.0250	-2.8799
55.0539	10.3777	54.9461	-2.4208
60.1237	9.7355	59.8763	-1.9260
65.1830	8.9450	64.8170	-1.4169
70.2310	8.0193	69.7690	-0.9235
75.2697	6.9685	74.7303	-0.4876
80.3221	5.7811	79.6779	-0.1730
85.3136	4.3952	84.6864	-0.0668
90.2196	2.9637	89.7804	-0.0212
95.1125	1.5006	94.8875	-0.0293
100.0035	0.0239	99.9965	-0.0239
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.2852

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NACA 63A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.8124	0.5000	-0.9616
0.7500	2.1365	0.7500	-1.2213
1.2500	2.6889	1.2500	-1.6157
2.5000	3.7234	2.5000	-2.3864
5.0000	5.2337	5.0000	-3.3965
7.5000	6.3833	7.5000	-4.1141
10.0000	7.3247	10.0000	-4.6721
15.0000	8.7955	15.0000	-5.4915
20.0000	9.8798	20.0000	-6.0429
25.0000	10.6658	25.0000	-6.3919
30.0000	11.1884	30.0000	-6.5650
35.0000	11.4514	35.0000	-6.5535
40.0000	11.4751	40.0000	-6.3712
45.0000	11.2711	45.0000	-6.0270
50.0000	10.8696	50.0000	-5.5534
55.0000	10.2947	55.0000	-4.9802
60.0000	9.5661	60.0000	-4.3309
65.0000	8.7015	65.0000	-3.6346
70.0000	7.7167	70.0000	-2.9224
75.0000	6.6379	75.0000	-2.2412
80.0000	5.4753	80.0000	-1.6473
85.0000	4.1705	85.0000	-1.1966
90.0000	2.8058	90.0000	-0.7830
95.0000	1.4309	95.0000	-0.4195
100.0000	0.0295	100.0000	-0.0295
L.E. radius = 1.794 percent c
slope of mean line at LE = 0.1902

NACA 63A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2464	1.4462	0.7536	-1.2213
0.4668	1.7669	1.0332	-1.4507
0.9186	2.3373	1.5814	-1.8548
2.0988	3.4246	2.9012	-2.5809
4.5367	4.9876	5.4633	-3.5452
7.0132	6.1783	7.9868	-4.2330
9.5085	7.1520	10.4915	-4.7679
14.5292	8.6757	15.4708	-5.5530
19.5728	9.8005	20.4272	-6.0800
24.6297	10.6162	25.3703	-6.4106
29.6952	11.1639	30.3048	-6.5697
34.7662	11.4444	35.2338	-6.5488
39.8392	11.4779	40.1608	-6.3624
44.9115	11.2765	45.0885	-6.0198
49.9800	10.8715	50.0200	-5.5513
55.0429	10.2895	54.9571	-4.9849
60.0983	9.5503	59.9017	-4.3440
65.1451	8.6741	64.8549	-3.6553
70.1830	7.6789	69.8170	-2.9484
75.2136	6.5897	74.7864	-2.2691
80.2556	5.4122	79.7444	-1.6735
85.2493	4.1033	84.7507	-1.2177
90.1743	2.7583	89.8257	-0.7967
95.0899	1.4070	94.9101	-0.4262
100.0029	0.0295	99.9971	-0.0295
L.E. radius = 1.794 percent c
slope of mean line at LE = 0.1902

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NACA 63A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	2.0580	0.5000	-1.0337
0.7500	2.4255	0.7500	-1.3279
1.2500	3.0516	1.2500	-1.8034
2.5000	4.2502	2.5000	-2.7320
5.0000	5.9782	5.0000	-3.9944
7.5000	7.2895	7.5000	-4.8987
10.0000	8.3552	10.0000	-5.6026
15.0000	10.0176	15.0000	-6.6454
20.0000	11.2343	20.0000	-7.3537
25.0000	12.1102	25.0000	-7.8114
30.0000	12.6808	30.0000	-8.0478
35.0000	12.9527	35.0000	-8.0554
40.0000	12.9493	40.0000	-7.8507
45.0000	12.6869	45.0000	-7.4479
50.0000	12.2021	50.0000	-6.8866
55.0000	11.5229	55.0000	-6.2036
60.0000	10.6729	60.0000	-5.4267
65.0000	9.6752	65.0000	-4.5926
70.0000	8.5529	70.0000	-3.7365
75.0000	7.3364	75.0000	-2.9142
80.0000	6.0381	80.0000	-2.1802
85.0000	4.5974	85.0000	-1.5935
90.0000	3.0895	90.0000	-1.0468
95.0000	1.5846	95.0000	-0.5618
100.0000	0.0351	100.0000	-0.0351
L.E. radius = 2.126 percent c
slope of mean line at LE = 0.1902

NACA 63A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2201	1.5843	0.7799	-1.3594
0.4336	1.9554	1.0664	-1.6392
0.8775	2.5970	1.6225	-2.1145
2.0418	3.8508	2.9582	-3.0071
4.4646	5.6518	5.5354	-4.2094
6.9347	7.0175	8.0653	-5.0722
9.4280	8.1271	10.5720	-5.7430
14.4508	9.8599	15.5492	-6.7371
19.5012	11.1297	20.4988	-7.4093
24.5675	12.0464	25.4325	-7.8407
29.6441	12.6502	30.3559	-8.0559
34.7271	12.9453	35.2729	-8.0496
39.8126	12.9543	40.1874	-7.8388
44.8969	12.6944	45.1031	-7.4376
49.9768	12.2044	50.0232	-6.8842
55.0497	11.5153	54.9503	-6.2107
60.1139	10.6518	59.8861	-5.4455
65.1679	9.6395	64.8321	-4.6207
70.2114	8.5031	69.7886	-3.7726
75.2467	7.2748	74.7533	-2.9542
80.2949	5.9572	79.7051	-2.2185
85.2876	4.5116	84.7124	-1.6260
90.2009	3.0287	89.7991	-1.0671
95.1042	1.5526	94.8958	-0.5718
100.0034	0.0351	99.9966	-0.0351
L.E. radius = 2.126 percent c
slope of mean line at LE = 0.1902

