Similarly shaped airfoils to NACA1409
New! Bulk download of polars in Excel format: NACA1409.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. MH 34
3. TP28-4
4. TP60J
5. NACA63-209
6. NACA63A209
7. NACA64-209
8. BOEING VERTOL V(1.95)3009-1.25
9. JWL074 8.5/1.2
10. Ritz 1-30-10
11. NACA63-209 a=0.0
12. SIKORSKY SC1095
13. Horten 9.00% thick 1.00% camber
14. DU 86-084/18
15. NACA63-209 a=0.2
16. NACA64-209 a=0.0
17. NACA64A209
18. NACA1408
19. NACA1410
20. NACA63A109
21. EH 1.0/9.0