Similarly shaped airfoils to GIII BL332


New! Bulk download of polars in Excel format: giiij.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
Dynamic plotter New!
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. GIII BL288
2. GIII BL369
3. GIII BL387
4. GIII BL207
5. GIII BL167
6. GIII BL145
7. TsAGI B 8.5% thick
8. NACA65-209 a=0.2
9. GIII BL126
10. BOEING-VERTOL VR-15
11. MH 23 8%
12. MH 34
13. DU 86-084/18
14. NACA64-209 a=0.2
15. NACA65-209 a=0.0
16. SIKORSKY SSC-A09
17. NACA64-209 a=0.0
18. TsAGI B 8.0% thick
19. NACA65-209 a=0.5
20. NACA63-209 a=0.2
21. DD928416