Similarly shaped airfoils to BOEING-VERTOL VR-9


New! Bulk download of polars in Excel format: vr9.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. SC(2)-0406
2. NACA0006
3. GOE 444
4. SC(2)-0606
5. GOE 445
6. EPPLER EA 8(-1)-006
7. NACA M1 (NACA-TR-221)
8. NACA M1
9. S1010 HPV airfoil
10. SC(2)-0706
11. ONERA OA206
12. BOEING VERTOL V13006-.7
13. GOE 443
14. TP96-0.5%
15. HQ 0/7
16. TsAGI B 6.0% thick
17. DA5206
18. TP29-7%
19. TP96-0.75%
20. NM08
21. HT13