Similarly shaped airfoils to MH 53
New! Bulk download of polars in Excel format: MH%2053.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
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2. NACA64A-010
3. NACA0010-34
4. GA 37A010
5. NACA66-110 a=0.0
6. NACA65-110 a=0.0
7. RAE 103
8. NACA66-109 a=0.0
9. NACA63A010
10. MH 52
11. NACA66-110 a=0.2
12. NACA65-110 a=0.2
13. NACA65A110
14. LWK 80-100
15. GA 40A010
16. ONERA D, SHARP TRAILING EDGE
17. ONERA D, BLUNT TRAILING EDGE
18. NACA66-009
19. NACA67-109 a=0.0
20. GA 35A010
21. NACA66-110