Similarly shaped airfoils to DU 86-084/18
New! Bulk download of polars in Excel format: du8608418.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 BL288
3. NACA65-209 a=0.2
4. NACA65-209 a=0.0
5. MH 34
6. GIII BL207
7. GIII BL332
8. NACA65-209 a=0.5
9. GIII BL167
10. SIKORSKY SSC-A09
11. NACA64-209 a=0.2
12. NACA64-209 a=0.0
13. MH 23 8%
14. GIII BL145
15. NACA65-209 a=0.6
16. RC-08(B)3
17. TsAGI B 8.5% thick
18. NACA65-209
19. RC08-64C
20. NACA64A209
21. NACA64-209 a=0.5