Embedded Files
Boundary Layers
Shock structures
credit: NASA
Turbulence
credit: NASA
credit: Argonne
Pipe flow: Moody chart
f=stress/(rho*u^2)
NACA TM 1292(1950) & Goldenfeld (2016)
f=(p2-p1)/(0.5*rho*u^2*L/d) where h=(p2-p1)/(rho*g)
Fluid Mechanics by Frank White
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