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NACA 64A204
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.4061	0.5000	-0.2724
0.7500	0.4931	0.7500	-0.3181
1.2500	0.6350	1.2500	-0.3793
2.5000	0.9043	2.5000	-0.4709
5.0000	1.3027	5.0000	-0.5732
7.5000	1.6152	7.5000	-0.6360
10.0000	1.8793	10.0000	-0.6816
15.0000	2.3063	15.0000	-0.7408
20.0000	2.6364	20.0000	-0.7731
25.0000	2.8900	25.0000	-0.7854
30.0000	3.0784	30.0000	-0.7804
35.0000	3.2075	35.0000	-0.7592
40.0000	3.2775	40.0000	-0.7199
45.0000	3.2794	45.0000	-0.6513
50.0000	3.2181	50.0000	-0.5580
55.0000	3.1014	55.0000	-0.4491
60.0000	2.9352	60.0000	-0.3315
65.0000	2.7225	65.0000	-0.2117
70.0000	2.4629	70.0000	-0.0961
75.0000	2.1581	75.0000	0.0047
80.0000	1.8015	80.0000	0.0704
85.0000	1.3753	85.0000	0.0700
90.0000	0.9309	90.0000	0.0516
95.0000	0.4671	95.0000	0.0242
100.0000	0.0060	100.0000	-0.0060
L.E. radius = 0.123 percent c
slope of mean line at LE = 0.0951

NACA 64A204
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4681	0.3920	0.5319	-0.2796
0.7146	0.4815	0.7854	-0.3234
1.2101	0.6247	1.2899	-0.3835
2.4543	0.8953	2.5457	-0.4734
4.9492	1.2959	5.0508	-0.5747
7.4475	1.6096	7.5525	-0.6370
9.9473	1.8745	10.0527	-0.6824
14.9496	2.3026	15.0504	-0.7412
19.9542	2.6335	20.0458	-0.7733
24.9601	2.8883	25.0399	-0.7855
29.9668	3.0775	30.0332	-0.7803
34.9742	3.2069	35.0258	-0.7591
39.9820	3.2774	40.0180	-0.7196
44.9899	3.2795	45.0101	-0.6511
49.9977	3.2181	50.0023	-0.5580
55.0050	3.1014	54.9950	-0.4491
60.0116	2.9348	59.9884	-0.3317
65.0173	2.7216	64.9827	-0.2122
70.0220	2.4618	69.9780	-0.0965
75.0260	2.1561	74.9740	0.0042
80.0312	1.7991	79.9688	0.0702
85.0305	1.3727	84.9695	0.0701
90.0215	0.9291	89.9785	0.0517
95.0108	0.4662	94.9892	0.0242
100.0003	0.0060	99.9997	-0.0060
L.E. radius = 0.123 percent c
slope of mean line at LE = 0.0951

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NACA 64A106
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.5417	0.5000	-0.4635
0.7500	0.6511	0.7500	-0.5535
1.2500	0.8233	1.2500	-0.6860
2.5000	1.1395	2.5000	-0.9160
5.0000	1.5901	5.0000	-1.2195
7.5000	1.9346	7.5000	-1.4404
10.0000	2.2228	10.0000	-1.6200
15.0000	2.6792	15.0000	-1.8937
20.0000	3.0264	20.0000	-2.0927
25.0000	3.2860	25.0000	-2.2326
30.0000	3.4718	30.0000	-2.3219
35.0000	3.5890	35.0000	-2.3647
40.0000	3.6372	40.0000	-2.3584
45.0000	3.6009	45.0000	-2.2868
50.0000	3.4894	50.0000	-2.1594
55.0000	3.3152	55.0000	-1.9890
60.0000	3.0878	60.0000	-1.7863
65.0000	2.8137	65.0000	-1.5579
70.0000	2.4961	70.0000	-1.3111
75.0000	2.1412	75.0000	-1.0586
80.0000	1.7538	80.0000	-0.8166
85.0000	1.3300	85.0000	-0.6061
90.0000	0.8978	90.0000	-0.4049
95.0000	0.4514	95.0000	-0.2062
100.0000	0.0091	100.0000	-0.0091
L.E. radius = 0.277 percent c
slope of mean line at LE = 0.0475

NACA 64A106
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4762	0.5292	0.5238	-0.4729
0.7236	0.6395	0.7764	-0.5605
1.2202	0.8141	1.2798	-0.6935
2.4657	1.1313	2.5343	-0.9203
4.9619	1.5840	5.0381	-1.2234
7.4606	1.9298	7.5394	-1.4434
9.9604	2.2186	10.0396	-1.6226
14.9622	2.6762	15.0378	-1.8955
19.9656	3.0241	20.0344	-2.0940
24.9700	3.2847	25.0300	-2.2333
29.9751	3.4709	30.0249	-2.3223
34.9807	3.5886	35.0193	-2.3647
39.9865	3.6372	40.0135	-2.3583
44.9925	3.6009	45.0075	-2.2868
49.9983	3.4894	50.0017	-2.1594
55.0037	3.3152	54.9963	-1.9890
60.0086	3.0878	59.9914	-1.7863
65.0129	2.8131	64.9871	-1.5584
70.0164	2.4947	69.9836	-1.3121
75.0193	2.1397	74.9807	-1.0596
80.0232	1.7522	79.9768	-0.8175
85.0227	1.3283	84.9773	-0.6069
90.0160	0.8961	89.9840	-0.4057
95.0081	0.4514	94.9919	-0.2062
100.0002	0.0091	99.9998	-0.0091
L.E. radius = 0.277 percent c
slope of mean line at LE = 0.0475

