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  • Supersonic Flow Over a Wedge - Pre-Analysis & Start-Up

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Step 2: We calculate the value of the free stream Mach Number normal to the shock so we can use normal shock relations to relate quantities upstream and downstream of the shock. 

 

Latex
\Large\
\\Large
\begin{equation}\nonumber
M_{1N} = M_1sin(\beta)
\end{equation}
\\

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