NACA63A420
NACA 63A-420
New! Bulk download of polars in Excel format: NACA63A420.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (20) | 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.
Known applications:
Grumman G-101 wing root
Grumman G-103 CS2F-1 wing root
Grumman G-104 wing root
Grumman G-106 wing root
Grumman G-115 wing root
Grumman G-117 E-1 Tracer wing root
Grumman G-117 WF-2 Tracer wing root
Grumman G-120 wing root
Grumman G-121 S2F-3 Tracker wing root
Grumman G-125 C-1 Trader wing root
Grumman G-125 TF-1Q wing root
Grumman G-126 wing root
Grumman G-137 wing root
Grumman G-142 wing root
Grumman G-165 wing root
Grumman G-215 wing root
Grumman G-89 S2F Tracker wing root
Grumman G-89 S-2 Tracker wing root
Grumman G-95 XWF-1 wing root
Grumman G-96 TF-1/C-1 Trader wing root