Similarly shaped airfoils to HAWKER TEMPEST 96.77% SEMISPAN
New! Bulk download of polars in Excel format: tempest3.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. GIII BL86
3. GIII BL75
4. NACA65A210
5. NACA65A110
6. NACA66-210 a=0.0
7. NACA65-210 a=0.0
8. NACA66-210
9. NACA64A210
10. NACA65-210
11. NACA66-210 a=0.2
12. NACA64A110
13. KC-135 BL200.76
14. NACA65-210 a=0.2
15. NACA65-211 a=0.0
16. NACA63A210
17. NACA65-211
18. NACA63A110
19. NACA64A211
20. NACA66-110 a=0.6
21. NACA1410