Similarly shaped airfoils to NPL FROM ARC CP 1372
New! Bulk download of polars in Excel format: nplx.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. RAE 5215
3. NYU/GRUMMAN K-1
4. GRUMMAN K-2
5. RAE 5213
6. RAE 5214
7. DSMA-523A
8. WHITCOMB INTEGRAL SUPERCRITICAL
9. DSMA-523B
10. NACA64-311
11. GOE 416A
12. NACA63-311
13. GOE 599
14. NACA64-211 a=0.8
15. NACA63-211 a=0.8
16. NACA63A211
17. NACA64-211
18. NACA65-311
19. NACA63-211
20. HQ 1.5/11
21. NACA64A211