Similarly shaped airfoils to QA002
New! Bulk download of polars in Excel format: QA002.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. QA001
3. QA001sm
4. NACA65A518
5. NACA65A517
6. NACA66-617
7. RONCZ 1082 VOYAGER ROOT OUTER AFT WING
8. NACA66-618
9. FX 60-177
10. GA 37A418
11. NACA64A518
12. RONCZ 1080 VOYAGER INNER AFT WING
13. NACA65-618
14. NACA66A517
15. NACA66-517 a=0.8
16. GA 40A418
17. NACA66A518
18. NACA66-518 a=0.8
19. GA 40-418
20. DU 80-176 V1 alt
21. FX S 03-182