Summary of Airfoil Data Page: 85 of 266
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REPORT NO. 824- NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS
NACA 65-008 BASIC THICKNESS FORM
z yl
(percent c) (percent c)
0 0
.5 .627
.75 .756
1.25 .945
2. 5 1. 267
5. 0 1. 745
7. 5 2. 118
10 2. 432
15 2. 931
20 3.312
25 3. 599
30 3.805
35 3.938
40 3. 998
45 3.974
50 3. 857
55 3. 638
60 3.337
65 2. 971
70 2. 553
75 2.096
80 1.617
85 1. 131
90 .664
95 .252
100 0
L. E. radius: 0.4:34 percent c(v/ )2
0
.978
1.010
1. 043
1. 086
1. 125
1. 145
1. 158
1. 178
1. 192
1.203
1.210
1. 217
1.222
1.226
1. 222
1. 193
1.163
1. 130
1. 094
1.055
1.014
.971
.92:13
.873
.817vl V
0
.989
1.005
1. 021
1. 042
1. 061
1. 070
1.076
1. 085
1. 092
1. 097
1.100
1. 103
1. 105
1. 107
1. 105
1.092
1.078
1.06,3
1.046
1.027
1. 007
.985
.961
.934
.904AtJ V
3. 695
2.010
1.696
1.340
.956
.689
.560
.477
.382
.323
.281
.248
.221
.199
.178
.160
.145
.128
.113
.098
.084
072
.059
.044
.031
0NACA 65-009 BASIC THICKNESS FORM
(percent c)
0
.700
.845
1. 058
1. 421
1. 961
2.383
2. 736
3.299
3. 727
4. 050
4. 282
4.431
4. 496
4. 469
4. 336
4. 086
3. 743
:1. :328
2. 856i
2. 342
1. 805
1. 260
.738
.280
0(v/ V)2
0
.945
. 985
1. 037
1. 089)
1. 134
1. 159
1.177
1. 200
1. 216
1. 229
1. 238
1. 246
1. 252
1.258
1. 25))
1. 220
1. 185
1. 145
1. 103
1 059
1. 013
. 963
.912
856i
.797vl V A./ V
0 3. 270
.972 1.962
.992 1. (655
1. 018 1.315
1.044 .950
1. 065 .687
1. 077 5160
1. (85 .477
1. 095 .382
1. 1 )03 .323
1.10 9 .280
1. 113 .248
1.116 .220)
1. 119 .198
1. 122 178
1. 118 . 160
1 1.5 144
1. (08 .128
1. 07 . 111
1. 150 .097
1. 029 .084
1. 0)6 . 071
981 .059
955 .044
.925 .030
. 893 0L. E. radius: 0.552 percent c
NACA 65-010 BASIC THICKNESS FORM
xz y(1
(percent c) (Ipercent c)
0 0 0
.5 .772 .911
. 5 . 932 . 960(
1.25 1. 169 1. 025
2. 5 1. 574 1. 085
5.0 2. 177 1. 143
7. 5 2. (i47 1. 177
10 3. 040 1. 197
15 3. 666 1. 224
20 4. 143 1. 242
25 4. 50:1 1. 257
30 4. 760 1. 268
35 4.924 1. 277
40 4. 996 1. 284
45 4. 963 1. 290
50 4. 812 1. 284
55 4. 510 1. 244
60 4. 146 1. 2(12
65 3.682 1. 158
70 3.156 1. 112
75 2. 584 1. 062
80 1. 987 1. 011
85 1.385 .958
90 . 810 .93
95 .306 .844
100 0 .781
L. E. radius: 0.687 percent cr/ V
0
. 954
. 980
1. 012
1. 042
1.069
1. 085
1. 094
1. 106
1.114
1.121
1. 126i
1. 130
1. 133
1. 13i
1. 133
1.115
1. 096
1. 076
1. 055
1.031
1. 005
. 979
.950
.919
. 8842. 967
1.911
1. 614
1. 292
.932
.679
558
.480
.383
.321
.280
.248
.222
.199
179
141
126
.11()
. 097
.082
. 070
.058
. 045
.03)
082
2V
(percent c)
0
.5
.75
1.25
2. 5
5.0
7.5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100I
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Abbott, Ira H.; von Doenhoff, Albert E. & Stivers, Louis S., Jr. Summary of Airfoil Data, report, 1945; (https://digital.library.unt.edu/ark:/67531/metadc65534/m1/85/: accessed March 28, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.