Similarly shaped airfoils to LS(1)-0417 (GA(W)-1)
New! Bulk download of polars in Excel format: NASA%20LS%281%29-0417.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (65) | 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. NACA65-518
3. NACA63A418
4. NACA63A417
5. NACA64A417
6. NACA65-418 a=0.8
7. NACA64(3)-418
8. NACA65-517
9. EPPLER 545
10. NACA64-518
11. NACA65-417 a=0.8
12. NACA65A417
13. NACA65-418
14. GA 37A318
15. NACA64-418 a=0.8
16. GOE 601
17. GA 35A318
18. DORNIER A-5
19. GA 37A317
20. GA 40A318
21. GA 35A317