Similarly shaped airfoils to NLR-7223-43
New! Bulk download of polars in Excel format: nl722343.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. HQ 1.5/9 B
3. HQ 1.5/9
4. NACA63A209
5. RG 14 9%
6. NACA64A209
7. RG 14
8. S2050 8.93%
9. SB96VS 9.75/1.25
10. NACA64-309
11. NACA64-209 a=0.8
12. NACA65-209 a=0.8
13. DD928416
14. HQ 1.5/8.5
15. NACA65-309
16. GIII BL332
17. GIII BL369
18. HQ 1.0/9
19. MH 34
20. NACA63-309
21. NACA63-209 a=0.8