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Fluid dynamics / Lift / Airfoil / Shock wave / Boundary layer / Pressure coefficient / Mach number / Computational fluid dynamics / Stall / Aerodynamics / Aerospace engineering / Fluid mechanics
Date: 2014-06-16 15:21:24
Fluid dynamics
Lift
Airfoil
Shock wave
Boundary layer
Pressure coefficient
Mach number
Computational fluid dynamics
Stall
Aerodynamics
Aerospace engineering
Fluid mechanics

564 AIAA JOURNAL VOL. 16, NO. 6

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