Similarly shaped airfoils to GOE 738
New! Bulk download of polars in Excel format: goe738.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. SSV2316 VANS RV-10
3. MID 371AW
4. DAVIS BASIC B-24 WING
5. NACA25015
6. NACA25014.5
7. NACA63-416 a=0.0
8. NACA2215
9. NACA63-316 a=0.2
10. Horten 15.00% thick 3.00% camber
11. NACA63-415 a=0.0
12. Horten 15.00% thick 2.00% camber
13. NACA63-315 a=0.2
14. HG 42
15. NACA63-416 a=0.2
16. HG 41
17. NACA2315
18. NACA63-316 a=0.0
19. NACA25014
20. NACA34015
21. NACA63-315 a=0.0