Similarly shaped airfoils to NACA22107
New! Bulk download of polars in Excel format: NACA22107.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. NACA23107
3. NACA23007
4. EH 1.0/7.0
5. TsAGI B 7.0% thick
6. TsAGI B 6.5% thick
7. SIKORSKY SSC-A07
8. salazV3tip
9. salazV3root
10. FAD17
11. PW Rennbrett Strak 2 final Mod_GDES
12. TP100
13. ONERA OA206
14. JWL097 7.7/1.6
15. TsAGI B 7.5% thick
16. BOEING VERTOL V13006-.7
17. PW2019 Strak 1 3m
18. AZ2007_8_1.2_tip
19. JWL065 7.9/1.7
20. JWL030 7.5/0.9
21. FAD16