Vector Calculus and Applications > Flows > Flashcards
Incompressible
delta . u = 0
Steady Flow
du/dt = 0
Acceleration
du/dt + (u.delta)u
Stagnation Points
anywhere u = 0
Particle Paths
dx/dt = ux, dy/dt = uy, dz/dt = uz
Streamlines
dx/ux=dy/uy=dz/uz
Vorticity
delta x u
Irrotational
zero vorticity