Similarly shaped airfoils to Horten 18.00% thick 1.00% camber
New! Bulk download of polars in Excel format: Horten%2018.00%25%20thick%201.00%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. Horten 19.00% thick 1.00% camber
3. Horten 17.00% thick 1.00% camber
4. NACA23017.424
5. Horten 18.00% thick 0.00% camber
6. NACA0018
7. NACA23118
8. GA 30-018
9. NACA24018
10. GA 30A018
11. NACA23017
12. NACA23018.87
13. TRAINER60
14. GA 30-017
15. GA 30A017
16. NACA23019
17. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
18. NACA0017
19. NACA23117
20. Horten 19.00% thick 2.00% camber
21. NACA25018