NACA 2410 airfoil — dimension sheet
Source: Xem Studio, https://xemstudio.com/objects/naca-2410-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 2410: 2 % 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  1.098  1.694  1.402  -1.448
2.5  2.297  2.412  2.703  -1.927
5  4.742  3.420  5.258  -2.482
7.5  7.217  4.168  7.783  -2.809
10  9.708  4.766  10.292  -3.016
15  14.722  5.664  15.278  -3.227
20  19.761  6.275  20.239  -3.275
25  24.814  6.666  25.186  -3.228
30  29.875  6.874  30.125  -3.124
40  40.000  6.833  40.000  -2.833
50  50.049  6.349  49.951  -2.460
60  60.084  5.566  59.916  -2.010
70  70.101  4.526  69.899  -1.526
80  80.095  3.252  79.905  -1.030
90  90.063  1.747  89.937  -0.525
95  95.036  0.905  94.964  -0.266
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-2410-airfoil/index.json
API: https://xemstudio.com/api/geometry?object=naca-2410-airfoil