Similarly shaped airfoils to NACA M23
New! Bulk download of polars in Excel format: m23.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA M23 (NACA-TR-221)
3. NACA M20
4. NACA M22
5. NACA M22 (NACA-TR-221)
6. GOE 336 (MVA H.44)
7. NACA M19 (NACA-TR-221)
8. NACA M19
9. GOE 311 (MVA H.43)
10. GOE 238 (HANSA-BRANDENBURG)
11. WACO COOTIE
12. NACA6209
13. GOE 199 (L.F.G. 5406)
14. GOE 308 (MVA H.40)
15. Horten 9.00% thick 7.00% camber
16. GOE 140 (MVA H.17)
17. GOE 207 (AVIATIK V8)
18. GOE 360
19. USA 25
20. GOE 287
21. NACA M8 (NACA-TR-221)