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NACA 64A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.9385	0.5000	-0.7036
0.7500	1.1169	0.7500	-0.8542
1.2500	1.4048	1.2500	-1.0755
2.5000	1.9429	2.5000	-1.4502
5.0000	2.7215	5.0000	-1.9459
7.5000	3.3168	7.5000	-2.3006
10.0000	3.8194	10.0000	-2.5888
15.0000	4.6117	15.0000	-3.0237
20.0000	5.2139	20.0000	-3.3352
25.0000	5.6653	25.0000	-3.5515
30.0000	5.9882	30.0000	-3.6853
35.0000	6.1927	35.0000	-3.7426
40.0000	6.2733	40.0000	-3.7163
45.0000	6.2054	45.0000	-3.5789
50.0000	6.0121	50.0000	-3.3520
55.0000	5.7123	55.0000	-3.0587
60.0000	5.3236	60.0000	-2.7158
65.0000	4.8540	65.0000	-2.3375
70.0000	4.3104	70.0000	-1.9348
75.0000	3.7060	75.0000	-1.5337
80.0000	3.0454	80.0000	-1.1598
85.0000	2.3127	85.0000	-0.8536
90.0000	1.5588	90.0000	-0.5678
95.0000	0.7886	95.0000	-0.2921
100.0000	0.0156	100.0000	-0.0156
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.0951

NACA 64A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4228	0.8685	0.5772	-0.7560
0.6639	1.0576	0.8361	-0.8995
1.1526	1.3529	1.3474	-1.1117
2.3872	1.8999	2.6128	-1.4781
4.8736	2.6877	5.1264	-1.9665
7.3689	3.2893	7.6311	-2.3166
9.8681	3.7942	10.1319	-2.6021
14.8738	4.5942	15.1262	-3.0329
19.8851	5.2015	20.1149	-3.3413
24.8998	5.6577	25.1002	-3.5549
29.9169	5.9840	30.0831	-3.6869
34.9354	6.1907	35.0646	-3.7429
39.9550	6.2732	40.0450	-3.7155
44.9750	6.2062	45.0250	-3.5778
49.9943	6.0121	50.0057	-3.3520
55.0123	5.7116	54.9877	-3.0593
60.0284	5.3211	59.9716	-2.7180
65.0423	4.8500	64.9577	-2.3406
70.0538	4.3048	69.9462	-1.9395
75.0631	3.6986	74.9369	-1.5383
80.0757	3.0344	79.9243	-1.1651
85.0740	2.3010	84.9260	-0.8582
90.0520	1.5514	89.9480	-0.5706
95.0264	0.7841	94.9736	-0.2937
100.0008	0.0156	99.9992	-0.0156
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.0951

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NACA 64A410
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0574	0.5000	-0.5989
0.7500	1.2576	0.7500	-0.7385
1.2500	1.5799	1.2500	-0.9240
2.5000	2.1979	2.5000	-1.2158
5.0000	3.1188	5.0000	-1.5691
7.5000	3.8357	7.5000	-1.8002
10.0000	4.4414	10.0000	-1.9811
15.0000	5.4119	15.0000	-2.2358
20.0000	6.1566	20.0000	-2.4006
25.0000	6.7252	25.0000	-2.4975
30.0000	7.1421	30.0000	-2.5359
35.0000	7.4188	35.0000	-2.5189
40.0000	7.5524	40.0000	-2.4382
45.0000	7.5191	45.0000	-2.2655
50.0000	7.3417	50.0000	-2.0225
55.0000	7.0398	55.0000	-1.7313
60.0000	6.6279	60.0000	-1.4123
65.0000	6.1139	65.0000	-1.0793
70.0000	5.5003	70.0000	-0.7486
75.0000	4.7956	75.0000	-0.4489
80.0000	3.9909	80.0000	-0.2218
85.0000	3.0459	85.0000	-0.1298
90.0000	2.0594	90.0000	-0.0755
95.0000	1.0373	95.0000	-0.0463
100.0000	0.0155	100.0000	-0.0155
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.1902

NACA 64A410
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3476	0.9140	0.6524	-0.6891
0.5797	1.1256	0.9203	-0.8094
1.0569	1.4622	1.4431	-0.9797
2.2758	2.0997	2.7242	-1.2560
4.7484	3.0381	5.2516	-1.5957
7.2387	3.7665	7.7613	-1.8211
9.7369	4.3821	10.2631	-1.9980
14.7480	5.3687	15.2520	-2.2459
19.7704	6.1270	20.2296	-2.4066
24.7998	6.7059	25.2002	-2.5002
29.8338	7.1305	30.1662	-2.5362
34.8709	7.4134	35.1291	-2.5177
39.9100	7.5515	40.0900	-2.4360
44.9499	7.5201	45.0501	-2.2634
49.9886	7.3422	50.0114	-2.0220
55.0246	7.0377	54.9754	-1.7331
60.0569	6.6224	59.9431	-1.4161
65.0846	6.1040	64.9154	-1.0852
70.1075	5.4860	69.8925	-0.7555
75.1262	4.7765	74.8738	-0.4559
80.1512	3.9650	79.8488	-0.2263
85.1476	3.0172	84.8524	-0.1316
90.1037	2.0380	89.8963	-0.0764
95.0527	1.0274	94.9473	-0.0465
100.0015	0.0155	99.9985	-0.0155
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.1902

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NACA 64A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1006	0.5000	-0.8207
0.7500	1.3113	0.7500	-1.0106
1.2500	1.6514	1.2500	-1.2845
2.5000	2.2825	2.5000	-1.7602
5.0000	3.1912	5.0000	-2.3926
7.5000	3.8858	7.5000	-2.8485
10.0000	4.4640	10.0000	-3.2178
15.0000	5.3823	15.0000	-3.7812
20.0000	6.0759	20.0000	-4.1899
25.0000	6.5933	25.0000	-4.4747
30.0000	6.9612	30.0000	-4.6557
35.0000	7.1897	35.0000	-4.7388
40.0000	7.2702	40.0000	-4.7136
45.0000	7.1747	45.0000	-4.5486
50.0000	6.9335	50.0000	-4.2734
55.0000	6.5700	55.0000	-3.9146
60.0000	6.1040	60.0000	-3.4952
65.0000	5.5471	65.0000	-3.0271
70.0000	4.9106	70.0000	-2.5293
75.0000	4.2073	75.0000	-2.0278
80.0000	3.4457	80.0000	-1.5546
85.0000	2.6148	85.0000	-1.1502
90.0000	1.7597	90.0000	-0.7644
95.0000	0.8921	95.0000	-0.3944
100.0000	0.0189	100.0000	-0.0189
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.0951

