Similarly shaped airfoils to NACA M20 (NACA-TR-221)
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
3. NACA M23 (NACA-TR-221)
4. GOE 336 (MVA H.44)
5. WACO COOTIE
6. GOE 311 (MVA H.43)
7. GOE 308 (MVA H.40)
8. GOE 238 (HANSA-BRANDENBURG)
9. GOE 199 (L.F.G. 5406)
10. GOE 140 (MVA H.17)
11. NACA6209
12. GOE 287
13. NACA M22
14. NACA M22 (NACA-TR-221)
15. NACA M19 (NACA-TR-221)
16. NACA M19
17. USA 25
18. GOE 610 B
19. GOE 360
20. NACA M8 (NACA-TR-221)
21. GOE 326 (PFALZ 55)