Similarly shaped airfoils to GIII BL126
New! Bulk download of polars in Excel format: giiie.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. NACA65-209 a=0.2
3. GIII BL288
4. GIII BL207
5. GIII BL167
6. DU 86-084/18
7. TsAGI B 8.5% thick
8. GIII BL145
9. NACA66-209 a=0.0
10. GIII BL332
11. RC-08(B)3
12. NACA66-209 a=0.2
13. RC08-64C
14. NACA64-209 a=0.0
15. SIKORSKY SSC-A09
16. TsAGI B 9.0% thick
17. NACA64-209 a=0.2
18. MH 34
19. TsAGI B 8.0% thick
20. NACA65-209 a=0.5
21. GIII BL369