Similarly shaped airfoils to BOEING-VERTOL VR-1


New! Bulk download of polars in Excel format: vr1.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. LOCKHEED C-5A BL1256
2. GA 35A211
3. GA 37A211
4. GA 30A211
5. GA 30-211
6. NACA63A211
7. NACA64A211
8. LOCKHEED C-141 BL610.61
9. NACA2411
10. HQ 1.5/11
11. GA 37A212
12. GA 35A212
13. NACA65-311
14. NACA65(1)-212 a=0.6
15. NACA65-211 a=0.6
16. NACA63A311
17. NACA64-312
18. LOCKHEED C-141 BL426.57
19. NACA65-211 a=0.5
20. NACA64A311
21. BOEING BACXXX