Similarly shaped airfoils to SIKORSKY SSC-A09
New! Bulk download of polars in Excel format: ssca09.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. NLR-7223-62
3. GIII BL332
4. GIII BL126
5. DU 86-084/18
6. NLR-1T
7. MH 34
8. GIII BL288
9. GIII BL369
10. BOEING 737 MIDSPAN
11. BOEING VERTOL V(1.95)3009-1.25
12. TsAGI B 9.0% thick
13. NACA65-209 a=0.0
14. NACA65-210 a=0.2
15. NACA65-209 a=0.2
16. NACA65-210 a=0.0
17. MH 24 9.01%
18. NACA64-210 a=0.2
19. RG-12
20. NACA64-210 a=0.0
21. Ritz 1-30-10