Similarly shaped airfoils to NACA65(4)-421
New! Bulk download of polars in Excel format: NACA65%284%29-421.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. NACA65-520
3. NACA65-420 a=0.8
4. NACA65-421
5. NACA64(4)-421
6. GA 40-320
7. GA 40A320
8. NACA64A420
9. NACA65-421 a=0.5
10. GA 37A320
11. NACA65-420 a=0.6
12. NACA63A420
13. NACA65-420
14. NACA65-620
15. NACA65A420
16. LS(1)-0421
17. GA 35A320
18. NACA65(4)-421 a=0.5
19. NACA65-420 a=0.5
20. NACA65-520 a=0.8
21. NACA64A520