Similarly shaped airfoils to BOEING VERTOL V13006-.7
New! Bulk download of polars in Excel format: v13006.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. TsAGI B 6.0% thick
3. TsAGI B 6.5% thick
4. EH 1.0/7.0
5. HT23
6. PW2019 tip airfoil 3m
7. GOE 598
8. RAF 25
9. BOEING-VERTOL VR-9
10. D6213-S
11. NACA22007
12. TP96-0.75%
13. TP96-1%
14. NACA22107
15. salazV3root
16. TP96-0.5%
17. FAD17
18. MJP712
19. SIKORSKY SSC-A07
20. TsAGI B 7.0% thick
21. NACA22005