Similarly shaped airfoils to NACA M19


New! Bulk download of polars in Excel format: m19.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.

1. NACA M19 (NACA-TR-221)
2. NACA M22 (NACA-TR-221)
3. NACA M22
4. GOE 379
5. GOE 380
6. GOE 369
7. GOE 402
8. GOE 381
9. GOE 264
10. GOE 376
11. GOE 373
12. GOE 155 (SSW D.1)
13. NACA M20 (NACA-TR-221)
14. NACA M20
15. GOE 269
16. GOE 123
17. GOE 401
18. GOE 199 (L.F.G. 5406)
19. NACA M23
20. NACA M23 (NACA-TR-221)
21. GOE 335 (D.F.W.)