Similarly shaped airfoils to NACA M5
New! Bulk download of polars in Excel format: m5.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. B-29 TIP
3. BOEING-VERTOL VR-14
4. JWL066 8.7/1.9
5. NACA25009
6. JWL075 8.8/1.76
7. GIII BL430
8. NACA25109
9. GIII BL387
10. TsAGI B 8.5% thick
11. NACA24009
12. BW 05 02 09
13. MH 20 9.01%
14. GIII BL369
15. TsAGI B 9.0% thick
16. GIII BL450
17. Horten 9.00% thick 2.00% camber
18. NACA24109
19. RC-08(N)1
20. NACA2209
21. BOEING-VERTOL VR-15