Similarly shaped airfoils to USA 45 M
New! Bulk download of polars in Excel format: usa45m.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. Ritz 3-30-12
3. BOEING-VERTOL VR-7 WITH TAB
4. MS3-11Retro
5. MH 70 11.08%
6. NACA63-612 a=0.0
7. NACA45012
8. NACA63-512 a=0.2
9. EPPLER 637
10. NACA45010.5
11. NACA64-612 a=0.0
12. EPPLER 334
13. BOEING-VERTOL VR-5
14. TsAGI R-3A (12%)
15. MS3,3-11GPT
16. NACA63-611 a=0.0
17. NACA63-612 a=0.2
18. NACA64-512 a=0.2
19. NACA63-511 a=0.2
20. NACA44012
21. MS3/11GPV