Similarly shaped airfoils to AMES A-01
New! Bulk download of polars in Excel format: ames01.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. AMES A-03
3. NACA23010.5
4. NACA24010.5
5. TsAGI B 10.5% thick
6. TsAGI B 10.0% thick
7. NACA25010.5
8. ONERA NACA CAMBRE
9. JWL081 11/1.3
10. FX 69-H-098
11. TsAGI B 11.0% thick
12. Sipkill 1.7/10
13. RC-10(B)3
14. NACA23010
15. LOCKHEED C-5A BL1256
16. NACA24010
17. KC-135 BL200.76
18. BOEING 737 OUTBOARD
19. NPL 9615
20. NPL 9660
21. Horten 11.00% thick 2.00% camber