Similarly shaped airfoils to NPL 9510
New! Bulk download of polars in Excel format: npl9510.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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. WHITCOMB INTEGRAL SUPERCRITICAL
3. DSMA-523A
4. SC(2)-0410
5. SC(2)-0610
6. SC(2)-0412
7. RAE 6-9CK
8. RAE 2822
9. SC(2)-0710
10. BOEING J
11. SC(2)-0612
12. GRUMMAN K-2
13. SC(2)-0712
14. NYU/GRUMMAN K-1
15. HN-478S
16. Horten 11.00% thick 0.00% camber
17. JWL069 11/0
18. GA 30-011
19. HN-976S
20. GA 35-011
21. GA 30A011