Similarly shaped airfoils to BOEING-VERTOL VR-14
New! Bulk download of polars in Excel format: vr14.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. GIII BL430
3. JWL066 8.7/1.9
4. GIII BL387
5. GIII BL369
6. NACA M5
7. JWL075 8.8/1.76
8. NACA25009
9. GIII BL450
10. NACA2209
11. NACA24009
12. GIII BL332
13. BOEING-VERTOL VR-15
14. DD928416
15. KC-135 BL351.6
16. RG 14
17. BOEING 707 .54 SPAN
18. PW98-mod sm
19. GIII BL288
20. NACA64-309 a=0.0
21. DP1.77/8.23_DS