Similarly shaped airfoils to NPL 9615
New! Bulk download of polars in Excel format: npl9615.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. ONERA NACA CAMBRE
3. Ritz 1-30-12
4. NPL 9626
5. Horten 11.00% thick 1.00% camber
6. NPL 9627
7. MJZ1211
8. GIII BL45
9. NACA1412
10. GIII BL0
11. NACA64-212 a=0.0
12. NACA23012
13. RC-12(N)1
14. NACA63A112
15. NACA65-212 a=0.0
16. NACA64-212 a=0.2
17. NACA64A112
18. NACA63-212 a=0.0
19. AMES A-01
20. HAWKER TEMPEST 61% SEMISPAN
21. NACA63A111