Similarly shaped airfoils to Horten 15.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Horten%2015.00%25%20thick%200.00%25%20camber.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. GA 30-015
3. GA 30A015
4. EPPLER 477
5. EPPLER 475
6. GA 30-014
7. GA 30A014
8. Horten 16.00% thick 0.00% camber
9. Horten 14.00% thick 0.00% camber
10. Horten 15.00% thick 1.00% camber
11. S8035 (14%)
12. GA 35A015
13. NACA63-015A
14. NACA63A015
15. NACA0016
16. GA 35-016
17. GA 30-016
18. GA 35-015
19. NACA63-015
20. EPPLER 478
21. FX 71-L-150/30