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
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
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2. NACA M22
3. GOE 336 (MVA H.44)
4. NACA M19
5. GOE 311 (MVA H.43)
6. GOE 238 (HANSA-BRANDENBURG)
7. WACO COOTIE
8. NACA6209
9. GOE 199 (L.F.G. 5406)
10. GOE 308 (MVA H.40)
11. Horten 9.00% thick 7.00% camber
12. GOE 140 (MVA H.17)
13. GOE 207 (AVIATIK V8)
14. GOE 360
15. USA 25
16. GOE 287
17. NACA6210
18. GOE 380
19. GOE 610 B
20. Horten 9.00% thick 8.00% camber
21. GOE 314 (HANSA-BRANDENBURG)