Area-Mach relation: Difference between revisions

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Created page with "Category:Compressible flow Category:Quasi-one-dimensional flow Category:Inviscid flow __TOC__ \section{The Area-Mach-Number Relation} \noindent Starting point - the continuity equation (Eqn. \ref{eq:governing:cont}):\\ \[d(\rho uA)=0 \Rightarrow \rho u A=const\]\\ \noindent This applies everywhere in the nozzle and therefore the sonic conditions can be used as a reference\\ \[\rho uA=\rho^*u^*A^*=\left\{u^*=a^*\right\}=\rho^*a^*A^*\]\\ \noindent divide..."
 
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[[Category:Inviscid flow]]
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[[Category:Compressible flow:Topic]]
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