Choked flow: Difference between revisions
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Created page with "Category:Compressible flow Category:Quasi-one-dimensional flow Category:Inviscid flow __TOC__ \section{Geometric Choking} \noindent For steady-state nozzle flow, the massflow is obtained as \\ \begin{equation} \dot{m}=\rho uA=const \label{eq:massflow:a} \end{equation}\\ \noindent Eqn. \ref{eq:massflow:a} can be evaluated at any location inside the nozzle and if evaluated at sonic conditions we get\\ \begin{equation} \dot{m}=\rho^* u^* A^* \label{eq:mass..." |
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