Similarly shaped airfoils to FX 84-W-097
New! Bulk download of polars in Excel format: fx84w097.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
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.
2. NACA63-410 a=0.5
3. S3021-095-84
4. S3014-095-85
5. NACA64-410 a=0.5
6. GA 35-310
7. NACA63-410 a=0.6
8. GA 37-310
9. ELINA
10. EPPLER 205
11. NACA64-410 a=0.6
12. SD8040 (10%)
13. GA 35A310
14. MH 117 9.8%
15. NACA63-510 a=0.0
16. GA 30-310
17. SD7084 (9.6%)
18. SD2083 (9.0%)
19. JWL045 9.2/2.7
20. NACA64-510 a=0.0
21. NACA3410