Similarly shaped airfoils to MH 49
New! Bulk download of polars in Excel format: mh49.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. EPPLER 186
3. EPPLER 228
4. RS006m75
5. LWK 79-100
6. RS001t10
7. Joukowsky 10.00% thick 0.00% camber
8. JHSYM-10
9. NACA22110
10. RS001t
11. Horten II Tropfen symmetric 10%
12. RS001m60
13. Joukowsky 11.00% thick 0.00% camber
14. HN-275S
15. HN-477S
16. Horten 10.00% thick 1.00% camber
17. NACA22010
18. NACA63-110 a=0.0
19. FX 79-L-100
20. RAE 100
21. NACA63-110 a=0.2