Similarly shaped airfoils to GIII BL145
New! Bulk download of polars in Excel format: giiif.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
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.
2. GIII BL207
3. GIII BL288
4. GIII BL332
5. GIII BL126
6. RC08-64C
7. MH 23 8%
8. NACA65-209 a=0.2
9. RC-08(B)3
10. NACA65-209 a=0.0
11. TsAGI B 8.0% thick
12. ZAGI 08
13. DU 86-084/18
14. TsAGI B 8.5% thick
15. GIII BL369
16. NACA65-209 a=0.5
17. BOEING-VERTOL VR-15
18. NACA64-209 a=0.2
19. NACA64-209 a=0.0
20. NACA66-209 a=0.2
21. NACA66-209 a=0.0