Similarly shaped airfoils to AH 82-150 A
New! Bulk download of polars in Excel format: ah82150a.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. NACA65-615
3. GA 40-415
4. GA 40A415
5. cristal_cb85_15_7
6. NACA65-515 a=0.8
7. NACA65-515 a=0.6
8. NACA65-716
9. GA 40-416
10. GA 37A415
11. GA 40A416
12. NACA65A515
13. NACA65-616
14. NACA65-515 a=0.5
15. NACA65(2)-415 a=0.5
16. NACA65-516 a=0.8
17. DU 99-146
18. NACA65-615 a=0.8
19. NACA64A515
20. NACA65-516 a=0.6
21. NACA66-615