Similarly shaped airfoils to TP28-4
New! Bulk download of polars in Excel format: TP28-4.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. NACA1409
3. TP60J
4. RS001m60
5. Joukowsky 10.00% thick 1.00% camber
6. HQ 1.0/9
7. HQ 1.0/10
8. NACA63-210
9. SIKORSKY SC1095
10. Ritz 1-30-10
11. NACA1410
12. NACA63-209
13. HM10011
14. NACA63-210 a=0.0
15. NACA63-110 a=0.6
16. SB96V 9.35/1.25
17. EPPLER 226
18. NACA63-110 a=0.8
19. NACA64-210
20. BOEING VERTOL V(1.95)3009-1.25
21. Joukowsky 9.00% thick 1.00% camber