Similarly shaped airfoils to TT54
New! Bulk download of polars in Excel format: TT54.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. JWL079 9.7/2.7
3. S3016-095-87
4. S3014-095-85
5. FAD14
6. SD7084 (9.6%)
7. Bartel 37 IIa 10%
8. NM19-S tip
9. MS2-9,5
10. NACA63-410 a=0.2
11. NM18 root
12. JWL077 10/2
13. NACA63-410 a=0.0
14. S3010-103-84
15. GA 30-310
16. SD8040 (10%)
17. SB99blkr root
18. USA 51
19. SD5060 (9.5%)
20. EPPLER 221
21. FAD13