Similarly shaped airfoils to NACA24009
New! Bulk download of polars in Excel format: NACA24009.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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. NACA23009
3. GIII BL430
4. NACA24109
5. GIII BL387
6. JWL075 8.8/1.76
7. JWL066 8.7/1.9
8. PW98 sm
9. NACA2209
10. Horten 9.00% thick 2.00% camber
11. NACA32009
12. NACA23109
13. GIII BL369
14. JWL068 9.5/1.7
15. ONERA OA209
16. GIII BL450
17. EH 1.5/9.0
18. PW106 sm
19. BOEING-VERTOL VR-14
20. BOEING VERTOL V(1.95)3009-1.25
21. PW51 sm