Similarly shaped airfoils to MID 327 18%
New! Bulk download of polars in Excel format: MID%20327%2018%25.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. NACA3418
3. GA 30-318
4. GA 30A317
5. GA 30A318
6. GA 35-318
7. NACA63-518
8. NACA63-418 a=0.6
9. NACA63(3)-418
10. GA 35-319
11. NACA63-418 a=0.8
12. LS(1)-0417MOD
13. NACA63-519
14. GA 35A318
15. NACA63-418 a=0.5
16. NACA63-419 a=0.6
17. NACA63-419 a=0.8
18. GA 30-316
19. GA 30-217
20. NACA63-419 a=0.5
21. NACA63A418