NACA 64A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4093	1.0098	0.5907	-0.8973
0.6487	1.2302	0.8513	-1.0721
1.1347	1.5794	1.3653	-1.3381
2.3655	2.2241	2.6345	-1.8023
4.8488	3.1444	5.1512	-2.4232
7.3429	3.8465	7.6571	-2.8738
9.8419	4.4307	10.1581	-3.2387
14.8486	5.3574	15.1514	-3.7960
19.8620	6.0594	20.1380	-4.1992
24.8797	6.5829	25.1203	-4.4801
29.9002	6.9553	30.0998	-4.6582
34.9225	7.1872	35.0775	-4.7393
39.9460	7.2703	40.0540	-4.7125
44.9700	7.1757	45.0300	-4.5473
49.9932	6.9335	50.0068	-4.2734
55.0147	6.5684	54.9853	-3.9161
60.0340	6.1010	59.9661	-3.4978
65.0505	5.5413	64.9495	-3.0319
70.0640	4.9014	69.9360	-2.5361
75.0751	4.1958	74.9249	-2.0355
80.0901	3.4316	79.9099	-1.5622
85.0880	2.5999	84.9120	-1.1571
90.0618	1.7497	89.9382	-0.7689
95.0315	0.8870	94.9685	-0.3966
100.0009	0.0189	99.9991	-0.0189
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.0951

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NACA 64A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.2497	0.5000	-0.7033
0.7500	1.4735	0.7500	-0.8698
1.2500	1.8465	1.2500	-1.1161
2.5000	2.5573	2.5000	-1.5136
5.0000	3.6038	5.0000	-2.0048
7.5000	4.4161	7.5000	-2.3403
10.0000	5.0961	10.0000	-2.6038
15.0000	6.1887	15.0000	-2.9890
20.0000	7.0243	20.0000	-3.2521
25.0000	7.6562	25.0000	-3.4188
30.0000	8.1164	30.0000	-3.5052
35.0000	8.4166	35.0000	-3.5149
40.0000	8.5492	40.0000	-3.4359
45.0000	8.4879	45.0000	-3.2358
50.0000	8.2630	50.0000	-2.9440
55.0000	7.8970	55.0000	-2.5877
60.0000	7.4097	60.0000	-2.1903
65.0000	6.8080	65.0000	-1.7679
70.0000	6.1017	70.0000	-1.3413
75.0000	5.2982	75.0000	-0.9416
80.0000	4.3960	80.0000	-0.6138
85.0000	3.3531	85.0000	-0.4238
90.0000	2.2634	90.0000	-0.2707
95.0000	1.1452	95.0000	-0.1476
100.0000	0.0189	100.0000	-0.0189
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.1902

NACA 64A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3211	1.0534	0.6789	-0.8285
0.5497	1.2963	0.9503	-0.9801
1.0215	1.6866	1.4785	-1.2041
2.2328	2.4218	2.7672	-1.5780
4.6990	3.4929	5.3010	-2.0504
7.1868	4.3219	7.8132	-2.3765
9.6845	5.0170	10.3155	-2.6329
14.6976	6.1306	15.3024	-3.0079
19.7243	6.9840	20.2757	-3.2635
24.7596	7.6304	25.2404	-3.4247
29.8005	8.1013	30.1995	-3.5071
34.8450	8.4096	35.1550	-3.5139
39.8920	8.5484	40.1080	-3.4329
44.9400	8.4897	45.0600	-3.2329
49.9864	8.2636	50.0136	-2.9434
55.0294	7.8945	54.9706	-2.5899
60.0679	7.4022	59.9321	-2.1959
65.1009	6.7951	64.8991	-1.7763
70.1280	6.0824	69.8720	-1.3519
75.1501	5.2733	74.8499	-0.9526
80.1798	4.3614	79.8202	-0.6227
85.1755	3.3151	84.8245	-0.4295
90.1231	2.2356	89.8769	-0.2739
95.0627	1.1299	94.9373	-0.1491
100.0018	0.0189	99.9982	-0.0189
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.1902

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NACA 64A612
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.4041	0.5000	-0.5959
0.7500	1.6432	0.7500	-0.7445
1.2500	2.0522	1.2500	-0.9577
2.5000	2.8404	2.5000	-1.2744
5.0000	4.0225	5.0000	-1.6248
7.5000	4.9505	7.5000	-1.8400
10.0000	5.7357	10.0000	-1.9960
15.0000	6.9997	15.0000	-2.2014
20.0000	7.9762	20.0000	-2.3177
25.0000	8.7229	25.0000	-2.3657
30.0000	9.2732	30.0000	-2.3565
35.0000	9.6440	35.0000	-2.2919
40.0000	9.8287	40.0000	-2.1589
45.0000	9.8013	45.0000	-1.9232
50.0000	9.5925	50.0000	-1.6146
55.0000	9.2240	55.0000	-1.2601
60.0000	8.7146	60.0000	-0.8857
65.0000	8.0693	65.0000	-0.5086
70.0000	7.2954	70.0000	-0.1536
75.0000	6.3925	75.0000	0.1437
80.0000	5.3505	80.0000	0.3238
85.0000	4.0955	85.0000	0.2986
90.0000	2.7679	90.0000	0.2202
95.0000	1.3979	95.0000	0.0977
100.0000	0.0187	100.0000	-0.0187
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.2852

