Similarly shaped airfoils to NACA22009
New! Bulk download of polars in Excel format: NACA22009.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. Horten 9.00% thick 1.00% camber
3. BOEING VERTOL V(1.95)3009-1.25
4. NACA23109
5. NACA22109
6. EH 1.0/9.0
7. EH 1.5/9.0
8. ONERA OA209
9. PW75
10. PW51
11. PW75 sm
12. PW51 sm
13. BOEING-VERTOL VR-15
14. JWL074 8.5/1.2
15. SIKORSKY SSC-A09
16. AZ2004_9
17. TsAGI B 8.5% thick
18. AZ2005tip
19. Horten 9.00% thick 2.00% camber
20. NACA63-209 a=0.0
21. JWL068 9.5/1.7