NACA 1410 airfoil — dimension sheet
Source: Xem Studio, https://xemstudio.com/objects/naca-1410-airfoil/  (sheet CC BY 4.0; files Xem Studio Design License, https://xemstudio.com/license/)
Basis: Computed from the NACA equations (Report 460 / Report 610, restated in NASA TM-4741)
Catalog version: 2026-10-20

Overall (mm): length 100.0, width 20.0, height 10.0
- NACA 1410: 1 % camber at 40 % chord, 10 % thick.
- NACA 4-digit: first digit = maximum camber in % of chord, second = its position in tenths of chord, last two = maximum thickness in % of chord (NACA Report 460).
- Ordinates are in % of chord from the leading edge, computed from the published equations with the closed-trailing-edge thickness coefficient (−0.1036, as in NASA TM-4741). The original reports use an open trailing edge (−0.1015); the difference is under 0.03 % of chord near the trailing edge.
- The file is a 100 mm chord section, 20 mm deep: scale it uniformly to your chord, or import the STEP and sweep or loft it into a wing. Thickness scales with chord; the shape is the same at any size.

x (% chord)  upper x  upper y  lower x  lower y
0  0.000  0.000  0.000  0.000
1.25  1.174  1.638  1.326  -1.515
2.5  2.398  2.298  2.602  -2.055
5  4.871  3.194  5.129  -2.725
7.5  7.358  3.837  7.642  -3.157
10  9.854  4.337  10.146  -3.462
15  14.861  5.061  15.139  -3.843
20  19.881  5.530  20.119  -4.030
25  24.907  5.809  25.093  -4.090
30  29.937  5.938  30.063  -4.063
40  40.000  5.833  40.000  -3.833
50  50.024  5.377  49.976  -3.433
60  60.042  4.678  59.958  -2.900
70  70.050  3.778  69.950  -2.278
80  80.048  2.698  79.952  -1.587
90  90.032  1.443  89.968  -0.832
95  95.018  0.746  94.982  -0.427
100  100.000  -0.000  100.000  0.000

Files elsewhere (not hosted by Xem Studio; license as stated by the publisher):
- NACA (NASA Technical Reports Server): Report 460: The characteristics of 78 related airfoil sections from tests in the variable-density wind tunnel (Jacobs, Ward, Pinkerton, 1933) — web — Publisher's page; dimensions are facts — https://ntrs.nasa.gov/citations/19930091108
- NASA: TM-4741: Computer program to obtain ordinates for NACA airfoils (Ladson, Brooks, Hill, Sproles, 1996) — web — Publisher's page; dimensions are facts — https://www.pdas.com/refs/tm4741.pdf

Free files (Xem Studio Design License, Xem Studio; STEP + STL, 1 parts): https://xemstudio.com/files/hardware/naca-1410-airfoil/index.json
API: https://xemstudio.com/api/geometry?object=naca-1410-airfoil