Similarly shaped airfoils to GA(PC)1 landing flap


New! Bulk download of polars in Excel format: GA%28PC%291_landing.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
Dynamic plotter New!
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.

1. NACA34016.5
2. NACA34017
3. GA(PC)1 climb flap
4. NACA25116.5
5. NACA34016
6. NACA25117
7. NACA33016.5
8. NACA25116
9. Horten 17.00% thick 3.00% camber
10. NACA33017
11. NACA33016
12. NACA25016.5
13. Horten 16.00% thick 3.00% camber
14. NACA25017
15. NACA25016
16. NACA24116.5
17. Horten 17.00% thick 2.00% camber
18. NACA33116.5
19. NACA34018
20. NACA35018
21. NACA24016.5