Similarly shaped airfoils to DP1.72/8.32_DS
New! Bulk download of polars in Excel format: DP1.72_8.32_DS.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. DP1.72/8.16_DS
3. DP1.77/8.23_DS
4. DP1.82/8.21_DS
5. DP1.68/8.37_DS
6. TP50-DS
7. S2055
8. NACA64A309
9. NACA65A309
10. NACA63A309
11. DP2.00/8.55_DS
12. BOEING 707 .99 SPAN
13. RG 14
14. DP2.06/8.67_DS
15. DP1.87/9.07_DS
16. DP2.05/8.65_DS
17. RG 12A-1.8/9.0
18. RG-12A 9.00%
19. NACA65-309
20. NACA65-309 a=0.8
21. HS 1.7/9