Similarly shaped airfoils to RAE 5214
New! Bulk download of polars in Excel format: rae5214.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. SB96V 9.35/1.25
4. NACA63-210 a=0.8
5. HQ 1.5/10
6. NACA63-310
7. TP-CIEL-S
8. HQ 1.0/10
9. HM10011
10. EM CY 1016 1510
11. NACA64-210 a=0.8
12. RG-12
13. S2050 8.93%
14. NACA63-210
15. NM20 root
16. SB96VS 9.75/1.25
17. NACA64-310
18. NACA63-210 a=0.6
19. AIR 100-2 Acro MM 576 1999
20. HQ 1.5/9 B
21. NLR-7223-43