NACA 64A612
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2373	1.0898	0.7627	-0.7524
0.4550	1.3545	1.0450	-0.8802
0.9123	1.7857	1.5877	-1.0619
2.1035	2.6112	2.8965	-1.3455
4.5518	3.8335	5.4482	-1.6699
7.0327	4.7902	7.9673	-1.8722
9.5288	5.5970	10.4712	-2.0208
14.5476	6.8989	15.4524	-2.2148
19.5872	7.9049	20.4128	-2.3242
24.6398	8.6753	25.3602	-2.3668
29.7009	9.2456	30.2991	-2.3542
34.7677	9.6310	35.2323	-2.2875
39.8381	9.8261	40.1619	-2.1528
44.9100	9.8035	45.0900	-1.9183
49.9796	9.5936	50.0204	-1.6133
55.0441	9.2205	54.9559	-1.2636
60.1018	8.7032	59.8982	-0.8937
65.1513	8.0483	64.8487	-0.5201
70.1919	7.2623	69.8081	-0.1665
75.2249	6.3489	74.7751	0.1320
80.2688	5.2881	79.7312	0.3200
85.2618	4.0264	84.7382	0.3020
90.1835	2.7186	89.8165	0.2239
95.0935	1.3714	94.9065	0.0999
100.0028	0.0187	99.9972	-0.0187
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.2852

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NACA 64A114
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1762	0.5000	-1.0091
0.7500	1.4133	0.7500	-1.2384
1.2500	1.7826	1.2500	-1.5799
2.5000	2.4716	2.5000	-2.1935
5.0000	3.4454	5.0000	-3.0312
7.5000	4.1810	7.5000	-3.6495
10.0000	4.7893	10.0000	-4.1574
15.0000	5.7458	15.0000	-4.9390
20.0000	6.4626	20.0000	-5.5152
25.0000	6.9906	25.0000	-5.9284
30.0000	7.3576	30.0000	-6.2032
35.0000	7.5741	35.0000	-6.3481
40.0000	7.6268	40.0000	-6.3487
45.0000	7.4842	45.0000	-6.1719
50.0000	7.1849	50.0000	-5.8548
55.0000	6.7554	55.0000	-5.4293
60.0000	6.2247	60.0000	-4.9187
65.0000	5.6012	65.0000	-4.3390
70.0000	4.9043	70.0000	-3.7109
75.0000	4.1514	75.0000	-3.0601
80.0000	3.3642	80.0000	-2.4156
85.0000	2.5423	85.0000	-1.8069
90.0000	1.7081	90.0000	-1.2065
95.0000	0.8702	95.0000	-0.6194
100.0000	0.0224	100.0000	-0.0224
L.E. radius = 1.324 percent c
slope of mean line at LE = 0.0475

NACA 64A114
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4481	1.1197	0.5519	-1.0634
0.6918	1.3628	0.8082	-1.2838
1.1836	1.7393	1.3164	-1.6186
2.4222	2.4356	2.5778	-2.2247
4.9121	3.4167	5.0879	-3.0561
7.4085	4.1565	7.5915	-3.6701
9.9078	4.7697	10.0922	-4.1736
14.9116	5.7314	15.0884	-4.9507
19.9195	6.4529	20.0805	-5.5228
24.9298	6.9845	25.0702	-5.9331
29.9417	7.3542	30.0583	-6.2056
34.9548	7.5728	35.0452	-6.3488
39.9685	7.6270	40.0315	-6.3482
44.9825	7.4851	45.0175	-6.1709
49.9960	7.1849	50.0040	-5.8548
55.0085	6.7554	54.9915	-5.4293
60.0197	6.2224	59.9803	-4.9208
65.0293	5.5973	64.9707	-4.3426
70.0371	4.8986	69.9629	-3.7159
75.0435	4.1454	74.9565	-3.0652
80.0521	3.3564	79.9479	-2.4217
85.0509	2.5342	84.9491	-1.8128
90.0357	1.7015	89.9643	-1.2111
95.0182	0.8669	94.9818	-0.6217
100.0005	0.0224	99.9995	-0.0224
L.E. radius = 1.324 percent c
slope of mean line at LE = 0.0475

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NACA 64A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.3436	0.5000	-0.9941
0.7500	1.5930	0.7500	-1.2222
1.2500	2.0083	1.2500	-1.5738
2.5000	2.7779	2.5000	-2.2010
5.0000	3.8877	5.0000	-3.0427
7.5000	4.7299	7.5000	-3.6551
10.0000	5.4309	10.0000	-4.1533
15.0000	6.5348	15.0000	-4.9141
20.0000	7.3711	20.0000	-5.4690
25.0000	7.9876	25.0000	-5.8601
30.0000	8.4233	30.0000	-6.1125
35.0000	8.6864	35.0000	-6.2341
40.0000	8.7634	40.0000	-6.2077
45.0000	8.6222	45.0000	-5.9979
50.0000	8.3060	50.0000	-5.6459
55.0000	7.8439	55.0000	-5.1875
60.0000	7.2609	60.0000	-4.6483
65.0000	6.5720	65.0000	-4.0466
70.0000	5.7926	70.0000	-3.4044
75.0000	4.9424	75.0000	-2.7541
80.0000	4.0356	80.0000	-2.1334
85.0000	3.0597	85.0000	-1.5839
90.0000	2.0571	90.0000	-1.0525
95.0000	1.0470	95.0000	-0.5447
100.0000	0.0242	100.0000	-0.0242
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.0951

NACA 64A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3901	1.2123	0.6099	-1.0998
0.6272	1.4747	0.8728	-1.3166
1.1093	1.9009	1.3907	-1.6596
2.3344	2.6895	2.6656	-2.2676
4.8124	3.8163	5.1876	-3.0951
7.3044	4.6703	7.6956	-3.6977
9.8027	5.3806	10.1973	-4.1886
14.8108	6.4992	15.1892	-4.9378
19.8274	7.3456	20.1726	-5.4854
24.8495	7.9722	25.1505	-5.8693
29.8751	8.4143	30.1249	-6.1172
34.9031	8.6829	35.0969	-6.2351
39.9325	8.7638	40.0675	-6.2061
44.9626	8.6240	45.0374	-5.9957
49.9915	8.3060	50.0085	-5.6459
55.0183	7.8418	54.9817	-5.1895
60.0421	7.2559	59.9579	-4.6528
65.0625	6.5633	64.9375	-4.0540
70.0792	5.7798	69.9208	-3.4145
75.0928	4.9269	74.9072	-2.7666
80.1111	4.0153	79.8889	-2.1459
85.1086	3.0383	84.8914	-1.5955
90.0761	2.0415	89.9239	-1.0606
95.0389	1.0392	94.9611	-0.5487
100.0012	0.0242	99.9988	-0.0242
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.0951

