Similarly shaped airfoils to LS(1)-0413 (GA(W)-2)


New! Bulk download of polars in Excel format: NASA%20LS%281%29-0413.xlsx


Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (17) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
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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1. MH 200 12.97%
2. NACA63A413
3. NACA64A413
4. NACA64A414
5. NACA63A414
6. NACA65-413
7. LS(1)-0413MOD
8. PSU-90-125WL
9. NACA64-514
10. NACA65-513
11. NACA65-413 a=0.8
12. NACA65-514
13. NACA64-414 a=0.8
14. NACA65-414 a=0.8
15. NACA65A413
16. HN-956
17. NACA65-414
18. NACA64-414
19. MH 201 13.08%
20. CB2513
21. Jedeslsky EJ1