Similarly shaped airfoils to GRUMMAN K-2
New! Bulk download of polars in Excel format: k2.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. WHITCOMB INTEGRAL SUPERCRITICAL
3. BOEING J
4. DSMA-523B
5. NPL FROM ARC CP 1372
6. SC(2)-0410
7. RAE 2822
8. RAE 6-9CK
9. SC(2)-0412
10. NPL 9510
11. NYU/GRUMMAN K-1
12. SC(2)-0610
13. RC-SC2
14. SC(2)-0612
15. SC(2)-0710
16. LOCKHEED C-5A BL488.2
17. RAE 5215
18. NACA65-211
19. LOCKHEED C-5A BL758.6
20. LOCKHEED C-5A BL576
21. NACA64A111