Similarly shaped airfoils to AH 79-K-135/20 B
New! Bulk download of polars in Excel format: ah79k135.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. GA 40-414
3. NACA65-514 a=0.5
4. GA 37A414
5. NACA65-514 a=0.2
6. NACA65-414 a=0.5
7. GA 35A414
8. NACA65-414 a=0.6
9. NACA65-514 a=0.6
10. GA 40A314
11. GA 40-314
12. AH 79-K-143/18
13. NACA65-614 a=0.0
14. GA 40A413
15. GA 37A413
16. GA 40-413
17. GA 37A314
18. NACA65-513 a=0.5
19. AH 79-K-132/20
20. GA 37-414
21. NACA65-513 a=0.2