Similarly shaped airfoils to HS 602
New! Bulk download of polars in Excel format: HS%20602.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. EM J19 3010
3. Joukowsky 10.00% thick 3.00% camber
4. EM J8 3010 DrW
5. EM J18 2610 27 48
6. FX 60-100 10.0% smoothed
7. EM J18 2510 26 51
8. NACA63-610
9. EM L3 2510
10. SB96 10.5/3.0
11. NACA63-510 a=0.8
12. Joukowsky 11.00% thick 3.00% camber
13. EM J8 2510 DrW
14. EM J20 2510
15. EPPLER 212
16. OAF102
17. HQ 3.0/10
18. MH 117 9.8%
19. NACA63-510
20. S2046
21. NACA64-610