Similarly shaped airfoils to NACA M20
New! Bulk download of polars in Excel format: m20.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
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. GOE 311 (MVA H.43)
3. GOE 336 (MVA H.44)
4. GOE 199 (L.F.G. 5406)
5. WACO COOTIE
6. GOE 140 (MVA H.17)
7. NACA6209
8. GOE 238 (HANSA-BRANDENBURG)
9. GOE 308 (MVA H.40)
10. GOE 360
11. GOE 610 B
12. GOE 174 (ALBATROS 5020)
13. GOE 124 (MVA H.4)
14. GOE 207 (AVIATIK V8)
15. NACA M19
16. GOE 287
17. USA 25
18. GOE 380
19. GOE 359
20. GOE 184 (MVA H.29)
21. GOE 155 (SSW D.1)