Similarly shaped airfoils to HM391-2
New! Bulk download of polars in Excel format: HM391-2.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. NACA23110.5
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4. NACA23110
5. NACA22010
6. NACA23010
7. NACA23010.5
8. Horten 10.00% thick 2.00% camber
9. NACA22010.5
10. NACA22110
11. NACA22110.5
12. Horten 11.00% thick 1.00% camber
13. Horten 11.00% thick 2.00% camber
14. BOEING-VERTOL V23010-1.58
15. JWL081 11/1.3
16. EPPLER 186
17. NACA32110.5
18. SIKORSKY SC1095
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20. LOCKHEED-GEORGIA SUPERCRITICAL
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