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
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 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