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NACA 64A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.5379	0.5000	-0.8366
0.7500	1.7962	0.7500	-1.0544
1.2500	2.2419	1.2500	-1.3743
2.5000	3.0834	2.5000	-1.9268
5.0000	4.3238	5.0000	-2.6363
7.5000	5.2812	7.5000	-3.1303
10.0000	6.0819	10.0000	-3.5255
15.0000	7.3558	15.0000	-4.1113
20.0000	8.3274	20.0000	-4.5248
25.0000	9.0570	25.0000	-4.8003
30.0000	9.5810	30.0000	-4.9602
35.0000	9.9144	35.0000	-5.0097
40.0000	10.0421	40.0000	-4.9307
45.0000	9.9346	45.0000	-4.6861
50.0000	9.6346	50.0000	-4.3175
55.0000	9.1721	55.0000	-3.8595
60.0000	8.5689	60.0000	-3.3413
65.0000	7.8372	65.0000	-2.7838
70.0000	6.9887	70.0000	-2.2123
75.0000	6.0408	75.0000	-1.6636
80.0000	4.9936	80.0000	-1.1873
85.0000	3.8049	85.0000	-0.8532
90.0000	2.5650	90.0000	-0.5565
95.0000	1.3011	95.0000	-0.2965
100.0000	0.0241	100.0000	-0.0241
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.1902

NACA 64A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2831	1.2533	0.7169	-1.0284
0.5071	1.5379	0.9929	-1.2217
0.9711	2.0051	1.5289	-1.5226
2.1710	2.8841	2.8290	-2.0403
4.6264	4.1617	5.3736	-2.7193
7.1100	5.1430	7.8900	-3.1977
9.6064	5.9645	10.3936	-3.5804
14.6222	7.2706	15.3778	-4.1478
19.6552	8.2688	20.3448	-4.5483
24.6992	9.0187	25.3008	-4.8130
29.7503	9.5597	30.2497	-4.9654
34.8062	9.9049	35.1938	-5.0093
39.8651	10.0418	40.1349	-4.9263
44.9252	9.9379	45.0748	-4.6812
49.9830	9.6361	50.0170	-4.3159
55.0366	9.1679	54.9634	-3.8633
60.0842	8.5571	59.9158	-3.3507
65.1250	7.8169	64.8750	-2.7982
70.1582	6.9604	69.8418	-2.2299
75.1854	6.0038	74.8146	-1.6831
80.2218	4.9440	79.7782	-1.2053
85.2164	3.7521	84.7836	-0.8665
90.1516	2.5264	89.8484	-0.5647
95.0776	1.2815	94.9224	-0.3007
100.0024	0.0241	99.9976	-0.0241
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.1902

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NACA 64A218
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.5552	0.5000	-1.1126
0.7500	1.8505	0.7500	-1.3961
1.2500	2.3322	1.2500	-1.8253
2.5000	3.2564	2.5000	-2.6070
5.0000	4.5692	5.0000	-3.6699
7.5000	5.5641	7.5000	-4.4436
10.0000	6.3902	10.0000	-5.0723
15.0000	7.6878	15.0000	-6.0392
20.0000	8.6644	20.0000	-6.7451
25.0000	9.3828	25.0000	-7.2434
30.0000	9.8868	30.0000	-7.5707
35.0000	10.1844	35.0000	-7.7304
40.0000	10.2543	40.0000	-7.6997
45.0000	10.0636	45.0000	-7.4417
50.0000	9.6678	50.0000	-7.0096
55.0000	9.1045	55.0000	-6.4473
60.0000	8.4027	60.0000	-5.7852
65.0000	7.5827	65.0000	-5.0476
70.0000	6.6603	70.0000	-4.2607
75.0000	5.6646	75.0000	-3.4653
80.0000	4.6142	80.0000	-2.6977
85.0000	3.4961	85.0000	-2.0069
90.0000	2.3454	90.0000	-1.3329
95.0000	1.2011	95.0000	-0.6932
100.0000	0.0296	100.0000	-0.0296
L.E. radius = 1.945 percent c
slope of mean line at LE = 0.0951

NACA 64A218
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3746	1.3749	0.6254	-1.2625
0.6084	1.6885	0.8916	-1.5304
1.0866	2.1868	1.4134	-1.9455
2.3049	3.1308	2.6951	-2.7089
4.7770	4.4679	5.2230	-3.7467
7.2665	5.4798	7.7335	-4.5072
9.7640	6.3179	10.2360	-5.1258
14.7731	7.6373	15.2269	-6.0759
19.7929	8.6296	20.2071	-6.7694
24.8193	9.3613	25.1807	-7.2584
29.8500	9.8749	30.1500	-7.5778
34.8836	10.1798	35.1164	-7.7320
39.9191	10.2552	40.0809	-7.6975
44.9552	10.0666	45.0448	-7.4382
49.9899	9.6687	50.0101	-7.0086
55.0218	9.1020	54.9782	-6.4497
60.0502	8.3952	59.9498	-5.7920
65.0743	7.5690	64.9257	-5.0596
70.0940	6.6415	69.9060	-4.2762
75.1100	5.6426	74.8900	-3.4823
80.1317	4.5855	79.8683	-2.7161
85.1287	3.4671	84.8713	-2.0243
90.0900	2.3253	89.9100	-1.3445
95.0463	1.1900	94.9537	-0.6996
100.0015	0.0296	99.9986	-0.0296
L.E. radius = 1.945 percent c
slope of mean line at LE = 0.0951

