Similarly shaped airfoils to NACA0010
New! Bulk download of polars in Excel format: NACA0010.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (23) | 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 30A010
3. SD8020-010-88
4. Horten 10.00% thick 0.00% camber
5. FX 76-100
6. RYAN BQM-34 FIREBEE WING
7. RAF 27
8. HN-840S
9. HN-312S
10. RAE 101
11. TP36-9.5%
12. RAE 102
13. HQ 0/10
14. EPPLER 228
15. RAE 100
16. ONERA D, SHARP TRAILING EDGE
17. GA 35A010
18. ONERA D, BLUNT TRAILING EDGE
19. HN-477S
20. HN-275S
21. NACA63A010