Similarly shaped airfoils to NLF(1)-0115
New! Bulk download of polars in Excel format: nlf0115.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. GA 37A215
3. GA 40-215
4. NACA65-415
5. NACA65A315
6. NACA65-315 a=0.8
7. NACA64A315
8. GA 35A215
9. GA 40A216
10. NACA65(2)-415
11. GA 40-216
12. NACA65-315 a=0.6
13. NACA65-416
14. SOMERS S102 (BLUNT)
15. NACA65-315 a=0.5
16. GA 37A216
17. LOCKHEED L-188 ROOT
18. NACA63A315
19. NACA65-316 a=0.8
20. NACA65-415 a=0.0
21. EPPLER 546