Similarly shaped airfoils to AH 93-W-145
New! Bulk download of polars in Excel format: ah93w145.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. NACA64-615 a=0.5
3. DEFIANT CANARD BL110
4. NACA63-614 a=0.5
5. NACA64-614 a=0.5
6. GA 35A414
7. FX 84-W-140
8. FX 79-W-151 A
9. GA 35-415
10. GA 37-415
11. NACA63-615 a=0.6
12. MS3,3-15GP
13. GA 30-414
14. NACA64-615 a=0.6
15. MID 321d
16. HQ 3.5/14
17. GA 30-413.5
18. MRC-16
19. GA 37-414
20. BOEING 106
21. GA 35-414