Similarly shaped airfoils to Horten 20.00% thick 0.00% camber
New! Bulk download of polars in Excel format: Horten%2020.00%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 30A020
3. GA 30-019
4. GA 30A019
5. Horten 19.00% thick 0.00% camber
6. Horten 20.00% thick 1.00% camber
7. NACA0021
8. GOE 460
9. Horten 19.00% thick 1.00% camber
10. GA 35A020
11. GOE 775
12. NACA63-021
13. GA 35-020
14. NACA64-021
15. NACA63A120
16. GA 30-018
17. GA 30A018
18. GA 37-020
19. GA 35A019
20. GA 37A020
21. NACA23019