compressible flow

Compressible flow - show that in the temperature-velocity phase plane that the singular points corresponding to the initial and final states of the

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16.120 Compressible Flow Problem Set # 3 Assigned: April 8, 2003 Due: April 10, 2003 Using a Navier-Stokes formulation, derive the set of governing first order, non-linear differential equations and interpret the physical meaning of the internal structure of a normal shock wave. Consider appropriate limiting cases. Using asymptotic expansions,
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Unformatted text preview: show that in the temperature-velocity phase plane that the singular points corresponding to the initial and final states of the internal structure are respectively a node and a saddle point. Harris April 8, 2003...
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This note was uploaded on 11/07/2011 for the course AERO 16.120 taught by Professor Wesleyharris during the Spring '03 term at MIT.

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