Similarly shaped airfoils to NACA45021
New! Bulk download of polars in Excel format: NACA45021.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. NACA35021
3. GOE 683
4. NACA34021
5. TsAGI B 20.0% thick
6. TsAGI B 20.5% thick
7. NACA45121
8. NACA44021
9. NACA45019
10. TsAGI B 19.5% thick
11. Horten 20.00% thick 4.00% camber
12. TsAGI B 21.0% thick
13. GOE 703
14. Horten 20.00% thick 3.00% camber
15. NACA35119
16. NACA35019
17. TsAGI B 19.0% thick
18. Horten 20.00% thick 5.00% camber
19. TsAGI B 21.5% thick
20. LS(1)-0421MOD
21. NACA44121