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NACA 64A221
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.7402	0.5000	-1.2238
0.7500	2.0684	0.7500	-1.5385
1.2500	2.6319	1.2500	-2.0383
2.5000	3.7021	2.5000	-2.9741
5.0000	5.2311	5.0000	-4.2673
7.5000	6.3848	7.5000	-5.2093
10.0000	7.3417	10.0000	-5.9761
15.0000	8.8364	15.0000	-7.1545
20.0000	9.9589	20.0000	-8.0159
25.0000	10.7817	25.0000	-8.6275
30.0000	11.3532	30.0000	-9.0295
35.0000	11.6832	35.0000	-9.2273
40.0000	11.7430	40.0000	-9.1906
45.0000	11.4986	45.0000	-8.8780
50.0000	11.0201	50.0000	-8.3623
55.0000	10.3540	55.0000	-7.6931
60.0000	9.5311	60.0000	-6.9077
65.0000	8.5746	65.0000	-6.0314
70.0000	7.5115	70.0000	-5.1023
75.0000	6.3743	75.0000	-4.1606
80.0000	5.1821	80.0000	-3.2485
85.0000	3.9246	85.0000	-2.4199
90.0000	2.6297	90.0000	-1.6044
95.0000	1.3538	95.0000	-0.8408
100.0000	0.0352	100.0000	-0.0352
L.E. radius = 2.366 percent c
slope of mean line at LE = 0.0951

NACA 64A221
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3607	1.5213	0.6393	-1.4088
0.5927	1.8666	0.9073	-1.7085
1.0668	2.4378	1.4332	-2.1965
2.2780	3.5332	2.7220	-3.1114
4.7429	5.0962	5.2571	-4.3749
7.2295	6.2711	7.7705	-5.2984
9.7258	7.2446	10.2742	-6.0525
14.7357	8.7683	15.2643	-7.2069
19.7584	9.9114	20.2416	-8.0512
24.7891	10.7516	25.2109	-8.6488
29.8249	11.3371	30.1751	-9.0400
34.8641	11.6775	35.1359	-9.2296
39.9057	11.7449	40.0943	-9.1871
44.9478	11.5023	45.0522	-8.8739
49.9882	11.0213	50.0118	-8.3612
55.0253	10.3496	54.9747	-7.6973
60.0581	9.5206	59.9419	-6.9175
65.0860	8.5567	64.9140	-6.0473
70.1086	7.4877	69.8914	-5.1224
75.1270	6.3446	74.8730	-4.1843
80.1519	5.1449	79.8481	-3.2756
85.1483	3.8870	84.8517	-2.4442
90.1036	2.6023	89.8964	-1.6214
95.0536	1.3389	94.9464	-0.8485
100.0017	0.0352	99.9983	-0.0352
L.E. radius = 2.366 percent c
slope of mean line at LE = 0.0951

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NACA 65A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.8919	0.5000	-0.6681
0.7500	1.0675	0.7500	-0.8158
1.2500	1.3582	1.2500	-1.0314
2.5000	1.8760	2.5000	-1.3923
5.0000	2.5731	5.0000	-1.8065
7.5000	3.1635	7.5000	-2.1470
10.0000	3.6597	10.0000	-2.4315
15.0000	4.4560	15.0000	-2.8696
20.0000	5.0689	20.0000	-3.1911
25.0000	5.5417	25.0000	-3.4270
30.0000	5.8939	30.0000	-3.5901
35.0000	6.1376	35.0000	-3.6863
40.0000	6.2733	40.0000	-3.7148
45.0000	6.2955	45.0000	-3.6679
50.0000	6.1919	50.0000	-3.5318
55.0000	5.9572	55.0000	-3.3038
60.0000	5.6048	60.0000	-2.9973
65.0000	5.1560	65.0000	-2.6381
70.0000	4.6185	70.0000	-2.2416
75.0000	3.9987	75.0000	-1.8236
80.0000	3.2980	80.0000	-1.4085
85.0000	2.5056	85.0000	-1.0430
90.0000	1.6881	90.0000	-0.6935
95.0000	0.8526	95.0000	-0.3553
100.0000	0.0157	100.0000	-0.0157
L.E. radius = 0.654 percent c
slope of mean line at LE = 0.0951

NACA 65A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4264	0.8298	0.5736	-0.7174
0.6678	1.0136	0.8322	-0.8555
1.1560	1.3090	1.3440	-1.0677
2.3913	1.8380	2.6087	-1.4162
4.8814	2.5441	5.1186	-1.8229
7.3761	3.1358	7.6239	-2.1632
9.8746	3.6365	10.1254	-2.4445
14.8789	4.4397	15.1211	-2.8783
19.8890	5.0573	20.1110	-3.1970
24.9025	5.5337	25.0975	-3.4308
29.9185	5.8893	30.0815	-3.5921
34.9362	6.1350	35.0638	-3.6871
39.9550	6.2725	40.0450	-3.7147
44.9745	6.2957	45.0255	-3.6673
49.9941	6.1919	50.0059	-3.5318
55.0130	5.9567	54.9870	-3.3044
60.0304	5.6024	59.9696	-2.9992
65.0459	5.1512	64.9541	-2.6418
70.0590	4.6117	69.9410	-2.2464
75.0702	3.9897	74.9298	-1.8294
80.0848	3.2847	79.9152	-1.4154
85.0829	2.4914	84.9171	-1.0486
90.0583	1.6784	89.9417	-0.6976
95.0295	0.8477	94.9705	-0.3573
100.0008	0.0157	99.9992	-0.0157
L.E. radius = 0.654 percent c
slope of mean line at LE = 0.0951

