The mass flow of a calorically perfect gas through a choked nozzle is given by [dot{m}=frac{p_{o} A^{*}}{sqrt{T_{o}}}
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The mass flow of a calorically perfect gas through a choked nozzle is given by
\[\dot{m}=\frac{p_{o} A^{*}}{\sqrt{T_{o}}} \sqrt{\frac{\gamma}{R}\left(\frac{2}{\gamma+1}\right)^{(\gamma+1) /(\gamma-1)}}\]
Derive this relation.
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Step by Step Answer:
To derive the mass flow equation for a calorically perfect gas through a choked nozzle we can start with the basic principles of compressible flow and ...View the full answer
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