Similarly shaped airfoils to Horten 18.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Horten%2018.00%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 30-018
3. GA 30A018
4. GA 30-017
5. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
6. GA 30A017
7. NACA0017
8. Horten 17.00% thick 0.00% camber
9. Horten 19.00% thick 0.00% camber
10. TRAINER60
11. Horten 18.00% thick 1.00% camber
12. GA 30-019
13. GA 35A018
14. NACA63A018
15. GA 35-019
16. GA 30A019
17. Horten 19.00% thick 1.00% camber
18. Horten 17.00% thick 1.00% camber
19. GA 35-018
20. GA 35A019
21. NACA63(3)-018