New York University 3 credits Aerospace Engineering
This course covers conservation equations for inviscid flows, one-dimensional flows, normal shock waves, one-dimensional flow with friction, one-dimensional flow with heat addition, oblique shock waves and Prandtl-Meyer expansion waves. | Prerequisite: ME 3333 and ME 3313. Prerequisites: (ME-UY 3333 with a Minimum Grade of D OR ME-UY 2313) AND ME-UY 3313 with a Minimum Grade of D.
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