Similarly shaped airfoils to WHITCOMB INTEGRAL SUPERCRITICAL
New! Bulk download of polars in Excel format: whitcomb.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-523B
3. GRUMMAN K-2
4. SC(2)-0412
5. BOEING J
6. NYU/GRUMMAN K-1
7. NPL FROM ARC CP 1372
8. RAE 2822
9. RAE 6-9CK
10. NPL 9510
11. SC(2)-0410
12. SC(2)-0612
13. SC(2)-0610
14. SC(2)-0712
15. SC(2)-0710
16. NACA63-212
17. NACA63-211
18. NACA64(1)-112
19. NACA64-212
20. NACA63-112 a=0.8
21. NACA64(1)-212