Similarly shaped airfoils to FX 049-915


New! Bulk download of polars in Excel format: fx049915.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
Dynamic plotter New!
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

Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.

1. GOE 324 (HANSA-BRANDENBURG)
2. GOE 654
3. GOE 322 (HANSA-BRANDENBURG IV.1)
4. GOE 530
5. GOE 404
6. AUGUST 160
7. NACA M21 (NACA-TR-221)
8. NACA M21
9. GOE 398
10. Glenn Martin 2
11. TsAGI R-3AM-C16-f6
12. NACA6215
13. GOE 549
14. GOE 758
15. GOE 387
16. NACA6212
17. GOE 584
18. NACA M24
19. GOE 615
20. MID 393
21. GOE 562