Similarly shaped airfoils to GIII BL387
New! Bulk download of polars in Excel format: giiil.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. GIII BL332
3. GIII BL430
4. GIII BL288
5. NACA24009
6. BOEING-VERTOL VR-14
7. NACA23009
8. DD928416
9. NACA25009
10. NACA M11
11. BOEING-VERTOL VR-15
12. NACA2209
13. RG 14
14. JWL075 8.8/1.76
15. TsAGI B 8.5% thick
16. NACA64-309 a=0.0
17. GIII BL207
18. NACA63-309 a=0.0
19. ONERA OA209
20. RG 14 9%
21. JWL066 8.7/1.9