Pressure Distribution Images The following CFD images were obtained by Professor Kunio Kuwahara, Institute of Space and Astronautical Science , Japan (used here with permission) In them note the stagnation pressure regions, low pressure regions, surface pressure distribution, boundary layer, layer, separation, vortices, and reverse flow
Airfoil:
NACA 0012,
Re = 1000,000
alpha = 10 Flow attached most of the surface. surface. BL thin, Small wake
alpha = 10 Near maximum efficiency, efficiency, Flow mostly attached. Can see two kinds of BL Not much wake region
alpha = 18, Near stall, Flow attached front half. Flow separation at mid chord. chord. Vortices, Significant Significant wake region (more pressure drag)
alpha = 22, Flow stalled. Flow separated on the airfoil Fully separated on the top, Large wake and reverse fl ow
Others
Imagine this dinosaur in a storm (250 mph winds) What kind of drag it would have Laminar separation over a sphere
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