Similarly shaped airfoils to NACA23009
New! Bulk download of polars in Excel format: NACA23009.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (133) | 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. NACA24009
3. BOEING VERTOL V(1.95)3009-1.25
4. ONERA OA209
5. NACA22009
6. EH 1.5/9.0
7. Horten 9.00% thick 2.00% camber
8. NACA32009
9. PW75
10. PW51
11. JWL068 9.5/1.7
12. PW75 sm
13. GIII BL387
14. PW51 sm
15. GIII BL369
16. BOEING-VERTOL VR-15
17. NACA24109
18. GIII BL332
19. TsAGI B 8.5% thick
20. TsAGI B 9.0% thick
21. AZ2004_9