Similarly shaped airfoils to NACA23010.5
New! Bulk download of polars in Excel format: NACA23010.5.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (6) | 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. NACA24010.5
3. LOCKHEED-GEORGIA SUPERCRITICAL
4. NACA23110
5. BOEING-VERTOL V23010-1.58
6. NACA32010.5
7. HM391-1
8. NACA24010
9. AMES A-01
10. Horten 11.00% thick 2.00% camber
11. NACA32010
12. NACA23110.5
13. NACA24110.5
14. Horten 10.00% thick 2.00% camber
15. HM391-2
16. JWL081 11/1.3
17. REPUBLIC S-3
18. JWL067 11.5/1.7
19. NACA25010.5
20. Sipkill 1.7/10
21. AMES A-03