Similarly shaped airfoils to Horten 19.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Horten%2019.00%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 30A019
3. GA 30-018
4. GA 30A018
5. NACA0018
6. Horten 18.00% thick 0.00% camber
7. Horten 20.00% thick 0.00% camber
8. Horten 19.00% thick 1.00% camber
9. US1000ROOT (Great Planes R/C Ultra-Sport 1000)
10. GA 30-020
11. GA 35A019
12. Horten 20.00% thick 1.00% camber
13. Horten 18.00% thick 1.00% camber
14. GA 30A020
15. GA 35-020
16. GA 35-019
17. GA 35A020
18. TRAINER60
19. NACA23018.87
20. NACA23019
21. GA 37-020