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NACA 65A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0495	0.5000	-0.7857
0.7500	1.2538	0.7500	-0.9611
1.2500	1.5990	1.2500	-1.2346
2.5000	2.1987	2.5000	-1.6896
5.0000	3.0105	5.0000	-2.2236
7.5000	3.6955	7.5000	-2.6619
10.0000	4.2707	10.0000	-3.0283
15.0000	5.1929	15.0000	-3.5938
20.0000	5.8999	20.0000	-4.0129
25.0000	6.4431	25.0000	-4.3231
30.0000	6.8464	30.0000	-4.5392
35.0000	7.1230	35.0000	-4.6704
40.0000	7.2733	40.0000	-4.7146
45.0000	7.2896	45.0000	-4.6622
50.0000	7.1565	50.0000	-4.4964
55.0000	6.8694	55.0000	-4.2144
60.0000	6.4464	60.0000	-3.8363
65.0000	5.9128	65.0000	-3.3910
70.0000	5.2802	70.0000	-2.8987
75.0000	4.5577	75.0000	-2.3746
80.0000	3.7461	80.0000	-1.8500
85.0000	2.8412	85.0000	-1.3712
90.0000	1.9129	90.0000	-0.9132
95.0000	0.9689	95.0000	-0.4677
100.0000	0.0191	100.0000	-0.0191
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

NACA 65A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4136	0.9648	0.5864	-0.8524
0.6532	1.1787	0.8468	-1.0206
1.1386	1.5303	1.3614	-1.2890
2.3706	2.1473	2.6294	-1.7254
4.8583	2.9697	5.1417	-2.2485
7.3517	3.6585	7.6483	-2.6858
9.8497	4.2397	10.1503	-3.0477
14.8548	5.1693	15.1452	-3.6079
19.8668	5.8829	20.1332	-4.0227
24.8830	6.4320	25.1170	-4.3292
29.9022	6.8397	30.0978	-4.5426
34.9234	7.1196	35.0766	-4.6718
39.9460	7.2723	40.0540	-4.7146
44.9694	7.2900	45.0306	-4.6616
49.9929	7.1565	50.0071	-4.4964
55.0156	6.8680	54.9845	-4.2157
60.0364	6.4426	59.9636	-3.8395
65.0547	5.9059	64.9452	-3.3965
70.0704	5.2709	69.9296	-2.9056
75.0835	4.5442	74.9165	-2.3839
80.1008	3.7292	79.8992	-1.8599
85.0985	2.8231	84.9015	-1.3804
90.0691	1.9002	89.9309	-0.9194
95.0351	0.9616	94.9649	-0.4712
100.0009	0.0191	99.9991	-0.0191
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

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NACA 65A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0495	0.5000	-0.7857
0.7500	1.2538	0.7500	-0.9611
1.2500	1.5990	1.2500	-1.2346
2.5000	2.1987	2.5000	-1.6896
5.0000	3.0105	5.0000	-2.2236
7.5000	3.6955	7.5000	-2.6619
10.0000	4.2707	10.0000	-3.0283
15.0000	5.1929	15.0000	-3.5938
20.0000	5.8999	20.0000	-4.0129
25.0000	6.4431	25.0000	-4.3231
30.0000	6.8464	30.0000	-4.5392
35.0000	7.1230	35.0000	-4.6704
40.0000	7.2733	40.0000	-4.7146
45.0000	7.2896	45.0000	-4.6622
50.0000	7.1565	50.0000	-4.4964
55.0000	6.8694	55.0000	-4.2144
60.0000	6.4464	60.0000	-3.8363
65.0000	5.9128	65.0000	-3.3910
70.0000	5.2802	70.0000	-2.8987
75.0000	4.5577	75.0000	-2.3746
80.0000	3.7461	80.0000	-1.8500
85.0000	2.8412	85.0000	-1.3712
90.0000	1.9129	90.0000	-0.9132
95.0000	0.9689	95.0000	-0.4677
100.0000	0.0191	100.0000	-0.0191
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

NACA 65A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4136	0.9648	0.5864	-0.8524
0.6532	1.1787	0.8468	-1.0206
1.1386	1.5303	1.3614	-1.2890
2.3706	2.1473	2.6294	-1.7254
4.8583	2.9697	5.1417	-2.2485
7.3517	3.6585	7.6483	-2.6858
9.8497	4.2397	10.1503	-3.0477
14.8548	5.1693	15.1452	-3.6079
19.8668	5.8829	20.1332	-4.0227
24.8830	6.4320	25.1170	-4.3292
29.9022	6.8397	30.0978	-4.5426
34.9234	7.1196	35.0766	-4.6718
39.9460	7.2723	40.0540	-4.7146
44.9694	7.2900	45.0306	-4.6616
49.9929	7.1565	50.0071	-4.4964
55.0156	6.8680	54.9845	-4.2157
60.0364	6.4426	59.9636	-3.8395
65.0547	5.9059	64.9452	-3.3965
70.0704	5.2709	69.9296	-2.9056
75.0835	4.5442	74.9165	-2.3839
80.1008	3.7292	79.8992	-1.8599
85.0985	2.8231	84.9015	-1.3804
90.0691	1.9002	89.9309	-0.9194
95.0351	0.9616	94.9649	-0.4712
100.0009	0.0191	99.9991	-0.0191
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

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NACA 65A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1893	0.5000	-0.6721
0.7500	1.4166	0.7500	-0.8282
1.2500	1.7930	1.2500	-1.0694
2.5000	2.4660	2.5000	-1.4485
5.0000	3.4156	5.0000	-1.8403
7.5000	4.2231	7.5000	-2.1547
10.0000	4.9027	10.0000	-2.4147
15.0000	5.9995	15.0000	-2.8014
20.0000	6.8475	20.0000	-3.0753
25.0000	7.5069	25.0000	-3.2668
30.0000	8.0024	30.0000	-3.3881
35.0000	8.3508	35.0000	-3.4456
40.0000	8.5533	40.0000	-3.4359
45.0000	8.6036	45.0000	-3.3487
50.0000	8.4862	50.0000	-3.1668
55.0000	8.1963	55.0000	-2.8876
60.0000	7.7509	60.0000	-2.5316
65.0000	7.1735	65.0000	-2.1320
70.0000	6.4727	70.0000	-1.7096
75.0000	5.6507	75.0000	-1.2870
80.0000	4.7004	80.0000	-0.9066
85.0000	3.5828	85.0000	-0.6428
90.0000	2.4175<