Similarly shaped airfoils to MS(1)-0317
New! Bulk download of polars in Excel format: NASA%20MS%281%29-0317.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA63A317
3. GA 35A218
4. GA 30-217
5. GA 35A217
6. NACA64A318
7. MH 95 15.86%
8. NACA64-418
9. GA 37-218
10. NACA64A317
11. NACA64-318 a=0.8
12. MH 94 16.03%
13. GA 37A218
14. GA 37A217
15. NACA64-318
16. GA 30A217
17. EPPLER 545
18. NACA65-318
19. GA 35-218
20. NACA65-318 a=0.8
21. NACA65-418