Similarly shaped airfoils to DSMA-523B
New! Bulk download of polars in Excel format: dsma523b.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. DSMA-523A
3. SC(2)-0412
4. RAE 6-9CK
5. RAE 2822
6. BOEING J
7. SC(2)-0612
8. GRUMMAN K-2
9. NYU/GRUMMAN K-1
10. SC(2)-0410
11. NPL 9510
12. NPL FROM ARC CP 1372
13. SC(2)-0712
14. SC(2)-0610
15. SC(2)-0710
16. NACA64(1)-112
17. NACA63-212
18. NACA63-112 a=0.8
19. NACA63-112
20. NACA64-212
21. NACA63A111