NACA 23024 airfoil — dimension sheet
Source: Xem Studio, https://xemstudio.com/objects/naca-23024-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 24.0
- NACA 23024: 5-digit 230 mean line (design lift coefficient 0.3, camber peak at 15 % chord), 24 % thick.
- NACA 5-digit 230xx: '2' × 3/2 = design lift coefficient 0.3; '30' = camber peak at 15 % chord on a simple mean line; last two digits = maximum thickness in % of chord (NACA Report 610; TM-4741).
- 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  0.277  4.017  2.223  -3.304
2.5  1.331  5.763  3.669  -4.431
5  3.853  8.171  6.147  -5.861
7.5  6.601  9.843  8.399  -6.860
10  9.423  11.049  10.577  -7.647
15  15.001  12.529  14.999  -8.852
20  20.253  13.239  19.747  -9.705
25  25.262  13.535  24.738  -10.222
30  30.265  13.544  29.735  -10.453
40  40.256  12.922  39.744  -10.272
50  50.233  11.674  49.767  -9.466
60  60.201  9.975  59.799  -8.209
70  70.160  7.928  69.840  -6.603
80  80.114  5.583  79.886  -4.700
90  90.060  2.950  89.940  -2.509
95  95.031  1.518  94.969  -1.297
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-23024-airfoil/index.json
API: https://xemstudio.com/api/geometry?object=naca-23024-airfoil