Similarly shaped airfoils to S3024 9.84%
New! Bulk download of polars in Excel format: s3024.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. EPPLER 193
3. GA 30A410
4. EPPLER E193gU-K24
5. GA 35A410
6. NACA63-510 a=0.5
7. NACA64-510 a=0.5
8. NACA63-510 a=0.6
9. GA 37A410
10. GOE 595
11. MID 321b
12. GA 35-410
13. S3025 9.38%
14. GA 37-410
15. MID 321c
16. NACA64-510 a=0.6
17. MVR22
18. GOE 670
19. GOE 602
20. GA 35-411
21. HQ 3.0/10