Similarly shaped airfoils to HM50
New! Bulk download of polars in Excel format: HM50.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. JWL081 11/1.3
3. FAD04
4. AZcombat1
5. BOEING-VERTOL V23010-1.58
6. MH 61 10.26%
7. JWL077 10/2
8. NACA63-311 a=0.0
9. HM10011
10. MH 60 10.08%
11. HM55
12. HM56
13. TPR-95-96-95
14. NACA25010.5
15. NACA24010.5
16. NACA63-311 a=0.2
17. JWL067 11.5/1.7
18. NACA2210
19. MH 44 9.66%
20. NACA25010
21. NACA63-211 a=0.5