Similarly shaped airfoils to I.S.A. 961
New! Bulk download of polars in Excel format: isa961.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
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2. I.S.A. 962
3. FAD21
4. GOE 286
5. NACA63-710 a=0.0
6. NACA64-710 a=0.0
7. AQUILA 9.3% smoothed
8. NACA63-610 a=0.2
9. GOE 385
10. GOE 316 (HANSA-BRANDENBURG IV.5)
11. GOE 309 (MVA H.41)
12. NACA64-610 a=0.2
13. GOE 318 (HANSA-BRANDENBURG VI.5)
14. GOE 596
15. Eiffel 428 (Bleriot)
16. NACA63-710 a=0.2
17. GOE 490
18. NACA65-710 a=0.0
19. NACA64-710 a=0.2
20. NACA45010
21. USA 26