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Fluid mechanics / Supercritical airfoil / Airfoil / Drag divergence Mach number / Shock wave / Wave drag / Lift / Pressure coefficient / Foil / Aerodynamics / Aerospace engineering / Fluid dynamics
Date: 2006-12-04 07:30:46
Fluid mechanics
Supercritical airfoil
Airfoil
Drag divergence Mach number
Shock wave
Wave drag
Lift
Pressure coefficient
Foil
Aerodynamics
Aerospace engineering
Fluid dynamics

NASA Technical Paper

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Source URL: www.southampton.ac.uk

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File Size: 3,14 MB

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