LANGLEY SUBSONIC WIND TUNNEL // NACA 2412 CAMBER
Laminar Smoke Streamline Deflection
ATTACHED LAMINAR FLOW
Angle of Attack (α)
+6.0°
Tunnel Velocity
Mach 0.32
LIFT COEFFICIENT (Cl)
0.86 Cl
LIFT-TO-DRAG RATIO
18.4 L/D