Similarly shaped airfoils to DP1.72/8.16_DS
New! Bulk download of polars in Excel format: DP1.72_8.16_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
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.
2. DP1.82/8.21_DS
3. DP1.72/8.32_DS
4. DP1.79/8.37_DS
5. DP1.68/8.37_DS
6. TP50-DS
7. S2055
8. DP2.00/8.55_DS
9. BOEING 707 .99 SPAN
10. DP2.06/8.67_DS
11. DP2.05/8.65_DS
12. NACA M11 (NACA-TR-221)
13. BOEING 707 .54 SPAN
14. NACA65A309
15. KC-135 BL351.6
16. NACA64A309
17. DP1.87/9.07_DS
18. RG 14
19. NACA63A309
20. RK40
21. NACA M11